Mixed flow exhaust thrust reverser with area control nozzle systems and methods

Patent metadata

Field	Value
Publication number	US-12146453-B2
Application number	US-202318299526-A
Country	US
Kind code	B2
Filing date	Apr 12, 2023
Priority date	Nov 22, 2021
Publication date	Nov 19, 2024
Grant date	Nov 19, 2024

Abstract

An articulating exhaust nozzle thrust reverser includes an outer articulating panel comprising an outer skin and an outer thrust reverser door and an inner articulating panel comprising a forward inner skin, an aft inner skin, and an inner thrust reverser door. The outer articulating panel is configured to pivot to vary a nozzle exit area. The forward inner skin is configured to pivot to vary a nozzle throat area. The outer thrust reverser door is pivotally coupled to the outer skin. The inner thrust reverser door is pivotally coupled to the aft inner skin. The outer articulating panel and the inner articulating panel may be individually operated to independently vary the exhaust nozzle throat area and/or the exhaust nozzle exit area.

First claim

The invention claimed is:

1. A method for articulating an exhaust nozzle to vary at least one of a nozzle throat area and a nozzle exit area, the method comprising:
moving a first nozzle actuator to vary an angle of an outer articulating panel of the exhaust nozzle with respect to a forward bulkhead and to at least one of maintain or vary the nozzle exit area;
moving a second nozzle actuator to vary an angle of an inner articulating panel of the exhaust nozzle with respect to the forward bulkhead;
varying an angle between a forward inner skin of the inner articulating panel and an aft inner skin of the inner articulating panel in response to performing the step of moving the second nozzle actuator to at least one of maintain or vary the nozzle throat area;
moving a first thrust reverser actuator to pivot an outer thrust reverser door between a stowed position and a deployed position, wherein the outer thrust reverser door is pivotally mounted to an outer skin of the outer articulating panel; and
moving a second thrust reverser actuator to pivot an inner thrust reverser door between a stowed position and a deployed position, wherein the inner thrust reverser door is pivotally mounted to the aft inner skin of the inner articulating panel.

2. The method of claim 1 , further comprising:
translating the outer skin with respect to a flap in response to varying the angle of the outer articulating panel of the exhaust nozzle with respect to the forward bulkhead to maintain a substantially continuous aerodynamic outer surface of the exhaust nozzle;
wherein the flap is pivotally coupled to the forward bulkhead; and
the outer skin is slidingly coupled to the flap.

3. The method of claim 1 , further comprising pivoting the outer skin of the outer articulating panel with respect to the forward bulkhead independent of the forward inner skin of the inner articulating panel.

Assignees

• Rohr Inc

Inventors

• Schrell Johann Steven

Classifications

• F05D2260/605

  Venting into the ambient atmosphere or the like · CPC title

• F05D2260/57

  using servos, independent actuators, etc. · CPC title

• F05D2240/128

  Nozzles · CPC title

• F05D2220/323

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

• F02K1/763

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