System and method for reducing idle thrust in a translating cowl thrust reverser

• US 10,344,709 B2
• Filed: 09/10/2015
• Issued: 07/09/2019
• Est. Priority Date: 09/10/2015
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Smith, Danis Burton, Alstad, Shawn, Romano, Robert, Knowles, Mark, Robinson, David
• Primary Examiner(s): Meade, Lorne E
• Application Number:
  US14/850,348
• Publication Number:
  US 20170074211A1
• Time in Patent Office: 1,398 Days
• CPC Class Codes: F02K 1/09 by axially moving an external member, e.g. a shroud F02K1/12 takes precedence
• CPC Class Codes: F02K 1/60 by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
• CPC Class Codes: F02K 1/605 the aft end of the engine cowling being movable to uncover openings for the reversed flow
• CPC Class Codes: F02K 1/70 using thrust reverser flaps or doors mounted on the fan housing
• 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: F02K 1/766 with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
• CPC Class Codes: F05D 2260/50 Kinematic linkage, i.e. transmission of position
• CPC Class Codes: F05D 2260/52 involving springs
• CPC Class Codes: F05D 2260/56 using cams or eccentrics

Abstract

A system and method for reducing idle thrust in a translating cowl reverser system is provided. The provided system and method provide a partial deployment, or thrust reverser system intermediate position for a translating cowl thrust reverser system.

Claims

1. A thrust reverser system for a turbofan engine, comprising:

a stationary structure configured to be mounted to the turbofan engine;

a transcowl mounted on the stationary structure and comprising a front edge, the transcowl configured for movement between a first position, in which the front edge abuts the stationary structure, and a second position, in which the transcowl is translated aft, thereby creating an aperture having a total deployment distance between the front edge and the stationary structure; and

wherein the stationary structure has a support beam extending aft therefrom, the support beam having a pair of pivot joints providing a respective pair of pivot axes located aft of the total deployment distance from the stationary structure;

a first displaceable blocker door and a second displaceable blocker door, the first and second displaceable blocker doors located aft of the total deployment distance aft of the stationary structure, the first and second displaceable blocker doors pivotally mounted to the support beam at respective one of the pair of pivot joints, the support beam and the first and second displaceable blocker doors being at least partially surrounded by the transcowl, the first and second displaceable blocker doors rotatable about a respective one of the pair of pivot axes and configured for pivoting between a stowed position and an aft-ward converging deployed position, the aft-ward converging deployed position defined as a trailing edge of the first displaceable blocker door and a trailing edge of the second displaceable blocker door closing together on an engine centerline to thereby direct turbofan engine airflow to discharge through the aperture to thereby generate reverse thrust;

an actuation system coupled to the transcowl and the first and second displaceable blocker doors, the actuation system configured to coordinate transcowl movement with pivoting of the first and second displaceable blocker doors, thereby creating

(i) a forward position, in which the transcowl is in the first position and the first and second displaceable blocker doors are in the stowed position,

(ii) a reverse position, in which (a) the transcowl is in the second position and (b) the first and second displaceable blocker doors are in the aft-ward converging deployed position, and

(iii) an intermediate position, in which (a) the transcowl is translated aft a predetermined distance that is less than the total deployment distance thereby creating a reduced aperture through which a portion of engine airflow discharges, and (b) the first and second displaceable blocker doors remain in the stowed position and aft of the total deployment distance aft of the stationary structure.

2. The thrust reverser system of claim 1, wherein the actuation system is configured to

(i) move the transcowl aft the predetermined distance without causing the first and second displaceable blocker doors to pivot away from the stowed position, and

(ii) synchronize pivoting of the first and second displaceable blocker doors with the transcowl movement such that the first and second displaceable blocker doors pivot between the stowed position and the aft-ward converging deployed position as the transcowl movement is between the intermediate position and the second position, respectively.

3. The thrust reverser system of claim 2, wherein the actuation system comprises:

a pair of linkage rods, each one of the pair of linkage rods comprising;

a first end and a second end, wherein the first end or the second end has a slot therethrough;

a first fastener; and

a second fastener; and

wherein a respective one of the pair of linkage rods is coupled on the first end to one of the first displaceable blocker door and the second displaceable blocker door by the first fastener and wherein the pair of linkage rods are coupled on their respective second end to the transcowl by the second fastener at a location that is aft of the total deployment distance aft of the stationary structure, and wherein one of the first fastener or second fastener is configured to travel within the slot of each one of the pair of linkage rods.

4. The thrust reverser system of claim 3, wherein the slot of each one of the pair of linkage rods is configured to permit transcowl movement between the first position and the intermediate position without pivoting the first and second displaceable blocker doors between the stowed position and the aft-ward converging deployed position.

5. The thrust reverser of claim 4, wherein:

the first and second displaceable blocker doors are among a plurality of displaceable blocker doors, the support beam is one of multiple support beams extending aft from the stationary structure, and each of the plurality of displaceable blocker doors is pivotally mounted aft of the total deployment distance aft of the stationary structure to one or more support beams and each are at least partially surrounded by the transcowl;

each one of the plurality of displaceable blocker doors is rotatable about a respective pivot axis and configured to be pivoted between a stowed position and an aft-ward converging deployed position when the transcowl moves between the first position and the second position, respectively; and

each one of the plurality of displaceable blocker doors is configured, when in the aft-ward converging deployed position, to redirect turbofan engine airflow through the aperture to thereby generate reverse thrust.

6. The thrust reverser system of claim 2, wherein the actuation system comprises:

a first compression spring coupled on a first end to the first displaceable blocker door and coupled on a second end to the transcowl; and

a second compression spring coupled on a first end to the second displaceable blocker door and coupled on a second end to the transcowl.

7. The thrust reverser system of claim 2, wherein the actuation system comprises:

a first rod comprising a first end and a second end, the first rod first end coupled to the transcowl;

a first lever arm having a first end and a second end, the first lever arm first end coupled to the second end of the first rod and the first lever arm second end coupled to the first displaceable blocker door;

a second rod comprising a first end and a second end, the second rod first end coupled to the transcowl; and

a second lever arm having a first end and a second end, the second lever arm first end coupled to the second end of the second rod and the second lever arm second end coupled to the second displaceable blocker door.

8. The thrust reverser system of claim 1, wherein the transcowl further comprises an inner surface having a contour formed therein to provide clearance for the first and second displaceable blocker doors as they pivot between the stowed position and the aft-ward converging deployed position.

9. The thrust reverser system of claim 1, wherein the predetermined distance is about 25% of the total deployment distance.

10. A method for producing a thrust reverser system for a turbofan engine, comprising:

mounting a stationary structure to the turbofan engine, the stationary structure having a support beam extending aft of the stationary structure, the support beam having a pair of pivot joints providing a respective pair of pivot axes;

mounting a transcowl on the stationary structure, the transcowl configured for movement between a first position, in which a front edge of the transcowl abuts the stationary structure, and a second position, in which the transcowl is translated aft a total deployment distance between the front edge and the stationary structure, thereby creating an aperture;

pivotally mounting a first displaceable blocker door and a second displaceable blocker door to a respective one of the pair of pivot joints on the support beam, wherein the first displaceable blocker door and the second displaceable blocker door are located aft of the total deployment distance aft of the stationary structure and rotatable about their respective pivot axes to pivot between a stowed position and an aft-ward converging deployed position, the aft-ward converging deployed position defined as a trailing edge of the first displaceable blocker door and a trailing edge of the second displaceable blocker door closing together on an engine centerline to thereby direct turbofan engine airflow to discharge through the aperture to thereby generate reverse thrust;

coupling an actuation system to the transcowl and to the first displaceable blocker door and the second displaceable blocker door;

coordinating, by the actuation system, transcowl movement with pivoting of the first and second displaceable blocker doors, thereby creating

(i) a forward position, in which the transcowl is abutted with the stationary structure and the first and second displaceable blocker doors are in the stowed position,

(ii) a reverse position, in which (a) the transcowl is translated aft the total deployment distance from the stationary structure, creating the aperture, and (b) the first and second displaceable blocker doors are in the aft-ward converging deployed position,

(iii) an intermediate position, in which (a) the transcowl is translated aft from the stationary structure by a predetermined distance that is less than the total deployment distance, thereby creating a reduced aperture through which a portion of engine airflow discharges, and (b) the first and second displaceable blocker doors remain in the stowed position and aft of the total deployment distance aft of the stationary structure.

11. The method of claim 10, further comprising:

moving the transcowl the predetermined distance without causing the first and second displaceable blocker doors to pivot away from the stowed position; and

using the actuation system to synchronize pivoting of the first and second displaceable blocker doors with the transcowl movement such that the first and second displaceable blocker doors pivot between the stowed position and the aft-ward converging deployed position as the transcowl moves between the intermediate position and the reverse position, respectively.