Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle comprising cooling air circulation ducts connected through contact surfaces

Patent metadata

Field	Value
Publication number	US-11713730-B2
Application number	US-202017753220-A
Country	US
Kind code	B2
Filing date	Aug 27, 2020
Priority date	Aug 30, 2019
Publication date	Aug 1, 2023
Grant date	Aug 1, 2023

Abstract

In a convergent-divergent flap pair for a turbojet engine nozzle of the variable-geometry convergent-divergent type, the convergent flap and the divergent flap include respective cooling-air ducts connected to one another through air passage openings formed in respective contact surfaces of the convergent flap and of the divergent flap arranged facing one another.

First claim

What is claimed is:

1. A convergent-divergent flap pair for a turbojet engine nozzle of the variable-geometry convergent-divergent type, comprising a convergent flap, and a divergent flap mounted pivotably on the convergent flap about a pivot axis, whereby the convergent-divergent flap pair is capable of going from a first extreme angular configuration, in which the convergent flap and the divergent flap make between them a maximum salient angle, to a second extreme angular configuration, in which the convergent flap and the divergent flap make between them a minimum salient angle smaller than the maximum salient angle,
wherein the convergent flap includes a respective inner wall, having a respective inner surface for channelling combustion gas and a respective outer surface, and a respective outer wall,
wherein the convergent flap includes a respective cooling air circulation duct defined between the respective outer surface of the respective inner wall of the convergent flap and the respective outer wall of the convergent flap,
wherein the divergent flap includes a respective inner wall and a respective outer wall, one of which has a respective inner surface for channelling combustion gas,
wherein the divergent flap includes a respective cooling-air duct defined between the respective outer surface of the respective inner wall of the divergent flap and the respective outer wall of the divergent flap,
wherein the convergent flap includes a convergent-flap contact surface in the shape of a cylinder portion, an axis of curvature of which is the pivot axis, and provided with first air passage openings opening into the respective cooling air circulation duct of the convergent flap,
wherein the divergent flap includes a divergent-flap contact surface in the shape of a cylinder portion, an axis of curvature of which is the pivot axis, and provided with second air passage openings opening into the respective cooling-air duct of the divergent flap,
wherein the divergent-flap contact surface is arranged directly opposite the convergent-flap contact surface, so that the divergent-flap contact surface slides along the convergent-flap contact surface when the divergent flap pivots with respect to the convergent flap,
wherein the first air passage openings and the second air passage openings are shaped and positioned so that the first air passage openings are arranged directly opposite the second air passage openings, respectively, and thus place in communication the respective cooling air circulation duct of the convergent flap and the respective cooling-air duct of the divergent flap, regardless of the angular configuration adopted by the convergent-divergent flap pair.

2. The convergent-divergent flap pair according to claim 1 , wherein a first duct, out of the respective cooling air circulation duct of the convergent flap and the respective cooling-air duct of the divergent flap, is interposed between the pivot axis and a corresponding surface out of the convergent-flap contact surface and the divergent-flap contact surface.

3. The convergent-divergent flap pair according to claim 2 , wherein the respective inner wall of the one out of the convergent flap and the divergent flap that includes said first duct has a curved end portion on which said corresponding surface is formed and including those out of the first air passage openings and the second air passage openings which belong to said corresponding surface.

4. The Convergent-divergent flap pair according to claim 2 , wherein the one out of the convergent flap and the divergent flap that includes the other duct out of the respective cooling air circulation duct of the convergent flap and the respective cooling-air duct of the divergent flap includes a respective closing wall, on which the other surface, out of the convergent-flap contact surface and the divergent-flap contact surface, is formed, said closing wall including those out of the first air passage openings and the second air passage openings which belong to said other surface, and said closing wall mutually connecting two respective ends of the inner wall and of the outer wall of the flap.

5. The convergent-divergent flap pair according to claim 2 , wherein said first duct is the respective cooling-air duct of the divergent flap.

6. The convergent-divergent flap pair according to claim 1 , wherein:
the convergent flap includes two respective lateral end walls each connecting the respective inner wall of the convergent flap to the respective outer wall of the convergent flap, so that the respective cooling air circulation duct of the convergent flap is further defined by the two respective lateral end walls of the convergent flap, and
the divergent flap includes two respective lateral end walls each connecting the respective inner wall of the divergent flap to the respective outer wall of the divergent flap, so that the respective cooling-air duct of the divergent flap is further defined by the two respective lateral end walls of the divergent flap.

7. The convergent-divergent flap pair according to claim 1 , wherein the respective inner wall of the divergent flap is the wall of the divergent flap that has said respective inner surface for channelling combustion gas, and the respective inner wall of the divergent flap further has a respective outer surface, and wherein the respective cooling-air duct of the divergent flap is a respective cooling air circulation duct defined by the respective outer surface of the respective inner wall of the divergent flap.

8. A nozzle of the variable-geometry convergent-divergent type for a turbojet engine, comprising convergent-divergent flap pairs distributed around an axis of the nozzle and at least some of which are convergent-divergent flap pairs according to claim 1 , and a channel for circulation of combustion gas defined at least by the respective inner surfaces for channelling combustion gas of the respective inner walls of the respective convergent flaps and of the respective divergent flaps of the convergent-divergent flap pairs.

9. A turbojet engine for an aircraft, comprising a reheat channel surrounded by a cooling plenum separated from the reheat channel by a thermal protection liner, and a nozzle according to claim 8 ,
wherein the respective cooling air circulation ducts of the convergent flaps of the convergent-divergent flap pairs of the nozzle are connected to the cooling plenum surrounding the reheat channel.

Assignees

• Safran Aircraft Engines

Inventors

• Kohn Thierry
• Eichstädt Frédéric Paul
• Lacombe Florent Luc
• Leglaye François
• Le Pannerer Brice Marie Yves Emile

Classifications

• F02K1/1223 Primary

  of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series · CPC title

• F02C7/18

  the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title

• F02K1/1292

  of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, the internal downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series and at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantially axially movable structure · CPC title

• F02K1/80

  Couplings or connections · CPC title

• F02K1/822

  Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors · CPC title