US Patent 7186079 Turbine engine disk spacers
Patent 7186079 was granted and assigned to United Technologies on March, 2007 by the United States Patent and Trademark Office.
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Patent Citations Received
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Patent Inventor Names
Gabriel L. Suciu0
James W. Norris0
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Patent abstract
A gas turbine engine rotor stack includes one or more longitudinally outwardly concave spacers. Outboard surfaces of the spacers may be in close facing proximity to inboard tips of vane airfoils. The spacers may provide a longitudinal compression force that increases with rotational speed.
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US Patent 07186079 Turbine engine disk spacers US Patent 7186079 Turbine engine disk spacers
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Patent Number
07186079
Patent Number
7186079
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Official Website
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Website URL
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US Patent 07186079 Turbine engine disk spacers
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Is a
Current assignee
Patent jurisdiction
Patent number
07186079
Date of patent
March 6, 2007
Patent application number
10985863
Date Filed
November 10, 2004
Patent primary examiner
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