Thrust reverser actuator damper system

• US 9,494,108 B2
• Filed: 10/16/2014
• Issued: 11/15/2016
• Est. Priority Date: 10/16/2014
• Status: Active Grant

• Current Assignee: ROHR Incorporated (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: ROHR Incorporated (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Gormley, Timothy
• Primary Examiner(s): SUNG, GERALD LUTHER
• Application Number:
  US14/516,217
• Publication Number:
  US 20160108853A1
• Time in Patent Office: 761 Days
• US Class Current: 1/1
• CPC Class Codes: F02K 1/72 the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
• CPC Class Codes: F02K 1/763 with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
• CPC Class Codes: F05D 2260/96 Preventing, counteracting or reducing vibration or noise

Abstract

A nacelle may comprise a thrust reverser. The thrust reverser may comprise a translating sleeve, a cascade array, and a TRAS actuator. The TRAS actuator may pass through an aperture in an aft cascade ring of the cascade array. A retainer may be coupled to the aft cascade ring. A damper may be coupled to the retainer. The damper may circumscribe the TRAS actuator. The damper may be configured to damp vibrations in the TRAS actuator. As an amplitude of vibration or deflection of the TRAS actuator increases, a reaction force applied by the damper on the TRAS actuator increases, which prevents the TRAS actuator from contacting the aft cascade ring.

Claims

1. A thrust reverser assembly comprising:

an aft cascade ring comprising an aperture;

a thrust reverser actuation system (“

TRAS”

) actuator extending through the aperture;

a retainer coupled to the aft cascade ring;

a damper coupled to the retainer, wherein the damper is in contact with the TRAS actuator, wherein the damper is configured to damp vibrations of the TRAS actuator; and

a bumper located between the damper and the retainer.

2. The thrust reverser assembly of claim 1, wherein the bumper comprises a first portion having a first diameter, and a second portion comprising a second diameter, wherein the second diameter is larger than the first diameter.

3. The thrust reverser assembly of claim 2, wherein the damper is coupled to the second portion of the bumper.

4. The thrust reverser assembly of claim 2, wherein the first portion is located within the retainer, and wherein the second portion is located forward of the retainer.

5. The thrust reverser assembly of claim 1, wherein the damper comprises a bulb seal.

6. The thrust reverser assembly of claim 1, wherein the damper is configured to apply a reaction force to the TRAS actuator, such that the reaction force increases as an amplitude of deflection of the TRAS actuator increases.

7. The thrust reverser assembly of claim 1, wherein the damper comprises an elastomer.

8. A thrust reverser assembly for an aircraft comprising:

a cascade comprising an aft cascade ring;

a thrust reverser actuation system (“

TRAS”

) actuator extending through the aft cascade ring;

a flexible damper circumscribing the TRAS actuator, wherein the flexible damper is configured to exert a small reaction force on the TRAS actuator in response to a small deflection of the TRAS actuator, and wherein the flexible damper is configured to exert a large reaction force on the TRAS actuator in response to the flexible damper bottoming out; and

a bumper coupled to the flexible damper, wherein the bumper is configured to prevent the TRAS actuator from contacting the aft cascade ring.

9. The thrust reverser assembly of claim 8, wherein the flexible damper is configured to damp vibrations in the TRAS actuator.

10. The thrust reverser assembly of claim 8, further comprising a retainer coupled to the aft cascade ring, wherein the retainer is coupled to the bumper.

11. The thrust reverser assembly of claim 8, wherein the flexible damper comprises an elastomer.

12. The thrust reverser assembly of claim 8, wherein the bumper comprises a first portion having a first diameter, and a second portion having a second diameter, wherein the second diameter is greater than the first diameter, and wherein the flexible damper is coupled to the second portion.

13. The thrust reverser assembly of claim 8, wherein the flexible damper is configured to exert a reaction force on the TRAS actuator which increases with an amplitude of a deflection of the TRAS actuator.

14. A thrust reverser assembly comprising:

an aft cascade ring comprising an aperture;

a thrust reverser actuation system (“

TRAS”

) actuator extending through the aperture;

a retainer coupled to the aft cascade ring; and

a damper coupled to the retainer, wherein the damper is in contact with the TRAS actuator, wherein the damper is configured to damp vibrations of the TRAS actuator, wherein the damper comprises a bulb seal.