Claims
- 1. A satellite solar generator assembly comprising:first and second joint parts connected with respective solar generator extension arms, a hinge pin pivotally connecting the first and second joint parts, a large pulley rotatably mounted at the hinge pin and fixed to the first joint part, a small pulley disposed on the second joint part at a spacing from the larger pulley, a cord partially wound on both the large and small pulleys, and a drive which in use operates to rotate the small pulley to wind the cord thereon, said cord being operable to rotate the large pulley and unfold the solar generator extension arms, wherein a ratio of a torque on the large pulley over a torque on the small pulley is equal to a ratio of the diameter of the large pulley over the diameter of the small pulley.
- 2. An assembly according to claim 1,wherein the drive includes a spring member which can be triggered by telecontrol.
- 3. An assembly according to claim 1,wherein the ratio of the sizes of the pulleys provides that less than one half of the torque required to unfold the joint part needs to be applied by the drive to the small pulley.
- 4. An assembly according to claim 1, wherein the ratio of the sizes of the pulleys provides that less than one half of the torque required to unfold the joint parts needs to be applied by the drive to the small pulley.
- 5. An assembly according to claim 2, wherein the spring member is configured to apply a substantially constant torque over the predetermined folding range of the joint part.
- 6. An assembly according to claim 4, wherein the predetermined folding range is 180°.
- 7. An assembly according to claim 5, wherein the ratio of the sizes of the pulleys provides that less than one half of the torque required to unfold the joint halves needs to be applied by the drive to the small pulley.
- 8. An assembly according to claim 1, wherein the drive is a motor driven chain drive.
- 9. An assembly according to claim 1, wherein the drive is a motor driven toothed-belt drive.
- 10. An assembly according to claim 1, wherein the drive is a motor driven gear drive.
Priority Claims (2)
Number |
Date |
Country |
Kind |
199 27 596 |
Jun 1999 |
DE |
|
100 23 852 |
May 2000 |
DE |
|
Parent Case Info
This application is a division of U.S. patent application Ser. No. 09/597,711, filed Jun. 19, 2000, and claims the priority of German Patent Document 199 27 596.3, filed Jun. 17, 1999, the disclosures of which applications are expressly incorporated by reference herein.
US Referenced Citations (19)
Foreign Referenced Citations (3)
Number |
Date |
Country |
3215431 |
Oct 1983 |
DE |
1055573 |
Feb 1954 |
FR |
01-282097 |
Nov 1989 |
JP |
Non-Patent Literature Citations (1)
Entry |
Kellermeier et al., “The Retractable Ultra-Lightweight (ULP) Solar Array for Retrievable Space Platforms”, Aircraft Engineering, pp. 2-5, Jan. 1984. |