US2419999A - Orienting mechanism for pulse echo systems - Google Patents

Orienting mechanism for pulse echo systems Download PDF

Info

Publication number
US2419999A
US2419999A US452392A US45239242A US2419999A US 2419999 A US2419999 A US 2419999A US 452392 A US452392 A US 452392A US 45239242 A US45239242 A US 45239242A US 2419999 A US2419999 A US 2419999A
Authority
US
United States
Prior art keywords
antenna
pulse
cathode ray
pulse echo
orienting mechanism
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 - Lifetime
Application number
US452392A
Inventor
George W Leck
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RCA Corp
Original Assignee
RCA Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from US398057A external-priority patent/US2410666A/en
Application filed by RCA Corp filed Critical RCA Corp
Priority to US452392A priority Critical patent/US2419999A/en
Application granted granted Critical
Publication of US2419999A publication Critical patent/US2419999A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02Arrangements 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
    • H01Q3/08Arrangements 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 two co-ordinates of the orientation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon Stands for scientific apparatus such as gravitational force meters
    • F16M11/02Heads
    • F16M11/04Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
    • F16M11/06Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
    • F16M11/12Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction
    • F16M11/121Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction constituted of several dependent joints
    • F16M11/123Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction constituted of several dependent joints the axis of rotation intersecting in a single point, e.g. by using gimbals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon Stands for scientific apparatus such as gravitational force meters
    • F16M11/02Heads
    • F16M11/04Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
    • F16M11/06Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
    • F16M11/12Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction
    • F16M11/125Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction for tilting and rolling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon Stands for scientific apparatus such as gravitational force meters
    • F16M11/02Heads
    • F16M11/04Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
    • F16M11/06Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
    • F16M11/12Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction
    • F16M11/14Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting in more than one direction with ball-joint
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon Stands for scientific apparatus such as gravitational force meters
    • F16M11/02Heads
    • F16M11/18Heads with mechanism for moving the apparatus relatively to the stand

Description

May 6, 1947. w, LECK 2,419,999
ORIENTING MECHANISM FOR PULSE ECHO SYSTEMS Original Filed June 14, 1941 PULJ E RECEIVER JP/VISE 41 7267747018 JP/Mss 04 ram/m me Mame Zinnentor fical qefiflcaii /r 58 attorneg Patented May 6 1947 JUNITE'D STATES P EN OFFICE I 419,999 I V ORIENTING MECHANISM-FQKPULSE cno V;SYSTEMS George Leck, Princeton Junction, N. J., as
1 sig'nor to Radio Corporation of America, a corporation of Delaware Original application June 14, 1 941, Serial,No. 398,057. Divided and this applicationjuly 27, 1942, Serial No. 452,392
4. Claims. (Cl.-a250-1:72)
. application is a division of my copending noid type motors I09 are-preferablymounted at application Serial No. 398,057; filed June 14, .1941, 120 intervals. The motorseach includeapolarentitled Qrienting mechanisms for pulse echo izedmagnetic armature or movable member III.
systems. The movable members -III areconnected by This :invention relates to scanning devices and .5 suitable links 3 to bearings H5 on the outer fiparticula'rly to improvements in devices for varyportion of the antenna reflector or other antenna the direction of a beam of energy from a member. The field coils of the motors are enerpulsetecho system and for directing in synchrogized by a three phase alternator I I1, which -is *nismtherewith the scanning beam of a cathode driven by a motor H9. The shaft I20 of the ray. indicator. alternator, or the driving motor I I9, is connected Pulse echosystems are used to detect objects through suitable gearing I2I to a rheostat I23 in and to indicate the direction-and distance of the the generator exciter circuit I24. The generator object. In such systems a directive antenna is output is thus varied according toany desired generally used for the pulse transmission and a pattern so that the three phase output voltage non-directive antenna-may servefor reception or follows, for example, a sawtooth pattern. The
vice versa, or directive antennas may be used for -motors I09 are successively energized by the three both transmission and reception. phase currents so that the antenna system under- While separate antennas may be used, the ingoes a circular rocking movement of an amplistant invention is described by referring to a tude varying according to the generator output. single directive antenna which may be used for The resulting antenna beam deflections follow a both transmission and reception. Such an anspiral pattern. That is, as the applied'voltages tenna system is described in the copending apincrease, because of the sawtooth wave form of plication Serial No. 184,354, filed January 11, the generator exciting voltage, the motors I09 1938, by Wolff and Hershberger for Signaling produce larger and larger movements and since system. the movements are preferably at 120 intervals in One of the objects of the instant invention is space and in time, the axis I26 of the antenna to provide improved means for scanning aregion I28 traces a helical pattern and the beam of by a beam of pulse energy. Another object is pulses from the antenna scan a, conical or hemito provide improved means for moving a beam of spherical region. The antenna system is conpulse energy and a cathode ray beam in synnected by a transmission line 49 to a pulse transchronism. Another object is to provide means mitter 5| and to a pulse receiver 53. The output for directing a beam of pulses throughout a conof the pulse receiver is applied to the control ical region and for synchronously directing a electrodes of the cathode ray tube I32 so that cathode ray beam in a helical pattern. received signals may brighten or dim the cathode The invention will be described by referring ray trace. The three phase currents may be apto the accompanying drawing, of which Fig. 1 is plied to a three coil deflecting system I30 ara schematic diagram of one embodiment providranged around the cathode ray indicator I32 to ing an electro-mechanical scanning, and Fig. 2 is rotate the cathode ray in synchronism with the a circuit diagram of a modification of Fig. 1, rotations of the antenna, and the sawtooth volt- Similar reference characters are applied to ages may be applied to produce radial movesimilar elements throughout the drawing. ments. The cathode ray will trace a helical pat- In my co-pending application, of which this tern on the fluorescent screen of the indicator, application is a division, there i described a mewhich may be provided with a suitable calibrated chanical system whereby a directive antenna is scale I34 to indicate the position of the reflectcaused to traverse a conical region. The connecing object with respect to predetermined cotions to the antenna from the pulse transmitting ordinates.
and receiving apparatus may be made as de- Instead of using polarized magnetic armatures scribed in the copending application of Wolff and in the solenoid motors I09 and applying sawtooth Hershberger mentioned heretofore. Fig. 1 proexciting voltages to the three phase generator, vides an electro-mechanical drive for actuating 59 the movable motor members III may be consist of the scanning mechanism of the directional ana second solenoid II2 to which the sawtooth tenna system. The directive antenna system IIII voltages from the potentiometer I23 may be apis mounted in a ball and socket or other universal plied. Under these circumstances, the three joint I03 which is supported by a post I05 exphase currents are applied, as shown in Fig. 2 tending from the base member I01. Three soleto the fixed windings and the direct currents are applied to the movable windings, or vice versa, so that the antennas will be deflected by variable amounts so that its axis follows a helical path as before. In either arrangement the connecting rods may be provided with biasing springs I25 to maintain. the zero or central position of the antenna, which has been omitted to avoid com plicating the diagram.
Thus the invention has been described as an improved means for scanning aregion by means of a beam of pulses. A cathode ray is moved in synchronism with the scanningbeam. Received pulse echoes are applied to modulate or vary the cathode ray so that an object will be indicated according to predeterminedcoordinates on the cathode ray tube screen. In this manner the sky from the horizon upwardly may be continuously scanned and reflections from an aircraft or surface vessel coming over the horizon will indicate the azimuth and elevation of the craft.
I claim as my invention:
1. A pulse echo scanning device including, in
combination, a directive antenna for radiating a beam of pulses and for receiving echo pulses from objects in said beam, a universal joint for supporting said antenna, three solenoid type motor each including a field winding and a movable member, means connecting said movable members to said antenna so that upon energizing said motors from a three phase source said antenna will follow a circular rocking movement, a radio receiver connected to said antenna and responsive to said echo pulses, a cathode ray indicator connected to said receiver for indicating said echo pulses, and means for deflecting said cathode ray in synchronism with said circular rocking movement.
2. A device according to claim 1 including means for varying the amount of energy applied to said motors so that the amplitude of said circular rocking movement is correspondingly varied. 3. A radio beam scanning device including an antenna system for establishing a sharply defined beam, a universal mounting for supporting said antenna system, three solenoid type motors each including a field winding and a movable member, means connecting said movable members to said antenna system, and means for energizing said motors from a three phase source so that said antenna will follow a circular rocking move- .ment.
4. A device according to claim 3 including means for varying the amplitude of said circular rocking movement.
GEORGE W. LECK.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
US452392A 1941-06-14 1942-07-27 Orienting mechanism for pulse echo systems Expired - Lifetime US2419999A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US452392A US2419999A (en) 1941-06-14 1942-07-27 Orienting mechanism for pulse echo systems

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US398057A US2410666A (en) 1941-06-14 1941-06-14 Orienting mechanism for pulse echo systems
US452392A US2419999A (en) 1941-06-14 1942-07-27 Orienting mechanism for pulse echo systems

Publications (1)

Publication Number Publication Date
US2419999A true US2419999A (en) 1947-05-06

Family

ID=27016102

Family Applications (1)

Application Number Title Priority Date Filing Date
US452392A Expired - Lifetime US2419999A (en) 1941-06-14 1942-07-27 Orienting mechanism for pulse echo systems

Country Status (1)

Country Link
US (1) US2419999A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2624043A (en) * 1946-01-23 1952-12-30 Harry L Gerwin Visual communication system
US2638035A (en) * 1951-01-29 1953-05-12 Automatic Temperature Control Co Inc Electrically controlled tiltable reflecting mirror device
US2733437A (en) * 1956-01-31 maeder
US3005200A (en) * 1954-03-15 1961-10-17 Thomas R O'meara Three-element, vector-phase radio direction finder
US3013392A (en) * 1957-02-28 1961-12-19 Gen Motors Corp Remote control positioning mechanism
US3071036A (en) * 1960-08-31 1963-01-01 William B Mcknight Nutational scanning mirror
US4538880A (en) * 1982-08-09 1985-09-03 The Boeing Company Electrodynamic scanner and stabilizer

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US503602A (en) * 1893-08-22 Electric search-light
US1654067A (en) * 1926-08-16 1927-12-27 Anderson Lawrence Electric headlight control
DE487861C (en) * 1928-10-02 1930-06-28 Emil Groh Dimmable headlights, especially for motor vehicles
US2003661A (en) * 1932-05-16 1935-06-04 Sperry Gyroscope Co Inc Searchlight director
US2151549A (en) * 1936-07-06 1939-03-21 Gen Electric Aircraft landing equipment
US2231929A (en) * 1937-04-29 1941-02-18 Sperry Gyroscope Co Inc Tridimensional radio direction indicator
US2257320A (en) * 1937-11-06 1941-09-30 Charles E Williams Direction finding system

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US503602A (en) * 1893-08-22 Electric search-light
US1654067A (en) * 1926-08-16 1927-12-27 Anderson Lawrence Electric headlight control
DE487861C (en) * 1928-10-02 1930-06-28 Emil Groh Dimmable headlights, especially for motor vehicles
US2003661A (en) * 1932-05-16 1935-06-04 Sperry Gyroscope Co Inc Searchlight director
US2151549A (en) * 1936-07-06 1939-03-21 Gen Electric Aircraft landing equipment
US2231929A (en) * 1937-04-29 1941-02-18 Sperry Gyroscope Co Inc Tridimensional radio direction indicator
US2257320A (en) * 1937-11-06 1941-09-30 Charles E Williams Direction finding system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2733437A (en) * 1956-01-31 maeder
US2624043A (en) * 1946-01-23 1952-12-30 Harry L Gerwin Visual communication system
US2638035A (en) * 1951-01-29 1953-05-12 Automatic Temperature Control Co Inc Electrically controlled tiltable reflecting mirror device
US3005200A (en) * 1954-03-15 1961-10-17 Thomas R O'meara Three-element, vector-phase radio direction finder
US3013392A (en) * 1957-02-28 1961-12-19 Gen Motors Corp Remote control positioning mechanism
US3071036A (en) * 1960-08-31 1963-01-01 William B Mcknight Nutational scanning mirror
US4538880A (en) * 1982-08-09 1985-09-03 The Boeing Company Electrodynamic scanner and stabilizer

Similar Documents

Publication Publication Date Title
US2410666A (en) Orienting mechanism for pulse echo systems
US2409456A (en) Radiant energy locating system
US2440777A (en) Tridimensional radio direction indicator
US2263377A (en) System for indicating the direction of propagation of electromagnetic waves
US2585855A (en) Radar ground-controlled approach system for aircraft
US2410831A (en) Scanning device
US2426217A (en) Direction and distance indicating system
US2514828A (en) Synthesized stereoscopic vision
US2419999A (en) Orienting mechanism for pulse echo systems
US2526314A (en) Radio detection and ranging system employing multiple scan
US3790943A (en) Radio frequency antenna system
US2455673A (en) Distance selective system
GB626351A (en) Improvements in or relating to radar systems
US2617093A (en) Radio apparatus for indicating speed and course of objects
US2524295A (en) Pulse-echo radio locator system
US2761134A (en) Means for operating antennas
US2458175A (en) Directive antenna control system
US2510692A (en) Direction finding system
US2557967A (en) Scanning apparatus for radar systems
US2518968A (en) Radar system providing plan position indicator and elevation views
US2569485A (en) Automatic ranging system
US2563998A (en) Direction finding apparatus
US2548900A (en) Data presentation apparatus
US2589813A (en) Antenna positioning system
US3613096A (en) Radio beacon