Rotational imbalance reduction

Patent metadata

Field	Value
Publication number	US-10309223-B2
Application number	US-201615266553-A
Country	US
Kind code	B2
Filing date	Sep 15, 2016
Priority date	Sep 15, 2016
Publication date	Jun 4, 2019
Grant date	Jun 4, 2019

Abstract

Various embodiments include apparatuses and systems for controlling rotational imbalance of a rotary element. In one embodiment, a rotational imbalance reduction apparatus includes at least one heating element for heating a location on a rotary element, a pulsing element configured to pulse actuate the heating element in synchronization with a multiple, fraction, or mixed fraction of the frequency of rotation of the rotary element, and a control system coupled with the pulsing element and the heating element, the control system actuating the heating element and the pulsing element to apply heat to the location of the rotary element in pulses synchronized with the multiple, fraction, or mixed fraction of the frequency of rotation of the rotary element.

First claim

What is claimed is:

1. A system comprising:
a turbomachine rotor assembly including a rotary element;
at least one heating element mounted proximate the rotary element; and
a control system coupled with the heating element, the control system:
determining whether a rotational imbalance of the turbomachine rotor assembly exceeds a predetermined level; and
actuating the at least one heating element to heat the rotary element in response to determining that the rotational imbalance of the turbomachine rotor assembly exceeds the predetermined level; and

wherein the at least one heating element comprises a first electrode and a second electrode, the first electrode coupled to a first power source, the second electrode coupled to a second power source; and
wherein the first power source is configured to supply high frequency, high voltage electricity relative to electricity supplied by the second power source, and the second power source is configured to supply high current, low voltage electricity relative to electricity supplied by the first power source.

2. The system of claim 1 , wherein the rotary element comprises a dopant on a surface location, the dopant increasing a heat response in the surface location upon actuating the heating element, the increasing heat response being relative to a material composing the surface location undoped.

3. The system of claim 1 , further comprising a sensor system including at least one sensor to detect vibration amplitude of the rotary element.

4. The system of claim 1 , wherein the at least one heating element comprises a light transmitter configured to transmit light onto the rotary element.

5. The system of claim 1 , wherein the at least one heating element comprises at least one electrode electrically configured to generate an arc of electricity from the at least one electrode to the rotary element.

6. The system of claim 1 , wherein the at least one heating element comprises at least one inductor configured to induce an eddy current in the rotary element.

7. A system comprising:
a turbomachine rotor assembly including a rotary element;
at least one heating element mounted proximate the rotary element, the at least one heating element comprising a plurality of heating elements arranged to form at least a portion of a ring around the rotary element, the plurality of heating elements including a first subset and a second subset of heating elements;
a control system coupled with the heating element, the control system:
determining whether a rotational imbalance of the turbomachine rotor assembly exceeds a predetermined level; and
actuating the at least one heating element to heat the rotary element in response to determining that the rotational imbalance of the turbomachine rotor assembly exceeds the predetermined level; and

a pulsing element coupled to the control system and configured to pulse actuate the plurality of heating elements in synchronization with a multiple, fraction, or mixed fraction of a frequency of rotation of the rotary element;
wherein the control system activates the first subset of the plurality of heating elements in first pulses synchronized with the multiple, fraction, or mixed fraction of the frequency of rotation of the rotary element, and the control system activates the second subset of the plurality of heating elements in second pulses synchronized with the multiple, fraction, or mixed fraction of the frequency of rotation of the rotary element, the first pulses being temporally offset from the second pulses.

8. The system of claim 7 , wherein the rotary element comprises a dopant on a surface location, the dopant increasing a heat response in the surface location upon actuating the heating element, the increasing heat response being relative to a material composing the surface location undoped.

9. The system of claim 7 , further comprising a sensor system including at least one sensor to detect vibration amplitude of the rotary element.

10. The system of claim 7 , wherein the at least one heating element comprises a light transmitter configured to transmit light onto the rotary element.

11. The system of claim 7 , wherein the at least one heating element comprises at least one inductor configured to induce an eddy current in the rotary element.

Assignees

• Gen Electric

Inventors

• Safari Zadeh Immanuel
• Fogarty James Michael
• Golebiowski Mateusz Wojciech

Classifications

• F01D5/26

  Antivibration means not restricted to blade form or construction or to blade-to-blade connections {or to the use of particular materials} · CPC title

• H05B6/102

  the metal pieces being rotated while induction heated · CPC title

• F01D5/08

  Heating, heat-insulating or cooling means {(specially adapted for radial flow machines or engines F01D5/04)} · CPC title

• F01D17/02

  Arrangement of sensing elements · CPC title

• F01D5/10

  Anti- vibration means {(specially adapted for radial flow machines or engines F01D5/04)} · CPC title