Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoir

US9604756B1 · US · B1

Patent metadata
FieldValue
Publication numberUS-9604756-B1
Application numberUS-201615200057-A
CountryUS
Kind codeB1
Filing dateJul 1, 2016
Priority dateMar 29, 2011
Publication dateMar 28, 2017
Grant dateMar 28, 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 process for testing a combustor of a gas turbine engine, where a large volume of compressed air is stored in a large reservoir of at least 10,000 m 3 such as an underground storage cavern, compressed air from the storage reservoir is passed through heat exchanger to preheat the compressed air to a temperature that would normally be discharged from a compressor, the preheated compressed air is burned with a fuel in the combustor, and additional compressed air from the reservoir is passed through an injector located downstream from the combustor to produce a decreased pressure such that a low atmospheric condition at the combustor exit is simulated.

First claim

Opening claim text (preview).

We claim the following: 1. A process for testing a combustor of a gas turbine engine under low atmospheric conditions comprising the steps of: filling an underground storage reservoir with compressed air; securing a combustor to be tested on a test stand; passing compressed air from the underground storage reservoir through a heater to increase a temperature of the compressed air; passing the heated compressed air into a combustor for testing; burning a fuel with the heated compressed air within the combustor; and, passing additional compressed air from the underground storage reservoir into an ejector located downstream of the combustor to decrease a pressure at an exhaust of the combustor to simulate a low atmospheric condition. 2. The process for testing a combustor of a gas turbine engine under low atmospheric conditions of claim 1 , and further comprising the step of: the step of heating the compressed air from the underground storage reservoir includes heating the compressed air without decreasing an oxygen level of the compressed air.

Assignees

Inventors

Classifications

  • Wind tunnels · CPC title

  • Wheeled or endless-tracked vehicles (G01M17/08 takes precedence) · CPC title

  • G01M15/14Primary

    Testing gas-turbine engines or jet-propulsion engines · CPC title

  • for storing compressed air · CPC title

  • B65D19/16Primary

    Collapsible pallets · CPC title

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Frequently asked questions

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What does patent US9604756B1 cover?
A process for testing a combustor of a gas turbine engine, where a large volume of compressed air is stored in a large reservoir of at least 10,000 m 3 such as an underground storage cavern, compressed air from the storage reservoir is passed through heat exchanger to preheat the compressed air to a temperature that would normally be discharged from a compressor, the preheated compressed air i…
Who is the assignee on this patent?
Brostmeyer Joseph D, Memmen Robert L, Florida Turbine Tech Inc
What technology area does this patent fall under?
Primary CPC classification G01M15/14. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Mar 28 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).