Segmented variable fan outlet guide vane with cam assembly and pass through actuation mechanisms

Patent metadata

Field	Value
Publication number	US-12398648-B2
Application number	US-202418600609-A
Country	US
Kind code	B2
Filing date	Mar 8, 2024
Priority date	Mar 17, 2023
Publication date	Aug 26, 2025
Grant date	Aug 26, 2025

Abstract

A fan assembly for a gas turbine engine includes a fan duct, a fan, and an outlet guide vane assembly located in the fan duct axially downstream of the fan. The outlet guide vane assembly includes a first variable leading edge outlet guide vane that extends radially relative to the central axis and includes a leading edge portion and a fixed aft portion, the leading edge portion including a tip segment configured to rotate about a leading edge pitch axis and a hub segment located radially inward of and separate from the tip segment, the hub segment configured to independently rotate about the leading edge pitch axis relative to the tip segment. The assembly further includes a single actuation assembly includes a cam rod and cams arranged thereon that is configured to rotate the tip and hub segments via the cams.

First claim

What is claimed is:

1. A fan assembly for a gas turbine engine, the fan assembly comprising
a fan duct arranged circumferentially around a central axis,
a fan comprising a plurality of fan blades that extend radially outward relative to the central axis and that are adapted to rotate about the central axis to force fan exit air toward an aft end of the fan duct, and
an outlet guide vane assembly located in the fan duct axially downstream of the fan and configured to adjust a direction of incoming fan exit air received from the plurality of fan blades, the outlet guide vane assembly including
a first variable leading edge outlet guide vane that extends radially relative to the central axis and includes a leading edge portion and a fixed aft portion, the leading edge portion including a first tip segment configured to rotate about a leading edge pitch axis and a first hub segment located radially inward of and separate from the first tip segment, the first hub segment configured to independently rotate about the leading edge pitch axis relative to the first tip segment, and
a first actuation assembly including a first cam rod, a first cam selectively coupled to the first cam rod, and a second cam selectively coupled to the first cam rod and radially spaced apart from the first cam, wherein the first cam rod is configured to be selectively rotated so as to rotate the first cam and the second cam, wherein rotation of the first cam causes rotation of the first tip segment about the leading edge pitch axis, wherein rotation of the second cam causes rotation of the first hub segment about the leading edge pitch axis, and wherein the first and second cams are configured to be selectively clocked to unique rotational positions on the first cam rod such that rotation of the first and second cams causes the first tip segment to be rotated to a first pitch angle relative to the incoming fan exit air and the first hub segment to be rotated to a second angle relative to the incoming fan exit air.

2. The fan assembly of claim 1 , wherein the first actuation assembly is configured to rotate the first tip segment and the first hub segment to the first pitch angle and the second pitch angle which is different than the first pitch angle.

3. The fan assembly of claim 2 , wherein the first actuation assembly further includes a first cam actuation rod rotatably coupled to the first tip segment and extending axially aft therefrom toward the first cam, and a second cam actuation rod rotatably coupled to the first hub segment extending axially aft therefrom toward the second cam.

4. The fan assembly of claim 3 , wherein an axially aft end of the first cam actuation rod engages an axially forward facing surface of the first cam such that rotation of the first cam in a first rotational direction causes the axially forward facing surface to move the first cam actuation rod axially forward, and wherein an axially aft end of the second cam actuation rod engages an axially forward facing surface of the second cam such that rotation of the second cam in the first rotational direction causes the axially forward facing surface to move the second cam actuation rod axially forward.

5. The fan assembly of claim 4 , wherein the first cam actuation rod is rotatably coupled to the first tip segment at a point offset from the leading edge pitch axis in a circumferential direction such that axially forward movement of the first cam actuation rod rotates the first tip segment in the first rotational direction, and wherein the second cam actuation rod is rotatably coupled to the first hub segment at a point offset from the leading edge pitch axis in the circumferential direction such that axially forward movement of the second cam actuation rod rotates the first hub segment in the first rotational direction.

6. The fan assembly of claim 5 , wherein the first tip segment includes a first cam actuation rod receiving recess formed at least partially in an aft side of the first tip segment, wherein the first cam actuation rod is rotatably mounted within the first cam actuation rod receiving recess, wherein the first hub segment includes a second cam actuation rod receiving recess formed at least partially in an aft side of the first hub segment, and wherein the second cam actuation rod is rotatably mounted within the second cam actuation rod receiving recess.

7. The fan assembly of claim 3 , wherein the first actuation assembly is arranged radially outward of the fixed aft portion and includes a first actuation head, and wherein the first cam rod is fixedly coupled to the first actuation head such that rotation of the first actuation head causes rotation of the first cam rod.

8. The fan assembly of claim 7 , wherein the first actuation assembly further includes a first actuation arm coupled to the first actuation head and extending generally axially aft therefrom, wherein pivoting of the first actuation arm about a rotation axis of the first actuation head causes rotation of the first actuation head which causes rotation of the first cam rod.

9. The fan assembly of claim 8 , wherein the fixed aft portion includes a cam rod receiving cavity formed therethrough, and wherein the first actuation head is circumferentially aligned with the fixed aft portion such that the first cam rod extends through the cam rod receiving cavity.

10. The fan assembly of claim 8 , wherein the first actuation head is circumferentially offset from the fixed aft portion such that the first cam rod radially extends circumferentially adjacent to the fixed aft portion.

11. The fan assembly of claim 8 , wherein the outlet guide vane assembly further includes a first annular ring extending circumferentially about the central axis, wherein an axially aft end of the first actuation arm is connected to the first annular ring, and wherein circumferential movement of the first annular ring causes movement of the first actuation arm generally circumferentially relative to the first actuation head which causes the first actuation arm to pivot about the rotation axis of the first actuation head which causes rotation of the first actuation head which causes rotation of the first cam rod.

12. A fan assembly for a gas turbine engine, the fan assembly comprising
a fan duct arranged circumferentially around a central axis,
a fan adapted to rotate about the central axis to force fan exit air toward an aft end of the fan duct, and
an outlet guide vane assembly located in the fan duct axially downstream of the fan and configured to adjust a direction of incoming fan exit air received from the plurality of fan blades, the outlet guide vane assembly including
a first variable leading edge outlet guide vane including a leading edge portion and a fixed aft portion, the leading edge portion including a first tip segment configured to rotate about a leading edge pitch axis, and
a first actuation assembly including a first cam rod extending through the fixed aft portion and a first cam selectively coupled to the first cam rod, wherein the first cam rod is configured to be selectively rotated so as to rotate the first cam, wherein rotation of the first cam causes rotation of the first tip segment about the leading edge pitch axis, and wherein the first cam is configured to be selectively clocked to rotational positions on the first cam rod such that rotation of the first cam causes the first tip segment to be rotated to a first pitch angle relative to the incoming fan exit air.

13. The fan assembly of claim 12 , wherein the leading edge portion further includes a first hub segment located radially inward of and separate from the first tip segment, the first hub segme

Assignees

• Rolls Royce Nam Tech Inc

Inventors

• Heeter Robert W
• Molnar Jr Daniel E
• Hebert Gregory J

Classifications

• F05D2220/36

  specially adapted for the fan of turbofan engines · CPC title

• F01D17/162

  for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F01D7/00 Primary

  Rotors with blades adjustable in operation; Control thereof (for reversing F01D1/30) · CPC title