Actively morphable vane

Patent metadata

Field	Value
Publication number	US-10273976-B2
Application number	US-201715423627-A
Country	US
Kind code	B2
Filing date	Feb 3, 2017
Priority date	Feb 3, 2017
Publication date	Apr 30, 2019
Grant date	Apr 30, 2019

Abstract

An actively morphable vane includes a leading edge, a trailing edge downstream of the leading edge, a tip end, a hub end spaced radially outward from the tip end, a pressure side comprising a pressure surface, and a suction side comprising a suction surface. The pressure surface extends continuously between the tip end, the hub end, the leading edge, and the trailing edge. The suction side is positioned opposite of the pressure side and the suction surface extends continuously between the tip end, the hub end, the leading edge, and the trailing edge. The actively morphable stator vane also includes an actuator in mechanical communication with the tip end. The actuator is operable to selectively morph the actively morphable stator vane between a first configuration and a second configuration. The first configuration is optimized for a first operating condition, and the second configuration is optimized for a second operating condition.

First claim

What is claimed is:

1. An actively morphable stator vane for a compressor, the actively morphable stator vane comprising:
a leading edge;
a trailing edge downstream of the leading edge;
a tip end;
a hub end spaced radially outward from the tip end;
a pressure side comprising a pressure surface, the pressure surface extending continuously between the tip end and the hub end and extending continuously between the leading edge and the trailing edge;
a suction side comprising a suction surface, the suction side positioned opposite of the pressure side, the suction surface extending continuously between the tip end and the hub end and extending continuously between the leading edge and the trailing edge; and
an actuator in mechanical communication with the tip end, the actuator operable to selectively morph the actively morphable stator vane between a first configuration and a second configuration by altering the shape of the pressure surface and the suction surface, the first configuration optimized for a first operating condition, and the second configuration optimized for a second operating condition, wherein the actuator is positioned at the hub end, the actively morphable vane further comprising a connector in mechanical communication with the tip end and the actuator, wherein the connector is a connector rod and the connector rod is connected to a center point of the tip end.

2. The actively morphable stator vane of claim 1 , wherein the leading edge and the trailing edge define a chord length therebetween, and the chord length in the first configuration is substantially the same as the chord length in the second configuration.

3. The actively morphable stator vane of claim 1 , further comprising a tip end chord defined by a straight line extending from the leading edge to the trailing edge at the tip end, a hub end chord defined by a straight line extending from the leading edge to the trailing edge at the hub end, and an angle defined by the tip end chord and the hub end chord, wherein the angle is larger in the second configuration than in the first configuration.

4. The actively morphable stator vane of claim 1 , wherein the vane comprises a composite material.

5. The actively morphable stator vane of claim 1 , wherein the stator vane is a variable angle vane.

6. The actively morphable stator vane of claim 1 , wherein the stator vane is a fixed angle vane which does not rotate relative to a casing of the compressor.

7. A method of operating a turbomachine, the turbomachine comprising a compressor, the compressor comprising an actively morphable stator vane, the actively morphable stator vane comprising a leading edge, a trailing edge downstream of the leading edge, a tip end, a hub end spaced radially outward from the tip end, a continuous pressure surface extending continuously between the tip end and the hub end and extending continuously between the leading edge and the trailing edge, and a continuous suction surface positioned opposite of the continuous pressure surface, the continuous suction surface extending continuously between the tip end and the hub end and extending continuously between the leading edge and the trailing edge, an actuator in mechanical communication with the tip end, wherein the actuator is positioned at the hub end, the actively morphable vane further comprising a connector in mechanical communication with the tip end and the actuator, wherein the connector is a connector rod and the connector rod is connected to a center point of the tip end, the method comprising: operating the turbomachine at a first operating condition; configuring the actively morphable stator vane in a first configuration while operating the turbomachine at the first operating condition; operating the turbomachine at a second operating condition; and configuring the actively morphable stator vane in a second configuration by altering the shape of the continuous pressure surface and the continuous suction surface while operating the turbomachine at the second operating condition.

8. The method of claim 7 , wherein configuring the actively morphable vane in a second configuration comprises twisting the actively morphable stator vane.

9. The method of claim 7 , wherein configuring the actively morphable stator vane in the second configuration comprises applying a torque to the tip end.

10. The method of claim 9 , wherein the actively morphable vane comprises a tip end chord defined by a straight line extending from the leading edge to the trailing edge at the tip end, a hub end chord defined by a straight line extending from the leading edge to the trailing edge at the hub end, and an angle defined by the tip end chord and the hub end chord, and wherein applying a torque to the tip end comprises rotating the tip end relative to the hub end such that the angle defined by the tip end chord and the hub end chord is greater in the second configuration than in the first configuration, without altering the shape of the tip end.

Assignees

• Gen Electric

Inventors

• Jemora Daniel
• Novak Damir
• Nachtigall Hermann

Classifications

• F04D27/0246

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• F04D29/563 Primary

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• F04D29/542

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