Controllable variable fan outlet guide vanes

Patent metadata

Field	Value
Publication number	US-11802490-B2
Application number	US-202117412218-A
Country	US
Kind code	B2
Filing date	Aug 25, 2021
Priority date	Aug 25, 2021
Publication date	Oct 31, 2023
Grant date	Oct 31, 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 outlet guide vanes including a first outlet guide vane configured to rotate to a first angle so as to redirect the fan exit air in a first direction and a second outlet guide vane configured to rotate to a second angle so as to redirect the fan exit air in a second direction. The second outlet guide vane is located at a different circumferential position than the first outlet guide vane.

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,
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 aft end of the fan duct, and
an outlet guide vane assembly located in the fan duct axially downstream of the inlet fan and configured to adjust a direction 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 at least one first variable-pitch outlet guide vane and at least one second variable-pitch outlet guide vane that each extend 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 fan exit air in a first direction, the at least one second variable-pitch outlet guide vane being located at a different circumferential position than the first variable-pitch outlet guide vane and being configured to rotate about a second pitch axis to a second vane-pitch angle in response to the gas turbine engine operating at the given operating condition so as to redirect the fan exit air in a second direction,
a second plurality of variable-pitch outlet guide vanes located axially downstream of the first plurality of variable-pitch outlet guide vanes and including at least one third variable-pitch outlet guide vane and at least one fourth variable-pitch outlet guide vane that each extend radially outward relative to the central axis, and
a plurality of first actuator arms, each first actuator arm being operably coupled to a respective first or second variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes, wherein rotation of each first or second variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes is caused by pivoting movement of a respective first actuator arm of the plurality of first actuator arms,

wherein each first actuator arm of the plurality of first actuator arms extends from the respective first or second variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes axially aft and beyond leading edges of the third or fourth variable-pitch outlet guide vanes 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,
wherein the control system is configured to rotate the at least one first variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes to the first vane-pitch angle and to rotate the at least one second variable-pitch outlet guide vane of the second plurality of variable-pitch outlet guide vanes to the second vane-pitch angle.

3. The fan assembly of claim 2 , wherein the first vane-pitch angle is different than the second vane-pitch angle.

4. The fan assembly of claim 3 , wherein the at least one first variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes includes at least two variable-pitch outlet guide vanes that are ganged with each other.

5. The fan assembly of claim 4 , further comprising:
a first connector arm that extends at least partially circumferentially about the central axis and that is coupled to each variable-pitch outlet guide vane of the at least two variable-pitch outlet guide vanes so as to gang the at least two variable-pitch outlet guide vanes together.

6. The fan assembly of claim 5 , wherein the at least one first actuator is operably coupled to the first connector arm, and wherein the at least one first actuator being configured to rotate at least one first variable-pitch outlet guide vane of the at least two variable-pitch outlet guide vanes so as to rotate every other first variable-pitch outlet guide vane of the of the at least two variable-pitch outlet guide vanes via the first connector arm.

7. The fan assembly of claim 3 , wherein the at least one first variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes includes at least two first variable-pitch outlet guide vanes that are each mechanically connected to each other, and the at least one second variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes includes at least two second variable-pitch outlet guide vanes that are each mechanically connected to each other.

8. The fan assembly of claim 7 , wherein the at least two first variable-pitch outlet guide vanes of the at least one first variable-pitch outlet guide vane of the first plurality of variable-pitch outlet guide vanes are ganged with each other, and the at least two second variable-pitch outlet guide vanes of the at least one second variable-pitch outlet guide vane of second plurality of variable-pitch outlet guide vanes are ganged with each other.

9. The fan assembly of claim 8 , wherein the at least two first variable-pitch outlet guide vanes that are ganged with each other include at least five vanes, and wherein the at least two second variable-pitch outlet guide vanes that are ganged with each other include at least five vanes.

10. The fan assembly of claim 8 , wherein the at least two first variable-pitch outlet guide vanes that are ganged with each other are configured to be fully closed while the at least two second variable-pitch outlet guide vanes that are ganged with each other are fully open in order to reduce a tendency for a local stall of the inlet fan.

11. The fan assembly of claim 3 , further comprising:
at least one third variable-pitch outlet guide vane that extends radially outward relative to the central axis, the third variable-pitch outlet guide vane being located at a different circumferential position than the first variable-pitch outlet guide vane and the second variable-pitch outlet guide vane, the third variable-pitch outlet guide vane being configured to rotate about a third pitch axis to a third vane-pitch angle in response to the gas turbine engine operating at the given operating condition so as to redirect the fan exit air in a third direction.

12. The fan assembly of claim 11 , wherein the third vane-pitch angle is different than the first vane-pitch angle and the second vane-pitch angle.

13. The fan assembly of claim 3 ,
wherein the third variable-pitch outlet guide vane is configured to rotate, via the control system, about a third pitch axis to a third vane-pitch angle in response to the gas turbine engine operating at the given operating condition so as to redirect the fan exit air in a third direction, and wherein the fourth variable-pitch outlet guide vane is located at a different circumferential position than the third variable-pitch outlet guide vane and is configured to rotate about a fourth pitch axis to a fourth vane-pitch angle in response to the gas turbine engine operating at the given operating condition so as to redirect the fan exit air in a fourth direction.

14. A fan assembly for a gas turbine engine the fan assembly comprising
a fan duct arranged circumferentially around a central axis,
an inlet fan comprising a plurality of fan blades adapted to force an airflow toward an aft end of the fan duct, and
an outlet guide vane assembly located in the fan duct axially downs

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

• F01D7/02

  having adjustment responsive to speed · CPC title

• F01D17/06

  responsive to speed · CPC title

• F05D2240/12

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

• F05D2250/90

  Variable geometry · CPC title