Segmented variable fan outlet guide vane with unique actuation mechanisms

Patent metadata

Field	Value
Publication number	US-12428974-B2
Application number	US-202418600596-A
Country	US
Kind code	B2
Filing date	Mar 8, 2024
Priority date	Mar 17, 2023
Publication date	Sep 30, 2025
Grant date	Sep 30, 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 two unique actuation assemblies each configured to rotate one of the tip and hub segments.

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 and reduce incidence between the outlet guide vane assembly and the fan exit air, 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 defining a trailing edge of the first variable leading edge outlet guide vane, 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,
a first actuation assembly arranged radially outward of the leading edge portion and including a first actuation head coupled to the first tip segment and a first actuation arm coupled to the first actuation head, wherein rotation of the first actuation arm causes rotation of the first actuation head which causes rotation of the first tip segment so as to selectively rotate the first tip segment about the leading edge pitch axis to a first pitch angle relative to the incoming fan exit air, and
a second actuation assembly arranged radially inward of the leading edge portion and including a second actuation head coupled to the first hub segment and a second actuation arm coupled to the second actuation head, wherein rotation of the second actuation arm causes rotation of the second actuation head which causes rotation of the first hub segment so as to selectively rotate the first hub segment independent of the first tip segment about the leading edge pitch axis to a second pitch 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 to the first pitch angle and the second actuation assembly is configured to rotate the first hub segment to the second pitch angle which is different than the first pitch angle.

3. The fan assembly of claim 2 , wherein the first hub segment includes a hinge rod extending radially outwardly from a radially outer side of the first hub segment and the first tip segment includes a hinge rod receiving cavity configured to securely receive the hinge rod.

4. The fan assembly of claim 3 , wherein the hinge rod of the first hub segment and the hinge rod receiving cavity of the first tip segment are each cylindrical and aligned with the leading edge pitch axis.

5. The fan assembly of claim 1 , wherein the first actuation head is coupled to a radially outer side of the first tip segment and is aligned with the leading edge pitch axis such that rotation of the first actuation head rotates the first tip segment about the leading edge pitch axis, and wherein the second actuation head is coupled to a radially inner side of the first hub segment and is aligned with the leading edge pitch axis such that rotation of the second actuation head rotates the first hub segment about the leading edge pitch axis.

6. The fan assembly of claim 5 , wherein the first actuation arm is fixedly coupled to the first actuation head at a first end of the first actuation arm and extends axially away from the first actuation head, wherein a second end of the first actuation arm opposite the first end is configured to be moved generally circumferentially relative to the first actuation head such that the first actuation arm is configured to be pivoted about the leading edge pitch axis along with the first actuation head, and wherein the second actuation arm is fixedly coupled to the second actuation head at a first end of the second actuation arm and extends axially away from the second actuation head, wherein a second end of the second actuation arm opposite the first end is configured to be moved generally circumferentially relative to the second actuation head such that the second actuation arm is configured to be pivoted about the leading edge pitch axis along with the second actuation head.

7. The fan assembly of claim 6 , wherein the outlet guide vane assembly further includes:
a first annular ring extending circumferentially about the central axis, and
a second annular ring arranged radially inward of the first annular ring and extending circumferentially about the central axis,
wherein the second end of the first actuation arm is connected to the first annular ring,
wherein the second end of the second actuation arm is connected to the second annular ring, and
wherein circumferential movement of the first and second annular rings causes movement of the first and second actuation arms generally circumferentially relative to the first and second actuation heads, respectively.

8. The fan assembly of claim 7 , wherein the outlet guide vane assembly further includes a plurality of variable leading edge outlet guide vanes that include the first variable leading edge outlet guide vane, each variable leading edge outlet guide vane of the plurality of variable leading edge outlet guide vanes including a respective tip segment and hub segment, and wherein the tip and hub segment of each variable leading edge outlet guide vane of the plurality of variable leading edge outlet guide vanes is connected to the first and second annular rings via a respective actuation arm, respectively, such that movement of the first and second annular rings causes movement of the respective actuation arms generally circumferentially which causes the respective actuation arms to pivot about rotation axes of the respective actuation heads such that the tip and hub segments of each variable leading edge outlet guide vane of the plurality of variable leading edge outlet guide vanes are rotated about respective leading edge axes.

9. The fan assembly of claim 6 , wherein the outlet guide vane assembly further includes:
a first annular ring segment extending partially circumferentially about the central axis, and
a second annular ring segment arranged radially inward of the first annular ring segment and extending partially circumferentially about the central axis,
wherein the second end of the first actuation arm is connected to the first annular ring segment,
wherein the second end of the second actuation arm is connected to the second annular ring segment, and
wherein circumferential movement of the first and second annular ring segments causes movement of the first and second actuation arms generally circumferentially relative to the first and second actuation heads, respectively.

10. The fan assembly of claim 9 , wherein the outlet guide vane assembly further includes:
a third annular ring segment radially aligned with the first annular ring segment, extending partially circumferentially about the central axis, and circumferentially offset from the first annular ring segment, and
a fourth annular ring segment radially aligned with the second annular ring segment, arranged radially inward of the first and second annular ring segments, extending partially circumferentially about the central axis, and circumferentially offset from the second annular ring segment,
wherein the outlet guide vane assembly further includes a plura

Assignees

• Rolls Royce Nam Tech Inc

Inventors

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

Classifications

• F05D2220/36

  specially adapted for the fan of turbofan engines · CPC title

• F05D2240/121

  related to the leading edge of a stator vane · CPC title

• F01D17/162 Primary

  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