Asymmetric load compensation system

Patent metadata

Field	Value
Publication number	US-11098677-B2
Application number	US-201815906234-A
Country	US
Kind code	B2
Filing date	Feb 27, 2018
Priority date	Apr 15, 2015
Publication date	Aug 24, 2021
Grant date	Aug 24, 2021

Abstract

This disclosure relates to a variable area nozzle of a gas turbine engine. The variable area nozzle includes, among other things, a control unit, a translatable structure, and a plurality of actuators configured to adjust the position of the translatable structure. The plurality of actuators are fluidly coupled to a common fluid source. The control unit is configured to provide instructions to at least one of the actuators to compensate for an asymmetric load from the translatable structure.

First claim

The invention claimed is:

1. A variable area nozzle for a gas turbine engine, comprising:
a control unit, wherein the control unit is a controller including memory, hardware, and software;
a translatable structure;
a plurality of actuators configured to adjust the position of the translatable structure, wherein the plurality of actuators each include a chamber and a piston moveable within the chamber, wherein each of the pistons includes a head and a shaft, wherein the plurality of actuators are fluidly coupled to a common fluid source, wherein each of the pistons is configured such that fluid is permitted to flow through the piston between a first side of the chamber and a second side of the chamber, wherein the first and second sides of the chamber are on opposite sides of the head of the respective piston; and
at least one position sensor configured to generate a signal indicative of the movement of the translatable structure, wherein the control unit is configured to use information from the at least one position sensor to identify an asymmetric load from the translatable structure, wherein the at least one position sensor is mounted to the shaft of one of the plurality of actuators,
wherein each of the pistons is configured such that the head and the shaft circumscribe a plenum,
wherein each of the pistons includes a first passageway fluidly coupling the first side of the respective chamber to the plenum,
wherein each of the pistons includes a second passageway fluidly coupling the second side of the respective chamber to the plenum, and
wherein each of the pistons is configured such that the first passageway and second passageway extend at least partially through the head of the respective piston.

2. The variable area nozzle as recited in claim 1 , further comprising a valve assembly operable to direct relatively high pressure fluid to one of the first and second sides of the chamber of at least one of the actuators to adjust the position of the translatable structure.

3. The variable area nozzle as recited in claim 2 , wherein at least one of the plurality of actuators includes an adjustable flow regulator operable to adjust the relative amount of fluid directed to the at least one actuator when the asymmetric load from the translatable structure is detected.

4. The variable area nozzle as recited in claim 1 , wherein: each of the pistons includes a first orifice within the first passageway, and
each of the pistons includes a second orifice within the second passageway.

5. The variable area nozzle as recited in claim 1 , wherein each piston is configured such that fluid is permitted to flow through the respective piston between the first side of the chamber and the second side of the chamber by flowing through the first passageway, the second passageway, and the plenum.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Stambaugh Craig T

Classifications

• F05D2250/73

  asymmetric · CPC title

• F02K1/763

  with actuating systems or actuating devices; Arrangement of actuators for thrust reversers · CPC title

• F02K1/15 Primary

  Control or regulation · CPC title

• F02K3/10

  by after-burners (F02K3/105 takes precedence) · CPC title

• F05D2270/64

  Hydraulic actuators · CPC title