US Patent 7225607 Gas turbine braking apparatus and method
Patent 7225607 was granted and assigned to Pratt & Whitney Canada on June, 2007 by the United States Patent and Trademark Office.
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Patent Inventor Names
Joseph Horace Brand0
Kevin Allan Dooley0
Ronald Trumper0
Stephen Arthur Anderson0
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Patent abstract
A device is provided which can serve one or more of the multiple functions of impeding rotation of a shaft de-coupled turbine rotor, selectively impeding rotation of a first spool of the engine, for example to permit a second spool to generate power for use in ground operation, and facilitating reduced aircraft ground speed.
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US Patent 07225607 Gas turbine braking apparatus and method US Patent 7225607 Gas turbine braking apparatus and method
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Patent Number
072256070
Patent Number
72256070
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
072256070
Date of Patent
June 5, 2007
0Patent Application Number
109276000
Date Filed
August 27, 2004
0Official Website
Patent Primary Examiner
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US Patent 07225607 Gas turbine braking apparatus and method
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
07225607
Date of patent
June 5, 2007
Patent application number
10927600
Date Filed
August 27, 2004
Patent primary examiner
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