Controllable magneto-rheological device for gas turbine engine

Patent metadata

Field	Value
Publication number	US-11002335-B2
Application number	US-201615346202-A
Country	US
Kind code	B2
Filing date	Nov 8, 2016
Priority date	Nov 8, 2016
Publication date	May 11, 2021
Grant date	May 11, 2021

Abstract

A controllable magneto-rheological device includes an annular cylinder formed by inner and outer walls connected at first and second opposing ends and forming an inner shaft configured to receive an operational component of an engine, generator or other device including one or more rotating structures. A magneto-rheological fluid is provided to fill a volume between the inner and outer walls of the annular cylinder. A plurality of electro-magnetic coils are positioned around the outer wall of the annular cylinder. One or more current controllers are coupled to the plurality of electro-magnetic coils for introducing a current through each of the electro-magnetic coils and corresponding magnetic flux through the magneto-rheological fluid. A level of current provided to each of the plurality of electro-magnetic coils directly affects the viscosity of the magneto-rheological fluid and thus the stiffness and damping levels of the controllable magneto-rheological device.

First claim

What is claimed is:

1. A controllable magneto-rheological device, comprising:
an annular cylinder formed by inner and outer walls connected at first and second opposing ends, the inner wall of the annular cylinder defining an inner shaft configured to receive an operational component;
a magneto-rheological fluid provided to fill a volume defined by and extending between the inner wall and the outer wall of the annular cylinder;
a plurality of coils positioned on an exterior surface of the outer wall of the annular cylinder, each of the plurality of coils formed from a conductive material to include any number of one or more turns per coil, each of the plurality of coils comprising an inner end and an outer end, the inner end connected to the outer wall of the annular cylinder, and each of the plurality of coils extending outwardly from the exterior surface of the outer wall along a radial direction; and
one or more current controllers coupled to the plurality of coils, the one or more current controllers configured to introduce a current through each of the plurality of coils and to generate a corresponding magnetic flux through the magneto-rheological fluid;
wherein a level of current provided to each of the plurality of coils by the one or more current controllers directly affects the viscosity of the magneto-rheological fluid and thus stiffness or damping levels of the controllable magneto-rheological device.

2. The controllable magneto-rheological device of claim 1 , wherein the one or more current controllers are configured to determine one or more signal characteristics of a waveform signal defining the current introduced through each of the plurality of coils, and wherein the one or more signal characteristics can be modified over time.

3. The controllable magneto-rheological device of claim 2 , wherein the one or more signal characteristics of the waveform signal defining the current introduced through each of the plurality of coils comprises one or more of an amplitude, phase and waveform shape.

4. The controllable magneto-rheological device of claim 1 , further comprising a plurality of magnetic cores, each magnetic core disposed within one of the plurality of coils.

5. The controllable magneto-rheological device of claim 1 , further comprising:
an operational component of an engine received within the inner shaft of the annular cylinder; and
one or more sensors for monitoring engine response, wherein the one or more sensors are coupled to the one or more current controllers such that the current provided to the plurality of coils is determined at least in part from the engine response.

6. The controllable magneto-rheological device of claim 5 , wherein the one or more sensors comprise one or more of a tachometer for determining engine operating speed and a vibration sensor for determining vibrational phenomena within the engine.

7. The controllable magneto-rheological device of claim 1 , wherein the plurality of coils comprise one or more annular stacks of coils positioned along a length of the annular cylinder such that one or more spacings are formed between adjacent annular stacks.

8. The controllable magneto-rheological device of claim 1 , further comprising one or more orifices formed between the inner and outer walls of the annular cylinder to create flow restriction of the magneto-rheological fluid within the annular cylinder.

9. The controllable magneto-rheological device of claim 1 , wherein a level of current provided from the one or more current controllers to each of the plurality of coils is substantially the same for all of the plurality of coils to create a symmetrical stiffness within the magneto-rheological device.

10. The controllable magneto-rheological device of claim 1 , wherein a first level of current is provided by the one or more current controllers to a first portion of the plurality of coils, wherein a second level of current is provided by the one or more current controllers to a second portion of the plurality of coils, and wherein the first level of current differs from the second level of current to create an asymmetrical stiffness within the magneto-rheological device.

11. A gas turbine engine, comprising:
a compressor section including one or more compressors;
a turbine section located downstream of the compressor section, the turbine section including one or more turbines;
one or more controllable magneto-rheological devices positioned relative to one or more operational components of the one or more compressors or the one or more turbines, each controllable magneto-rheological device comprising:
an annular cylinder formed by inner and outer walls connected at first and second opposing ends, the inner wall of the annular cylinder defining an inner shaft configured to receive one or more operational components of the one or more compressors or the one or more turbines;
a magneto-rheological fluid provided to fill a volume defined by and between the inner wall and the outer wall of the annular cylinder;
a plurality of coils positioned on an exterior surface of the outer wall of the annular cylinder, each of the plurality of coils formed from a conductive material to include any number of one or more turns per coil, each of the plurality of coils comprising an inner end and an outer end, the inner end connected to the outer wall of the annular cylinder, and each of the plurality of coils extending outwardly from the exterior surface of the outer wall along a radial direction; and
one or more current controllers coupled to the plurality of coils, the one or more current controllers configured to introduce a current through each of the plurality of coils and to generate a corresponding magnetic flux through the magneto-rheological fluid.

12. The gas turbine engine of claim 11 , wherein the one or more current controllers are configured to determine one or more of an amplitude, phase or waveform shape for a waveform signal defining the current introduced through each of the plurality of coils, and wherein the amplitude, phase or waveform shape for the waveform signal can be modified over time.

13. The gas turbine engine of claim 11 , further comprising one or more sensors for detecting speed or vibration of the gas turbine engine, wherein the one or more sensors are coupled to the one or more current controllers such that a current level provided to the plurality of coils is determined at least in part from the speed or the vibration of the gas turbine engine.

14. The gas turbine engine of claim 11 , further comprising one or more orifices formed between the inner and outer walls of the annular cylinder to create flow restriction of the magneto-rheological fluid within the annular cylinder.

15. The gas turbine engine of claim 11 , wherein the plurality of coils comprise one or more annular stacks of coils positioned along a length of the annular cylinder such that one or more spacings are formed between adjacent annular stacks.

16. A method for controlling a magneto-rheological device, comprising:
acquiring, by one or more processors, sensor data from one or more sensors positioned within an operational device;
determining, by the one or more processors, one or more frequency components of the sensor data as corresponding to a source of vibration within the operational device;
determining, by the one or more processors, one or more stiffness/damping modes for operation of a magneto-rheological device, wherein the one or more stiffness/damping modes are determined based at least in part on the sensor data and the one or more frequency components;
genera

Assignees

• Gen Electric

Inventors

• Ghosh Shuvajyoti
• Payyoor Narayanan
• Bhavanam Surender Reddy
• Schmidt Richard
• Steen Tod Robert

Classifications

• F01D25/164 Primary

  Flexible supports; Vibration damping means associated with the bearing · CPC title

• F16F15/18

  using electric, {magnetic or electromagnetic} means ({suppression of vibrations of rotating systems by use of non-rotating magnetic or electromagnetic means F16F15/03;} dynamo-electric devices H02K; {control effected upon generator excitation circuit to reduce harmful effects of overloads or transients H02P9/10}) · CPC title

• F16F15/16

  using a fluid {or pasty material}(F16F9/53, F16F15/13157 take precedence; devices connecting input and output members F16D) · CPC title

• F16C27/045

  with a fluid film, e.g. squeeze film damping · CPC title

• F16C19/26

  with a single row of rollers · CPC title