Systems for controlling variable outlet guide vanes

Patent metadata

Field	Value
Publication number	US-11879343-B2
Application number	US-202117412220-A
Country	US
Kind code	B2
Filing date	Aug 25, 2021
Priority date	Aug 25, 2021
Publication date	Jan 23, 2024
Grant date	Jan 23, 2024

Abstract

A fan assembly includes a fan duct, an inlet fan, an outlet guide vane assembly, and a control system. The inlet fan includes fan blades adapted to rotate about a central axis 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. The outlet guide vane assembly includes a plurality of guide vanes that extend radially relative to the central axis and are configured to rotate to a first vane-pitch angle. The control system is configured to rotate the guide vanes redirect the fan exit air, vary a pressure downstream of the fan inlet, minimize intake flow distortion experienced by the inlet fan, reduce inlet fan vibratory response and/or improve fan operability margins.

First claim

What is claimed is:

1. A fan assembly adapted 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,
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 a first variable-pitch outlet guide vane that extends radially relative to the central axis, the first variable-pitch outlet guide vane being configured to rotate to a first vane-pitch angle, and
a control system configured to rotate the first variable-pitch outlet guide vane about a first vane-pitch axis that extends radially relative to the central axis to redirect the fan exit air,
wherein the control system is configured to rotate the first plurality of variable-pitch outlet guide vanes to a first arrangement of vane-pitch angles including the first vane-pitch angle in order to (i) reduce vibratory response of the plurality of fan blades in response to the fan assembly experiencing at least one given operability condition and (ii) redirect the fan exit air and minimize intake flow distortion experienced by the inlet fan in response to at least one air flow characteristic,
wherein the control system includes a processor and a non-transitory computer readable data storage medium, wherein the control system is configured to (i) store the first arrangement as a predetermined first arrangement, (ii) store the at least one given operability condition as at least one predetermined given operability condition, and (iii) store the at least one air flow characteristic as at least one predetermined air flow characteristic in the non-transitory computer readable data storage medium, wherein the predetermined first arrangement corresponds to at least one of the at least one predetermined given operability condition and the at least one predetermined air flow characteristic, and wherein the control system is configured to rotate the first plurality of variable-pitch outlet guide vanes to the predetermined first arrangement in response to at least one of the fan assembly experiencing the at least one predetermined given operability condition and the at least one predetermined air flow characteristic being present in the inlet air entering the inlet fan or the fan exit air, and
wherein the at least one predetermined given operability condition includes a threshold inlet fan speed at which flutter begins to occur.

2. The fan assembly of claim 1 , wherein the control system further includes a neural network configured to perform machine learning, the neural network configured to iterate over the predetermined first arrangement in order to calculate at least one second arrangement in which the first plurality of variable-pitch outlet guide vanes are configured to be rotated to in response to at least one of the fan assembly experiencing at least one operability condition and at least one air flow characteristic being present in the inlet air entering the inlet fan or the fan exit air that is not included in the at least one predetermined given operability condition and the at least one predetermined air flow characteristic.

3. The fan assembly of claim 1 , wherein the control system is further configured to rotate the first plurality of variable-pitch outlet guide vanes to a safe zone arrangement in response to at least one of the fan assembly experiencing at least one operability condition and at least one air flow characteristic being present in the inlet air entering the inlet fan or the fan exit air that is not included in the at least one predetermined given operability condition and the at least one predetermined air flow characteristic.

4. The fan assembly of claim 1 , wherein the outlet guide vane assembly further includes a second plurality of variable-pitch outlet guide vanes arranged axially downstream of the first plurality of variable-pitch outlet guide vanes, wherein second plurality of variable-pitch outlet guide vanes includes a second variable-pitch outlet guide vane that extends radially relative to the central axis, the second variable-pitch outlet guide vane being configured to rotate to a second vane-pitch angle.

5. The fan assembly of claim 4 , wherein the control system is further configured to rotate the second variable-pitch outlet guide vane about a second vane-pitch axis that extends radially relative to the central axis to further redirect the fan exit air after the fan exit air passes over the first plurality of variable-pitch outlet guide vanes.

6. The fan assembly of claim 5 , wherein the control system is further configured to rotate the first plurality of variable-pitch outlet guide vanes so as to redirect the fan exit air in a first direction, and wherein the control system is further configured to rotate the second plurality of variable-pitch outlet guide vanes so as to redirect the fan exit air in a second direction.

7. The fan assembly of claim 6 , wherein the first direction and the second direction are parallel.

8. The fan assembly of claim 7 , wherein the first direction and the second direction are not parallel.

9. The fan assembly of claim 7 , wherein the first direction is not parallel with the central axis and the second direction is parallel with the central axis.

10. A fan assembly adapted 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,
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 a first variable-pitch outlet guide vane that extends radially relative to the central axis, the first variable-pitch outlet guide vane being configured to rotate to a first vane-pitch angle, and
a control system configured to rotate the first variable-pitch outlet guide vane about a first vane-pitch axis that extends radially relative to the central axis to redirect the fan exit air,
wherein the control system includes a processor and a non-transitory computer readable data storage medium and is configured to rotate the first plurality of variable-pitch outlet guide vanes to a first arrangement of vane-pitch angles including the first vane-pitch angle in order to reduce vibratory response of the plurality of fan blades in response to the fan assembly experiencing at least one given operability condition,
wherein the predetermined first arrangement corresponds to at least one of the at least one predetermined given operability condition, and wherein the control system is configured to rotate the first plurality of variable-pitch outlet guide vanes to the predetermined first arrangement in response to at least one of the fan assembly experiencing the at least one predetermined given operability condition, and
wherein the at least one predetermined given operability condition includes a threshold inlet fan speed at which flutter begins to occur.

11. The fan assembly of claim 10 , wherein the control system is further configured to rotate the first plurality of variable-pitch outlet guide vanes to a first arrangement of vane-pitch angles including the first vane-pitch ang

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

• F01D9/041

  using blades (F01D5/148 takes precedence) · CPC title

• F04D29/563

  specially adapted for elastic fluid pumps · CPC title

• F05D2220/32

  in gas turbines · CPC title