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US3631505A - Expandable antenna - Google Patents

Expandable antenna
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Publication number
US3631505A
US3631505AUS21745AUS3631505DAUS3631505AUS 3631505 AUS3631505 AUS 3631505AUS 21745 AUS21745 AUS 21745AUS 3631505D AUS3631505D AUS 3631505DAUS 3631505 AUS3631505 AUS 3631505A
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United States
Prior art keywords
arms
linked
contour
hub
fully extended
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Expired - Lifetime
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US21745A
Inventor
Robert R Carman
Howard W Barrett
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Lockheed Martin Tactical Systems Inc
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Goodyear Aerospace Corp
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Assigned to LORAL CORPORATIONreassignmentLORAL CORPORATIONASSIGNMENT OF ASSIGNORS INTEREST.Assignors: GOODYEAR AEROSPACE CORPORATION
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Abstract

The invention relates to a large expandable antenna or reflector which can be packaged in a small volume. The antenna can be parabolic, spherical or flat. Radial ribs, interconnected in a scissorslike pattern, extend from a center hub. One set of the elements are fabricated to the desired reflector contour while the alternate elements are straight elements which deploy and support the contour elements. A flexible screen or reflector surface between the contoured elements provides the reflector surface.

Description

United States Patent Inventors Robert R. Cannan Tallmadge; Howard W. Barrett, Akron, both of Ohio App]. No. 21,745 Filed Mar. 23, 1970 Patented Dec. 28, 1971 Assignee Goodyear Aerospace Corporation Akron, Ohio EXPANDABLE ANTENNA 7 Claims, 7 Drawing Figs.
11.8. CI 343/915 Int. Cl H0lq 15/20 Field of Search 343/840,
[56] References Cited UNITED STATES PATENTS 3,496,687 2/1970 Greenberg et al. 343/915 2,945,234 7/1960 Driscoll 343/915 3,174,397 3/1965 343/915 3,406,404 10/1968 343/915 3,509,576 4/1970 McLain 343/840 Primary Examiner-Eli Lieberman Attorneys.l. G. Pere and L. A. Germain PATENTEU BEB28 :sn
SHEET 2 [IF 4 mvsmons HOWARD W BARRETT ROBERT R. CARMAN ATTORNEYS PAIENTED M628 1971 SHEET 3 [IF 4 FIG.3
INVENTORS ATTORNEYS Pmzmmmzemn Y 3.631.505
SHEET [1F 4 ATTORNEYS EXPANDABLE ANTENNA Heretofore it has been known that there have been many and various types of packageable antennas which may be deployed from a small packaged configuration to a larger reflective configuration. Certain of these antennas have utilized a lazy tong construction for deployment such as U.S. Pat. No. 1,851,178, 1,689,337, and 3,213,457. However, none of these prior art structures have included the ability to achieve a predetermined surface contour through such lazy tong structure for deployment. Hence, their adaptability to large complex curved reflectors is not apparent or possible.
Therefore, it is the general object of the invention to provide a large expandable antenna or reflector which can be packaged in a small volume that utilizes a lazy tong deployment structure, but wherein the reflector surface can be parabolic, spherical or flat.
A further object of the invention is to provide a low-cost, packageable, but highly reliable expandable antenna that will achieve a high degree of precision in its reflective service upon expansion.
The aforesaid objects of the invention and other objects which will become apparent as the description proceeds are achieved by providing an expandable antenna which comprises a plurality of linked arms arranged in pairs as a lazy tong, a plurality of such lazy tongs arranged in radially directed equally spaced manner about a central point, means to effect controlled extension and retraction of the linked arms from the ends adjacent said center point, one pair of linked arms of each set of lazy tongs defining a predetermined complex shape when fully extended, and the other pair of linked arms having a greater extended length and effecting supporting action of said one pair of linked arms, and flexible reflector means connected between said one pair of linked arms to form a reflective surface when said arms are fully extended.
For a better understanding of the invention, reference should be had to the accompanying drawings wherein FIG. I is a perspective view of the antenna of the invention in the fully stowed relationship in a suitable storage container;
FIG. 2 is a perspective view of the antenna of FIG. 1 in the partially deployed condition;
FIG. 3 is a perspective view of the antenna of FIG. 1 in the fully deployed condition;
FIG. 4 is a perspective view of the antenna of FIG. 1 showing a single lazy tong arm in the fully deployed position;
FIG. 5 is an enlarged side elevational view of the hinged relation of the set of links defining the contoured configuratron;
FIG. 6 is an enlarged view of the adjustable relationship of the supporting links; and
FIG. 7 is a schematic view of the link relationship showing how the pivoted position of the supporting links must be determined.
With reference to the embodiment of the invention illustrated in the drawings, thenumeral 10 indicates generally a packageable antenna which in its stowed condition can be carried inside a small cylindrically shaped container 12 for example. Essentially, the structure of theantenna 10 comprises abase hub 14 which normally may be fixed to the base 14a of the container 12. Amovable hub 16 is provided which may preferably be guided in a movable parallel relationship tohub 14 by slidably engaging a plurality of rods indicated generally by numeral 18 extending perpendicularly from the surface ofhub 14. The rod package 18 will slidably be received through appropriate holes in thehub 16. The invention preferably contemplates that the adjustable relationship ofhub 16 with relation tohub 14 may be achieved by a long screw 20 threadably received through the axis ofhub 16 and rotatably driven in controllable relationship by a motor 22 carried by thebase hub 14. Hence, it should be understood that rotation of a screw 20 in either direction will cause a slow but highly powerful controlled movement ofhub 16 relative to hub 14in either an outward or inward direction depending upon the direction of rotation of screw 20.
The invention contemplates that in order to prevent damage to themovable hub 16 and to the overall structure thatappropriate microswitches 24 and 26 be mounted on the top of the triangular rod frame 18 and thebase hub 14, respectively, as most clearly seen in FIG. 3. These switches 24 and 26 stop the motor 22 as the movable hub reaches and closes these switches during the movement thereof.
The essence of the invention is achieved by utilizing the base structure defined above with a plurality of lazy tong arrangements, each indicated generally bynumeral 30. These lazy tong arrangements are radially directed with respect to the hubs at substantially equal spaced angular positions, as best seen in FIG. 4.
Each of the lazy tongs comprises a series of levers pivotally linked at their ends in the usual lazy tong configuration. One set of levers is indicated generally by thenumeral 30 with the other set indicated generally bynumeral 32. Preferably, the invention contemplates that the levers will be made of metal and theset 30 will be pivotally connected at their radially inward end to themovable hub 16. It also should be noted that the pivoted end of thelevers 30 is enlarged and angled as at 30a so as to facilitate pivotal movement through relatively large angles. Also, it should be noted as illustrated in FIG. 6, that theends 30a are adjustably mounted tohub 16 byscrews 31. This adjustability allows proper alignment of thelevers 30 so that the configuration oflevers 32 will be proper, as more fully defined hereinafter.
The set oflevers 30 are pivotally connected at their ends bypins 30b, while the set oflevers 32 are pivotally connected at their ends bypins 32b. Thelever sets 30 are pivotally connected at about their center points to about the center points oflevers 32 byappropriate pins 34. The exact relation betweenlevers 30 and 32 will be defined hereinafter with reference to FIG. 7. Thelever sets 32 are fabricated to a desired reflector contour while the other set oflevers 30 are straight elements which deploy and support thecontour elements 32. Hence, in the example illustrated, thelevers 32 are contoured to a parabolic shape in their fully extended condition of FIG. 3. It can be seen that thelevers 30 are longer and hence are not fully extended when the lever set 32 is fully extended so that quite firm and adequate support of thecontoured levers 32 is achieved by thelevers 30 by somewhat of a truss arrangement. A reflective surface is provided by connecting a flexible screen between adjacentcontoured lever sets 32 so that this stretches tightly into position, as illustrated in FIG. 3, when the levers are fully extended. In order to more easily permit the flexiblereflective material 50 to be attached to the edges oflevers 32 without interferring with the movement oflevers 30, thelevers 32 are preferably made of parallel spaced side-by-side elements 320 and 32d, respectively, as is most clearly illustrated in FIG. 4 of the drawings, so thatlevers 30 can be pivotally received therebetween.
The parabolic reflector achieved by theflexible screen 50 betweenlever elements 32 is not bothered by the radial protrusion of those portions oflevers 30 which extend above the surface thereof. Further, the invention contemplates that when thelevers 32 are moved in from their lazy tong arrangement to the packaged configuration of FIG. 1 by the upward movement ofhub 16, that such curved levers orlengths 32 will tend to flatten to the straight line configuration oflevers 30. This is accomplished by designing thelevers 32 with a cross section to limit the induced stresses so that when flattened, they will be of value less than the yield stress of the material. This permits flattening when packaged to the configuration of FIG. 11, and a return to their parabolic curved configuration when extended to the full length by the lazy tong achieved by the movement ofhub 16.
Naturally, while the invention discloses a flexible screen reflector, any flexible material which might be designed to reflect electromagnetic or radio waves, or solar energy, might also be appropriately utilized. For example, some type of aluminized thin plastic sheet might be utilized for a solar reflective surface.
While the invention illustrates that the levers orelements 32 are doubleparallel bars 320 and 32d, the invention contemplates that any suitable type of construction to achieve the lazy tong relationship with a suitable curvature of theelements 32 and still allowing the attachment ofa flexible skin to the adjacent edges will certainly meet the objects of the invention. For example, a single lever with a small slot in the center thereof would achieve the same results as thedouble elements 32c and 32d. However, even if thelevers 30 are pivotally attached outside the edges oflevers 32, the flexible skin may simply extend therearound and accomplish the purposes of the invention.
FIG. 5 illustrates a spring loading of theelements 32. Essentially, this is achieved by providing a coiled spring 33 surrounding thehinge pins 32b and normally biasing theelements 32 to the open contoured position. Also, the invention contemplates that thehinge 32b may be of the type that limits the angular rotation between theelements 32 in the open direction and preferably limits this opened relationship to about 180 or slightly less to approximate the curved configuration between theelements 32.
FIG. 6 illustrates the adjustable pivoted relation of theends 30a oflevers 30. Essentially thescrew 31 is adjustable in height in relation tohub 16 by means ofnuts 31a and 31b respectively. The adjustment of the pivot point of theend lever 30 in effect controls the extension and contoured height ofelements 32. Hence, this adjustability is important.
FIG. 7 schematically illustrates the lazy tong at its fully extended position to achieve the necessary curvature of theelements 32. It is an important feature of the invention that the pivot points 30b forlevers 30 fall on lines essentially perpendicular to the pivot points 32b ofelements 32 as illustrated. The pivotal connection oflevers 30 toelements 32 then falls wherever they cross, as dictated by the pivotal connection of the ends oflevers 30 on the perpendiculars indicated bylines 29 in FIG. 7. If thelevers 30 are not so pivotally connected then theelements 32 will not properly unfold into the desired lazy tong configuration.
Hence, it is seen that the objects of the invention have been achieved by providing a lazy tong relationship with a fixed hub and a movable hub, limiting switches associated with the hub to control the extendable movement of the lazy tong, and wherein one of the sets of each lazy tong is shorter than the other, and has a contoured configuration so that when extended a desired shape and total around a central hub is achieved. It should be noted however, that the means to extend the lazy tong configuration is not important, except that some suitable means must be provided.
While in accordance with the patent statues only the best known embodiment of the invention has been illustrated and described in detail, it is to be particularly understood that the invention is not limited thereto or thereby, but that the inventive scope is defined in the appended claims.
What is claimed is:
1. An expandable antenna which comprises a pair of support hubs,
means to controllably move the hubs relative to each other,
a pair of sets linked arms arranged as a lazy tong structure having the end of one set of arms pivotally mounted to one hub, and the end of the other set of arms pivotally mounted to the other hub, which is characterized by the sets of arms defining the lazy tongs arranged in equally spaced radial relation around the entire circumference of the hubs, one set of arms of each such lazy tong defining a predetermined contour when extended to their full length, said other set of arms of each said lazy tong having a greater extended length and serving to support the fully extended length of said one set of arms, and
flexible reflector means attached between adjacent said one sets of arms which stretches tight to the contour of said one set of arms when extended to in combination define a desired contoured reflective surface, said contoured reflective surface being the same as would be geometrically generated by rotation of said one set of arms when extended about an axis through the center ofthe planes of the pair of hubs and normal thereto.
2. An antenna according to claim 1 where one of the hubs is fixed and the other hub is movable relative to the first hub, which includes a screw connecting said one hub in relative relation to the fixed hub, means to effect rotation of the screw, and means to limit rotation of the screw upon predetermined movement ofsaid one hub relative to the fixed hub.
3. An antenna according to claim 1 where said one set of arms has each length thereof performed to a predetermined contour, but where in the collapsed relationship of the lazy tong, said one set of arms is flattened to a straight configuration which is less than the yield point of the material of the arm.
4. An expandable structure which comprises a set of linked contour arms and a set of linked support arms arranged in pairs as a lazy tong, a plurality of identical such lazy tongs arranged in a radially directed equally spaced manner around a central axis, means to efl'ect controlled extension and contraction of the linked arms from the ends adjacent said central axis, the set of linked contour arms of each lazy tong defining a predetermined contour when fully extended, said contour falling in the surface of a contoured figure generated by rotation of a set of fully extended linked contoured arms about said central axis, and the set of linked support arms having a greater extended length and forming triangular support for said set of linked contour arms at their fully extended length, and flexible means connected between every set of linked contour arms, said flexible means forming a contoured surface the same as generated by rotation of the fully extended set of linked contour arms around the central axis when said sets of linked contour arms are fully extended.
5. A structure according to claim 4 where the pivot points of the other set of linked arms lie on a line extending substantially perpendicularly from the pivot points of said one set of linked arms according to the contour defined thereby when fully extended.
6. A structure according to claim 4 where spring bias means are associated with all the pivot points of said one set of linked arms tending to bias such arms to the open fully extended position.
7. A structure according to claim 4 where said one set of linked arms has structural characteristics so as to be bent flat when in the folded condition without exceeding the yield strength of the material thereof.

Claims (7)

1. An expandable antenna which comprises a pair of support hubs, means to controllably move the hubs relative to each other, a pair of sets of linked arms arranged as a lazy tong structure having the end of one set of arms pivotally mounted to one hub, and the end of the other set of arms pivotally mounted to the other hub, which is characterized by the sets of arms defining the lazy tongs arranged in equally spaced radial relation around the entire circumference of the hubs, one set of arms of each such lazy tong defining a predetermined contour when extended to their full length, said other set of arms of each said lazy tong having a greater extended length and serving to support the fully extended length of said one set of arms, and flexible reflector means attached between adjacent said one sets of arms which stretches tight to the contour of said one set of arms when extended to in combination define a desired contoured reflective surface, said contoured reflective surface being the same as would be geometrically generated by rotation of said one set of arms when extended about an axis through the center of the planes of the pair of hubs and normal thereto.
4. An expandable structure which comprises a set of linked contour arms and a set of linked support arms arranged in pairs as a lazy tong, a plurality of identical such lazy tongs arranged in a radially directed equally spaced manner around a central axis, means to effect controlled extension and contraction of the linked arms from the ends adjacent said central axis, the set of linked contour arms of each lazy tong defining a predetermined contour when fully extended, said contour falling in the surface of a contoured figure generated by rotation of a set of fully extended linked contoured arms about said central axis, and the set of linked support arms having a greater extended length and forming triangular support for said set of linked contour arms at their fully extended length, and flexible means connected between every set of linked contour arms, said flexible means forming a contoured surface the same as generated by rotation of the fully extended set of linked contour arms around the central axis when said sets of linked contour arms are fully extended.
US21745A1970-03-231970-03-23Expandable antennaExpired - LifetimeUS3631505A (en)

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Cited By (24)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3729743A (en)*1971-10-261973-04-24NasaCollapsible structure for an antenna reflector
DE3044630A1 (en)*1980-11-271982-06-03Messerschmitt-Bölkow-Blohm GmbH, 8000 MünchenFolding aerial for satellite relay station - is constructed as chain of four sided elements which unfolds to make large aerial dish
US4352113A (en)*1980-07-111982-09-28Societe Nationale Industrielle AerospatialeFoldable antenna reflector
US4658265A (en)*1984-06-261987-04-14Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter HaftungFoldable and unfoldable antenna reflector
DE3532851A1 (en)*1985-09-141987-04-16Messerschmitt Boelkow Blohm Unfoldable and re-foldable antenna reflector
US4780726A (en)*1984-12-031988-10-25Trw Inc.Depolyable reflector
US4825225A (en)*1987-01-271989-04-25Waters Terrance JHyperboloidal deployable space antenna
GB2234119A (en)*1989-05-231991-01-23Bell Stephen WRadar reflector deployment system
US4989015A (en)*1987-10-261991-01-29Hughes Aircraft CompanyUnfurlable mesh reflector
US5061929A (en)*1990-05-231991-10-29Firdell Multiflectors LimitedDeployment of radar reflectors
US5061945A (en)*1990-02-121991-10-29Hull Harold LPortable satellite antenna system
US5451975A (en)*1993-02-171995-09-19Space Systems/Loral, Inc.Furlable solid surface reflector
US5777582A (en)*1995-05-161998-07-07Cal CorporationDeployable double-membrane surface antenna
US5864324A (en)*1996-05-151999-01-26Trw Inc.Telescoping deployable antenna reflector and method of deployment
JP2001080600A (en)*1999-09-172001-03-27Natl Space Development Agency Of Japan Expandable mesh antenna, its folding device and its folding method
US6340956B1 (en)*1999-11-122002-01-22Leland H. BowenCollapsible impulse radiating antenna
US20100328171A1 (en)*2009-06-252010-12-30Hong Kong Applied Science And Technology Research Institute Co., Ltd.Rollable and/or Foldable Antenna Systems and Methods for Use Thereof
US9550584B1 (en)*2010-09-302017-01-24MMA Design, LLCDeployable thin membrane apparatus
US20190214737A1 (en)*2018-01-082019-07-11Umbra Lab, Inc.Articulated folding rib reflector for concentrating radiation
US20200274248A1 (en)*2019-02-252020-08-27Eagle Technology, LlcDeployable reflectors
US20220247086A1 (en)*2019-06-172022-08-04Nec CorporationAntenna apparatus, radio transmitter, and antenna diameter adjustment method
RU1841324C (en)*1977-01-262022-10-04Акционерное общество "Центральный научно-исследовательский радиотехнический институт имени академика А.И. Берга" radar reflector
US20220359992A1 (en)*2019-09-242022-11-10Airbus Defence and Space S.A.Deployable assembly for antennas
US20240154317A1 (en)*2022-11-072024-05-09Eagle Technology, LlcScissors radial deployable antenna reflector structure

Citations (5)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2945234A (en)*1958-05-051960-07-12Avco Mfg CorpCollapsible reflecting structure for electric waves
US3174397A (en)*1962-09-101965-03-23Rayan Aeronautical CoDeployment mechanism for satellite mirror structure
US3406404A (en)*1964-10-161968-10-15Ryan Aeronautical CoFurlable and unfurlable member
US3496687A (en)*1967-03-221970-02-24North American RockwellExtensible structure
US3509576A (en)*1967-12-041970-04-28Lockheed Aircraft CorpCollapsible parabolic antenna formed of a series of truncated fabric cones

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2945234A (en)*1958-05-051960-07-12Avco Mfg CorpCollapsible reflecting structure for electric waves
US3174397A (en)*1962-09-101965-03-23Rayan Aeronautical CoDeployment mechanism for satellite mirror structure
US3406404A (en)*1964-10-161968-10-15Ryan Aeronautical CoFurlable and unfurlable member
US3496687A (en)*1967-03-221970-02-24North American RockwellExtensible structure
US3509576A (en)*1967-12-041970-04-28Lockheed Aircraft CorpCollapsible parabolic antenna formed of a series of truncated fabric cones

Cited By (32)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3729743A (en)*1971-10-261973-04-24NasaCollapsible structure for an antenna reflector
RU1841324C (en)*1977-01-262022-10-04Акционерное общество "Центральный научно-исследовательский радиотехнический институт имени академика А.И. Берга" radar reflector
RU1841325C (en)*1977-02-162022-10-04Акционерное общество "Центральный научно-исследовательский радиотехнический институт имени академика А.И. Берга" Drop down reflector
US4352113A (en)*1980-07-111982-09-28Societe Nationale Industrielle AerospatialeFoldable antenna reflector
DE3044630A1 (en)*1980-11-271982-06-03Messerschmitt-Bölkow-Blohm GmbH, 8000 MünchenFolding aerial for satellite relay station - is constructed as chain of four sided elements which unfolds to make large aerial dish
US4658265A (en)*1984-06-261987-04-14Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter HaftungFoldable and unfoldable antenna reflector
US4780726A (en)*1984-12-031988-10-25Trw Inc.Depolyable reflector
DE3532851A1 (en)*1985-09-141987-04-16Messerschmitt Boelkow Blohm Unfoldable and re-foldable antenna reflector
US4825225A (en)*1987-01-271989-04-25Waters Terrance JHyperboloidal deployable space antenna
US4989015A (en)*1987-10-261991-01-29Hughes Aircraft CompanyUnfurlable mesh reflector
GB2234119B (en)*1989-05-231993-09-01Bell Stephen WDeployment of radar reflectors
GB2234119A (en)*1989-05-231991-01-23Bell Stephen WRadar reflector deployment system
US5061945A (en)*1990-02-121991-10-29Hull Harold LPortable satellite antenna system
US5061929A (en)*1990-05-231991-10-29Firdell Multiflectors LimitedDeployment of radar reflectors
US5451975A (en)*1993-02-171995-09-19Space Systems/Loral, Inc.Furlable solid surface reflector
US5777582A (en)*1995-05-161998-07-07Cal CorporationDeployable double-membrane surface antenna
US5864324A (en)*1996-05-151999-01-26Trw Inc.Telescoping deployable antenna reflector and method of deployment
JP2001080600A (en)*1999-09-172001-03-27Natl Space Development Agency Of Japan Expandable mesh antenna, its folding device and its folding method
US6340956B1 (en)*1999-11-122002-01-22Leland H. BowenCollapsible impulse radiating antenna
US20100328171A1 (en)*2009-06-252010-12-30Hong Kong Applied Science And Technology Research Institute Co., Ltd.Rollable and/or Foldable Antenna Systems and Methods for Use Thereof
US8421683B2 (en)2009-06-252013-04-16Hong Kong Applied Science And Technology Research Institute Co., Ltd.Rollable and/or foldable antenna systems and methods for use thereof
US9550584B1 (en)*2010-09-302017-01-24MMA Design, LLCDeployable thin membrane apparatus
US20190214737A1 (en)*2018-01-082019-07-11Umbra Lab, Inc.Articulated folding rib reflector for concentrating radiation
US10847893B2 (en)*2018-01-082020-11-24Umbra Lab, Inc.Articulated folding rib reflector for concentrating radiation
US20200274248A1 (en)*2019-02-252020-08-27Eagle Technology, LlcDeployable reflectors
US11942687B2 (en)*2019-02-252024-03-26Eagle Technology, LlcDeployable reflectors
US20220247086A1 (en)*2019-06-172022-08-04Nec CorporationAntenna apparatus, radio transmitter, and antenna diameter adjustment method
US11955714B2 (en)*2019-06-172024-04-09Nec CorporationAntenna apparatus, radio transmitter, and antenna diameter adjustment method
US20220359992A1 (en)*2019-09-242022-11-10Airbus Defence and Space S.A.Deployable assembly for antennas
US11784415B2 (en)*2019-09-242023-10-10Airbus Defence and Space S.A.Deployable assembly for antennas
US20240154317A1 (en)*2022-11-072024-05-09Eagle Technology, LlcScissors radial deployable antenna reflector structure
US12142833B2 (en)*2022-11-072024-11-12Eagle Technology, LlcScissors radial deployable antenna reflector structure

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DateCodeTitleDescription
ASAssignment

Owner name:LORAL CORPORATION,NEW YORK

Free format text:ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:GOODYEAR AEROSPACE CORPORATION;REEL/FRAME:004869/0167

Effective date:19871218

Owner name:LORAL CORPORATION, 600 THIRD AVENUE, NEW YORK, NEW

Free format text:ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:GOODYEAR AEROSPACE CORPORATION;REEL/FRAME:004869/0167

Effective date:19871218


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