US Patent 9353641 Controlling blade tip clearances in a turbine engine
Patent 9353641 was granted and assigned to Snecma on May, 2016 by the United States Patent and Trademark Office.
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Patent abstract
A turbine engine including a controller controlling clearance between tips of moving blades of a high-pressure turbine and an outer casing surrounding the blades, by cooling the outer casing by the impact of air taken from a high-pressure compressor stage of the engine, and by electric heating of top and bottom portions of the outer casing.
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US Patent 09353641 Controlling blade tip clearances in a turbine engine US Patent 9353641 Controlling blade tip clearances in a turbine engine
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Patent Number
0935364100
Patent Number
935364100
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Is a
Current Assignee
Patent Jurisdiction
Patent Number
093536410
Date of Patent
May 31, 2016
0Patent Application Number
133946360
Date Filed
September 7, 2010
0Official Website
Patent Primary Examiner
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
093536410
Date of Patent
May 31, 2016
0Patent Application Number
133946360
Date Filed
September 7, 2010
0Official Website
Patent Primary Examiner
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US Patent 09353641 Controlling blade tip clearances in a turbine engine
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
09353641
Date of patent
May 31, 2016
Patent application number
13394636
Date Filed
September 7, 2010
Patent primary examiner
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