CA2133038C - Plane array antenna for receiving satellite broadcasting - Google Patents
Plane array antenna for receiving satellite broadcastingInfo
- Publication number
- CA2133038C CA2133038C CA002133038A CA2133038A CA2133038C CA 2133038 C CA2133038 C CA 2133038C CA 002133038 A CA002133038 A CA 002133038A CA 2133038 A CA2133038 A CA 2133038A CA 2133038 C CA2133038 C CA 2133038C
- Authority
- CA
- Canada
- Prior art keywords
- array antenna
- plane array
- main body
- antenna main
- converter
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/06—Arrays of individually energised antenna units similarly polarised and spaced apart
- H01Q21/061—Two dimensional planar arrays
- H01Q21/068—Two dimensional planar arrays using parallel coplanar travelling wave or leaky wave aerial units
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/32—Adaptation for use in or on road or rail vehicles
- H01Q1/325—Adaptation for use in or on road or rail vehicles characterised by the location of the antenna on the vehicle
- H01Q1/3275—Adaptation for use in or on road or rail vehicles characterised by the location of the antenna on the vehicle mounted on a horizontal surface of the vehicle, e.g. on roof, hood, trunk
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
- H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
- H01Q3/04—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying one co-ordinate of the orientation
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Waveguide Aerials (AREA)
- Waveguide Connection Structure (AREA)
- Details Of Aerials (AREA)
Abstract
A plane array antenna for receiving a satellite broadcasting, with an optimum combination of the plane array antenna main body having a tilt angle, the converter combined with this antenna main body through the power supply portion, and the rotation mechanism for rotating the antenna main body within almost a horizontal plane for tracing the azimuthal angle direction. The plane array antenna main body has the central power supply type structure having the power supply portion formed at the center of the rotation.
The converter includes the dielectric substrate having the microstrip channel formed on the substrate and the casing for accommodating the substrate, and is fixed downward the antenna main body and supports the main body. The power supply portion includes the power supply probe with an insulation covering, having a space formed at its front end portion with the antenna main body, with the front end portion inserted into the space, having the central portion piercing through the casing of the converter, and having the lowest end portion combined with the microstrip channel. The rotation mechanism includes the cylinder body projecting downwards from the bottom surface of the antenna main body at the outside of the converter and the driving mechanism for providing a rotation power to the cylinder body.
The converter includes the dielectric substrate having the microstrip channel formed on the substrate and the casing for accommodating the substrate, and is fixed downward the antenna main body and supports the main body. The power supply portion includes the power supply probe with an insulation covering, having a space formed at its front end portion with the antenna main body, with the front end portion inserted into the space, having the central portion piercing through the casing of the converter, and having the lowest end portion combined with the microstrip channel. The rotation mechanism includes the cylinder body projecting downwards from the bottom surface of the antenna main body at the outside of the converter and the driving mechanism for providing a rotation power to the cylinder body.
Description
FIELD OF THE INVENTION
The present invention relates to a plane array antenna for receiving satellite broadcasting programs to be utilized by being loaded on a car or the like.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a partial cross sectional diagram -for showing the structure of the periphery of the power supply portion of the plane array antenna according to one embodiment of the present invention.
Fig. 2 is a cross sectional diagram of an enlarged portion of the periphery of the power supply portion shown in Fig. 1.
Fig. 3 is a plane diagram for showing the whole of the above embodiment.
Fig. 4 is a partial cross sectional diagram for showing one example of another structure of the periphery of the power supply portion shown in Fig. 1.
Fig. 5 is a perspective diagram for showing the structure of the leakage wave wave guide cross slot array antenna which is one representative example of the central power supply type plane array antenna.
DESCRIPTION OF THE RELATED ART
Along with the diffusion of satellite ...' :;.'.~. ~,.' 2133038 :~:
:
broadcasting in recent years, there have been many studies being carried out on car-loaded antennas for receiving a satellite broadcasting. For this type of car-loaded antenna, how to reduce the height for fitting the antenna is one of the important technical issues because the antenna is usually fitted on the top of the car which runs on a load with height restrictions.
Further, since the antenna for receiving a satellite broadcasting is fitted on the top of the car with a limited space, how to reduce the area for installing the antenna is also one of the impor~ant technical issues.
In order to reduce the height for fitting the antenna ; ~-for receiving a satellite broadcasting, a structure for horizontally fitting the plane array antenna having a 15 tilt angle on the top of the car is considered to be ~ ~-advantageous. Main beams irradiated from this type of plane array antenna are being irradiated in the direction which is deviated by a tilt angle from the -normal direction of the plane array antenna.
In a car-loaded antenna, an automatic tracing mechanism for controlling both an azimuth angle and an elevation angle of the antenna is necessary so that the antenna can always trace a broadcasting satellite that changes every moment along with the move of the car.
25 The automatic tracing mechanism not only occupies a ;
substantial portion of the manufacturing expenses of the whole receiving system but also increases the height and area for fitting the antenna. Therefore, how to ' 2133038 simplify the automatic tracing system has been one of the important technical issues. Changes of an azimuth angle occurs over 360~ along with the move of the car, and therefore, it is considered realistic to achieve the tracing in the direction of the azimuth angle by a mechanical rotation mechanism. In contrast to this trend, changes of an elevation angle occur along with the longitude or the slope from the horizontal plane, that is, the slope of the load of about ~ 5~. There-fore, the range of the changes of the elevation angle isrelatively limited. As a result, it has been considered advantageous to economize the whole of the receiving system by employing an elevation angle direction non-tracing system for not performing a mechanical tracing in the elevation angle, or a lln;~ial tracing system for tracing only the azimuth angle direction, by setting in advance the directivity in the elevation angle direction of the antenna to be wider.
A plane array antenna for receiving a satellite broadcasting which is designed to achieve the above-described uniaxial tracing system is described in the paper (A.P 93-25) titled "A SINGLE-LAYER STRUCTURE
LEAKAGE WAVE GUIDE SLOT ARRAY CAR-LOADED ANTENNA FOR '~
RECEIVING SATELLITE BROADCASTING", reported by Hirokawa et al. in the technical research report of the Institute of Electronics, Information and C~- n; cation Engineers tJapan), held in May 1993. This paper describes a -leakage wave guide slot array antenna of a type, in , "~
which electric power is supplied in the rotation center ~hereinafter, this type will be called as a central power supply type), having a structure as shown in the perspective view in Fig. 5. A main body of the slot :
array antenna is formed by 12 radiation wave guides llA
to llL disposed mutually adjacent in parallel with each other and T-shaped power supply wave guides 12 for supplying a radiation power to each radiation wave .
guide. Each of the T-shaped power supply wave guides 12 is structured by a first part 12A which is extended in its layout direction (or row direction) by forming a combining window with one end of each radiation wave ~::
guide and a second part 12B which is extended from a :~
power supply probe 13 formed at the rotation center 15 position in the azimuth angle direction of the antenna ;
main body, and both of the first and second parts 12A
and 12B form a T branch. Each of the radiation wave guides llA to llL is structured by a leakage wave guide which is formed with cross slots 14 in the axial direction by a suitable number, for example, 13 to 17, each having the same offset volume, to achieve a beam wid~h of about + 5~ around the tilt angle direction of 52~ ~:
The above paper suggests an advantage that, according to the structure of the central power supply type shown in Fig. 5, when a power supply portion by the power supply probe 13 disposed at the center of the ::
rotation is structured by a rotary joint or the like, .
- _ 5 _ only the antenna can be rotated within an almost horizontal plane at the time of uniaxial tracing, by keeping fixed the converter to be connected to this power supply portion at the lower side of the antenna main body.
The above paper by Hirokawa et al. shows a structure which enables only the antenna body to be rotated by employing the central power supply type antenna structure and the power supply portion having the rotary joint structure. However, a further sufficient investigation is necessary in order to achieve an optimum structure. In the central power supply type antenna, the power supply system and the mechanical system for the rotation are concentrated and complicated at the center portion of the antenna because the center portion is important for both of the systems.
An attempt to avoid the complication of both the electrical and mechanical systems would result in insufficient electrical and mechanical characteristics.
If the power supply portion of the rotary joint structure and the converter are connected with a flexible coaxial cable, for example, it is possible to release the converter from the center portion and thus concentrate the rotation mechanical system in the center portion. However, since the frequency of the signal is as high as 12 GHz, there is a problem that a longer coaxial cable causes an increase in the transmitting loss and a deterioration of the S/N ratio. On the other hand, a fixing of the converter at the center portion of the antenna main body causes a problem that this converter becomes a hindrance so that a usual rotation mechanism of combining the rotation axis of the motor to the rotation center of the antenna main body can not be employed.
Sl~MMARY OF THE lNV~iN'l'lON
It is, therefore, an object of the present invention to provide a central power supply type plane 10 array antenna, having a structure of an optimum combi- -nation of a central power supply type antenna structure, a current supply portion of a rotary joint structure and a rotation mechanism.
According to the plane array antenna of the present invention for receiving a satellite broad-casting, a main body of the plane array antenna includes a central power supply type structure having a power supply portion formed at the center of the rotation. A
converter includes a dielectric substrate having a microstrip channel formed on the substrate and a casing for accommodating this dielectric substrate. The converter is fixed at a lower side of the main body of -the plane array antenna and rotatably supports the main body of the plane array antenna. A power supply portion 25 includes a power supply probe that has an insulation ;~
covering of which upper end portion forms a space with the antenna main body, with the upper end portion ' . : . ., . . :
' 2133038 , inserted into this space, of which center portion pierces through the casing of the converter and of which lower end portion is combined with the microstrip channel formed on the dielectric substrate of the converter. A rotation mechanism for tracing the azimuth angle direction includes a cylindrical body which projects downwards from the bottom of the antenna main body at the outside of the converter and a driving mechanism for providing a rotation power to this cylindrical body.
When the main body of the plane array antenna formed by a leakage wave guide slot array antenna or the like is formed by a central power supply type structure as shown in Fig. 5, conditions can be obtained for lS enabling only the main body of the plane array antenna to be rotated while keeping the converter fixed. To be more specific, the upper end portion of the power supply probe is inserted into the rotation center position of the antenna main body and the lower end portion of the 20 power supply probe is combined with the microstrip ~;~
channel formed on the dielectric substrate of the converter so that the antenna main body and the converter can be connected in the shortest distance with a transmission channel of the simplest coaxial struc- -ture. As a result, a power supply mechanism of a simple design with a i ni insertion loss can be achieved.
When the antenna main body is rotatably supported by the ~' casing of the converter through which the power supply probe pierces and when the drivin~ mechanism is released to the outside of the converter that is fixed at the center of the antenna main body, complication of the power supply system and the mechanical system that tends to occur at the center portion of the antenna can be effectively avoided and an optimum structure with both excellent electrical and mechanical characteristics can be obtained.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Fig. 1 is a partial cross sectional diagram for showing the structure of the periphery of the power supply of leakage wave guide slot array antenna for receiving a satellite broadcasting according to one embodiment of the present invention, Fig. 2 is a partial enlarged diagram of the periphery of the power supply shown in Fig. 1 and Fig. 3 is a plane diagram of the whole system. 10 designates a main body of the plane array antenna. In the present embodiment, the main body of the plane array antenna has the same structure as that of the leakage wave guide slot array antenna of the central power supply type shown in Fig. 5. 20 designates a converter, that includes a dielectric substrate 21 on which a microstrip channel is formed and a casing 22 made of metal for accommodating the ' dielectric substrate 21. The converter 20 is fixed on a bottom surface 41 of a radome 40. 13 designates a power supply probe for structuring a power supply portion, and g this power supply probe is structured by a cylindrical central pin 13a and a cylindrical insulation covering 13b for covering the central pin.
Referring to the partial enlarged diagram in Fig. 2, the power supply probe 13 is inserted into a second part 12B of the power supply wave guide while forming a fine space between the upper end portion of the power supply probe and the plane array antenna main -body 10. The central portion of the power supply probe 13 pierces through the casing 22 of the converter and the lower end portion of the power supply probe 13 is connected in a stand-straight state by soldering and bonding on a microstrip channel 21a formed on the -dielectric substrate 21 of the converter 20. The casing 22 of the converter for allowing the central portion of the power supply probe 13 to pierce through it includes a cylinder portion 22a for holding the power supply -probe 13 while compressing the power supply probe in an axial core direction and a flange portion 22b formed at the front end portion of the cylinder portion 22a for rotatably supporting the plane array antenna main body 10 through an insulation sheet 22c. The radius of the flange portion 22b is set to a value which is almost equal to a 1/4 wavelength of the received signal.
Referring to Figs. 1 and 3, the rotation mechanism is structured by a cylinder body 31 which projects downwards from the bottom of the plane array antenna main body 10 at the outside of the converter 20 ; ~
.: ' .':
--' 2133038 fixed on the bottom surface 41 of the radome 40 and a driving mechanism for providing a rotation power to this cylinder body. The cylinder body 31 has hills and valleys formed at predetermined distances on the outer periphery of the cylinder body in the circumferential direction, and this is achieved by bond fixing a timing belt on a plane outer periphery. Referring to the plane diagram in Fig. 3, the driving mechanism is structured by a timing belt 34 for engaging with the outer periphery of the cylinder body 31, a pulley 33 for engaging with the timing belt at the outside of the cylinder body 31 and a motor 32 for rotating the pulley ;
33. In Fig. 3, 41 designates a bottom surface encircled by a side wall of the radome 40. The casing is fixed on this bottom surface to keep wind-prevention, moisture-prevention and dust-prevention states inside the radome 40.
A wave received by the radiation wave guides llA to llL shown in Fig. 5 and propagated through the power supply wave guides 12 reaches the power supply probe 13 shown in Fig. 2 and is combined with the upper end portion of the power supply probe. The intermediate portion of the power supply probe 13 forms a coaxial channel having the center pin 13a as an internal conductor and the cylinder portion 22a of the casing 21 as an external conductor. Accordingly, the upper end portion of the power supply probe 13 functions as a wave guide/coaxial mode converter for converting the wave ., , - , 2133~38 propagated in the wave guide mode into a wave in the coaxial mode. On the other hand, the lower end portion of the power supply probe 13 functions as a coaxial/
microstrip mode converter for converting the wave propagated in the coaxial mode at the central portion of the probe 13 into the propagation mode of the microstrip mode and propagating the converted wave to the micro-strip channel. The received wave that has been converted into the microstrip mode is then converted 10 into an intermediate frequency signal by a down :
converter circuit (not shown) installed on the dielectric substrate, and is supplied to a BS tuner through a coaxial connector 23 and a coaxial cable 24 as shown in Fig. 1.
15Referring to Fig. 2, the thin (for example, about 0.2 mm to 0.5 mm thickness) insulation sheet 22c is sandwiched between the metal bottom surface of the ~ '~
plane array antenna main body 10 and the metal flange portion 22b. This insulation sheet 22c prevents an abrasion due to a friction between the metals. Accord-ingly, tetra fluoride ethylene of a small coefficient of kinetic friction (TFE; for example, a product name "TEFLON") or the like is suitable as the raw material of the insulation sheet 22c. Also, mainly from the view-point of the electric characteristics of low loss, tetrafluoride ethylene or the like is suitable as the raw material of the covering 13b of the power supply probe 13. At the position where the insulation sheet 22c is ;
.,''.
. .
present, a radial line is formed for radially propagat-ing the wave externally by the surface at which the bottom surface of the antenna main body and the flange portion face each other. A leakage of the wave through the radial line occurs and a propagation loss from the antenna main body to the converter and a subsequent deterioration of frequency characteristics occur. To -avoid this problem, the length of the radial line is set to be almost equal to 1/4 of the wavelength of the received wave. As a result, the outside end portion of the radial line is an open end and the above-described problem due to the leakage of the wave is restricted to the in;
The power supply probe 13 also functions as a central axis in the rotation mechanism which is formed in combination with the driving mechanism formed outside of the converter 20. The antenna is usually installed inside the radome and, therefore, there is no risk of an occurrence of a strong external force being applied in the lateral direction to the power supply probe 13 due to a wind pressure. Further, because of the uniaxial tracing system for not tracing in the elevation direction, the antenna main body 10 and the casing 20 are maintained almost horizontally, so that there is no risk of a large lateral direction external force being applied to the power supply probe 13. However, various types of lateral direction external force are applied to the power supply probe 13, such as a tensile force to .
the motor 32 side by the timing belt 34, oscillations :
and shocks generated along with the running of the car, etc. Nhen such a lateral direction external force as described is transmitted to the junction between the 5 terminal portion of ~he power supply probe 13 and the :
microstrip channel 21a, there is a risk of the junction being damaged by a shearing force.
To avoid the above problem, the cylinder '~ .
portion 22a of the casing 22 is strongly compressed in ' 10 the center direction by a calking or the like and a : ~-larger portion of the lateral direction external force transmitted to the power supply probe 13 is transmitted to the casing 22 through the cylinder portion 22a. In order to prevent a damage at the fixed portion between ' the power supply probe 13 and the microstrip channel, a structure may be adopted in which the lower end portion of the center pin 13a of the power supply pin probe 13 :
is connested to the microstrip channel 21a through a flexible metal foil placed at the connection point.
A structure as shown in Fig. 4 may be also adopted in which a disk-shaped metal engagement member 22d covered with TFE or the like on its surface is ~ :
placed between the bottom surface of the plane array :' antenna main body 10 and the flange portion 22b ~o form 25 a fine space between the two and rotatably support the :
antenna main body 10 by the flange portion 22b, and at the same time, to form a relatively large space between :
the cylinder portion 22a of the casing 22 and the power ' 21330~8 supply probe 13. In other words, the lateral direction external force applied to the antenna main body 10 is transmitted directly only to the flange portion 22b -through the engagement member 22d. A vertical direction external force applied to the an~enna main body 10 is all transmitted only to the flange portion 22 in the same manner as the weight of the antenna main body 10.
With the above-described structure, the external force applied to the plane array antenna main body 10 can all be transmitted directly to the casing 22 through the engagement member 22d and the flange portion 22a, with no external force being transmitted to the power supply probe 13 at all.
In the structure shown in Fig. 4, there is a risk that an inner peripheral distance between the power supply probe 13 and the cylinder portion 22a fluctuates due to the manufacturing conditions or a distortion of the cylinder portion 22a by the lateral direction load during the use of the system, leading to a fluctuation in the electrical characteristics. In order to avoid this risk, a metal film 13c is formed on the outer periphery of the insulation covering 13b at the center portion of the power supply probe 13 so that the power supply probe 13 itself takes a coaxial cable structure.
The structure of the coaxial cable can also be applied to the case of Fig. 1.
The above description has been made to explain the present invention in the case where the plane array antenna main body is structured by the leakage wave guide cross slot array antenna. However, it is obvious that the present invention can also be applied to other ' suitable forms of central power supply type plane array antenna, such as an antenna which is a combination between a radial line and a helical antenna device, an antenna which is a combination between a radial line and a microstrip antenna device, etc.
In the above embodiments, the structure using a timing belt, a pulley and a motor has been shown as an example of the driving mechanism. However, it is also obvious that the driving mechanism can also be achieved by using a pinion which is a cylinder body projected downwards the antenna main body, and a rack which is proceeded or receded by the motor by being engaged with this pinion.
Further, the above embodiments have the structure in which the cylinder portion 22a for piercing the power supply probe 13 through it and for rotatably supporting the antenna main body lO and the flange portion 22b are integrally formed with the casing 22 of the converter 20. However, it is obvious that the cylinder portion and the flange portion may be formed separate from the casing 22 and afterward these are fixed to the casing 22.
The case of using a metal casing for the converter has been shown in the above from a viewpoint of an electrostatic shielding. However, such a ;-~
."' ..~ .
' 2133038 structure may be adopted in which the casing is formed by a resin to avoid a corrosion and a metal thin plate is applied to the inner side of the casing for an electrostatic shielding. Further, as the structure of 5 Fig. 3, instead of using the insulation sheet 22c, such a structure may be adopted in which a resin such as TFE
or the like is coated or plated to the flange portion 22b or to the bottom surface of the antenna main body which is in contact with the flange portion.
As described in detail in the above, the plane array antenna for receiving a satellite broadcasting according to the present invention has a structure for combining the power supply probe with the microstrip channel formed on the dielectric substrate of the 15 converter so that the antenna main body and the converter can be connected in the shortest distance by a transmission channel of the most simple structure. As a result, a power supply mechanism with a ; n i insertion loss can be achieved in a simple design.
Further, the plane array antenna for receiving a satellite broadcasting according to the present invention has a structure that the antenna main body is rotatably supported by the casing of the converter through which the power supply probe is pierced and the driving mechanism is released to the outside of the converter which is fixed to the center portion of the antenna main body, so that a complication of the power supply system and the mechanical system which tend to be ,.-. .
' 2133038 integrated at the center portion of the antenna can be effectively avoided. Thus, an optimum structure with both excellent electrical and mechanical characteristics ~'~
can be achieved.
' ~ ~ ' . ' :, :,.~
.
: ~.
The present invention relates to a plane array antenna for receiving satellite broadcasting programs to be utilized by being loaded on a car or the like.
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a partial cross sectional diagram -for showing the structure of the periphery of the power supply portion of the plane array antenna according to one embodiment of the present invention.
Fig. 2 is a cross sectional diagram of an enlarged portion of the periphery of the power supply portion shown in Fig. 1.
Fig. 3 is a plane diagram for showing the whole of the above embodiment.
Fig. 4 is a partial cross sectional diagram for showing one example of another structure of the periphery of the power supply portion shown in Fig. 1.
Fig. 5 is a perspective diagram for showing the structure of the leakage wave wave guide cross slot array antenna which is one representative example of the central power supply type plane array antenna.
DESCRIPTION OF THE RELATED ART
Along with the diffusion of satellite ...' :;.'.~. ~,.' 2133038 :~:
:
broadcasting in recent years, there have been many studies being carried out on car-loaded antennas for receiving a satellite broadcasting. For this type of car-loaded antenna, how to reduce the height for fitting the antenna is one of the important technical issues because the antenna is usually fitted on the top of the car which runs on a load with height restrictions.
Further, since the antenna for receiving a satellite broadcasting is fitted on the top of the car with a limited space, how to reduce the area for installing the antenna is also one of the impor~ant technical issues.
In order to reduce the height for fitting the antenna ; ~-for receiving a satellite broadcasting, a structure for horizontally fitting the plane array antenna having a 15 tilt angle on the top of the car is considered to be ~ ~-advantageous. Main beams irradiated from this type of plane array antenna are being irradiated in the direction which is deviated by a tilt angle from the -normal direction of the plane array antenna.
In a car-loaded antenna, an automatic tracing mechanism for controlling both an azimuth angle and an elevation angle of the antenna is necessary so that the antenna can always trace a broadcasting satellite that changes every moment along with the move of the car.
25 The automatic tracing mechanism not only occupies a ;
substantial portion of the manufacturing expenses of the whole receiving system but also increases the height and area for fitting the antenna. Therefore, how to ' 2133038 simplify the automatic tracing system has been one of the important technical issues. Changes of an azimuth angle occurs over 360~ along with the move of the car, and therefore, it is considered realistic to achieve the tracing in the direction of the azimuth angle by a mechanical rotation mechanism. In contrast to this trend, changes of an elevation angle occur along with the longitude or the slope from the horizontal plane, that is, the slope of the load of about ~ 5~. There-fore, the range of the changes of the elevation angle isrelatively limited. As a result, it has been considered advantageous to economize the whole of the receiving system by employing an elevation angle direction non-tracing system for not performing a mechanical tracing in the elevation angle, or a lln;~ial tracing system for tracing only the azimuth angle direction, by setting in advance the directivity in the elevation angle direction of the antenna to be wider.
A plane array antenna for receiving a satellite broadcasting which is designed to achieve the above-described uniaxial tracing system is described in the paper (A.P 93-25) titled "A SINGLE-LAYER STRUCTURE
LEAKAGE WAVE GUIDE SLOT ARRAY CAR-LOADED ANTENNA FOR '~
RECEIVING SATELLITE BROADCASTING", reported by Hirokawa et al. in the technical research report of the Institute of Electronics, Information and C~- n; cation Engineers tJapan), held in May 1993. This paper describes a -leakage wave guide slot array antenna of a type, in , "~
which electric power is supplied in the rotation center ~hereinafter, this type will be called as a central power supply type), having a structure as shown in the perspective view in Fig. 5. A main body of the slot :
array antenna is formed by 12 radiation wave guides llA
to llL disposed mutually adjacent in parallel with each other and T-shaped power supply wave guides 12 for supplying a radiation power to each radiation wave .
guide. Each of the T-shaped power supply wave guides 12 is structured by a first part 12A which is extended in its layout direction (or row direction) by forming a combining window with one end of each radiation wave ~::
guide and a second part 12B which is extended from a :~
power supply probe 13 formed at the rotation center 15 position in the azimuth angle direction of the antenna ;
main body, and both of the first and second parts 12A
and 12B form a T branch. Each of the radiation wave guides llA to llL is structured by a leakage wave guide which is formed with cross slots 14 in the axial direction by a suitable number, for example, 13 to 17, each having the same offset volume, to achieve a beam wid~h of about + 5~ around the tilt angle direction of 52~ ~:
The above paper suggests an advantage that, according to the structure of the central power supply type shown in Fig. 5, when a power supply portion by the power supply probe 13 disposed at the center of the ::
rotation is structured by a rotary joint or the like, .
- _ 5 _ only the antenna can be rotated within an almost horizontal plane at the time of uniaxial tracing, by keeping fixed the converter to be connected to this power supply portion at the lower side of the antenna main body.
The above paper by Hirokawa et al. shows a structure which enables only the antenna body to be rotated by employing the central power supply type antenna structure and the power supply portion having the rotary joint structure. However, a further sufficient investigation is necessary in order to achieve an optimum structure. In the central power supply type antenna, the power supply system and the mechanical system for the rotation are concentrated and complicated at the center portion of the antenna because the center portion is important for both of the systems.
An attempt to avoid the complication of both the electrical and mechanical systems would result in insufficient electrical and mechanical characteristics.
If the power supply portion of the rotary joint structure and the converter are connected with a flexible coaxial cable, for example, it is possible to release the converter from the center portion and thus concentrate the rotation mechanical system in the center portion. However, since the frequency of the signal is as high as 12 GHz, there is a problem that a longer coaxial cable causes an increase in the transmitting loss and a deterioration of the S/N ratio. On the other hand, a fixing of the converter at the center portion of the antenna main body causes a problem that this converter becomes a hindrance so that a usual rotation mechanism of combining the rotation axis of the motor to the rotation center of the antenna main body can not be employed.
Sl~MMARY OF THE lNV~iN'l'lON
It is, therefore, an object of the present invention to provide a central power supply type plane 10 array antenna, having a structure of an optimum combi- -nation of a central power supply type antenna structure, a current supply portion of a rotary joint structure and a rotation mechanism.
According to the plane array antenna of the present invention for receiving a satellite broad-casting, a main body of the plane array antenna includes a central power supply type structure having a power supply portion formed at the center of the rotation. A
converter includes a dielectric substrate having a microstrip channel formed on the substrate and a casing for accommodating this dielectric substrate. The converter is fixed at a lower side of the main body of -the plane array antenna and rotatably supports the main body of the plane array antenna. A power supply portion 25 includes a power supply probe that has an insulation ;~
covering of which upper end portion forms a space with the antenna main body, with the upper end portion ' . : . ., . . :
' 2133038 , inserted into this space, of which center portion pierces through the casing of the converter and of which lower end portion is combined with the microstrip channel formed on the dielectric substrate of the converter. A rotation mechanism for tracing the azimuth angle direction includes a cylindrical body which projects downwards from the bottom of the antenna main body at the outside of the converter and a driving mechanism for providing a rotation power to this cylindrical body.
When the main body of the plane array antenna formed by a leakage wave guide slot array antenna or the like is formed by a central power supply type structure as shown in Fig. 5, conditions can be obtained for lS enabling only the main body of the plane array antenna to be rotated while keeping the converter fixed. To be more specific, the upper end portion of the power supply probe is inserted into the rotation center position of the antenna main body and the lower end portion of the 20 power supply probe is combined with the microstrip ~;~
channel formed on the dielectric substrate of the converter so that the antenna main body and the converter can be connected in the shortest distance with a transmission channel of the simplest coaxial struc- -ture. As a result, a power supply mechanism of a simple design with a i ni insertion loss can be achieved.
When the antenna main body is rotatably supported by the ~' casing of the converter through which the power supply probe pierces and when the drivin~ mechanism is released to the outside of the converter that is fixed at the center of the antenna main body, complication of the power supply system and the mechanical system that tends to occur at the center portion of the antenna can be effectively avoided and an optimum structure with both excellent electrical and mechanical characteristics can be obtained.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Fig. 1 is a partial cross sectional diagram for showing the structure of the periphery of the power supply of leakage wave guide slot array antenna for receiving a satellite broadcasting according to one embodiment of the present invention, Fig. 2 is a partial enlarged diagram of the periphery of the power supply shown in Fig. 1 and Fig. 3 is a plane diagram of the whole system. 10 designates a main body of the plane array antenna. In the present embodiment, the main body of the plane array antenna has the same structure as that of the leakage wave guide slot array antenna of the central power supply type shown in Fig. 5. 20 designates a converter, that includes a dielectric substrate 21 on which a microstrip channel is formed and a casing 22 made of metal for accommodating the ' dielectric substrate 21. The converter 20 is fixed on a bottom surface 41 of a radome 40. 13 designates a power supply probe for structuring a power supply portion, and g this power supply probe is structured by a cylindrical central pin 13a and a cylindrical insulation covering 13b for covering the central pin.
Referring to the partial enlarged diagram in Fig. 2, the power supply probe 13 is inserted into a second part 12B of the power supply wave guide while forming a fine space between the upper end portion of the power supply probe and the plane array antenna main -body 10. The central portion of the power supply probe 13 pierces through the casing 22 of the converter and the lower end portion of the power supply probe 13 is connected in a stand-straight state by soldering and bonding on a microstrip channel 21a formed on the -dielectric substrate 21 of the converter 20. The casing 22 of the converter for allowing the central portion of the power supply probe 13 to pierce through it includes a cylinder portion 22a for holding the power supply -probe 13 while compressing the power supply probe in an axial core direction and a flange portion 22b formed at the front end portion of the cylinder portion 22a for rotatably supporting the plane array antenna main body 10 through an insulation sheet 22c. The radius of the flange portion 22b is set to a value which is almost equal to a 1/4 wavelength of the received signal.
Referring to Figs. 1 and 3, the rotation mechanism is structured by a cylinder body 31 which projects downwards from the bottom of the plane array antenna main body 10 at the outside of the converter 20 ; ~
.: ' .':
--' 2133038 fixed on the bottom surface 41 of the radome 40 and a driving mechanism for providing a rotation power to this cylinder body. The cylinder body 31 has hills and valleys formed at predetermined distances on the outer periphery of the cylinder body in the circumferential direction, and this is achieved by bond fixing a timing belt on a plane outer periphery. Referring to the plane diagram in Fig. 3, the driving mechanism is structured by a timing belt 34 for engaging with the outer periphery of the cylinder body 31, a pulley 33 for engaging with the timing belt at the outside of the cylinder body 31 and a motor 32 for rotating the pulley ;
33. In Fig. 3, 41 designates a bottom surface encircled by a side wall of the radome 40. The casing is fixed on this bottom surface to keep wind-prevention, moisture-prevention and dust-prevention states inside the radome 40.
A wave received by the radiation wave guides llA to llL shown in Fig. 5 and propagated through the power supply wave guides 12 reaches the power supply probe 13 shown in Fig. 2 and is combined with the upper end portion of the power supply probe. The intermediate portion of the power supply probe 13 forms a coaxial channel having the center pin 13a as an internal conductor and the cylinder portion 22a of the casing 21 as an external conductor. Accordingly, the upper end portion of the power supply probe 13 functions as a wave guide/coaxial mode converter for converting the wave ., , - , 2133~38 propagated in the wave guide mode into a wave in the coaxial mode. On the other hand, the lower end portion of the power supply probe 13 functions as a coaxial/
microstrip mode converter for converting the wave propagated in the coaxial mode at the central portion of the probe 13 into the propagation mode of the microstrip mode and propagating the converted wave to the micro-strip channel. The received wave that has been converted into the microstrip mode is then converted 10 into an intermediate frequency signal by a down :
converter circuit (not shown) installed on the dielectric substrate, and is supplied to a BS tuner through a coaxial connector 23 and a coaxial cable 24 as shown in Fig. 1.
15Referring to Fig. 2, the thin (for example, about 0.2 mm to 0.5 mm thickness) insulation sheet 22c is sandwiched between the metal bottom surface of the ~ '~
plane array antenna main body 10 and the metal flange portion 22b. This insulation sheet 22c prevents an abrasion due to a friction between the metals. Accord-ingly, tetra fluoride ethylene of a small coefficient of kinetic friction (TFE; for example, a product name "TEFLON") or the like is suitable as the raw material of the insulation sheet 22c. Also, mainly from the view-point of the electric characteristics of low loss, tetrafluoride ethylene or the like is suitable as the raw material of the covering 13b of the power supply probe 13. At the position where the insulation sheet 22c is ;
.,''.
. .
present, a radial line is formed for radially propagat-ing the wave externally by the surface at which the bottom surface of the antenna main body and the flange portion face each other. A leakage of the wave through the radial line occurs and a propagation loss from the antenna main body to the converter and a subsequent deterioration of frequency characteristics occur. To -avoid this problem, the length of the radial line is set to be almost equal to 1/4 of the wavelength of the received wave. As a result, the outside end portion of the radial line is an open end and the above-described problem due to the leakage of the wave is restricted to the in;
The power supply probe 13 also functions as a central axis in the rotation mechanism which is formed in combination with the driving mechanism formed outside of the converter 20. The antenna is usually installed inside the radome and, therefore, there is no risk of an occurrence of a strong external force being applied in the lateral direction to the power supply probe 13 due to a wind pressure. Further, because of the uniaxial tracing system for not tracing in the elevation direction, the antenna main body 10 and the casing 20 are maintained almost horizontally, so that there is no risk of a large lateral direction external force being applied to the power supply probe 13. However, various types of lateral direction external force are applied to the power supply probe 13, such as a tensile force to .
the motor 32 side by the timing belt 34, oscillations :
and shocks generated along with the running of the car, etc. Nhen such a lateral direction external force as described is transmitted to the junction between the 5 terminal portion of ~he power supply probe 13 and the :
microstrip channel 21a, there is a risk of the junction being damaged by a shearing force.
To avoid the above problem, the cylinder '~ .
portion 22a of the casing 22 is strongly compressed in ' 10 the center direction by a calking or the like and a : ~-larger portion of the lateral direction external force transmitted to the power supply probe 13 is transmitted to the casing 22 through the cylinder portion 22a. In order to prevent a damage at the fixed portion between ' the power supply probe 13 and the microstrip channel, a structure may be adopted in which the lower end portion of the center pin 13a of the power supply pin probe 13 :
is connested to the microstrip channel 21a through a flexible metal foil placed at the connection point.
A structure as shown in Fig. 4 may be also adopted in which a disk-shaped metal engagement member 22d covered with TFE or the like on its surface is ~ :
placed between the bottom surface of the plane array :' antenna main body 10 and the flange portion 22b ~o form 25 a fine space between the two and rotatably support the :
antenna main body 10 by the flange portion 22b, and at the same time, to form a relatively large space between :
the cylinder portion 22a of the casing 22 and the power ' 21330~8 supply probe 13. In other words, the lateral direction external force applied to the antenna main body 10 is transmitted directly only to the flange portion 22b -through the engagement member 22d. A vertical direction external force applied to the an~enna main body 10 is all transmitted only to the flange portion 22 in the same manner as the weight of the antenna main body 10.
With the above-described structure, the external force applied to the plane array antenna main body 10 can all be transmitted directly to the casing 22 through the engagement member 22d and the flange portion 22a, with no external force being transmitted to the power supply probe 13 at all.
In the structure shown in Fig. 4, there is a risk that an inner peripheral distance between the power supply probe 13 and the cylinder portion 22a fluctuates due to the manufacturing conditions or a distortion of the cylinder portion 22a by the lateral direction load during the use of the system, leading to a fluctuation in the electrical characteristics. In order to avoid this risk, a metal film 13c is formed on the outer periphery of the insulation covering 13b at the center portion of the power supply probe 13 so that the power supply probe 13 itself takes a coaxial cable structure.
The structure of the coaxial cable can also be applied to the case of Fig. 1.
The above description has been made to explain the present invention in the case where the plane array antenna main body is structured by the leakage wave guide cross slot array antenna. However, it is obvious that the present invention can also be applied to other ' suitable forms of central power supply type plane array antenna, such as an antenna which is a combination between a radial line and a helical antenna device, an antenna which is a combination between a radial line and a microstrip antenna device, etc.
In the above embodiments, the structure using a timing belt, a pulley and a motor has been shown as an example of the driving mechanism. However, it is also obvious that the driving mechanism can also be achieved by using a pinion which is a cylinder body projected downwards the antenna main body, and a rack which is proceeded or receded by the motor by being engaged with this pinion.
Further, the above embodiments have the structure in which the cylinder portion 22a for piercing the power supply probe 13 through it and for rotatably supporting the antenna main body lO and the flange portion 22b are integrally formed with the casing 22 of the converter 20. However, it is obvious that the cylinder portion and the flange portion may be formed separate from the casing 22 and afterward these are fixed to the casing 22.
The case of using a metal casing for the converter has been shown in the above from a viewpoint of an electrostatic shielding. However, such a ;-~
."' ..~ .
' 2133038 structure may be adopted in which the casing is formed by a resin to avoid a corrosion and a metal thin plate is applied to the inner side of the casing for an electrostatic shielding. Further, as the structure of 5 Fig. 3, instead of using the insulation sheet 22c, such a structure may be adopted in which a resin such as TFE
or the like is coated or plated to the flange portion 22b or to the bottom surface of the antenna main body which is in contact with the flange portion.
As described in detail in the above, the plane array antenna for receiving a satellite broadcasting according to the present invention has a structure for combining the power supply probe with the microstrip channel formed on the dielectric substrate of the 15 converter so that the antenna main body and the converter can be connected in the shortest distance by a transmission channel of the most simple structure. As a result, a power supply mechanism with a ; n i insertion loss can be achieved in a simple design.
Further, the plane array antenna for receiving a satellite broadcasting according to the present invention has a structure that the antenna main body is rotatably supported by the casing of the converter through which the power supply probe is pierced and the driving mechanism is released to the outside of the converter which is fixed to the center portion of the antenna main body, so that a complication of the power supply system and the mechanical system which tend to be ,.-. .
' 2133038 integrated at the center portion of the antenna can be effectively avoided. Thus, an optimum structure with both excellent electrical and mechanical characteristics ~'~
can be achieved.
' ~ ~ ' . ' :, :,.~
.
: ~.
Claims (38)
1. A plane array antenna for receiving a satellite broadcast, comprising:
a plane array antenna main body;
a feeding probe electromagnetically combined with said plane array antenna main body and including an insulation covering;
a converter for converting a frequency of a radio signal received by said plane array antenna main body, said converter including a dielectric substrate with a microstrip line formed thereon and a casing accommodating said dielectric substrate therein; and a rotation mechanism for rotating said plane array antenna main body within a substantially horizontal plane to track a direction from which said satellite broadcast is transmitted; wherein:
said feeding probe extends through said casing of said converter so that an upper part of said feeding probe is inserted into said plane array antenna main body with a gap formed therebetween and a lower part of said feeding probe is electrically connected to said microstrip line formed on said dielectric substrate of said converter; and said converter is fixed at a foundation of said plane array antenna and includes a rotation supporting member, formed on said casing of said converter, for rotatably supporting said plane array antenna main body by using said feeding prove as a central axis.
a plane array antenna main body;
a feeding probe electromagnetically combined with said plane array antenna main body and including an insulation covering;
a converter for converting a frequency of a radio signal received by said plane array antenna main body, said converter including a dielectric substrate with a microstrip line formed thereon and a casing accommodating said dielectric substrate therein; and a rotation mechanism for rotating said plane array antenna main body within a substantially horizontal plane to track a direction from which said satellite broadcast is transmitted; wherein:
said feeding probe extends through said casing of said converter so that an upper part of said feeding probe is inserted into said plane array antenna main body with a gap formed therebetween and a lower part of said feeding probe is electrically connected to said microstrip line formed on said dielectric substrate of said converter; and said converter is fixed at a foundation of said plane array antenna and includes a rotation supporting member, formed on said casing of said converter, for rotatably supporting said plane array antenna main body by using said feeding prove as a central axis.
2. A plane array antenna according to claim 1, wherein said rotation mechanism includes a cylindrical body projecting downwardly from a bottom surface of said plane array antenna main body at an outside of said converter and a driving mechanism for rotating said cylindrical body.
3. A plane array antenna according to claim 2, wherein:
said cylindrical body of said rotation mechanism has trenches at predetermined intervals along a circumference of an outer periphery of said cylindrical body; and said driving mechanism includes a timing belt engaging with said trenches along the outer periphery of said cylindrical body, a pulley engaged with said timing belt at an outside of said cylindrical body and a motor for rotating said pulley.
said cylindrical body of said rotation mechanism has trenches at predetermined intervals along a circumference of an outer periphery of said cylindrical body; and said driving mechanism includes a timing belt engaging with said trenches along the outer periphery of said cylindrical body, a pulley engaged with said timing belt at an outside of said cylindrical body and a motor for rotating said pulley.
4. A plane array antenna according to claim 1, wherein said rotation supporting member has cylindrical portion for coaxially surrounding said feeding probe and a flange portion, formed at an upper part of said cylindrical portion, for rotatably supporting said plane array antenna main body.
5. A plane array antenna according to claim 3, wherein said rotation supporting member has a cylindrical portion for coaxially surrounding said feeding probe and a flange portion, formed at an upper part of said cylindrical portion, for rotatably supporting said plane array antenna main body.
6. A plane array antenna according to claim 4, wherein said flange portion has a radius which is substantially equal to 1/4 of a wavelength of a received radio signal.
7. A plane array antenna according to claim 5, wherein said flange portion has a radius which is substantially equal to 1/4 of a wavelength of a received radio signal.
8. A plane array antenna according to claim 4, wherein said plane array antenna main body is rotatably supported by said flange portion through a disk-shaped engaging member which prohibits a relative displacement between said plane array antenna main body and said flange portion in the horizontal direction and forms a gap between said plane array antenna main body and said flange portion.
9. A plane array antenna according to claim 5, wherein said plane array antenna main body is rotatably supported by said flange portion through a disk-shaped engaging member which prohibits a relative displacement between said plane array antenna main body and said flange portion in the horizontal direction and forms a gap between said plane array antenna main body and said flange portion.
10. A plane array antenna according to claim 6, wherein said plane array antenna main body is rotatably supported by said flange portion through a disk-shaped engaging member which prohibits a relative displacement between said plane array antenna main body and said flange portion in the horizontal direction and forms a gap between said plane array antenna main body and said flange portion.
11. A plane array antenna according to claim 7, wherein said plane array antenna main body is rotatably supported by said flange portion through a disk-shaped engaging member which prohibits a relative displacement between said plane array antenna main body and said flange portion in the horizontal direction and forms a gap between said plane array antenna main body and said flange portion.
12. A plane array antenna according to claim 1, wherein said feeding probe has a metal film formed on an outer periphery of said insulation covering at least a central part thereof.
13. A plane array antenna according to claim 1, wherein said plane array antenna main body includes radiation wave guides disposed in parallel with each other and feeding wave guide for electromagnetically combining said radiation wave guides with said feeding probe.
14. A plane array antenna for receiving a satellite broadcast, comprising:
a plane array antenna main body;
a feeding probe electromagnetically combined with said plane array antenna main body and including an insulation covering;
a converter for converting a frequency of a radio signal received by said plane array antenna main body, said converter including a dielectric substrate having a microstrip line formed thereon and a casing for accommodating said dielectric substrate therein;
and a rotation mechanism for rotating said plane array antenna main body within a substantially horizontal plane to track a direction from which said satellite broadcast is transmitted; wherein:
said feeding probe extends through said casing of said converter so that an upper part of said feeding probe is inserted into said plane array antenna main body with a gap formed therebetween and a lower part of said feeding probe is electrically connected to said microstrip line formed on said dielectric substrate of said converter; and said converter is fixed at a foundation of said plane array antenna and includes a rotation supporting member formed on said casing of said converter, said rotation supporting member having a cylindrical portion for coaxially surrounding said feeding probe and a flange portion, formed at an upper part of said cylinder portion, for rotatably supporting said plane array antenna main body through a disk-shaped engaging member which prohibits a relative displacement between said plane array antenna main body and said flange portion in the horizontal direction and forms another gap between said plane array antenna main body and said flange portion.
a plane array antenna main body;
a feeding probe electromagnetically combined with said plane array antenna main body and including an insulation covering;
a converter for converting a frequency of a radio signal received by said plane array antenna main body, said converter including a dielectric substrate having a microstrip line formed thereon and a casing for accommodating said dielectric substrate therein;
and a rotation mechanism for rotating said plane array antenna main body within a substantially horizontal plane to track a direction from which said satellite broadcast is transmitted; wherein:
said feeding probe extends through said casing of said converter so that an upper part of said feeding probe is inserted into said plane array antenna main body with a gap formed therebetween and a lower part of said feeding probe is electrically connected to said microstrip line formed on said dielectric substrate of said converter; and said converter is fixed at a foundation of said plane array antenna and includes a rotation supporting member formed on said casing of said converter, said rotation supporting member having a cylindrical portion for coaxially surrounding said feeding probe and a flange portion, formed at an upper part of said cylinder portion, for rotatably supporting said plane array antenna main body through a disk-shaped engaging member which prohibits a relative displacement between said plane array antenna main body and said flange portion in the horizontal direction and forms another gap between said plane array antenna main body and said flange portion.
15. A plane array antenna according to claim 14, wherein said rotation mechanism includes a cylindrical body projecting downwardly from a bottom surface of said plane array antenna main body at an outside of said converter and a driving mechanism for rotating said cylindrical body.
16. A plane array antenna according to claim 15, wherein:
said cylindrical body of said rotation mechanism has trenches at predetermined intervals along a circumference of an outer periphery of said cylindrical body; and said driving mechanism includes a timing belt engaging with said trenches along the outer periphery of said cylindrical body, a pulley engaged with said timing belt at an outside of said cylindrical body and a motor for rotating said pulley.
said cylindrical body of said rotation mechanism has trenches at predetermined intervals along a circumference of an outer periphery of said cylindrical body; and said driving mechanism includes a timing belt engaging with said trenches along the outer periphery of said cylindrical body, a pulley engaged with said timing belt at an outside of said cylindrical body and a motor for rotating said pulley.
17. A plane array antenna according to claim 14, wherein said flange portion has a radius which is substantially equal to 1/4 of a wavelength of a received radio signal.
18. A plane array antenna according to claim 16, wherein said flange portion has a radius which is substantially equal to 1/4 of a wavelength of a received radio signal.
19. A plane array antenna for receiving a satellite broadcast, comprising:
a plane array antenna main body having wave guides;
a rotation mechanism for rotating said plane array antenna main body within a substantially horizontal plane to track a direction from which said satellite broadcast is transmitted;
a feeding probe placed at a center of rotation of said plane array antenna main body;
a converter, fixed at a foundation of said plane array antenna and electromagnetically combined with said plane array antenna main body through said feeding probe, for converting a frequency of a radio signal received by said wave guides of said plane array antenna main body; and a rotation supporting member, formed on a casing of said converter, for rotatably supporting said plane array antenna main body;
wherein said feeding probe extends through said casing of said converter so that an upper part of said feeding probe is inserted into one of said wave guides of said plane array antenna main body.
a plane array antenna main body having wave guides;
a rotation mechanism for rotating said plane array antenna main body within a substantially horizontal plane to track a direction from which said satellite broadcast is transmitted;
a feeding probe placed at a center of rotation of said plane array antenna main body;
a converter, fixed at a foundation of said plane array antenna and electromagnetically combined with said plane array antenna main body through said feeding probe, for converting a frequency of a radio signal received by said wave guides of said plane array antenna main body; and a rotation supporting member, formed on a casing of said converter, for rotatably supporting said plane array antenna main body;
wherein said feeding probe extends through said casing of said converter so that an upper part of said feeding probe is inserted into one of said wave guides of said plane array antenna main body.
20. A plane array antenna according to claim 19, wherein a lower part of said feeding probe is electrically connected to a microstrip line formed on a dielectric substrate of said converter.
21. A plane array antenna according to claim 19, wherein:
said upper part of said feeding probe includes first converter means for converting a radio signal of a wave guide mode received by said plane array antenna main body into a coaxial mode signal; and a lower part of said feeding probe includes second converter means for converting said coaxial mode signal into a microstrip mode signal.
said upper part of said feeding probe includes first converter means for converting a radio signal of a wave guide mode received by said plane array antenna main body into a coaxial mode signal; and a lower part of said feeding probe includes second converter means for converting said coaxial mode signal into a microstrip mode signal.
22. A plane array antenna according to claim 19, wherein said rotation mechanism includes a cylindrical body projecting downwardly from a bottom surface of said plane array antenna main body at an outside of said converter and a driving mechanism for rotating said cylindrical body.
23. A plane array antenna according to claim 19, wherein said rotation supporting member includes a cylindrical portion for coaxially surrounding said feeding probe and a flange portion, formed at an upper part of said cylindrical portion, for rotatably supporting said plane array antenna main body.
24. A plane array antenna according to claim 23, wherein said flange portion has a radius which is substantially equal to 1/4 of a wavelength of a received radio signal.
25. A plane array antenna according to claim 23, wherein said plane array antenna main body is rotatably supported by said flange portion through a disk-shaped engaging member which prohibits a relative displacement between said plane array antenna main body and said flange portion in the horizontal direction and forms a gap between said plane array antenna main body and said flange portion.
26. A plane array antenna according to claim 19, wherein said plane array antenna main body includes radiation wave guides disposed in parallel with each other and a feeding wave guide for electromagnetically combining said radiation wave guides with said feeding probe.
27. A plane array antenna according to claim 19, wherein said rotation supporting member rotatably supports said plane array antenna main body by using said feeding robe as a central axis.
28. A plane array antenna according to claim 19, wherein said plane array antenna tracks the direction from which said satellite broadcast is transmitted only within said substantially horizontal plane and around one axis.
29. A plane array antenna for receiving a satellite broadcast, comprising:
a plane array antenna main body having wave guides;
a rotation mechanism for rotating said plane array antenna main body within a substantially horizontal plane to track a direction from which said satellite broadcast is transmitted;
a feeding probe placed at a center of rotation of said plane array antenna main body;
a converter, fixed at a foundation of said plane array antenna and electromagnetically combined with said plane array antenna main body through said feeding probe, for converting a frequency of a radio signal received by said wave guides of said plane array antenna main body; and a rotation supporting member, formed on a casing of said converter, for rotatably supporting said plane array antenna main body;
wherein said feeding probe extends through said casing of said converter so that an upper part of said feeding probe is inserted into one of said wave guides of said plane array antenna main body and a lower part of said feeding probe is electrically connected to said converter.
a plane array antenna main body having wave guides;
a rotation mechanism for rotating said plane array antenna main body within a substantially horizontal plane to track a direction from which said satellite broadcast is transmitted;
a feeding probe placed at a center of rotation of said plane array antenna main body;
a converter, fixed at a foundation of said plane array antenna and electromagnetically combined with said plane array antenna main body through said feeding probe, for converting a frequency of a radio signal received by said wave guides of said plane array antenna main body; and a rotation supporting member, formed on a casing of said converter, for rotatably supporting said plane array antenna main body;
wherein said feeding probe extends through said casing of said converter so that an upper part of said feeding probe is inserted into one of said wave guides of said plane array antenna main body and a lower part of said feeding probe is electrically connected to said converter.
30. A plane array antenna according to claim 29, wherein said rotation supporting member includes a cylindrical portion for coaxially surrounding said feeding probe and a flange portion, formed at an upper part of said cylindrical portion, for rotatably supporting said plane array antenna main body.
31. A plane array antenna according to claim 29, wherein a lower part of said feeding probe is electrically connected to a microstrip line formed on a dielectric substrate of said converter.
32. A plane array antenna according to claim 29, wherein:
said upper part of said feeding probe includes first converter means for converting a radio signal of a wave guide mode received by said plane array antenna main body into a coaxial mode signal; and said lower part of said feeding probe includes second converter means for converting said coaxial mode signal into a microstrip mode signal.
said upper part of said feeding probe includes first converter means for converting a radio signal of a wave guide mode received by said plane array antenna main body into a coaxial mode signal; and said lower part of said feeding probe includes second converter means for converting said coaxial mode signal into a microstrip mode signal.
33. A plane array antenna according to claim 29, wherein said rotation mechanism includes a cylindrical body projecting downwardly from a bottom surface of said plane array antenna main body at an outside of said converter and a driving mechanism for rotating said cylindrical body.
34. A plane array antenna according to claim 29, wherein said rotation supporting member rotatably supports said plane array antenna main body by using said feeding probe as a central axis.
35. A plane array antenna according to claim 30, wherein said flange portion has a radius which is substantially equal to 1/4 of a wavelength of a received radio signal.
36. A plane array antenna according to claim 30, wherein said plane array antenna main body is rotatably supported by said flange portion through a disk-shaped engaging member which prohibits a relative displacement between said plane array antenna main body and said flange portion in the horizontal direction and forms a gap between said plane array antenna main body and said flange portion.
37. A plane array antenna according to claim 29, wherein said plane array antenna main body includes radiation wave guides disposed in parallel with each other and a feeding wave guide for electromagnetically combining said radiation wave guides with said feeding probe.
38. A plane array antenna according to claim 29, wherein said plane array antenna tracks the direction from which said satellite broadcast is transmitted only within said substantially horizontal plane and around one axis.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP05-277891 | 1993-10-08 | ||
| JP27789193A JP3364295B2 (en) | 1993-10-08 | 1993-10-08 | Planar array antenna for satellite broadcasting reception |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2133038A1 CA2133038A1 (en) | 1995-04-09 |
| CA2133038C true CA2133038C (en) | 1998-03-31 |
Family
ID=17589732
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002133038A Expired - Fee Related CA2133038C (en) | 1993-10-08 | 1994-09-27 | Plane array antenna for receiving satellite broadcasting |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US5519409A (en) |
| EP (1) | EP0647976A3 (en) |
| JP (1) | JP3364295B2 (en) |
| KR (1) | KR950012537A (en) |
| CN (1) | CN1039174C (en) |
| CA (1) | CA2133038C (en) |
| TW (1) | TW263621B (en) |
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| JP3647257B2 (en) * | 1998-04-27 | 2005-05-11 | アルプス電気株式会社 | Mobile satellite communication antenna device |
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| US7339520B2 (en) * | 2000-02-04 | 2008-03-04 | The Directv Group, Inc. | Phased array terminal for equatorial satellite constellations |
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| US20070103366A1 (en) * | 2003-11-27 | 2007-05-10 | Park Chan G | Antenna system for tracking moving object mounted satellite and its operating method |
| JP4263213B2 (en) * | 2004-03-17 | 2009-05-13 | 横浜ゴム株式会社 | Antenna device |
| US7292059B2 (en) * | 2005-03-31 | 2007-11-06 | Credence Systems Corporation | Power supply assembly for a semiconductor circuit tester |
| IL202732A0 (en) * | 2009-12-15 | 2010-11-30 | Dotan Ltd | Tracking station base |
| WO2018211695A1 (en) * | 2017-05-19 | 2018-11-22 | 三菱電機株式会社 | Array antenna device |
| FR3082362B1 (en) * | 2018-06-12 | 2021-06-11 | Thales Sa | BEAM FORMATION DEPOINTING SYSTEM |
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| US3795914A (en) * | 1972-09-20 | 1974-03-05 | E Systems Inc | Rotating beacon antenna with polarization filter |
| JPS5415584Y2 (en) * | 1974-03-28 | 1979-06-22 | ||
| GB8501225D0 (en) * | 1985-01-17 | 1985-02-20 | Cossor Electronics Ltd | Antenna |
| GB2208969B (en) * | 1987-08-18 | 1992-04-01 | Arimura Inst Technology | Slot antenna |
| IT1225343B (en) * | 1988-11-22 | 1990-11-13 | Sel Elettronica Soc Coop A R L | INDOOR ANTENNA FOR RECEIVING TELEVISION SIGNALS |
| US5210542A (en) * | 1991-07-03 | 1993-05-11 | Ball Corporation | Microstrip patch antenna structure |
| JP3056313B2 (en) * | 1991-11-29 | 2000-06-26 | アルプス電気株式会社 | Antenna device |
-
1993
- 1993-10-08 JP JP27789193A patent/JP3364295B2/en not_active Expired - Fee Related
-
1994
- 1994-09-27 CA CA002133038A patent/CA2133038C/en not_active Expired - Fee Related
- 1994-10-01 TW TW083109099A patent/TW263621B/zh active
- 1994-10-05 EP EP94115694A patent/EP0647976A3/en not_active Withdrawn
- 1994-10-07 CN CN94116845A patent/CN1039174C/en not_active Expired - Fee Related
- 1994-10-07 US US08/319,527 patent/US5519409A/en not_active Expired - Fee Related
- 1994-10-07 KR KR1019940025756A patent/KR950012537A/en active IP Right Grant
Also Published As
| Publication number | Publication date |
|---|---|
| CN1039174C (en) | 1998-07-15 |
| KR950012537A (en) | 1995-05-16 |
| CN1106576A (en) | 1995-08-09 |
| JP3364295B2 (en) | 2003-01-08 |
| CA2133038A1 (en) | 1995-04-09 |
| US5519409A (en) | 1996-05-21 |
| EP0647976A2 (en) | 1995-04-12 |
| JPH07111416A (en) | 1995-04-25 |
| EP0647976A3 (en) | 1997-10-22 |
| TW263621B (en) | 1995-11-21 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |