Variable area exhaust nozzle system and method for control thereof

Patent metadata

Field	Value
Publication number	US-11732673-B2
Application number	US-202117386065-A
Country	US
Kind code	B2
Filing date	Jul 27, 2021
Priority date	Jul 27, 2021
Publication date	Aug 22, 2023
Grant date	Aug 22, 2023

Abstract

A variable area exhaust nozzle defining an actual area ratio for a gas turbine engine that includes a shroud assembly having a fixed shroud and an adjustable cowl, an adjustable plug, a nozzle adjustment assembly, and a controller configured to receive data indicative of an operating speed of the gas turbine engine; determine a target area ratio based at least in part on received data indicative of the operating speed of the gas turbine engine; and operate the nozzle adjustment assembly to selectively adjust at least one of the adjustable cowl or the adjustable plug such that the actual area ratio is substantially equivalent to the target area ratio.

First claim

What is claimed is:

1. A variable area exhaust nozzle for a gas turbine engine, the gas turbine engine defining an axial direction, the variable area exhaust nozzle comprising:
a shroud assembly comprising a fixed shroud and an adjustable cowl mechanically coupled to the fixed shroud, the fixed shroud defining an aft end and the adjustable cowl having a forward end;
an adjustable plug slidably positioned within the fixed shroud and being movable between a retracted position and an extended position along the axial direction, wherein an annular passage is defined between the adjustable cowl and the adjustable plug, and wherein the variable area exhaust nozzle defines an actual area ratio equivalent to a nozzle exit area over a nozzle throat area; and
a nozzle adjustment assembly for selectively positioning at least one of the adjustable cowl or the adjustable plug,
wherein the adjustable cowl is movable between a retracted position and an extended position along the axial direction, and
wherein the adjustable cowl is immediately adjacent the aft end of the fixed shroud in the retracted position and is spaced apart along the axial direction to define a radial bypass passage between the aft end of the fixed shroud and the forward end of the adjustable cowl when the adjustable cowl is in the extended position.

2. The variable area exhaust nozzle of claim 1 , the variable area exhaust nozzle further comprising:
a controller operably coupled to the nozzle adjustment assembly, the controller being configured to:
receive data indicative of an operating speed of the gas turbine engine;
determine a target area ratio based at least in part on received data indicative of the operating speed of the gas turbine engine; and
operate the nozzle adjustment assembly to selectively adjust at least one of the adjustable cowl or the adjustable plug such that the actual area ratio is substantially equivalent to the target area ratio.

3. The variable area exhaust nozzle of claim 2 , wherein the target area ratio is between about 1 and about 1.3.

4. The variable area exhaust nozzle of claim 2 , wherein the target area ratio is between about 1 and about 1.3, and wherein the adjustable cowl defines a cowl stroke length between about 20 centimeters and about 30 centimeters.

5. The variable area exhaust nozzle of claim 4 , wherein the adjustable plug defines a plug stroke length between about 60 centimeters and about 90 centimeters.

6. The variable area exhaust nozzle of claim 1 , wherein the adjustable plug is movable between a retracted position and an extended position along the axial direction.

7. The variable area exhaust nozzle of claim 1 , wherein the adjustable cowl defines a cowl stroke length between about 20 centimeters and about 30 centimeters.

8. The variable area exhaust nozzle of claim 1 , wherein the adjustable plug comprises:
a shaft slidably coupled to the gas turbine engine and defining an aft end; and
a profiled tail cone defined at the aft end of the shaft.

9. The variable area exhaust nozzle of claim 8 , wherein the nozzle adjustment assembly comprises:
a cowl adjustment mechanism mechanically coupling the adjustable cowl to the fixed shroud for selectively moving the adjustable cowl relative to the fixed shroud; and
a plug adjustment mechanism slidably coupling the adjustable plug to the gas turbine engine for selectively moving the adjustable plug relative to the fixed shroud.

10. The variable area exhaust nozzle of claim 9 , wherein the shroud assembly comprises:
one or more support structures, wherein the one or more support structures are positioned proximate an aft end of the shroud assembly.

11. The variable area exhaust nozzle of claim 10 , wherein the one or more support structures further comprise:
a first support member; and
a second support member, wherein each of the first support member and the second support member are mechanically coupled to the adjustable cowl.

12. The variable area exhaust nozzle of claim 11 , wherein the cowl adjustment mechanism further comprises:
a first track extending along the axial direction of the first support member;
a second track extending along the axial direction of the second support member; and
at least one cowl adjusting actuator mechanically coupled to the first track, the second track, or both.

13. The variable area exhaust nozzle of claim 9 , wherein the plug adjustment mechanism further comprises:
a lever arm attached to the shaft of the adjustable plug; and
at least one plug adjusting actuator mechanically coupled to the lever arm.

14. The variable area exhaust nozzle of claim 13 , wherein the at least one plug adjusting actuator is a hydraulic actuator or an electric actuator.

15. The variable area exhaust nozzle of claim 1 , wherein the adjustable plug defines a plug stroke length between about 60 centimeters and about 90 centimeters.

16. A method of operating a variable exhaust nozzle for a gas turbine engine defining an axial direction, the variable exhaust nozzle including a shroud assembly comprising a fixed shroud and an adjustable cowl mechanically coupled to the fixed shroud and being movable along the axial direction, an adjustable plug slidably positioned within the fixed shroud and being movable along the axial direction, and a nozzle adjustment assembly for selectively positioning at least one of the adjustable cowl or the adjustable plug, wherein the variable exhaust nozzle defines an actual area ratio equivalent to a nozzle exit area over a nozzle throat area, wherein the adjustable cowl is immediately adjacent an aft end of the fixed shroud in a retracted position and spaced apart along the axial direction to define a radial bypass passage between the aft end of the fixed shroud and a forward end of the adjustable cowl when the adjustable cowl is in an extended position, the method comprising:
receiving data indicative of an operating speed of the gas turbine engine;
determining a target area ratio based at least in part on received data indicative of the operating speed of the gas turbine engine; and
operating the nozzle adjustment assembly to selectively adjust the adjustable cowl such that the actual area ratio is substantially equivalent to the target area ratio,
wherein operating the nozzle adjustment assembly to selectively adjust the adjustable cowl comprises spacing apart the adjustable cowl from the fixed shroud along the axial direction to define the radial bypass passage.

17. The method of claim 16 , wherein the target area ratio is between about 1 to 1.3.

18. The method of claim 16 , wherein operating the nozzle adjustment assembly further comprises:
operating a cowl adjustment mechanism.

19. The method of claim 18 , wherein operating at least one of the cowl adjustment mechanism comprises:
positioning the adjustable cowl in a retracted position, the extended position, or a position between the retracted position and the extended position.

20. The method of claim 18 , wherein operating the nozzle adjustment assembly further comprises operating a plug adjustment mechanism by positioning the adjustable plug in a retracted position, an extended position, or a position between the retracted position and the extended position.

Assignees

• Gen Electric

Inventors

• Dindar Mustafa
• Renggli Bernard James
• Hank Andrew J
• Dwyer Daniel Robert
• Spruill Jeffrey S

Classifications

• F02K1/09 Primary

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

• B64D33/04

  of exhaust outlets or jet pipes · CPC title

• F02K1/08 Primary

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

• F02K1/18

  automatic · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title