IP Library Granted Patent US 7,013,650
Granted Patent B2
US 7,013,650 · App. 10/885,479 · Granted Mar 21, 2006

Flexible flap for a variable-section turbomachine nozzle

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Quick Facts
Patent No.
US 7,013,650
App. No.
10/885,479
Granted
Mar 21, 2006
Kind
B2
Abstract

In a variable-section turbomachine nozzle, a plurality of flexible follower flaps are provided that are interposed between adjacent controlled flaps against which the follower flaps are held by fastener means, each follower flap comprising a plurality of independent transverse boxes mounted side by side in a support sheet, the boxes contacting one another via their longitudinal edges and being held in the support sheet via their lateral edges which are engaged in the longitudinal edges of the support sheet, which longitudinal edges define respective bearing zones for bearing against the adjacent controlled flaps.

Claims (25)

1. A flexible follower flap for a variable-section turbomachine nozzle, the flexible follower flap being interposed between two adjacent controlled flaps against which it is held by fastener means, the flexible follower flap comprising a plurality of independent transverse boxes mounted side by side in a support sheet, the boxes being in contact with one another via their raised longitudinal edges and being held in the support sheet by their lateral edges which are engaged in longitudinal edges of the support sheet.

2. A flexible follower flap according to claim 1 , wherein said longitudinal edges of the support sheet engaging the lateral edges of the boxes define respective bearing zones for bearing against the adjacent controlled flaps.

3. A flexible follower flap according to claim 1 , wherein said longitudinal edges of the support sheet include holding notches for holding the transverse boxes in position, each notch receiving the ends of the raised longitudinal edges of two adjacent boxes.

4. A flexible follower flap according to claim 1 , wherein one of the boxes of said plurality of transverse boxes further comprises a transverse holder strip for holding the follower flap in a rest position.

5. A flexible follower flap according to claim 4 , wherein said holder strip constitutes the terminal transverse arm of a short upright extending radially from a longitudinal edge of said transverse box.

6. A flexible follower flap according to claim 4 , wherein said transverse box is an end transverse box of the follower flap.

7. A flexible follower flap according to claim 1 , wherein said support sheet is constituted by a metal plate of a material that is relatively flexible and that withstands high temperatures.

8. A variable-section turbomachine nozzle including a plurality of flexible follower flaps according to claim 1 .

9. A flexible follower flap for a variable-section turbomachine nozzle, said flexible follower flap comprising:

a plurality of independent transverse boxes, each of said boxes including raised longitudinal edges and lateral edges; and

a support sheet having longitudinal edges, wherein said boxes are mounted side by side in said support sheet with said boxes being in contact with one another via their raised longitudinal edges and being held in said support sheet by their lateral edges which are engaged in said longitudinal edges of said support sheet.

10. A flexible follower flap according to claim 9 , wherein said longitudinal edges of the support sheet engaging the lateral edges of the boxes define respective bearing zones for bearing against an adjacent controlled flap.

11. A flexible follower flap according to claim 9 , wherein said longitudinal edges of the support sheet include holding notches for holding the transverse boxes in position, each notch receiving the ends of the raised longitudinal edges of two adjacent boxes.

12. A flexible follower flap according to claim 9 , wherein one of the boxes of said plurality of transverse boxes further comprises a transverse holder strip for holding the follower flap in a rest position.

13. A flexible follower flap according to claim 12 , wherein said holder strip constitutes the terminal transverse arm of a short upright extending radially from a longitudinal edge of said transverse box.

14. A flexible follower flap according to claim 12 , wherein said transverse box is an end transverse box of the follower flap.

15. A flexible follower flap according to claim 9 , wherein said support sheet is flexible.

16. A variable-section turbomachine nozzle including a plurality of flexible follower flaps according to claim 9 .

17. A flexible follower flap for a variable-section turbomachine nozzle, said flexible follower flap comprising:

a plurality of independent transverse components, each of said components comprising two raised longitudinal edges and two lateral edges; and

a support sheet comprising two longitudinal edges with spaced-apart notches formed along each of the longitudinal edges,

wherein each of said components is held in said support sheet by engagement of the lateral edges of said component and the longitudinal edges of said support sheet, and wherein each of said notches formed said longitudinal edges of said support sheet receives a portion of the raised longitudinal edges of adjacently positioned components.

18. A flexible follower flap according to claim 17 , wherein said longitudinal edges of the support sheet engaging the lateral edges of the components define respective bearing zones for bearing against adjacent controlled flaps.

19. A flexible follower flap according to claim 17 , wherein one of the components of said plurality of transverse components further comprises a transverse holder strip for holding the follower flap in a rest position.

20. A variable-section turbomachine nozzle including a plurality of flexible follower flaps according to claim 17 .

Assignments (2)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →