Single movement convergent and convergent-divergent nozzle

Patent metadata

Field	Value
Publication number	US-11680495-B2
Application number	US-202217719290-A
Country	US
Kind code	B2
Filing date	Apr 12, 2022
Priority date	Feb 27, 2020
Publication date	Jun 20, 2023
Grant date	Jun 20, 2023

Abstract

A variable exhaust nozzle for use with a gas turbine engine includes an outer shroud and an inner plug that can move relative to the outer shroud. The relative movement of the inner plug and the outer shroud changes the shape of the variable exhaust nozzle from one that converges in area to one that converges and then diverges in area.

First claim

What is claimed is:

1. A variable exhaust nozzle for a gas turbine engine, the variable exhaust nozzle comprising
an outer shroud arranged circumferentially about an axis and fixed relative to the axis to define an outer boundary surface of an exhaust nozzle flow path, the outer shroud extends axially between a forward axial location and a terminal shroud end, and
an inner plug arranged circumferentially about the axis to define an inner boundary surface of the exhaust nozzle flow path, the inner plug extends axially between a forward end and a terminal tail end, and the inner boundary surface increases in diameter and then decreases in diameter as the inner plug extends axially aft from the forward end to the terminal tail end,
wherein a variable area region of the exhaust nozzle flow path is defined axially between the forward end of the inner plug and the terminal shroud end and defined radially between the outer boundary surface and the inner boundary surface,
wherein the inner plug is configured to translate axially relative to the outer shroud between an open position in which the outer boundary surface and the inner boundary surface cooperate to cause the variable area region of the exhaust nozzle flow path to converge in area to a first throat located at the terminal shroud end without diverging in area and a closed position in which the outer boundary surface and the inner boundary surface cooperate to cause the variable area region of the exhaust nozzle flow path to converge in area to a second throat and then diverge in area aft of the second throat, and the second throat is spaced apart axially from the forward end of the inner plug and the terminal shroud end,
wherein the outer shroud has a smallest inner diameter located at the terminal shroud end.

2. The variable exhaust nozzle of claim 1 , wherein the terminal tail end is located axially aft of the terminal shroud end when the inner plug is in the open position.

3. The variable exhaust nozzle of claim 1 , wherein a minimum area of the variable area region when the inner plug is in the open position is greater than the minimum area of the variable area region when the inner plug is in the closed position.

4. The variable exhaust nozzle of claim 1 , wherein the variable area region of the exhaust nozzle flow path diverges in area aft of the second throat without converging in area aft of the second throat.

5. The variable exhaust nozzle of claim 1 , wherein the inner plug is movable relative to the axis between a plurality of positions between the open position and the closed position and the variable exhaust nozzle further comprises an actuation controller configured to selectively move the inner plug and to stop and hold the inner plug relative to the axis in the open position, the closed position, and at least one of the plurality of positions.

6. The variable exhaust nozzle of claim 5 , wherein the inner plug is configured to default to one of the open position and the closed position in response to failure of the actuation controller.

7. The variable exhaust nozzle of claim 5 , wherein the actuation controller is configured to receive a first input indicative that the gas turbine engine is in a take-off mode and to move the inner plug to the open position in response to receiving the first input and the actuation controller is configured to receive a second input indicative that the gas turbine engine is in a cruise mode and to move the inner plug to the closed position in response to receiving the second input.

8. The variable exhaust nozzle of claim 1 , wherein the forward end of the inner plug is curvilinear and continuously decreases in slope as it extends aft to a maximum diameter of the inner plug.

9. A variable exhaust nozzle comprising
an outer shroud arranged circumferentially about an axis, the outer shroud having a terminal shroud end, and
an inner plug arranged circumferentially about the axis, the inner plug having a forward portion that extends axially aft and radially outward relative to the axis to a maximum diameter of the inner plug and an aft portion that extends axially aft and radially inward from the maximum diameter, the inner plug and the outer shroud cooperate to form an exhaust nozzle flow path having a variable area region defined axially between the forward portion of the inner plug and the terminal shroud end of the outer shroud,
wherein at least one of the outer shroud and the inner plug is movable relative to the axis between a first position in which the variable area region converges in area to a throat located aft of the maximum diameter of the inner plug, a second position in which the variable area region converges and then diverges in area, and a plurality of positions between the first position and the second position,
wherein the forward portion of the inner plug is convex and the aft portion of the inner plug is concave.

10. The variable exhaust nozzle of claim 9 , wherein the outer shroud has a smallest inner diameter located at the terminal shroud end.

11. The variable exhaust nozzle of claim 9 , wherein the outer shroud converges radially inward without diverging radially outward as the outer shroud extends axially aft to the terminal shroud end.

12. The variable exhaust nozzle of claim 9 , wherein the variable exhaust nozzle further comprises an actuation controller configured to selectively move the at least one of the outer shroud and the inner plug and to stop and hold the at least one of the outer shroud and the inner plug relative to the axis.

13. The variable exhaust nozzle of claim 12 , wherein the at least one of the outer shroud and the inner plug is configured to default to one of the first position and the second position in response to failure of the actuation controller.

14. The variable exhaust nozzle of claim 9 , further comprising an actuation controller configured to move the at least one of the outer shroud and the inner plug, the actuation controller is further configured to receive a first input indicative that a gas turbine engine is in a take-off mode and to move the at least one of the outer shroud and the inner plug to the first position in response to receiving the first input, and the actuation controller is further configured to receive a second input indicative that the gas turbine engine is in a cruise mode and to move the at least one of the outer shroud and the inner plug to the second position in response to receiving the second input.

15. The variable exhaust nozzle of claim 9 , wherein a minimum area of the variable area region when the at least one of the outer shroud and the inner plug is in the first position is greater than the minimum area of the variable area region when the at least one of the outer shroud and the inner plug is in the second position.

16. A method comprising
providing an inner plug arranged circumferentially about an axis and an outer shroud arranged circumferentially about the inner plug, the outer shroud having a terminal shroud end, and the inner plug having a first portion that extends axially aft and radially outward to a maximum diameter of the inner plug and a second portion that extends axially aft and radially inward from the maximum diameter, the inner plug and the outer shroud cooperating to form an exhaust nozzle flow path having a variable area region defined axially between the first portion of the inner plug and the terminal shroud end of the outer shroud,
moving at least one of the outer shroud and the inner plug relative to the axis to a first position in which the variable area region converges in area to a first throa

Assignees

• Rolls Royce Nam Tech Inc

Inventors

• Sanderson Andrew
• Sutterfield David L
• Lerg Bryan H

Classifications

• F02K1/08

  by axially moving or transversely deforming an internal member, e.g. the exhaust cone · CPC title

• F05D2240/1281

  Plug nozzles · CPC title

• F01D17/167 Primary

  of vanes moving in translation · CPC title

• F02K1/04 Primary

  Mounting of an exhaust cone in the jet pipe · CPC title

• F02K1/09

  by axially moving an external member, e.g. a shroud (F02K1/12 takes precedence) · CPC title