IP Library Granted Patent US 9,643,367
Granted Patent B2
US 9,643,367 · App. 13/522,603 · Granted May 9, 2017

Method for producing a composite mirror and composite mirror obtained with same

Inventors: Christian Desagulier (Paris, FR); Stephane Baril (Triel sur Seine, FR)
Assignee: ASTRIUM SAS
B29D11/00596G02B5/0808G02B7/183
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Quick Facts
Patent No.
US 9,643,367
App. No.
13/522,603
Granted
May 9, 2017
Kind
B2
Abstract

A method for producing a composite mirror. It comprises the steps of providing a glass blank with low coefficient of expansion, machining a convex shape ( 4 ) in the glass blank, laying a front skin ( 6 ) impregnated with resin over the convex shape ( 4 ) of the glass blank ( 2 ), machining in a rear supporting structure ( 8 ) a concave shape matching the convex shape machined in the glass blank ( 2 ), gluing the concave shape ( 10 ) of the supporting structure ( 8 ) onto the convex shape of the glass blank ( 2 ), machining a convex shape in the supporting structure, laying a rear skin ( 14 ) impregnated with resin on a mold, gluing the rear skin ( 14 ) onto the convex shape of the supporting structure ( 8 ), turning over the assembly so that the blank ( 2 ) lies in the upper portion of the assembly, machining and polishing a mirror in the glass blank ( 2 ).

Claims (14)

1. A method for producing a composite mirror for an observation satellite, comprising the steps of:

providing a glass blank with a low coefficient of expansion;

machining a convex shape in the glass blank;

laying a front skin impregnated with resin over the convex shape of the glass blank;

machining, in a rear supporting structure, a concave shape matching the convex shape machined in the glass blank;

gluing the concave shape of the supporting structure onto the convex shape of the glass blank;

machining a convex shape in the supporting structure;

laying a rear skin impregnated with resin in a mould with a low coefficient of expansion whose shape matches the convex shape of the supporting structure;

gluing the rear skin onto the convex shape of the supporting structure, turning over the assembly formed by the glass blank, the front skin, the supporting structure and the rear skin so that the blank lies in the upper portion of the assembly; and

machining and polishing a mirror in the glass blank.

2. The method for producing a mirror according to claim 1 , wherein the surface of the mirror is coated with a layer of aluminium or a layer of silver on which a silica layer is deposited.

3. The method for producing a mirror according to claim 1 or 2 , wherein the supporting structure is a honeycomb structure.

4. A method for producing a mirror according to claim 1 or 2 , wherein the supporting structure is formed of juxtaposed equilateral triangles.

5. The method for producing a mirror according to one of claim 1 or 2 , wherein the front skin is fixed onto the convex shape of the glass blank without adding any binding adhesive other than the impregnated resin.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 16, 2019
From: AIRBUS DEFENCE AND SPACE SAS
To: ARIANEGROUP SAS
Reel/Frame 048019/0098 →
CHANGE OF NAME Recorded Jan 14, 2019
From: ASTRIUM SAS
To: AIRBUS DEFENCE AND SPACE SAS
Reel/Frame 047989/0857 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 18, 2012
From: DESAGULIER, CHRISTIAN; BARIL, STEPHANE
To: ASTRIUM SAS
Reel/Frame 028577/0270 →
Priority Claims (1)
FR 10 50354 · Jan 20, 2010 · national
Continuity (1)
Related Publication 20120295521A1 · Nov 22, 2012