Mounting device for supporting a component, especially a mirror or an antenna reflector in a spacecraft

• US 4,533,100 A
• Filed: 07/03/1984
• Issued: 08/06/1985
• Est. Priority Date: 04/03/1981
• Status: Expired due to Term

• Current Assignee: Aerospatiale Societe Nationale Industrielle, REOSC Co.
• Original Assignee: Aerospatiale Societe Nationale Industrielle, REOSC Co.
• Inventors: Paseri, Jacques
• Primary Examiner(s): Blix, Trygve M.
• Assistant Examiner(s): Corl, Rodney
• Application Number:
  US06/626,484
• Time in Patent Office: 399 Days
• Field of Search: 244/158 R, 244/173, 403/291, 403/57, 403/58, 248/485, 248/630, 248/183, 343/DIG. 2, 350/307, 308/2 A, 308/2 R, 267/160
• US Class Current: 244/158.1
• CPC Class Codes: B64G 1/66 Arrangements or adaptations of apparatus or instruments, not otherwise provided for
• CPC Class Codes: F16C 11/12 incorporating flexible connections, e.g. leaf springs
• CPC Class Codes: F16C 2380/00 Electrical apparatus in general H01 - H05
• CPC Class Codes: F16F 15/073 using only leaf springs
• CPC Class Codes: G02B 7/182 for mirrors
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: Y10S 343/02 Satellite-mounted antenna

Abstract

The invention relates to a mounting device for supporting a component, especially a mirror or an antenna reflector in a spacecraft. The device comprises a combination of flexible blades disposed between the support, and between the intermediate piece and the component.

Claims

1. A device for mounting a component in a support, especially an optical element or an antenna reflector in a spacecraft, said device comprising:

a first flexible plane blade rigidly secured to the support and extending along a first axis towards the component;

a first piece rigidly secured to said first blade and to which are fixed without clearance an end of each blade of a first pair of flexible plane blades, said blades of said pair extending in two secant planes the intersection of which is parallel to a second axis;

a second piece rigidly secured to said component and to which are fixed without clearance an end of each blade of a second pair of flexible plane blades, said blades of said second pair extending in two other secant planes the intersection of which is parallel to a third axis, said first, second and third axes being arranged according to the three directions of a triorthogonal system; and

an intermediate piece to which are fixed without clearance the other ends of the blades of said first pair and of said second pair;

whereby said component may translate in a plane containing said first and third axes and rotate about said second and third axes, with respect to said support.

2. A device according to claim 1, wherein the ends of the blades of said first pair and of said second pair are embedded in the pieces to which they are fixed.

3. A device according to claim 1 or 2, wherein said first piece and said second piece have faces opposite to said intermediate piece.

4. A device according to claim 1, wherein said second piece is located between two parts forming said first piece.

5. A device according to claim 1, wherein said first flexible blade and said first piece are different portions of a single piece.

6. A device according to claim 1 or 2, in combination with two other mounting devices which are identical with said device, the three devices being spaced at 120°

on a circle around said component.

7. A device according to claim 1 wherein said component is an optical piece.

8. A device according to claim 7, wherein said optical piece is a mirror.

9. A device according to claim 7 wherein said optical piece has an optical axis which is parallel or orthogonal to said first axis.

10. A device according to claim 1 wherein said component is an antenna reflector.

11. A device according to claim 1 wherein said support is located in a spacecraft.