IP Library Granted Patent US 8,156,727
Granted Patent B2
US 8,156,727 · App. 12/275,729 · Granted Apr 17, 2012

Fan nozzle of adjustable section

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Quick Facts
Patent No.
US 8,156,727
App. No.
12/275,729
Granted
Apr 17, 2012
Kind
B2
Abstract

An adjustable section nozzle having a ring of deformable panels arranged close to its trailing edge is disclosed. Each panel has a dual-strip type structure made up of two materials presenting different coefficients of expansion, together with controlled heater devices that are thermally coupled to the set of panels.

Claims (14)

1. An adjustable-section fan nozzle comprising:

a ring of deformable panels arranged close to a trailing edge of the adjustable-section fan nozzle,

wherein each deformable panel comprises a dual-strip structure comprising an inner strip of thermally-insulating material together with at least one outer strip of metal, said inner and outer strips presenting different coefficients of expansion and being assembled in full flat contact one against another so that a variation in temperature induces deformation of said dual-strip structure caused by the difference between said coefficients of expansion,

wherein controlled heater means comprise electrical resistances distributed over the surfaces of the at least one outer strip of metal and in thermal contact therewith, and

wherein the assembled inner and outer strips cause each deformable panel to curve in a direction tending to reduce a flow section at an outlet from the nozzle when said controlled heater means are actuated.

2. A nozzle according to claim 1 , wherein said thermally-insulating material is a composite material.

3. A nozzle according to claim 1 , wherein each deformable panel is substantially trapezoidal in shape.

4. A nozzle according to claim 1 , wherein said deformable panels are mounted in an annular space defined in a wall of said adjustable-section fan nozzle.

5. A nozzle according to claim 4 , wherein said deformable panels are continuous with an inside face of said wall when said controlled heater means are not in service.

6. A bypass turbojet, including a fan nozzle according to claim 1 .

7. A nozzle according to claim 1 , wherein an additional insulating layer covers an outer surface of each panel.

8. A nozzle according to claim 1 , wherein an outer wall of said adjustable-section fan nozzle includes an inner annular casing and an outer annular casing defining an annular cavity therebetween, and said panels are housed in said annular cavity.

9. A nozzle according to claim 8 , wherein said inner strip presents a stub with a first surface which abuts said inner annular casing and a second surface which abuts said outer annular casing.

10. A nozzle according to claim 2 , wherein the composite material is based on carbon.

Assignments (3)
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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 2, 2009
From: DIJOUD, DELPHINE EDITH; FAUVELET, BENOIT MARC MICHEL; VINCENT, THOMAS ALAIN CHRISTIAN
To: SNECMA
Reel/Frame 022189/0046 →