Variable tandem fan outlet guide vanes

Patent metadata

Field	Value
Publication number	US-11788429-B2
Application number	US-202117412226-A
Country	US
Kind code	B2
Filing date	Aug 25, 2021
Priority date	Aug 25, 2021
Publication date	Oct 17, 2023
Grant date	Oct 17, 2023

Abstract

A fan assembly includes a fan duct, an inlet fan, and an outlet guide vane assembly. The inlet fan includes blades adapted to force fan exit air toward an aft end of the fan duct. The outlet guide vane assembly is located in the fan duct downstream of the inlet fan and is configured to adjust a direction of the fan exit air received from the blades. The outlet guide vane assembly includes a first plurality of vanes configured to rotate to redirect the fan exit air in a first direction, and a second plurality of vanes located downstream of the first plurality of vanes. The second plurality of vanes are configured to rotate to redirect the fan exit air flowing in the first direction in a second direction to minimize losses created by distortions in fan inlet air and created by the first vanes.

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 radially inner side of the fan duct defined by a radially inner annular wall that surrounds an engine core of the gas turbine engine,
an inlet 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 axially forwardmost end of the radially inner annular wall that is axially aft of the inlet fan such that the fan exit air is split into a first portion of the fan exit air that flows radially inwardly of the radially inner annular wall and into the engine core and a second portion of the fan exit air flows into the fan duct and toward an aft end of the fan duct,
an outlet guide vane assembly located in the fan duct axially downstream of the inlet fan and axially downstream of the axially forwardmost end of the radially inner annular wall, the outlet guide vane assembly configured to adjust a direction of the second portion of the fan exit air received from the plurality of fan blades, the outlet guide vane assembly including
a first plurality of variable-pitch outlet guide vanes including a first variable-pitch outlet guide vane that extends radially outward relative to the central axis, the first variable-pitch outlet guide vane being configured to rotate about a first pitch axis to a first vane-pitch angle in response to the gas turbine engine operating at a given operating condition so as to redirect the second portion of the fan exit air in a first direction, and
a second plurality of variable-pitch outlet guide vanes located axially downstream of the first plurality of variable-pitch outlet guide vanes and including a second variable-pitch outlet guide vane that extends radially outward relative to the central axis, the second variable-pitch outlet guide vane being configured to rotate about a second pitch axis to a second vane-pitch angle in order to redirect the second portion of the fan exit air flowing in the first direction in a second direction to minimize losses created by distortions in fan inlet air and created by the first variable-pitch outlet guide vane redirecting the second portion of the fan exit air in the first direction,

a first connector arm that extends circumferentially about the central axis and that is coupled to each first variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes so as to gang the first plurality of variable-pitch outlet guide vanes together,
a second connector arm that extends circumferentially about the central axis and that is coupled to each second variable-pitch outlet guide vane of the second plurality of variable-pitch outlet guide vanes so as to gang the second plurality of variable-pitch outlet guide vanes together,
a plurality of first actuator arms, each first actuator arm being operably coupled to a respective first variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes and to the first connector arm, wherein circumferential movement of the first connector arm causes rotation of each first variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes via the plurality of first actuator arms, and
a plurality of second actuator arms, each second actuator arm being operably coupled to a respective second variable-pitch outlet guide vane of the second plurality of variable-pitch outlet guide vanes and to the second connector arm, wherein circumferential movement of the second connector arm causes rotation of each second variable-pitch outlet guide vane of the second plurality of variable-pitch outlet guide vanes via the plurality of second actuator arms,
wherein no additional vanes or blades are positioned axially between the first plurality of variable-pitch outlet guide vanes and the second plurality of variable-pitch outlet guide vanes such that the first plurality of variable-pitch outlet guide vanes and the second plurality of variable-pitch outlet guide vanes are located axially proximal to each other, and
wherein each first actuator arm of the plurality of first actuator arms extends from the respective first variable-pitch outlet guide vane to the first connector arm axially aft and beyond leading edges of the second plurality of variable-pitch outlet guide vanes.

2. The fan assembly of claim 1 , further comprising:
a control system configured to rotate the first plurality of variable-pitch outlet guide vanes and to rotate the second plurality of variable-pitch outlet guide vanes,
wherein the control system is configured to rotate the first plurality of variable-pitch outlet guide vanes and the second plurality of variable-pitch outlet guide vanes such that the first direction is different than the second direction.

3. The fan assembly of claim 2 , wherein the second direction is parallel with the central axis such that the second portion of the fan exit air exiting the second plurality of variable-pitch outlet guide vanes returns to an axial flow after passing over the outlet guide vane assembly.

4. The fan assembly of claim 3 , wherein the control system is configured to rotate each first variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes in unison and is further configured to rotate each second variable-pitch outlet guide vane of the second plurality of variable-pitch outlet guide vanes in unison.

5. The fan assembly of claim 4 , wherein the first plurality of variable-pitch outlet guide vanes are each mechanically connected to each other and the second plurality of variable-pitch outlet guide vanes are each mechanically connected to each other.

6. The fan assembly of claim 5 , wherein the first plurality of variable-pitch outlet guide vanes are ganged with each other and the second plurality of variable-pitch outlet guide vanes are ganged with each other.

7. The fan assembly of claim 1 , further comprising:
at least one first actuator operably coupled to the first connector arm, the at least one first actuator being configured to rotate at least one first variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes so as to rotate every other first variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes via the first connector army wherein the at least one first actuator is aligned with the first pitch axis; and
at least one second actuator operably coupled to the second connector arm, the at least one second actuator being configured to rotate at least one second variable-pitch outlet guide vane of the second plurality of variable-pitch outlet guide vanes so as to rotate every other second variable-pitch outlet guide vane of the second plurality of variable-pitch outlet guide vanes via the second connector arm, wherein the at least one second actuator is aligned with the second pitch axis.

8. The fan assembly of claim 1 , wherein the control system includes at least one sensor including at least one of a dynamic sensor, a static wall pressure sensor, an altitude sensor, an angle of attack of the plurality of fan blades sensor, an airspeed sensor, and a sensor configured to measure a rotational speed of the fan blades.

9. The fan assembly of claim 1 , wherein the control system includes at least one sensor located within the fan duct proximate to the plurality of fan blades, the at least one sensor including at least one of a dynamic sensor, a static wall pressure sensor, and a sensor configured to measure a rotational speed of the fan blades.

10. The fan assembly of

Assignees

• Rolls Royce Corp

Inventors

• Hall Christopher D
• Bryan William B
• Molnar Jr Daniel E

Classifications

• 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

• F01D17/02

  Arrangement of sensing elements · CPC title

• F01D17/06

  responsive to speed · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F05D2240/12

  Fluid guiding means, e.g. vanes · CPC title