US3117318A - Radar reflector - Google Patents
Radar reflector Download PDFInfo
- Publication number
- US3117318A US3117318A US25583A US2558360A US3117318A US 3117318 A US3117318 A US 3117318A US 25583 A US25583 A US 25583A US 2558360 A US2558360 A US 2558360A US 3117318 A US3117318 A US 3117318A
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- bodies
- reflector
- radar
- assembly
- reflectors
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q15/00—Devices for reflection, refraction, diffraction or polarisation of waves radiated from an antenna, e.g. quasi-optical devices
- H01Q15/14—Reflecting surfaces; Equivalent structures
- H01Q15/18—Reflecting surfaces; Equivalent structures comprising plurality of mutually inclined plane surfaces, e.g. corner reflector
Definitions
- This invention relates to improvements in radar reflectors. More particularly it has reference to reilectors of the character of that disclosed in a United States Patent Number 2,763,000 issued on September l1, 1956 to Edward K. P. Graham, described as comprising eight pyramidic reecting bodies combined into a unit to provide reflecting power in all directions in a single plane.
- the present invention resides in certain improvements in radar reflectors of the general character of the disclosure of the above identified Graham patent which provides, by reason of a certain change in relationship of the relecting bodies, a unit of greater eillciency, which improves the target brightness on the viewing screen; which is more compact in its construction; which provides that all reflected rays will be reflected parallel to the incident rays, and which provides that the reilector unit can be rotated 45 in elevation or 360 azimuth with substantially constant performance.
- the present invention resides in the specillc arrangement and relationship of the eight trihedral reflectors assembled in a circle to form a composite retlector that is especially useful on small boats and which will perform well through 360 of rotation regardless of roll or pitch of the reflector support.
- the present invention is based upon that principle of radar operation that a pulse of high frequency energy transmitted in the form of a narrow beam will be rellected, at least in part, by a target object, back toward the pulse transmitter for reception and presentation as a pip on the viewing screen of the radar set.
- the brightness of the target, as it appears on the screen is a function of the amount of energy reflected to the radar set by the target.
- FIG. l is a top view of the present reflector showing eight pyramidic reflecting bodies, as assembled for normal use of the reilector.
- FIG. 2 is a side View of the assembly of reflecting bodies shown in FIG. 1.
- FIG. 3 is a vertical, cross-section of the reflector, taken on line 3 3 in FIG. l.
- FIG. 4 is a horizontal section, taken on line 4 4 in FIG. 2.
- the present eight reilector bodies are symmetrically arranged about a central vertical axial line AI. equally spaced therefrom at 45 intervals.
- the unit provided by the arrangement of reector bodies will herein be described as comprising an upper assembly of four bodies, each of which bodies is designated, in its entirety, by reference numeral lila, and a lower assembly of four bodies, each of which is designated, in its entirety, by reference numeral b.
- the four bodies 10a comprising the upper assembly are mounted at the same horizontal level, outwardly faced relative to the common axial line AL and equally spaced therefrom with the outer bounding edges of their three sides coinciding with the four vertical sides of a square.
- the four bodies 10b of the lower assembly likewise, are mounted at the same horizontal level; are faced outwardly and are evenly spaced from the central axial line AL of the unit, at intervals thereabout with their bounding edges at the open side of the trihedral reflectors, likewise coinciding with the four sides of a square but which square has been rotatably advanced 45 relative to the square rst mentioned in connection with the description of the upper assembly.
- Each reflector body comprises three equally dimensioned sidewalls of isosceles triangular form, each with a 90 vertex angle and 45 base angles; these three angles being designated, in FIG. 2, at a, b and b, respectively.
- the base edges of the triangular top walls of the upper trihedral bodies coincide with the same horizontal plane. It has been shoum in FIG. 1 that the top walls of two adjacent reilector bodies are riveted or otherwise xedly secured to angularly directed flanges Zllf at opposite ends of upper horizontal supporting plates 2li-20.
- the two upper horizontal plates 20-20' are fixedly joined at their inside edges, as shown at 21 in FIG. 1, to rigidly secure the four reflecting bodies of the upper assembly in that 90 angular relationship in which they are shown in FIGS. 1 and 3.
- the four reflector bodies 10b of the lower assembly have the bottom walls thereof similarly llxed to the lower horizontal supporting plates 25--25 and are held thereby in a 90 angular relationship to each other, but in the illustrated 45 angular relationship to the bodies of the upper set that has been shown particularly in FIGS. 1 and 4 of the drawings.
- each assembly is horizontally spaced. It is further to be observed that the base edges of the sidewalls of each of the reflector bodies of the lower assembly converge upwardly and are disposed between the downwardly diverging sidewalls of adjacent reflector bodies of the upper set. The reversed position of bodies of the upper and lower assemblies permits the four bodies of each assembly to be alternately received between bodies of the other assembly, as has been well shown in FIGS. 2 and 4.
- the horizontal supporting plates Ztl- 20' and 25-25 that mount the assemblies of units are recessed at their inside edges to provide central Vertical passages designated by numeral 50 in FIG. l.
- the mast is adapted to extend vertically through the passages 50.
- a pair of elongated angle members or clamping bars 51 are mounted in parallel relationship on the upper surface of plates Ztl-20. The ends of each clamping bar extend over a pair of elongated apertures 60 provided in the plates 20-20, and as shown in FIGURE 1, the apertures 60 extend perpendicular to the longitudinal axis of the clamping bars 51. Screws 62 extend vertically downwardly through bores formed in the ends of the clamping bars 51 and through the apertures 60.
- Each angle member or clamping bar 51 includes a vertically extending leg which has bores provided in each end thereof. Threaded studs 66 extend through these bores and each stud 66 has a nut 68 threaded on each of its outer ends as shown in FIGURE 1. The studs 66 also extendV across diametrically opposite sides of the passages 50 and in perpendicular relationship to the clamping bars 51.
- the plates 25-25' also have a pair of clamping barsV 51" secured to their lower surfaces in the same manner andV by the same means as the bars 51 are secured to the plates Ztl-20.
- the clamping bars 51 also adjustably connected together by threaded studs 66' as shown in FIG- URE 3. To secure the antenna unit to a mast extending through the passages 50, it is only necessary to loosen the nuts 64 and then urge the clamping bars into clamping engagement with the mast by rotating the nuts 68 onto the studs 66. This permits the screws 62 to slide within the apertures 60. The nuts 64 are then tightened on the screws 62 to secure the clamping bars tothe mounting plates.
- a pulse transmitted from a radar set will be' received thereby from any horizontal direction and will be reflected back along lines parallel to the lines of the transmitted pulse to give a bright target indication on the radar screen.
- a radar reflector unit comprising eight substantially identical reflectors, each reector comprising three plates of isosceles triangular form joined together at their edges so as to form a pyramid having three closed sides converging to an apex and an open triangular base having three edges of equal length, a rst group comprising four of said reectors and a second group comprising four of said reectors, the reilectors of each group xedly arranged in equal angular spacing about a vertical axis, the bases of both groups of reflectors each lying in substantially vertical planes and the apexes of both groups of reectors located between said bases and said axis, the basesA of the rst group having upper edges dening a rst squareA and lying in an upper horizontal plane, the bases of the second group having lower edges defining a second square of the same size as said rst square being angularly displaced 45 about said axis relative to said rst
Description
Jan. 7, 1964 w. L. JONES 3,117,318
RADAR REFLECTOR Filed April 29, 1960 2 sheets-sheet 1 L 1NVENTOR W/Lu/e L. JONES ATTORNEYASl W. L. JONES RADAR REFLECTOR 2 Sheets-Sheet 2 Filed April 29, 1960 INVENTOR MLBUR L. JONES ATTORNEYJ nited States ate Wash., assigner of one-half to Stanley T. Lovejoy, Seattle, Wash.
Fired Apr. 2s, 1960, ser. No. 25,583 1 claim. (el. 343-18) This invention relates to improvements in radar reflectors. More particularly it has reference to reilectors of the character of that disclosed in a United States Patent Number 2,763,000 issued on September l1, 1956 to Edward K. P. Graham, described as comprising eight pyramidic reecting bodies combined into a unit to provide reflecting power in all directions in a single plane.
The present invention resides in certain improvements in radar reflectors of the general character of the disclosure of the above identified Graham patent which provides, by reason of a certain change in relationship of the relecting bodies, a unit of greater eillciency, which improves the target brightness on the viewing screen; which is more compact in its construction; which provides that all reflected rays will be reflected parallel to the incident rays, and which provides that the reilector unit can be rotated 45 in elevation or 360 azimuth with substantially constant performance.
More specifically stated, the present invention resides in the specillc arrangement and relationship of the eight trihedral reflectors assembled in a circle to form a composite retlector that is especially useful on small boats and which will perform well through 360 of rotation regardless of roll or pitch of the reflector support.
The present invention is based upon that principle of radar operation that a pulse of high frequency energy transmitted in the form of a narrow beam will be rellected, at least in part, by a target object, back toward the pulse transmitter for reception and presentation as a pip on the viewing screen of the radar set. The brightness of the target, as it appears on the screen is a function of the amount of energy reflected to the radar set by the target.
In the present instance, brightness of the pip is enhanced by the improved arrangement of the radar reilectors, as will later be explained.
In accomplishing the previously mentioned and other objects of the present invention, I have provided the improved details of construction and assembly, the preferred forms of which are illustrated in the accompanying drawings, wherein:
FIG. l is a top view of the present reflector showing eight pyramidic reflecting bodies, as assembled for normal use of the reilector.
FIG. 2 is a side View of the assembly of reflecting bodies shown in FIG. 1.
FIG. 3 is a vertical, cross-section of the reflector, taken on line 3 3 in FIG. l.
FIG. 4 is a horizontal section, taken on line 4 4 in FIG. 2.
Referring more in detail to the drawings:
It has been well shown in FIG. l that the present eight reilector bodies are symmetrically arranged about a central vertical axial line AI. equally spaced therefrom at 45 intervals. The unit provided by the arrangement of reector bodies will herein be described as comprising an upper assembly of four bodies, each of which bodies is designated, in its entirety, by reference numeral lila, and a lower assembly of four bodies, each of which is designated, in its entirety, by reference numeral b. The four bodies 10a comprising the upper assembly are mounted at the same horizontal level, outwardly faced relative to the common axial line AL and equally spaced therefrom with the outer bounding edges of their three sides coinciding with the four vertical sides of a square.
The four bodies 10b of the lower assembly, likewise, are mounted at the same horizontal level; are faced outwardly and are evenly spaced from the central axial line AL of the unit, at intervals thereabout with their bounding edges at the open side of the trihedral reflectors, likewise coinciding with the four sides of a square but which square has been rotatably advanced 45 relative to the square rst mentioned in connection with the description of the upper assembly.
Each reflector body comprises three equally dimensioned sidewalls of isosceles triangular form, each with a 90 vertex angle and 45 base angles; these three angles being designated, in FIG. 2, at a, b and b, respectively. The base edges of the triangular top walls of the upper trihedral bodies coincide with the same horizontal plane. It has been shoum in FIG. 1 that the top walls of two adjacent reilector bodies are riveted or otherwise xedly secured to angularly directed flanges Zllf at opposite ends of upper horizontal supporting plates 2li-20. The two upper horizontal plates 20-20' are fixedly joined at their inside edges, as shown at 21 in FIG. 1, to rigidly secure the four reflecting bodies of the upper assembly in that 90 angular relationship in which they are shown in FIGS. 1 and 3.
The four reflector bodies 10b of the lower assembly have the bottom walls thereof similarly llxed to the lower horizontal supporting plates 25--25 and are held thereby in a 90 angular relationship to each other, but in the illustrated 45 angular relationship to the bodies of the upper set that has been shown particularly in FIGS. 1 and 4 of the drawings.
It is to be observed by reference to FIGS. 1 and 2 that the four reflector bodies that constitute each assembly are horizontally spaced. It is further to be observed that the base edges of the sidewalls of each of the reflector bodies of the lower assembly converge upwardly and are disposed between the downwardly diverging sidewalls of adjacent reflector bodies of the upper set. The reversed position of bodies of the upper and lower assemblies permits the four bodies of each assembly to be alternately received between bodies of the other assembly, as has been well shown in FIGS. 2 and 4. It will further be understood that, by reason of the isosceles triangular form of the wall forming members of the eight reflector bodies, the disposition of bodies of one group between bodies of the other group provides for the crossing or overlapping of the upper corner portions of the upper assembly of bodies with the lower corner portions of the lower assembly of bodies, as has been illustrated both in FIGS. 1 and 4.
To functionally support the unit from a vertical mast or pole, not shown, the horizontal supporting plates Ztl- 20' and 25-25 that mount the assemblies of units are recessed at their inside edges to provide central Vertical passages designated by numeral 50 in FIG. l. The mast is adapted to extend vertically through the passages 50. A pair of elongated angle members or clamping bars 51 are mounted in parallel relationship on the upper surface of plates Ztl-20. The ends of each clamping bar extend over a pair of elongated apertures 60 provided in the plates 20-20, and as shown in FIGURE 1, the apertures 60 extend perpendicular to the longitudinal axis of the clamping bars 51. Screws 62 extend vertically downwardly through bores formed in the ends of the clamping bars 51 and through the apertures 60. A nut 64 is threaded on the lower end of each screw 62 so that when the nuts are tightened, the clamping bars 51 are secured to the plates 20-20. Each angle member or clamping bar 51 includes a vertically extending leg which has bores provided in each end thereof. Threaded studs 66 extend through these bores and each stud 66 has a nut 68 threaded on each of its outer ends as shown in FIGURE 1. The studs 66 also extendV across diametrically opposite sides of the passages 50 and in perpendicular relationship to the clamping bars 51. The plates 25-25' also have a pair of clamping barsV 51" secured to their lower surfaces in the same manner andV by the same means as the bars 51 are secured to the plates Ztl-20. The clamping bars 51 also adjustably connected together by threaded studs 66' as shown in FIG- URE 3. To secure the antenna unit to a mast extending through the passages 50, it is only necessary to loosen the nuts 64 and then urge the clamping bars into clamping engagement with the mast by rotating the nuts 68 onto the studs 66. This permits the screws 62 to slide within the apertures 60. The nuts 64 are then tightened on the screws 62 to secure the clamping bars tothe mounting plates.
Assuming that thev reflecting unit is so constructed and properly mounted by a vertical mast, a pulse transmitted from a radar set will be' received thereby from any horizontal direction and will be reflected back along lines parallel to the lines of the transmitted pulse to give a bright target indication on the radar screen.
The angular and intermeshed arrangement of reflectors of the two assemblies places them at the same horizontal level, and in a compact circular arrangement, not disclosed in any similar. device known. to me.
There is a proven and decided advantage in that overlapping relationship of units of the upper and lower groups, shown in FIGS. 1 and 4, that is made possible by the spacing of the units in each group so that the vertex portions of their outwardly opening end areas can be brought within the base angle or corner portions of adjacent reflector bodies of the other group.
The details of construction provide a relatively simple and inexpensive unit to manufacture and the unit may be readily applied to or removed from a mast or the like.
What I claim as new is:
A radar reflector unit comprising eight substantially identical reflectors, each reector comprising three plates of isosceles triangular form joined together at their edges so as to form a pyramid having three closed sides converging to an apex and an open triangular base having three edges of equal length, a rst group comprising four of said reectors and a second group comprising four of said reectors, the reilectors of each group xedly arranged in equal angular spacing about a vertical axis, the bases of both groups of reflectors each lying in substantially vertical planes and the apexes of both groups of reectors located between said bases and said axis, the basesA of the rst group having upper edges dening a rst squareA and lying in an upper horizontal plane, the bases of the second group having lower edges defining a second square of the same size as said rst square being angularly displaced 45 about said axis relative to said rst square, the apexes and bases of all said reflectors being substantially equally spaced from said axis, each base of each group having a corner vertically spaced from its horizontal edge which lies substantially in the horizontal plane defined by the horizontal edges of bases of the other group, the bases of all said reflectors delining a polygon having eight equal sides, and securing means securing all said reflectors together and adapted to secure said reflector unit to a vertical mast coaxial with said axis, said securing means comprising spaced upper and lower horizontal plates each having canted edges secured to said reflectors and each having a central opening therethrough adapted to receive said mast therethrough, a pair of parallel clamping bars on opposite sides of each opening, means adjustablyV securing each pair of clamping bars to one of said horizontal plates and a pair of threaded members extending perpendicular to each pair of said clamping bars and adjustably connecting their ends together whereby the bars may be urged into gripping relationship with said mast.
References Cited in the le of this patent UNITED STATES PATENTS 540,093 Fitzgerald May 28, 1895 2,763,000 Graham Sept. 1l, 1956 3,010,103 Hopper et al. Nov. 21, 1961 3,041,603 Davis June 26, 1962 FOREIGN PATENTS 727,512 Great Britain Apr. 6, 1955 966,872' Germany Sept. 12, 1957
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US25583A US3117318A (en) | 1960-04-29 | 1960-04-29 | Radar reflector |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US25583A US3117318A (en) | 1960-04-29 | 1960-04-29 | Radar reflector |
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US3117318A true US3117318A (en) | 1964-01-07 |
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US25583A Expired - Lifetime US3117318A (en) | 1960-04-29 | 1960-04-29 | Radar reflector |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3371345A (en) * | 1966-05-26 | 1968-02-27 | Radiation Inc | Radar augmentor |
US3421137A (en) * | 1966-02-23 | 1969-01-07 | Us Navy | Echo repeater and/or target simulator |
JPS49124930U (en) * | 1973-02-23 | 1974-10-25 | ||
DE2550709A1 (en) * | 1975-11-12 | 1977-05-18 | Hans E Dr Ing Speckter | Cluster reflector for targets with weak reflections - consists of six corner reflectors with their axes of symmetry at specified angles to each other |
EP0032604A1 (en) * | 1980-01-16 | 1981-07-29 | Vesteralen Industrier A/S | Radar reflector |
WO1989007840A1 (en) * | 1988-02-19 | 1989-08-24 | Woodville Polymer Engineering Limited | Radar reflectors |
US5474264A (en) * | 1992-05-18 | 1995-12-12 | Aerospatiale Societe Nationale Industrielle | Low mass velocity-aberration correcting retroreflector geodetic satellite |
US5570230A (en) * | 1993-12-31 | 1996-10-29 | Aerospatiale Societe Nationale Industrielle | Retroreflector for laser geodesy with omnidirectional correction of speed aberrations |
WO2019012503A1 (en) * | 2017-07-14 | 2019-01-17 | Tubitak | Omnidirectional back reflection passive decoy |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US540093A (en) * | 1895-05-28 | Combined pipe-holder and vise | ||
GB727512A (en) * | 1952-11-14 | 1955-04-06 | Nat Res Dev | Improved radar reflector |
US2763000A (en) * | 1952-10-16 | 1956-09-11 | Sveuska Aktiebolaget Gasaccumu | Reflector for radar purposes |
DE966872C (en) * | 1955-03-31 | 1957-09-12 | Julius & August Erbsloeh K G | Radar reflector for ships |
US3010103A (en) * | 1956-01-16 | 1961-11-21 | Del Mar Eng Lab | Radar reflective tow target |
US3041603A (en) * | 1955-01-26 | 1962-06-26 | Charles W Davis | Passive reflector for microwave links |
-
1960
- 1960-04-29 US US25583A patent/US3117318A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US540093A (en) * | 1895-05-28 | Combined pipe-holder and vise | ||
US2763000A (en) * | 1952-10-16 | 1956-09-11 | Sveuska Aktiebolaget Gasaccumu | Reflector for radar purposes |
GB727512A (en) * | 1952-11-14 | 1955-04-06 | Nat Res Dev | Improved radar reflector |
US3041603A (en) * | 1955-01-26 | 1962-06-26 | Charles W Davis | Passive reflector for microwave links |
DE966872C (en) * | 1955-03-31 | 1957-09-12 | Julius & August Erbsloeh K G | Radar reflector for ships |
US3010103A (en) * | 1956-01-16 | 1961-11-21 | Del Mar Eng Lab | Radar reflective tow target |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3421137A (en) * | 1966-02-23 | 1969-01-07 | Us Navy | Echo repeater and/or target simulator |
US3371345A (en) * | 1966-05-26 | 1968-02-27 | Radiation Inc | Radar augmentor |
JPS49124930U (en) * | 1973-02-23 | 1974-10-25 | ||
JPS5349313Y2 (en) * | 1973-02-23 | 1978-11-27 | ||
DE2550709A1 (en) * | 1975-11-12 | 1977-05-18 | Hans E Dr Ing Speckter | Cluster reflector for targets with weak reflections - consists of six corner reflectors with their axes of symmetry at specified angles to each other |
EP0032604A1 (en) * | 1980-01-16 | 1981-07-29 | Vesteralen Industrier A/S | Radar reflector |
WO1989007840A1 (en) * | 1988-02-19 | 1989-08-24 | Woodville Polymer Engineering Limited | Radar reflectors |
US4996536A (en) * | 1988-02-19 | 1991-02-26 | Woodville Polymer Engineering Limited | Radar reflectors |
US5474264A (en) * | 1992-05-18 | 1995-12-12 | Aerospatiale Societe Nationale Industrielle | Low mass velocity-aberration correcting retroreflector geodetic satellite |
US5570230A (en) * | 1993-12-31 | 1996-10-29 | Aerospatiale Societe Nationale Industrielle | Retroreflector for laser geodesy with omnidirectional correction of speed aberrations |
WO2019012503A1 (en) * | 2017-07-14 | 2019-01-17 | Tubitak | Omnidirectional back reflection passive decoy |
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