IP Library Granted Patent US 6,930,654
Granted Patent B2
US 6,930,654 · App. 10/630,899 · Granted Aug 16, 2005

Deployable antenna reflector

Assignee: Astrium GmbH
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Quick Facts
Patent No.
US 6,930,654
App. No.
10/630,899
Granted
Aug 16, 2005
Kind
B2
Abstract

A deployable antenna reflector comprising a central dish and a plurality of deployable sheet-like panels arranged around the central dish. The reflector further comprises a central supporting body, whereon the central dish is fixedly mounted and whereto the deployable sheet-like panels are hinged. The rotation axes of the individual deployable sheet-like panels are tilted with respect to the center point of the central dish. In the stowed configuration of the reflector, the deployable sheet-like panels are at least partially deflected in order to minimize the envelope of the reflector and that the panels relax upon deployment.

Claims (38)

1. A deployable antenna reflector, comprising:

a central dish fixedly mounted on a central supporting body;

a plurality of deployable sheet-like panels hinged to said central supporting body and arranged around the central dish;

wherein the rotation axes of each of individual ones of said deployable sheet-like panels are tilted with respect to a center point of the central dish, and wherein, in a stowed configuration of the reflector, upper corner edges of the deployable sheet-like panels are at least partially deflected in order to minimize an envelope of the reflector and the panels relax upon entering a deployment configuration.

2. The deployable antenna reflector according to claim 1 , wherein each of said sheet-like panels is supported by a rib which connects said each sheet-like panel to the central supporting body via mechanical bushings.

3. The deployable antenna reflector according to claim 2 , wherein each sheet-like panel includes a torque spring acting on the rotation axis thereby driving the sheet-like panels from the stowed configuration into the deployed configuration.

4. The deployable antenna reflector according to claim 2 , wherein a damping device is mounted on one of the sheet-like panels in order to simultaneously damp the motion of the sheet-like panels during deployment.

5. The deployable antenna reflector according to claim 2 , wherein the central supporting body is a hollow ring made of carbon fiber reinforced plastic.

6. The deployable antenna reflector according to claim 2 , wherein the deployable sheet-like panels are made of carbon fiber reinforced plastic.

7. The deployable antenna reflector according to claim 1 , wherein each sheet-like panel includes a torque spring acting on the rotation axis thereby driving the sheet-like panels from the stowed configuration into the deployed configuration.

8. The deployable antenna reflector according to claim 7 , wherein a damping device is mounted on one of the sheet-like panels in order to simultaneously damp the motion of the sheet-like panels during deployment.

9. The deployable antenna reflector according to claim 7 , wherein the central supporting body is a hollow ring made of carbon fiber reinforced plastic.

10. The deployable antenna reflector according to claim 7 , wherein the deployable sheet-like panels are made of carbon fiber reinforced plastic.

11. The deployable antenna reflector according to claim 1 , wherein the central supporting body is a hollow ring made of carbon fiber reinforced plastic.

12. The deployable antenna reflector according to claim 1 , wherein the deployable sheet-like panels are made of carbon fiber reinforced plastic.

13. The A deployable antenna reflector comprising:

a central dish fixedly mounted on a central supporting body;

a plurality of deployable sheet-like panels hinged to said central supporting body and arranged around the central dish;

wherein the rotation axes of each of individual ones of said deployable sheet-like panels are tilted with respect to a center point of the central dish, and wherein, in a stowed configuration of the reflector, the deployable sheet-like panels are at least partially deflected in order to minimize an envelope of the reflector and the panels relax upon entering a deployment configuration, wherein brackets are mounted at the outer end of each sheet-like panel forming a closed formlocking structural ring in the stowed configuration of the reflector.

14. The deployable antenna reflector according to claim 13 , wherein, in the stowed configuration of the reflector, the structural ring is loaded by a circumferential rope allowing to compress the individual brackets with respect to each other.

15. The deployable antenna reflector according to claim 13 , wherein a damping device is mounted on one of the sheet-like panels in order to simultaneously damp the motion of the sheet-like panels during deployment.

16. The deployable antenna reflector according to claim 13 , wherein the central supporting body is a hollow ring made of carbon fiber reinforced plastic.

17. A deployable antenna reflector, comprising:

a central dish fixedly mounted on a central supporting body;

a plurality of deployable sheet-like panels hinged to said central supporting body and arranged around the central dish;

wherein the rotation axes of each of individual ones of said deployable sheet-like panels are tilted with respect to a center point of the central dish, and wherein, in a stowed configuration of the reflector, the deployable sheet-like panels are at least partially deflected in order to minimize an envelope of the reflector and the panels relax upon entering a deployment configuration, wherein a damping device is mounted on one of the sheet-like panels in order to simultaneously damp the motion of the sheet-like panels during deployment; and

wherein the damping device cooperates with a cable drum on which a damping rope is wound said damping rope being guided around the formlocking ring in the stowed configuration.

18. A deployable antenna reflector, comprising:

a central dish fixedly mounted on a central supporting body;

a plurality of deployable sheet-like panels hinged to said central supporting body and arranged around the central dish;

wherein the rotation axes of each of individual ones of said deployable sheet-like panels are tilted with respect to a center point of the central dish, and wherein, in a stowed configuration of the reflector, the deployable sheet-like panels are at least partially deflected in order to minimize an envelope of the reflector and the panels relax upon entering a deployment configuration;

each of said sheet-like panels is supported by a rib which connects said each sheet-like panel to the central supporting body via mechanical bushings; and

wherein brackets are mounted at the outer end of each sheet-like panel forming a closed formlocking structural ring in the stowed configuration of the reflector.

19. A deployable antenna reflector comprising:

a central dish fixedly mounted on a central supporting body;

a plurality of deployable sheet-like panels hinted to said central supporting body and arranged around the central dish;

wherein the rotation axes of each of individual ones of said deployable sheet-like panels are tilted with respect to a center point of the central dish, and wherein, in a stowed configuration of the reflector, the deployable sheet-like panels are at least partially deflected in order to minimize an envelope of the reflector and the panels relax upon entering a deployment configuration, wherein each sheet-like panel includes a torque spring acting on the rotation axis thereby driving the sheet-like panels from the stowed configuration into the deployed configuration; and

brackets are mounted at the outer end of each sheet-like panel forming a closed formlocking structural ring in the stowed configuration of the reflector.

Assignments (3)
MERGER Recorded Jan 10, 2019
From: AIRBUS DS GMBH
To: AIRBUS DEFENCE AND SPACE GMBH
Reel/Frame 048043/0373 →
CHANGE OF NAME Recorded Oct 30, 2018
From: ASTRIUM GMBH
To: AIRBUS DS GMBH
Reel/Frame 047906/0600 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 23, 2003
From: SCHMID, MANFRED; SCHEULEN, DIETMAR; BARHO, REINER; WEIMER, PETER
To: ASTRIUM GMBH
Reel/Frame 014829/0707 →
Priority Claims (1)
EP 02017163 · Jul 31, 2002 · regional
Continuity (1)
Related Publication 20040104861A1 · Jun 3, 2004