US3541569A - Expandable parabolic reflector - Google Patents
Expandable parabolic reflector Download PDFInfo
- Publication number
- US3541569A US3541569A US711801A US3541569DA US3541569A US 3541569 A US3541569 A US 3541569A US 711801 A US711801 A US 711801A US 3541569D A US3541569D A US 3541569DA US 3541569 A US3541569 A US 3541569A
- Authority
- US
- United States
- Prior art keywords
- reflector
- spindle
- rib
- central
- rib members
- 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
Links
Images
Classifications
-
- 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
- H01Q15/16—Reflecting surfaces; Equivalent structures curved in two dimensions, e.g. paraboloidal
- H01Q15/161—Collapsible reflectors
Definitions
- the device of this invention is an expandable parabolic reflector which is comprised of a plurality of rib members radially extending from a relatively fixed central member, with each of the members shaped to form a skeleton structure of a parabolic reflector.
- a thin collapsible sheet of conductive material attached and stretched between the rib members forms the reflector surface.
- a spindle member is rotatably mounted to the central member and cables, or Wires, are extending from points spaced on the outer surface of the spindle to the outermost tips of the rib members.
- Means are also provided for rotating the spindle member with respect to the central member to wind the cables and in turn the rib members and reflector around the central member.
- the spindle is rotated in an opposite direction unwinding the cable and allowing the spring action of the ribs to open the reflector material between the ribs.
- the spindle continues to rotate thus increasing the tension on the cables and stretching the reflector into the desired shape.
- This invention pertains to the field of parabolic reflectors and, more particularly, to a parabolic type reflector which may be collapsed and expanded when desired.
- Parabolic reflectors find their most common use in the communications field as antennas.
- spacecraft must be provided with various types of antennas in order to communicate with various ground areas.
- size and volume limitations of launch vehicle fairings often require that such antennas be capable of being folded to a small fraction of their open diameter and total volume with their deployment occurring after orbit has been achieved.
- One of the prior art devices consists of umbrella-type antennas which have rigid ribs that are extended in a manner similar to an umbrella.
- the umbrella antenna is disclosed in a paper entitled The Development of High Gain Deployable Antennas for Communications Satellites, AIAA Paper No. 66-306, by S. A. Milliken, Hughes Aircraft Co., El Segundo, May 1966.
- Another folda-ble antenna design consisting of a series of spirally-formed fiber glass rods which support a metallic-rooted plastic mesh is disclosed in the article Lightweight Antenna for Space Vehicles, Product Engineering, Nov. 22, 1965, page 60.
- the expanding of the antenna is accomplished by utilizing the elastic energy of the fiber glass rods and controlling the rate of opening with a braking device.
- the reflector of this invention differs from the prior art devices in that no heavy mechanical linkages, such as those used on the umbrella-type reflectors, are used and in that the reflector is expanded with elastic energy and rigidly stretched in the open position to provide a relatively stable paraboloid focal point and corresponding paraboloid of revolution.
- a substantially cylindrical central member has mounted on its periphery a plurality of rib-like members which extend radially from the central member.
- Each of the rib members is shaped to form the skeleton structure of a parabolic reflector.
- a thin collapsible sheet of conductive material is attached and stretched between the rib members to form a parabolic reflector.
- a spindle member is rotatably mounted to the central member and cables or wires are extending from points spaced on the outer periphery of the spindle to the outermost tips of the rib members.
- Means are provided for rotating the spindle member with respect to the central member to wind the cable and in turn the rib member and the reflector around the central member.
- the spindle member is rotated in an opposite direction until the reflector is expanded.
- the spindle member is then further rotated such that the cable now pulls the rib members stressing the reflector material forming it into a rigid parabolic shape.
- FIG. 1 is a perspective view of the preferred embodiment of the invention
- FIG. 2 is a perspective view in partial cutaway of a portion of the embodiment illustrated in FIG. 1;
- FIG. 3 illustrates a structural member utilized in the embodiment shown in FIG. 1;
- FIG. 4a and FIG. 4b are top views of the structural member illustrated in FIG. 3;
- FIG. 5 illustrates a second embodiment of the invention.
- the reflector 10 consists of a plurality of flexible ribs 14 which are fixedly attached and extend radially from a central core member 20.
- the ribs are relatively thin and flexible in the plane defined by the reflector surface but in the plane perpendicular to the reflector surface the ribs are fairly wide and rigid.
- the ribs 14 are symmetrically disposed about the outer periphery of the central member 20. This symmetry need not be maintained for all types of reflectors.
- Each of the rib members 14 has a surface 30 formed into the shape of a parabola, or other desired shape, so as to form a skeleton structure to which a conductive reflective flexible covering may be attached.
- a central hollow shaft member 22 extends vertically through the central core member 20 along the axes defining the focus of a paraboloid.
- the spindle member 18 resembling an inverted funnel is rotatably mounted to the shaft member 22. Cables 16, or flexible wires, extend from points 24 on the tips of each of the rib members 14 to corresponding points 28 on the periphery of the spindle member 18.
- the reflector 10 may be collapsed by rotating the spindle member 28 in the direction A indicated by the double headed direction arrow 19. With the spindle rotating in this direction, the cables 16 are wound around the outer surface of the spindle member pulling the tips of the structural rib members 14 towards the central shaft 22. This process continues until the structural rib members are compactly wound around the central core member 20.
- the spindle member is shaped in the form of an inverted funnel to provide varying degrees of torque to pull the tips 24 etficiently towards the center. For example, in the fully extended position shown in FIG. 1, the torque required to initially move, and start, the tip members in toward the central core member 20 is relatively low.
- the moment arm transmitting the torque to the cable is then equal to the distance between the periphery of the spindle member 18 and the central axis of the shaft 22.
- the cable 16 As the cable 16 is wound onto the funnel, the cable slides up towards the narrow portion of the spindle thereby decreasing the distance between the central axis of shaft 22 and the outer surface or torque transmitting surface of the spindle member 18.
- the winding of the cable will decrease in speed but the force applied thereto will increase.
- This particular feature automatically takes care of the increase in resistance caused by the spring constant of the structural rib members and the normal folding resistance in the conductive reflector material 12.
- the spindle To release the reflector in a controlled manner, the spindle is rotated in the B direction of the double action arrow '19.
- the flexible material used for the reflector 12 may be a continuously reflective medium such as metallic coated plastic film, or a conductive mesh material aflixed to the structural rib members 14 by any suitable means such as a contact type cement.
- each of the structural rib members 14 is provided with an individual cable to help collapse and extend that member. It is not necessary that each of the structural ribs have such a cable arrangement. For example, every second rib could have such a cable with the reflective material providing the necessary torque transmittal to the adjacent rib to collapse and controllably extend that rib.
- the central core member 20 and r the spindle member 18 are shown partially cut away.
- the outer periphery of the central core member 20 is formed into the shape of a series of saw tooth steps 34.
- the plurality of structural rib members 14 are recessed onto or into these steps and aflixed to the central core member 20 by means of fasteners 32 which may be bolts or a welding process.
- the shaft member 22 is hollow and extends upward to the central portion of the central core member 20 and is fixedly attached to the central core member 20.
- the spindle member 18 resembling the inverted funnel is rotatably attached to the shaft member 2 2 by means of race-type ball bearings 36.
- a worm gear 38 is fixedly attached to the spindle member 18.
- a screw gear 58 when rotated drives the worm gear which in turns drives the spindle member 18 about the central axes of the shaft 22.
- the screw gear 58 is connected to the electric motor 52 by the wheel gears 54 and 56.
- the motor 52 is fixedly attached to the central core member 20 by means of brackets 60 or other suitable apparatus.
- Opening 62 are provided in the shaft 22 for the electrical leads 64 which are connected to the motor 60 and to the power source 66.
- the power source 66 may be batteries, or solar cells, or any other power source adequate to drive the motor 52.
- FIG. 3 illustrates one of the structural rib members 14 more clearly defining the parabolic curvature 30.
- the tip 24 having the opening for attaching the cables 16 and the openings 32 for attaching the rib members to the central housing member 20.
- the portion of the rib which is attached to the central housing is relatively thick as compared to the tip. By slimming the rib member down as it approaches the tip, a considerable savings in weight can be achieved.
- the structural rib 14 may be formed in many shapes; two of which are shown in FIGS. 4a and 4b. In FIG.
- the rib is formed with a curvature corresponding to moving the tip 24 to the position defined by the line 40 and forming the rib in an unstressed position at this point such that when no pressure is applied, the rib will remain fixed at the point 40.
- the rib tip 24 is forced into the position defined by the line 42.
- the spring tension in the rib 14 attempts to return the rib to the position 40 and thereby maintains a constant tension or pressure which tends to begin the folding phase of the collapsible reflector as soon as the spindle begins to unwind about the shaft.
- FIG. 4b in this figure the rib member 14 is initially formed along the dotted position indicated by the line 42. As the reflector is expanded and tension is applied to the tip, the rib unfolds and assumes the position defined by the line 44.
- the expandable reflector shown therein is similar to the embodiment illustrated in FIGS. 1 to 4 except that in this embodiment the shaft 22 extends upward from the reflector towards the focus point and a cylindrical central member 50 is mounted for rotation about the axis 22 in a similar manner as was mounted the spindle -18.
- Wires, or cables 16 extend from peripheral points about the central member 50 to tips of the rib members 14.
- the central cylindrical member 50 is rotated about the axis 22 to wind on its outer surface the cables 16 which in turn pull the rib member 14 upwards and around the axis 22.
- the member 50 and its associated components should be made of a dielectric material which will not hamper the reception of electromagnetic radiation.
- An expandable structure comprising in combination:
- rib members fixedly attached to said central member and extending radially therefrom, wherein said rib members are shaped to form a parabolic skeleton; spindle member rotatably mounted to said shaft; plurality of cables extending from the tips of said rib members to the outermost surface of said spindle member;
- a collapsible sheet of conductive material attached between each of said rib members, said conductive material when stretched between said ribs forming a parabolic reflector, the focal point of which lies along the axis of said shaft and positioned at a point corresponding to the position of said spindle;
Description
NOV. 17, 1970 w, BERKS ETAL 7 3,541,569
EXPANDABLE PARABOLIC REFLECTOR Filed March 8, 1968 2 Sheets-Sheet 1 Roy M. Acker William I. Berks Webster D. Smith mvsmons ATTORNEY Nov. 17, 1970 w. BERKS ETAL 3,541,569
EXPANDABLE PARABOLIC REFLECTOR Filed Maroh8, 1968 2 Sheets-Sheet 2 0 54 I 58 5o 3a 56 I i P l Fig.4A H 45 Roy MAcker William I. Berks Webster D. Smith INVENTOR.
BY a. (m.
ATTORNEY United States Patent US. Cl. 343-915 6 Claims ABSTRACT OF THE DISCLOSURE The device of this invention is an expandable parabolic reflector which is comprised of a plurality of rib members radially extending from a relatively fixed central member, with each of the members shaped to form a skeleton structure of a parabolic reflector. A thin collapsible sheet of conductive material attached and stretched between the rib members forms the reflector surface. A spindle member is rotatably mounted to the central member and cables, or Wires, are extending from points spaced on the outer surface of the spindle to the outermost tips of the rib members. Means are also provided for rotating the spindle member with respect to the central member to wind the cables and in turn the rib members and reflector around the central member. To expand the reflector, the spindle is rotated in an opposite direction unwinding the cable and allowing the spring action of the ribs to open the reflector material between the ribs. The spindle continues to rotate thus increasing the tension on the cables and stretching the reflector into the desired shape.
BACKGROUND OF THE INVENTION This invention pertains to the field of parabolic reflectors and, more particularly, to a parabolic type reflector which may be collapsed and expanded when desired. Parabolic reflectors find their most common use in the communications field as antennas. In the presentday scientific world, spacecraft must be provided with various types of antennas in order to communicate with various ground areas. Where increasing data requirements demand higher gains and hence larger antennas, size and volume limitations of launch vehicle fairings often require that such antennas be capable of being folded to a small fraction of their open diameter and total volume with their deployment occurring after orbit has been achieved.
One of the prior art devices consists of umbrella-type antennas which have rigid ribs that are extended in a manner similar to an umbrella. The umbrella antenna is disclosed in a paper entitled The Development of High Gain Deployable Antennas for Communications Satellites, AIAA Paper No. 66-306, by S. A. Milliken, Hughes Aircraft Co., El Segundo, May 1966.
Another folda-ble antenna design consisting of a series of spirally-formed fiber glass rods which support a metallic-rooted plastic mesh is disclosed in the article Lightweight Antenna for Space Vehicles, Product Engineering, Nov. 22, 1965, page 60. The expanding of the antenna is accomplished by utilizing the elastic energy of the fiber glass rods and controlling the rate of opening with a braking device.
The reflector of this invention differs from the prior art devices in that no heavy mechanical linkages, such as those used on the umbrella-type reflectors, are used and in that the reflector is expanded with elastic energy and rigidly stretched in the open position to provide a relatively stable paraboloid focal point and corresponding paraboloid of revolution.
SUMMARY OF THE INVENTION In the preferred embodiment of this invention, a substantially cylindrical central member has mounted on its periphery a plurality of rib-like members which extend radially from the central member. Each of the rib members is shaped to form the skeleton structure of a parabolic reflector. A thin collapsible sheet of conductive material is attached and stretched between the rib members to form a parabolic reflector. A spindle member is rotatably mounted to the central member and cables or wires are extending from points spaced on the outer periphery of the spindle to the outermost tips of the rib members. Means are provided for rotating the spindle member with respect to the central member to wind the cable and in turn the rib member and the reflector around the central member. To expand the reflector the spindle member is rotated in an opposite direction until the reflector is expanded. The spindle member is then further rotated such that the cable now pulls the rib members stressing the reflector material forming it into a rigid parabolic shape.
Accordingly, it is an object of the present invention to provide an improved expandable reflector.
It is a further object of the present invention to provide a reflector which may be folded into a relatively small space.
It is another object of the present invention to provide a reflector which is relatively rigid in its expanded position.
The aforementioned and other objects of the present invention will become more apparent when taken in conjunction with the following description and drawings, throughout which like characters indicate like parts, and which drawings form a part of this application.
BRIEF DESCRIPTION OF THE THE DRAWINGS FIG. 1 is a perspective view of the preferred embodiment of the invention;
FIG. 2 is a perspective view in partial cutaway of a portion of the embodiment illustrated in FIG. 1;
FIG. 3 illustrates a structural member utilized in the embodiment shown in FIG. 1;
FIG. 4a and FIG. 4b are top views of the structural member illustrated in FIG. 3; and
FIG. 5 illustrates a second embodiment of the invention.
BRIEF DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring to FIG. 1, wherein the expandable reflector 10 is shown in its fully expanded position. The reflector 10 consists of a plurality of flexible ribs 14 which are fixedly attached and extend radially from a central core member 20. The ribs are relatively thin and flexible in the plane defined by the reflector surface but in the plane perpendicular to the reflector surface the ribs are fairly wide and rigid. In the embodiment shown in FIG. 1, the ribs 14 are symmetrically disposed about the outer periphery of the central member 20. This symmetry need not be maintained for all types of reflectors. Each of the rib members 14 has a surface 30 formed into the shape of a parabola, or other desired shape, so as to form a skeleton structure to which a conductive reflective flexible covering may be attached. A central hollow shaft member 22 extends vertically through the central core member 20 along the axes defining the focus of a paraboloid. The spindle member 18 resembling an inverted funnel is rotatably mounted to the shaft member 22. Cables 16, or flexible wires, extend from points 24 on the tips of each of the rib members 14 to corresponding points 28 on the periphery of the spindle member 18.
In operation, the reflector 10 may be collapsed by rotating the spindle member 28 in the direction A indicated by the double headed direction arrow 19. With the spindle rotating in this direction, the cables 16 are wound around the outer surface of the spindle member pulling the tips of the structural rib members 14 towards the central shaft 22. This process continues until the structural rib members are compactly wound around the central core member 20. The spindle member is shaped in the form of an inverted funnel to provide varying degrees of torque to pull the tips 24 etficiently towards the center. For example, in the fully extended position shown in FIG. 1, the torque required to initially move, and start, the tip members in toward the central core member 20 is relatively low. The moment arm transmitting the torque to the cable is then equal to the distance between the periphery of the spindle member 18 and the central axis of the shaft 22. As the cable 16 is wound onto the funnel, the cable slides up towards the narrow portion of the spindle thereby decreasing the distance between the central axis of shaft 22 and the outer surface or torque transmitting surface of the spindle member 18. The winding of the cable will decrease in speed but the force applied thereto will increase. This particular feature automatically takes care of the increase in resistance caused by the spring constant of the structural rib members and the normal folding resistance in the conductive reflector material 12. To release the reflector in a controlled manner, the spindle is rotated in the B direction of the double action arrow '19. A point will be reached where further unwinding of the spindle will not extend the tip members 24 any farther. By rotating the spindle 18 past this point, the cable 16 will attempt to extend the tip members even farther thereby stretching or placing the structural rib members in a stressed condition forming a substantially rigid structure that is capable of defining the focus point of the paraboloid with a relatively high degree of accuracy. The flexible material used for the reflector 12 may be a continuously reflective medium such as metallic coated plastic film, or a conductive mesh material aflixed to the structural rib members 14 by any suitable means such as a contact type cement. In FIG. 1, each of the structural rib members 14 is provided with an individual cable to help collapse and extend that member. It is not necessary that each of the structural ribs have such a cable arrangement. For example, every second rib could have such a cable with the reflective material providing the necessary torque transmittal to the adjacent rib to collapse and controllably extend that rib.
Referring to FIG. 2, the central core member 20 and r the spindle member 18 are shown partially cut away. The outer periphery of the central core member 20 is formed into the shape of a series of saw tooth steps 34. The plurality of structural rib members 14 are recessed onto or into these steps and aflixed to the central core member 20 by means of fasteners 32 which may be bolts or a welding process. The shaft member 22 is hollow and extends upward to the central portion of the central core member 20 and is fixedly attached to the central core member 20. The spindle member 18 resembling the inverted funnel is rotatably attached to the shaft member 2 2 by means of race-type ball bearings 36. A worm gear 38 is fixedly attached to the spindle member 18. A screw gear 58 when rotated drives the worm gear which in turns drives the spindle member 18 about the central axes of the shaft 22. The screw gear 58 is connected to the electric motor 52 by the wheel gears 54 and 56. The motor 52 is fixedly attached to the central core member 20 by means of brackets 60 or other suitable apparatus.
FIG. 3 illustrates one of the structural rib members 14 more clearly defining the parabolic curvature 30. The tip 24 having the opening for attaching the cables 16 and the openings 32 for attaching the rib members to the central housing member 20. As shown, the portion of the rib which is attached to the central housing is relatively thick as compared to the tip. By slimming the rib member down as it approaches the tip, a considerable savings in weight can be achieved. The structural rib 14 may be formed in many shapes; two of which are shown in FIGS. 4a and 4b. In FIG. 4a, the rib is formed with a curvature corresponding to moving the tip 24 to the position defined by the line 40 and forming the rib in an unstressed position at this point such that when no pressure is applied, the rib will remain fixed at the point 40. As the reflector is then expanded, the rib tip 24 is forced into the position defined by the line 42. The spring tension in the rib 14 attempts to return the rib to the position 40 and thereby maintains a constant tension or pressure which tends to begin the folding phase of the collapsible reflector as soon as the spindle begins to unwind about the shaft. Referring now to FIG. 4b; in this figure the rib member 14 is initially formed along the dotted position indicated by the line 42. As the reflector is expanded and tension is applied to the tip, the rib unfolds and assumes the position defined by the line 44.
Referring to FIG. 5, the expandable reflector shown therein is similar to the embodiment illustrated in FIGS. 1 to 4 except that in this embodiment the shaft 22 extends upward from the reflector towards the focus point and a cylindrical central member 50 is mounted for rotation about the axis 22 in a similar manner as was mounted the spindle -18. Wires, or cables 16 extend from peripheral points about the central member 50 to tips of the rib members 14. In operation, the central cylindrical member 50 is rotated about the axis 22 to wind on its outer surface the cables 16 which in turn pull the rib member 14 upwards and around the axis 22. In this particular embodiment, because the focuse point of the antenna is licated somewhere within the central rotating member 50, the member 50 and its associated components should be made of a dielectric material which will not hamper the reception of electromagnetic radiation.
While there has been shown what are considered to be the preferred embodiments of the present invention, it will be manifest that many changes and modifications may be made therein without departing from the essential spirit of the invention. It is intended, therefore, in the annexed claims, to cover all such changes and modifications as may fall within the true scope of the invention.
What is claimed is:
1. An expandable structure comprising in combination:
a central member;
a shaft extending through said central member;
a plurality of rib members fixedly attached to said central member and extending radially therefrom, wherein said rib members are shaped to form a parabolic skeleton; spindle member rotatably mounted to said shaft; plurality of cables extending from the tips of said rib members to the outermost surface of said spindle member;
a collapsible sheet of conductive material attached between each of said rib members, said conductive material when stretched between said ribs forming a parabolic reflector, the focal point of which lies along the axis of said shaft and positioned at a point corresponding to the position of said spindle; and
means for rotating said spindle member about said shaft.
2. The invention, according to claim 1, wherein said spindle member is shaped as a funnel to provide a varying torque to said tip members.
3. The invention, according to claim 1, wherein said spindle member is made of a dielectric type material.
4. The invention, according to claim 1, wherein said rib members in the expanded position extend radially from said central member along substantially straight lines.
5. The invention according to claim 1, wherein said rib members in the expanded position extend radially from said central member along substantially curved lines.
6. The invention, according to claim 1, wherein said rib members are made from material exhibiting springtype properties.
References Cited UNITED STATES PATENTS ELI LIEBERMAN, Primary Examiner 10 W. H. PUNTER, Assistant Examiner US. Cl. X.R.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US71180168A | 1968-03-08 | 1968-03-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3541569A true US3541569A (en) | 1970-11-17 |
Family
ID=24859584
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US711801A Expired - Lifetime US3541569A (en) | 1968-03-08 | 1968-03-08 | Expandable parabolic reflector |
Country Status (1)
Country | Link |
---|---|
US (1) | US3541569A (en) |
Cited By (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3762207A (en) * | 1971-12-03 | 1973-10-02 | Weiser Robodyne Corp | Method of fabricating curved surfaces |
US3927227A (en) * | 1974-02-27 | 1975-12-16 | Nasa | Method for manufacturing mirrors in zero gravity environment |
US4030103A (en) * | 1975-12-10 | 1977-06-14 | Lockheed Missiles & Space Company, Inc. | Deployable offset paraboloid antenna |
US4498087A (en) * | 1981-06-25 | 1985-02-05 | Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung | Apparatus for unfolding an antenna netting reflector |
DE3621578A1 (en) * | 1986-06-27 | 1988-01-07 | Dornier System Gmbh | FOLDABLE CONCAVE CURVED ANTENNA REFLECTOR |
US4750002A (en) * | 1986-09-12 | 1988-06-07 | Harris Corporation | Antenna panel having adjustable supports to improve surface accuracy |
US4862190A (en) * | 1987-05-15 | 1989-08-29 | Trw Inc. | Deployable offset dish structure |
US5061945A (en) * | 1990-02-12 | 1991-10-29 | Hull Harold L | Portable satellite antenna system |
DE4137974A1 (en) * | 1991-11-19 | 1993-05-27 | Guenther Boehmig | Foldable satellite reception aerial - has metallised, textile fabric as reflector, whose struts are curved strips forming paraboloid |
US5421376A (en) * | 1994-01-21 | 1995-06-06 | Lockheed Missiles & Space Co., Inc. | Metallized mesh fabric panel construction for RF reflector |
US5446474A (en) * | 1994-01-19 | 1995-08-29 | Lockheed Missiles & Space Company, Inc. | Redeployable furlable rib reflector |
US5488383A (en) * | 1994-01-21 | 1996-01-30 | Lockheed Missiles & Space Co., Inc. | Method for accurizing mesh fabric reflector panels of a deployable reflector |
US5515067A (en) * | 1992-03-24 | 1996-05-07 | Agence Spatiale Europenne | Self-supporting shell for use in space |
US5574472A (en) * | 1991-09-27 | 1996-11-12 | Hughes Electronics | Simplified spacecraft antenna reflector for stowage in confined envelopes |
US6028569A (en) * | 1997-07-07 | 2000-02-22 | Hughes Electronics Corporation | High-torque apparatus and method using composite materials for deployment of a multi-rib umbrella-type reflector |
US6373449B1 (en) | 1999-09-21 | 2002-04-16 | The Johns Hopkins University | Hybrid inflatable antenna |
US20040104861A1 (en) * | 2002-07-31 | 2004-06-03 | Manfred Schmid | Deployable antenna reflector |
US7557995B1 (en) | 2006-07-11 | 2009-07-07 | Itt Manufacturing Enterprises, Inc. | Deployable telescope shade |
US20120326921A1 (en) * | 2011-06-22 | 2012-12-27 | David Geen | Antenna Apparatus |
US20140142769A1 (en) * | 2007-10-01 | 2014-05-22 | Koninklijke Philips N.V. | Building management system with active building skin, an environmental resource collector for use in such a system and a method of managing resources used in a building |
CN105140618A (en) * | 2015-10-10 | 2015-12-09 | 中国电子科技集团公司第五十四研究所 | Rapidly-deployable parabolic antenna unit mechanism |
CN105206912A (en) * | 2015-10-10 | 2015-12-30 | 中国电子科技集团公司第五十四研究所 | Parabolic antenna capable of being rapidly unfolded |
US9331394B2 (en) | 2011-09-21 | 2016-05-03 | Harris Corporation | Reflector systems having stowable rigid panels |
WO2017221872A1 (en) * | 2016-06-21 | 2017-12-28 | 株式会社Qps研究所 | Expandable antenna |
DE102016012402A1 (en) * | 2016-10-17 | 2018-04-19 | Stefan Alfred Maier | Device (45) arranged as a precision mirror / parabolic mirror of segment parts and a method that the mirror segments set in motion to the total mirror surface differently structured to take in the rest position, wind forces the attack surface. |
GB2555656A (en) * | 2016-11-08 | 2018-05-09 | Oxford Space Systems | Deployable wrapped rib assembly |
WO2019087236A1 (en) * | 2017-10-30 | 2019-05-09 | 株式会社Qps研究所 | Reflector, developed antenna, and aerospace vehicle |
US10797400B1 (en) | 2019-03-14 | 2020-10-06 | Eagle Technology, Llc | High compaction ratio reflector antenna with offset optics |
US10811759B2 (en) | 2018-11-13 | 2020-10-20 | Eagle Technology, Llc | Mesh antenna reflector with deployable perimeter |
US11139549B2 (en) | 2019-01-16 | 2021-10-05 | Eagle Technology, Llc | Compact storable extendible member reflector |
US20220181789A1 (en) * | 2019-04-18 | 2022-06-09 | Institute For Q-Shu Pioneers Of Space, Inc. | Antenna apparatus and spacecraft |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3010372A (en) * | 1960-02-11 | 1961-11-28 | Wade E Lanford | Folding apparatus |
US3064534A (en) * | 1960-04-13 | 1962-11-20 | United Aircraft Corp | Reflector for space vehicle |
US3217328A (en) * | 1963-03-08 | 1965-11-09 | Electro Optical Systems Inc | Antenna with wire mesh reflector collapsing in a pinwheel manner |
US3286259A (en) * | 1964-04-30 | 1966-11-15 | Goodyear Aerospace Corp | Unfurlable reflector |
US3406404A (en) * | 1964-10-16 | 1968-10-15 | Ryan Aeronautical Co | Furlable and unfurlable member |
-
1968
- 1968-03-08 US US711801A patent/US3541569A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3010372A (en) * | 1960-02-11 | 1961-11-28 | Wade E Lanford | Folding apparatus |
US3064534A (en) * | 1960-04-13 | 1962-11-20 | United Aircraft Corp | Reflector for space vehicle |
US3217328A (en) * | 1963-03-08 | 1965-11-09 | Electro Optical Systems Inc | Antenna with wire mesh reflector collapsing in a pinwheel manner |
US3286259A (en) * | 1964-04-30 | 1966-11-15 | Goodyear Aerospace Corp | Unfurlable reflector |
US3406404A (en) * | 1964-10-16 | 1968-10-15 | Ryan Aeronautical Co | Furlable and unfurlable member |
Cited By (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3762207A (en) * | 1971-12-03 | 1973-10-02 | Weiser Robodyne Corp | Method of fabricating curved surfaces |
US3927227A (en) * | 1974-02-27 | 1975-12-16 | Nasa | Method for manufacturing mirrors in zero gravity environment |
US4030103A (en) * | 1975-12-10 | 1977-06-14 | Lockheed Missiles & Space Company, Inc. | Deployable offset paraboloid antenna |
US4498087A (en) * | 1981-06-25 | 1985-02-05 | Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung | Apparatus for unfolding an antenna netting reflector |
DE3621578A1 (en) * | 1986-06-27 | 1988-01-07 | Dornier System Gmbh | FOLDABLE CONCAVE CURVED ANTENNA REFLECTOR |
EP0252247A1 (en) * | 1986-06-27 | 1988-01-13 | Dornier Gmbh | Collapsible antenna reflector with a concave surface |
US4899167A (en) * | 1986-06-27 | 1990-02-06 | Dornier System Gmbh | Collapsible antenna |
US4750002A (en) * | 1986-09-12 | 1988-06-07 | Harris Corporation | Antenna panel having adjustable supports to improve surface accuracy |
US4862190A (en) * | 1987-05-15 | 1989-08-29 | Trw Inc. | Deployable offset dish structure |
US5061945A (en) * | 1990-02-12 | 1991-10-29 | Hull Harold L | Portable satellite antenna system |
US5574472A (en) * | 1991-09-27 | 1996-11-12 | Hughes Electronics | Simplified spacecraft antenna reflector for stowage in confined envelopes |
DE4137974A1 (en) * | 1991-11-19 | 1993-05-27 | Guenther Boehmig | Foldable satellite reception aerial - has metallised, textile fabric as reflector, whose struts are curved strips forming paraboloid |
US5515067A (en) * | 1992-03-24 | 1996-05-07 | Agence Spatiale Europenne | Self-supporting shell for use in space |
US5446474A (en) * | 1994-01-19 | 1995-08-29 | Lockheed Missiles & Space Company, Inc. | Redeployable furlable rib reflector |
US5421376A (en) * | 1994-01-21 | 1995-06-06 | Lockheed Missiles & Space Co., Inc. | Metallized mesh fabric panel construction for RF reflector |
US5488383A (en) * | 1994-01-21 | 1996-01-30 | Lockheed Missiles & Space Co., Inc. | Method for accurizing mesh fabric reflector panels of a deployable reflector |
US6028569A (en) * | 1997-07-07 | 2000-02-22 | Hughes Electronics Corporation | High-torque apparatus and method using composite materials for deployment of a multi-rib umbrella-type reflector |
US6373449B1 (en) | 1999-09-21 | 2002-04-16 | The Johns Hopkins University | Hybrid inflatable antenna |
US20040104861A1 (en) * | 2002-07-31 | 2004-06-03 | Manfred Schmid | Deployable antenna reflector |
US6930654B2 (en) * | 2002-07-31 | 2005-08-16 | Astrium Gmbh | Deployable antenna reflector |
US7557995B1 (en) | 2006-07-11 | 2009-07-07 | Itt Manufacturing Enterprises, Inc. | Deployable telescope shade |
US20140142769A1 (en) * | 2007-10-01 | 2014-05-22 | Koninklijke Philips N.V. | Building management system with active building skin, an environmental resource collector for use in such a system and a method of managing resources used in a building |
US9348328B2 (en) * | 2007-10-01 | 2016-05-24 | Koninklijke Philips N.V. | Building management system with active building skin, an environmental resource collector for use in such a system and a method of managing resources used in a building |
US20120326921A1 (en) * | 2011-06-22 | 2012-12-27 | David Geen | Antenna Apparatus |
US9331394B2 (en) | 2011-09-21 | 2016-05-03 | Harris Corporation | Reflector systems having stowable rigid panels |
CN105140618B (en) * | 2015-10-10 | 2018-01-30 | 中国电子科技集团公司第五十四研究所 | A kind of parabola antenna unit mechanisms of rapid deployment |
CN105140618A (en) * | 2015-10-10 | 2015-12-09 | 中国电子科技集团公司第五十四研究所 | Rapidly-deployable parabolic antenna unit mechanism |
CN105206912A (en) * | 2015-10-10 | 2015-12-30 | 中国电子科技集团公司第五十四研究所 | Parabolic antenna capable of being rapidly unfolded |
JPWO2017221872A1 (en) * | 2016-06-21 | 2019-04-11 | 株式会社Qps研究所 | Deployment antenna |
WO2017221872A1 (en) * | 2016-06-21 | 2017-12-28 | 株式会社Qps研究所 | Expandable antenna |
EP3474381A4 (en) * | 2016-06-21 | 2020-01-22 | Institute for Q-shu Pioneers of Space, Inc. | Expandable antenna |
US11223139B2 (en) * | 2016-06-21 | 2022-01-11 | Institute For Q-Shu Pioneers Of Space, Inc. | Expandable antenna |
DE102016012402A1 (en) * | 2016-10-17 | 2018-04-19 | Stefan Alfred Maier | Device (45) arranged as a precision mirror / parabolic mirror of segment parts and a method that the mirror segments set in motion to the total mirror surface differently structured to take in the rest position, wind forces the attack surface. |
GB2555656A (en) * | 2016-11-08 | 2018-05-09 | Oxford Space Systems | Deployable wrapped rib assembly |
WO2019087236A1 (en) * | 2017-10-30 | 2019-05-09 | 株式会社Qps研究所 | Reflector, developed antenna, and aerospace vehicle |
US11381001B2 (en) | 2017-10-30 | 2022-07-05 | Institute For Q-Shu Pioneers Of Space, Inc. | Reflector, deployable antenna, and spacecraft |
US10811759B2 (en) | 2018-11-13 | 2020-10-20 | Eagle Technology, Llc | Mesh antenna reflector with deployable perimeter |
US11139549B2 (en) | 2019-01-16 | 2021-10-05 | Eagle Technology, Llc | Compact storable extendible member reflector |
US11862840B2 (en) | 2019-01-16 | 2024-01-02 | Eagle Technologies, Llc | Compact storable extendible member reflector |
US10797400B1 (en) | 2019-03-14 | 2020-10-06 | Eagle Technology, Llc | High compaction ratio reflector antenna with offset optics |
US20220181789A1 (en) * | 2019-04-18 | 2022-06-09 | Institute For Q-Shu Pioneers Of Space, Inc. | Antenna apparatus and spacecraft |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3541569A (en) | Expandable parabolic reflector | |
US3863870A (en) | Spin stabilized vehicle and solar cell arrangement therefor | |
US6104358A (en) | Low cost deployable reflector | |
US5977932A (en) | Self-deploying helical structure | |
US3477662A (en) | Pneumatic tube deployment means,and solar cell therewith | |
EP0184330B1 (en) | Deployable reflector | |
US4030102A (en) | Deployable reflector structure | |
US8356774B1 (en) | Structure for storing and unfurling a flexible material | |
US20040194397A1 (en) | Elongated truss boom structures for space applications | |
US3360798A (en) | Collapsible reflector | |
US4725025A (en) | Deployment system | |
US11177576B2 (en) | Antenna having deployable antenna fins and associated methods | |
JPS6255723B2 (en) | ||
EP3598576B1 (en) | Reflecting systems, such as reflector antenna systems, with tension-stabilized reflector positional apparatus | |
JPH06291537A (en) | Expanded antenna reflector and expansion method therefor | |
US3217328A (en) | Antenna with wire mesh reflector collapsing in a pinwheel manner | |
US3450372A (en) | Self-projectable element for a space vehicle | |
Ochoa et al. | Deployable helical antenna for nano-satellites | |
CN114030657A (en) | Solar wing device capable of being repeatedly folded and unfolded and using method | |
US3809337A (en) | Spin stabilized vehicle and solar cell arrangement therefor | |
Murphey | Historical perspectives on the development of deployable reflectors | |
US3722840A (en) | Spin stabilized vehicle and solar cell arrangement therefor | |
CN113682857B (en) | Large parabolic film structure winding and folding tool system and folding method | |
US11124319B2 (en) | Re-useable, deployable, sun-shade and solar sail mechanism | |
CN112531349B (en) | Antenna unfolding mechanism |