System for actuating an exhaust cowl

Patent metadata

Field	Value
Publication number	US-10371089-B2
Application number	US-201514600824-A
Country	US
Kind code	B2
Filing date	Jan 20, 2015
Priority date	Jan 20, 2015
Publication date	Aug 6, 2019
Grant date	Aug 6, 2019

Abstract

In various embodiments, a cowl actuation system may comprise a cowl, an actuator, a bell crank, and a guide arm. The cowl may be configured to modulate at least a portion of the exhaust flow of a gas turbine engine. The bell crank may have a first end and a second end. The first end may be operatively coupled to the actuator. The second end may be operatively coupled to the cowl. The bell crank may be configured to pivot about a first point located between the first end and the second end. The first point may also be located along a diameter. The guide arm may have a third end and a fourth end. The third end may be mounted to a second point. The fourth end may be operatively coupled to the cowl. The second point may be located along the diameter.

First claim

What is claimed is:

1. A gas turbine engine comprising:
an exhaust cowl that is adjustable and is configured to direct a main exhaust from a turbine section of the gas turbine engine;
an outer cowl disposed outboard of the exhaust cowl of the gas turbine engine, wherein an annular flow path is defined between the exhaust cowl and the outer cowl, wherein the outer cowl is configured to modulate an annular exhaust flow through the annular flow path;
an actuator;
a bell crank operatively coupled in load transferring communication between the actuator and the outer cowl, the bell crank configured to pivot about a first point, the first point located along a circumference; and
a guide arm coupled to the outer cowl, wherein the guide arm is not directly coupled to the bell crank, the guide arm having a first end and a second end, the first end configured to pivot about a second point, wherein the second point is located along the circumference such that the first point and the second point are axially fixed and commonly aligned along the circumference, wherein the guide arm is not coupled in load transferring communication between the actuator and the outer cowl, wherein movement of the outer cowl is caused by load transfer from the actuator through the bell crank;
wherein the outer cowl is configured to rotate circumferentially and translate axially.

2. The gas turbine engine of claim 1 , wherein the outer cowl is configured to translate from a closed position to an open position.

3. The gas turbine engine of claim 1 , wherein the outer cowl is actuated from a closed position to an open position to control an annular exhaust flow and in response to the actuator pivoting the bell crank from a first position to a second position.

4. The gas turbine engine of claim 1 , wherein the outer cowl defines a first bump and wherein a static structure of the exhaust cowl defines a second bump.

5. The gas turbine engine of claim 4 , wherein where the outer cowl is in the open position the first bump is spaced relative to the second bump to provide a first section of the annular flow path that has a first radial dimension that is substantially uniform with a second radial dimension of a second section of the annular flow path that is upstream of the first section, the first bump, and the second bump.

6. The gas turbine engine of claim 5 , wherein an interior surface of the outer cowl is configured to contact the second bump to seal the flow path.

7. The gas turbine engine of claim 1 , wherein the bell crank and the guide arm are coupled to a common structure.

8. The gas turbine engine of claim 7 , wherein the actuator causes the bell crank to pivot from a first position to a second position which also causes the guide arm to actuate from a third position to a fourth position.

9. The gas turbine engine of claim 8 , wherein the common structure moves axially and rotates circumferentially in response to the bell crank pivoting between the first position and the second position.

10. A gas turbine engine, comprising:
a fan configured to create a fan flow;
a compressor configured to compress gas;
a combustor in fluid communication with the compressor;
a turbine in fluid communication with the combustor, the turbine configured to drive the fan;
an exhaust cowl that is adjustable and is configured to direct a main exhaust from the turbine;
an outer cowl disposed outboard of the exhaust cowl, wherein an annular flow path is defined between the exhaust cowl and the outer cowl, wherein the outer cowl is configured to modulate an annular exhaust flow through the annular flow path; and
a cowl actuation system coupled to the outer cowl and comprising:
an actuator configured to modulate the outer cowl,
a bell crank having a first end and a second end, the first end operatively coupled to the actuator and the second end operatively coupled to the outer cowl such that the bell crank is coupled in load transferring communication between the actuator and the outer cowl, the bell crank configured to pivot about a first point located between the first end and the second end, the first point located along a circumference, and
a guide arm having a third end and a fourth end, the third end mounted to a second point and the fourth end operatively coupled to the outer cowl, wherein the guide arm is not directly coupled to the bell crank, wherein the second point is located along the circumference such that the first point and the second point are axially fixed and commonly aligned along the circumference, wherein the guide arm is not coupled in load transferring communication between the actuator and the outer cowl such that the guide arm pivots in response to movement of the outer cowl, wherein movement of the outer cowl is caused by load transfer from the actuator through the bell crank,
wherein the outer cowl is configured to rotate circumferentially and translate axially.

11. The gas turbine engine of claim 10 , wherein the outer cowl is actuated from a closed position to an open position to actuate the annular exhaust flow and in response to the actuator pivoting the bell crank from a first position to a second position.

12. The gas turbine engine of claim 11 , wherein the outer cowl defines a first bump, wherein a static structure of the exhaust cowl defines a second bump, wherein in response to the outer cowl being in the open position the first bump is spaced relative to the second bump to provide a first section of the annular flow path that has a first radial dimension that is substantially uniform with a second radial dimension of a second section of the annular flow path that is upstream of the first section, the first bump, and the second bump.

13. A cowl actuation system, comprising:
an outer cowl configured to modulate an annular exhaust flow of a gas turbine engine, wherein the outer cowl is disposed outboard of an exhaust cowl of the gas turbine engine, wherein an annular flow path is defined between the exhaust cowl and the outer cowl such that the outer cowl is configured to modulate the annular exhaust flow through the annular flow path, wherein the exhaust cowl is adjustable and is configured to direct a main exhaust from a turbine section of the gas turbine engine;
an actuator;
a bell crank having a first end and a second end, the first end operatively coupled to the actuator and the second end operatively coupled to the outer cowl such that the bell crank is coupled in load transferring communication between the actuator and the outer cowl, the bell crank configured to pivot about a first point located between the first end and the second end, the first point located along a circumference; and
a guide arm having a third end and a fourth end, the third end mounted to a second point and the fourth end operatively coupled to the outer cowl, wherein the guide arm is not directly coupled to the bell crank, wherein the second point is located along the circumference such that the first point and the second point are axial fixed and commonly aligned along the circumference, wherein the guide arm is not coupled in load transferring communication between the actuator and the outer cowl such that the guide arm pivots in response to movement of the outer cowl, wherein movement of the outer cowl is caused by load transfer from the actuator through the bell crank.

14. The cowl actuation system of claim 13 , wherein the outer cowl is actuated from a closed position to an open position to actuate the annular exhaust flow and in response to the actuator pivoting the bell crank from a first position to a second position.

15. The cowl actuatio

Assignees

• United Technologies Corp

Inventors

• Peters Donald W
• Bangerter James P

Classifications

• F02K1/15

  Control or regulation · CPC title

• F02K1/09 Primary

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

• F16H21/04

  Guiding mechanisms, e.g. for straight-line guidance · CPC title

• F02C3/10

  with another turbine driving an output shaft but not driving the compressor · CPC title

• F02K1/10

  by distorting the jet pipe or nozzle · CPC title