Wireless power for gas turbine engine instrumentation

US9664116B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9664116-B2
Application numberUS-201414296851-A
CountryUS
Kind codeB2
Filing dateJun 5, 2014
Priority dateJun 27, 2013
Publication dateMay 30, 2017
Grant dateMay 30, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A gas turbine engine includes a compressor section, a combustor section and a turbine section mounted relative to an engine static structure. A module includes instrumentation that is mounted to the engine static structure. The module includes an energy harvesting power source that is configured to provide electricity to the instrumentation during engine operation and is independent of an external electrical power source.

First claim

Opening claim text (preview).

The invention claimed is: 1. A gas turbine engine comprising: a compressor section, a combustor section and a turbine section mounted relative to an engine static structure; a module including instrumentation mounted to the engine static structure, the module including an energy harvesting power source configured to provide electricity to the instrumentation during engine operation independent of an external electrical power source, wherein the energy harvesting power source includes a heat source and is configured to provide the electricity in response to a heat flux from the heat source, wherein the heat flux is provided by a cooling fluid within the module, and the module has a cooling line input for receiving the cooling fluid, a valve is connected to the cooling line input that is configured to control a flow of the cooling fluid provided via the cooling line input. 2. The gas turbine engine according to claim 1 , wherein the energy harvesting power source includes a thermocouple is arranged adjacent to the heat source and configured to provide the electricity in response to the heat flux. 3. The gas turbine engine according to claim 1 , wherein the energy harvesting power source includes a Peltier cell arranged adjacent to the heat source and configured to provide the electricity in response to the heat flux. 4. A station probe comprising: a rake portion that includes a plurality of sensors; an environmental container attached to one end of the rake portion, the environmental container including: signal conditioning circuitry for analyzing sensor signals received from the plurality of sensors to generate measured sensor values; a cooling line input for receiving a cooling fluid; a valve connected to the cooling line input that controls a flow of cooling fluid provided via the cooling line input; a temperature sensor internal to the environmental container that provides temperature feedback regarding an internal temperature of the environmental container; and a communication module for communicating the measured sensor values to a control room; and an energy harvesting power source in electrical communication with at least one of the signal conditioning circuitry and the communication module, wherein the energy harvesting power source includes a heat source and is configured to provide electricity in response to a heat flux from the heat source, and the heat flux is provided by the cooling fluid. 5. The station probe of claim 4 , wherein the environmental container includes a controller connected to control a position of the valve based on a monitored internal temperature of the environmental container to regulate the flow of cooling fluid provided via the cooling line input. 6. A station probe comprising: a rake portion that includes a plurality of sensors; and an environmental container attached to one end of the rake portion, the environmental container comprising: inputs connected to receive sensor signals from the plurality of sensors; signal conditioning circuitry for interpreting inputs provided by the plurality of sensors to generate measured sensor values; a cooling line input that receives a cooling fluid; a valve that controls a flow of cooling fluid provided via the cooling line input; a temperature sensor internal to the environmental container that provides temperature feedback regarding an internal temperature of the environmental container; a controller connected to control a position of the valve based on a monitored internal temperature of the environmental container to regulate the flow of cooling fluid provided via the cooling line input; and an energy harvesting power source in electrical communication with at least one of the signal conditioning circuitry and the communication module, wherein the energy harvesting power source includes a heat source and is configured to provide electricity in response to a heat flux from the heat source, and the heat flux is provided by the cooling fluid.

Assignees

Inventors

Classifications

  • Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title

  • F02C7/32Primary

    Arrangement, mounting, or driving, of auxiliaries · CPC title

  • Details concerning sensor power supply · CPC title

  • Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C5/00) · CPC title

  • Vibration harvesters · CPC title

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What does patent US9664116B2 cover?
A gas turbine engine includes a compressor section, a combustor section and a turbine section mounted relative to an engine static structure. A module includes instrumentation that is mounted to the engine static structure. The module includes an energy harvesting power source that is configured to provide electricity to the instrumentation during engine operation and is independent of an exter…
Who is the assignee on this patent?
United Technologies Corp
What technology area does this patent fall under?
Primary CPC classification F02C7/32. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue May 30 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).