IP Library Granted Patent US 9,381,719
Granted Patent B2
US 9,381,719 · App. 12/305,656 · Granted Jul 5, 2016

Assembly of prepregs for producing structures, for example ones which deploy through inflation

Inventors: Brigitte Defoort (Saint Medard en Jalles, FR); Dominique Lacour (Tresses, FR); Olivier Le-Couls (Saint Medard en Jalles, FR)
Assignee: ASTRIUM SAS
B32B7/045B29C65/14B29C65/1496B29C65/48B29C65/4845B29C66/1122B29C66/21B29C66/52241B29C66/721B29C66/72141B29C66/7394B29C70/305B29C70/54B29C70/86C08G59/68B29C35/0894B29C53/30B29C65/1403B29C65/1406B29C65/1409B29C65/1435B29C65/4815B29C66/63B29C66/71B29C66/7212B29C66/73754B29C66/73941B29C2035/0827B29K2063/00B29K2105/243B29K2105/258B29L2022/02B29L2031/3097B29L2031/605B29L2031/703B64G2001/224Y10T156/1049Y10T156/1051Y10T428/13Y10T428/1362Y10T428/2457Y10T428/24479Y10T428/24488Y10T428/24802Y10T428/24826
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Quick Facts
Patent No.
US 9,381,719
App. No.
12/305,656
Granted
Jul 5, 2016
Kind
B2
Abstract

The invention relates to a method of assembling pre-impregnated plies by local isolated polymerization of the assembly region ( 30 ) under the action of a radiation to which the resin of the prepreg is sensitive. The assembly method makes it possible in particular to produce very large sized gossamer structures ( 7 ) in the form of a concertina-folded tube which is deployed by injecting pressurized gas once in space then stiffened by polymerization under the effect of the same radiation. The pylon concerned ( 7 ) thus comprises two structural elements ( 10, 20 ) secured end to end while at the same time maintaining its flexibility and firmness qualities.

Claims (77)

1. A method of assembling a first structural element comprising a first prepreg ply extending in a first direction and a second structural element comprising a second prepreg ply extending in the first direction, the method comprising:

superimposing the first prepreg ply of the first structural element and the second prepreg ply of the second structural element to form a junction zone, wherein the junction zone comprises:

a first assembly strip having a width W 1 in the first direction and a length L 1 in a second direction, which is perpendicular to the first direction;

a second assembly strip having a width W 2 in the first direction and a length L 2 in the second direction; and

an intermediate strip, which separates the first assembly strip and the second assembly strip; and

irradiating discrete points of the first assembly strip and the second assembly strip with visible light, UV light, or electrons, thereby locally cross polymerizing and bonding the first and second prepregs at the discrete points in the first and second assembly strips,

wherein the first and second prepregs are at least partially polymerizable under a predetermined radiation and are not polymerized and remain juxtaposed in the intermediate strip,

wherein the discrete points in the first assembly strip are arranged such that:

projections of each of the discrete points in the first assembly strip, in the first direction, onto an imaginary line extending along the length L 1 forms a continuous line C 1 along the entire length of the imaginary line extending along the length L 1 , wherein at each location along the continuous line C 1 a single discrete point projects onto the continuous line C 1 from the first assembly strip; and

projections of each of the discrete points in the first assembly strip, in the second direction, onto an imaginary line extending along the width W 1 forms a continuous line C 1 ′ along the entire width of the imaginary line extending along the width W 1 ,

wherein the discrete points in the second assembly strip are arranged such that:

projections of each of the discrete points in the second assembly strip, in the first direction, onto an imaginary line extending along the length L 2 forms a continuous line C 2 along the entire length of the imaginary line extending along the length L 2 , wherein at each location along the continuous line C 2 a single discrete point projects onto the continuous line C 2 from the second assembly strip; and

projections of each of the discrete points in the second assembly strip, in the second direction, onto an imaginary line extending along the width W 2 forms a continuous line C 2 ′ along the entire width of the imaginary line extending along the width W 1 .

2. The method of claim 1 , further comprising:

placing a mask comprising an opaque part and a part enabling the passage of the radiation on the junction zone prior to the irradiation; and then

irradiating through the mask, thereby cross polymerizing the discrete points,

wherein the discrete points have a geometry of the mask.

3. The method of claim 1 , wherein the irradiating is carried out with light, and the first and second prepregs comprise a fibrous material impregnated with a composition comprising:

an epoxy or epoxy-acrylate resin; and

a photo-initiator,

wherein the photo-initiator is an iron-arene complex salt of formula (I):

wherein:

A is an arene group; and

X is a non nucleophilic anion.

4. The method of claim 1 , wherein the first structural element further comprises a first film on a face of the first prepreg ply and the second structural element further comprises a second film on a face of the second prepreg ply, wherein the first and second film are each transparent to the radiation.

5. The method of claim 1 , wherein the first and second structural elements are tubular and the method further comprises:

positioning the first element and the second element end to end on a mandrel.

6. The method of claim 1 , further comprising, prior to assembly:

folding an end portion of the first element.

7. The method of claim 1 , further comprising, after the assembly:

folding a non folded part of the first element, the junction zone, and the second element.

8. An inflatable space structure, obtained by a method of assembling a first structural element comprising a first prepreg ply extending in a first direction and a second structural element comprising a second prepreg ply extending in the first direction, the method comprising:

superimposing the first prepreg ply of the first structural element and the second prepreg ply of the second structural element to form a junction zone, wherein the junction zone is divided into:

a first assembly strip having a width W 1 in the first direction and a length L 1 in a second direction, which is perpendicular to the first direction;

a second assembly strip having a width W 2 in the first direction and a length L 2 in the second direction; and

an intermediate strip, which separates the first assembly strip and the second assembly strip,

irradiating discrete points of the first assembly strip and second assembly strip with visible light, UV light, or electrons, thereby locally cross polymerizing and bonding the first and second prepegs at the discrete points in the first and second assembly strips,

wherein the first and second prepregs are at least partially polymerizable under a predetermined radiation and are not polymerized and remain juxtaposed in the intermediate strip,

wherein the discrete points in the first assembly strip are arranged such that:

projections of each of the discrete points in the first assembly strip, in the first direction, onto an imaginary line extending along the length L 1 forms a continuous line C 1 along the entire length of the imaginary line extending along the length L 1 , wherein at each location along the continuous line C 1 a single discrete point projects onto the continuous line C 1 from the first assembly strip; and

projections of each of the discrete points in the first assembly strip, in the second direction, onto an imaginary line extending along the width W 1 forms a continuous line C 1 ′ along the entire width of the imaginary line extending along the width W 1 ,

wherein the discrete points in the second assembly strip are arranged such that:

projections of each of the discrete points in the second assembly strip, in the first direction, onto an imaginary line extending along the length L 2 forms a continuous line C 2 along the entire length of the imaginary line extending along the length L 2 , wherein at each location along the continuous line C 2 a single discrete point projects onto the continuous line C 2 from the second assembly strip; and

projections of each of the discrete points in the second assembly strip, in the second direction, onto an imaginary line extending along the width W 2 forms a continuous line C 2 ′ along the entire width of the imaginary line extending along the width W 1 .

9. The inflatable space structure of claim 8 , wherein the first and second prepregs comprise a fibrous material impregnated with a composition comprising:

an epoxy or epoxy-acrylate resin; and

a photo-initiator,

wherein the photo-initiator is an iron-arene complex salt of formula (I):

wherein:

A is an arene group; and

X is a non nucleophilic anion.

10. A structure, comprising:

a first element comprising a first prepreg ply extending in a first direction; and

a second element comprising a second prepreg ply extending in the first direction,

wherein the first and second prepreg ply are sensitive to a polymerization radiation,

wherein the first prepreg ply and the second prepreg ply are superimposed to form a junction zone, wherein the junction zone comprises:

a first assembly strip having a width W 1 in the first direction and a length L 1 in a second direction, which is perpendicular to the first direction;

a second assembly strip having a width W 2 in the first direction and a length L 2 in the second direction; and

an intermediate zone, which separates the first assembly strip and the second assembly strip,

wherein the first and second prepregs are bonded together in the first and second assembly strips by irradiating discrete points of the first and second assembly strips with visible light, UV light, or electrons, thereby cross polymerizing and bonding the first and second prepegs at the discrete points in the first and second assembly strips, and wherein the first and second prepegs are juxtaposed without cross-linking polymerization in the intermediate zone,

wherein the discrete points in the first assembly strip are arranged such that:

projections of each of the discrete points in the first assembly strip, in the first direction, onto an imaginary line extending along the length L 1 forms a continuous line C 1 along the entire length of the imaginary line extending along the length L 1 , wherein at each location along the continuous line C 1 a single discrete point projects onto the continuous line C 1 from the first assembly strip; and

projections of each of the discrete points in the first assembly strip, in the second direction, onto an imaginary line extending along the width W 1 forms a continuous line C 1 ′ along the entire width of the imaginary line extending along the width W 1 ,

wherein the discrete points in the second assembly strip are arranged such that:

projections of each of the discrete points in the second assembly strip, in the first direction, onto an imaginary line extending along the length L 2 forms a continuous line C 2 along the entire length of the imaginary line extending along the length L 2 , wherein at each location along the continuous line C 2 a single discrete point projects onto the continuous line C 2 from the second assembly strip; and

projections of each of the discrete points in the second assembly strip, in the second direction, onto an imaginary line extending along the width W 2 forms a continuous line C 2 ′ along the entire width of the imaginary line extending along the width W 1 .

11. The structure of claim 10 , wherein the first and second elements are tubular and the junction zone extends over the circumference of a tube.

12. The structure of claim 10 , having at least a part that is concertina folded.

13. The structure of claim 10 , comprising a fold in the junction zone.

14. An inflatable space manipulation pylon, comprising the structure of claim 10 .

15. The structure of claim 10 , wherein the first and second prepregs comprise a fibrous material impregnated with a composition comprising:

an epoxy or epoxy-acrylate resin; and

a photo-initiator,

wherein the photo-initiator is an iron-arene complex salt of formula (I):

wherein:

A is an arene group; and

X is a non nucleophilic anion.

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 Dec 23, 2008
From: DEFOORT, BRIGITTE; LACOUR, DOMINIQUE; LE-COULS, OLIVIER
To: ASTRIUM SAS
Reel/Frame 022022/0535 →
Priority Claims (1)
FR 06 52943 · Jul 12, 2006 · national
Continuity (1)
Related Publication 20100166988A1 · Jul 1, 2010