Engine having variable pitch outlet guide vanes

Patent metadata

Field	Value
Publication number	US-11585354-B2
Application number	US-202217840685-A
Country	US
Kind code	B2
Filing date	Jun 15, 2022
Priority date	Oct 7, 2015
Publication date	Feb 21, 2023
Grant date	Feb 21, 2023

Abstract

An un-ducted turbofan engine defining a radial direction and an axial direction that includes a core engine, a fan, a plurality of variable outlet guide vanes, and a pitch change mechanism. Each of the plurality of variable outlet guide vanes are attached in a rotatable manner to the core engine of the un-ducted turbofan engine. The pitch change mechanism is positioned radially between the engine air flowpath and the plurality of variable outlet guide vanes and coupled to at least one variable outlet guide vane of the plurality of variable outlet guide vanes for changing a pitch of the at least one variable outlet guide vane.

First claim

What is claimed is:

1. An un-ducted turbofan engine defining a radial direction and an axial direction, the un-ducted turbofan engine comprising:
a core engine defining an engine air flowpath, the core engine having an outer casing defining an inlet to the engine air flowpath that is annular about the axial direction;
a fan located upstream of the inlet, the fan comprising a plurality of un-ducted fan blades;
a plurality of variable outlet guide vanes for directing air from the plurality of un-ducted fan blades, each variable outlet guide vane of the plurality of variable outlet guide vanes defining an inner end along the radial direction and an outer end along the radial direction, each variable outlet guide vane of the plurality of variable outlet guide vanes attached at the inner end to the core engine, at least one variable outlet guide vane of the plurality of variable outlet guide vanes attached in a rotatable manner to the core engine of the un-ducted turbofan engine; and
a pitch change mechanism positioned radially between the engine air flowpath and the plurality of variable outlet guide vanes and coupled to the at least one variable outlet guide vane of the plurality of variable outlet guide vanes for changing a pitch of the at least one variable outlet guide vane.

2. The un-ducted turbofan engine of claim 1 , wherein each variable outlet guide vane of the plurality of variable outlet guide vanes is positioned aft of the plurality of un-ducted fan blades of the fan.

3. The un-ducted turbofan engine of claim 1 , wherein the core engine defining the engine air flowpath comprises a compressor section, a combustion section, and a turbine section, wherein the engine air flowpath extends through the compressor section, the combustion section, and the turbine section.

4. The un-ducted turbofan engine of claim 1 , wherein the engine air flowpath comprises an inlet, wherein the inlet is positioned axially between the fan and the plurality of variable outlet guide vanes.

5. The un-ducted turbofan engine of claim 1 , wherein the pitch change mechanism is coupled to each variable outlet guide vane of the plurality of variable outlet guide vanes.

6. The un-ducted turbofan engine of claim 1 , wherein the pitch change mechanism comprises a rack and pinion gear system.

7. The un-ducted turbofan engine of claim 1 , wherein each variable outlet guide vane of the plurality of variable outlet guide vanes is attached to the core engine of the un-ducted turbofan engine using an attachment device.

8. The un-ducted turbofan engine of claim 7 , wherein the attachment device comprises:
an inner race attached to a base of at least one of the variable outlet guide vane of the plurality of variable outlet guide vanes; and
an outer race attached to a frame member of the un-ducted turbofan engine, and
a bearing member positioned between the inner race and the outer race.

9. The un-ducted turbofan engine of claim 1 , wherein each variable outlet guide vane of the plurality of variable outlet guide vanes is attached to the core engine of the un-ducted turbofan engine using a corresponding plurality of attachment devices.

10. The un-ducted turbofan engine of claim 1 , wherein the pitch change mechanism is coupled to each of the variable outlet guide vanes of the plurality of variable outlet guide vanes for changing the pitch of each of the variable outlet guide vanes of the plurality of variable outlet guide vanes in unison.

11. The un-ducted turbofan engine of claim 10 , wherein the pitch change mechanism comprises a ring gear that is coupled to each of the variable outlet guide vanes of the plurality of variable outlet guide vanes, wherein the pitch change mechanism is configured to move the ring gear about a circumferential direction of the un-ducted turbofan engine, wherein moving the ring gear about the circumferential direction changes the pitch of each of the variable outlet guide vanes of the plurality of variable outlet guide vanes in unison.

12. The un-ducted turbofan engine of claim 11 , wherein the pitch change mechanism comprises a pinion gear that meshes with the ring gear, wherein the pinion gear of the pitch change mechanism is configured to move the ring gear about the circumferential direction of the un-ducted turbofan engine.

13. The un-ducted turbofan engine of claim 1 , wherein the pitch change mechanism is coupled to each of the variable outlet guide vanes of the plurality of variable outlet guide vanes for changing the pitch of one or more of the variable outlet guide vanes of the plurality of variable outlet guide vanes relative to the remaining variable outlet guide vanes of the plurality of variable outlet guide vanes.

14. The un-ducted turbofan engine of claim 13 , wherein the pitch change mechanism is configured as a swash plate.

15. The un-ducted turbofan engine of claim 1 , wherein each variable outlet guide vane of the plurality of variable outlet guide vanes is positioned aft of the plurality of un-ducted fan blades of the fan, wherein the core engine defining the engine air flowpath comprises a compressor section, a combustion section, and a turbine section, wherein the engine air flowpath extends through the compressor section, the combustion section, and the turbine section, and wherein the engine air flowpath comprises an inlet, wherein the inlet is positioned axially between the fan and the plurality of variable outlet guide vanes.

16. The un-ducted turbofan engine of claim 15 , wherein the pitch change mechanism is coupled to each of the variable outlet guide vanes of the plurality of variable outlet guide vanes for changing the pitch of each of the variable outlet guide vanes of the plurality of variable outlet guide vanes in unison.

17. The un-ducted turbofan engine of claim 16 , wherein the pitch change mechanism comprises a ring gear that is coupled to each of the variable outlet guide vanes of the plurality of variable outlet guide vanes, wherein the pitch change mechanism is configured to move the ring gear about a circumferential direction of the un-ducted turbofan engine, wherein moving the ring gear about the circumferential direction changes the pitch of each of the variable outlet guide vanes of the plurality of variable outlet guide vanes in unison.

18. The un-ducted turbofan engine of claim 17 , wherein the pitch change mechanism comprises a pinion gear that meshes with the ring gear, wherein the pinion gear of the pitch change mechanism is configured to move the ring gear about the circumferential direction of the un-ducted turbofan engine.

19. The un-ducted turbofan engine of claim 15 , wherein the pitch change mechanism is coupled to each of the variable outlet guide vanes of the plurality of variable outlet guide vanes for changing the pitch of one or more of the variable outlet guide vanes of the plurality of variable outlet guide vanes relative to the remaining variable outlet guide vanes of the plurality of variable outlet guide vanes.

20. The un-ducted turbofan engine of claim 19 , wherein the pitch change mechanism is configured as a swash plate.

Assignees

• Gen Electric

Inventors

• Miller Brandon Wayne
• Becker Jr Thomas Lee

Classifications

• F04D29/522

  especially adapted for elastic fluid pumps · CPC title

• F04D29/563 Primary

  specially adapted for elastic fluid pumps · CPC title

• F02C9/54

  by throttling the working fluid, by adjusting vanes · CPC title

• B64C11/06

  for variable-pitch blades · CPC title

• B64C11/00

  Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft · CPC title