Process and apparatus for the release of a prestress initially applied to a mechanism such as a bearing on board a space vehicle

• US 5,030,016 A
• Filed: 07/11/1990
• Issued: 07/09/1991
• Est. Priority Date: 07/11/1990
• Status: Expired due to Fees

• Current Assignee: Aerospatiale Societe Nationale Industrielle
• Original Assignee: Aerospatiale Societe Nationale Industrielle
• Inventors: Schoeffter, Jean-Pierre
• Primary Examiner(s): Hannon, Thomas R.
• Application Number:
  US07/551,567
• Time in Patent Office: 363 Days
• Field of Search: 384/448, 384/476, 384/490, 384/493, 384/504, 384/517, 384/537, 384/540, 384/542, 384/556, 384/563, 384/627, 384/903, 29/898.09
• US Class Current: 384/448
• CPC Class Codes: B64G 1/222 for deploying structures between a stowed and deployed state
• CPC Class Codes: B64G 1/2228 characterised by the hold-down or release mechanisms
• CPC Class Codes: B64G 1/44 using radiation, e.g. deployable solar arrays
• CPC Class Codes: F16C 19/163 with angular contact
• CPC Class Codes: F16C 19/543 in O-arrangement
• CPC Class Codes: F16C 2202/28 Shape memory material
• CPC Class Codes: F16C 2326/47 Cosmonautic vehicles, i.e. bearings adapted for use in outer-space
• CPC Class Codes: F16C 25/083 with resilient means acting axially on a race ring to preload the bearing
• CPC Class Codes: F16C 41/04 Preventing damage to bearings during storage or transport thereof or when otherwise out of use
• CPC Class Codes: Y10T 29/497 Pre-usage process, e.g., preloading, aligning

Abstract

In space vehicles, mechanisms such as ball bearings (14, 14'"'"') are subject to an initial preload or prestress enabling them to withstand the vibrations caused by the launch and without leading to any clearance or play. A member (34) made from a shape memory material e.g. makes it possible under the effect of its elongation, to release said preload when the vehicle is in the operational mode. The control of the release can take place by means of a heating resistor (36), whose energization leads to the member (34) clearing its shape change temperature.

Claims

1. Apparatus for the release of a prestress or preload initially applied by prestressing or preloading means between the moving parts of a mechanism on board a space vehicle, when the latter is in the operational mode, said apparatus comprising a member made from a shape memory material associated with the prestress or preload means, so as to control a release of the prestress or preload applied between said parts under the effect of a change to its shape, when clearing a phase change temperature of the shape memory material.

2. Apparatus according to claim 1, wherein the mechanism comprises at least one bearing having a fixed ring and a rotary ring between which are placed the rolling members, the prestressing means acting on the fixed ring via a first tubular spacer, so as to initially apply an axial prestress to said fixed ring.

3. Apparatus according to claim 2, wherein the shape memory material member is a second tubular spacer arranged coaxially to the first spacer, the clearing of the phase change temperature having the effect of elongating the second spacer and of transferring the prestress from the fixed ring to the second tubular spacer.

4. Apparatus according to claim 2, wherein the prestressing means act on said parts via elastic means.

5. Apparatus according to claim 4, wherein the elastic means are interposed between the first tubular spacer and the fixed ring of the bearing.

6. Apparatus according to claim 2, wherein the fixed ring is an inner ring of the bearing mounted on a fixed spindle, the prestressing means incorporating a nut screwed onto a threaded end of said spindle traversing the first tubular spacer.

7. Apparatus according to claim 2 also comprising heating means located in the vicinity of said shape memory material member.

8. Process for the release of a prestress initially applied between the moving parts of a mechanism carried on a space vehicle, when the latter is in the operational mode, comprising controlling a shape change of a shape memory material member associated with said mechanism, so as to obtain a release of the prestress applied between the parts by making said member clear a phase change temperature of the shape memory material.

9. Process according to claim 8, wherein said member is made to clear the phase change temperature of the shape memory material by heating said member with the aid of heating means located in the vicinity thereof.

10. Process according to claim 8, wherein said member is made to clear the phase change temperature of the shape memory material by heating the member by solar power.