US Patent 7484935 Turbine rotor hub contour
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Patent abstract
Disclosed herein is a turbine rotor having a contoured hub comprising a cambered surface extending from a leading edge of the rotor hub to a trailing edge of the rotor hub along an axial direction of the rotor hub. A turbine rotor and a gas turbine engine comprising a turbine rotor flow path having a cambered surface are also disclosed, together with a method providing a turbine rotor flow path for a turbine rotor hub.
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US Patent 07484935 Turbine rotor hub contour US Patent 7484935 Turbine rotor hub contour
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Patent Number
0748493500
Patent Number
748493500
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Patent Jurisdiction
Patent Number
074849350
Date of Patent
February 3, 2009
0Patent Application Number
111444720
Date Filed
June 2, 2005
0Official Website
Patent Primary Examiner
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Patent Jurisdiction
Patent Number
074849350
Date of Patent
February 3, 2009
0Patent Application Number
111444720
Date Filed
June 2, 2005
0Official Website
Patent Primary Examiner
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US Patent 07484935 Turbine rotor hub contour
Infobox
Is a
Patent jurisdiction
Patent number
07484935
Date of patent
February 3, 2009
Patent application number
11144472
Date Filed
June 2, 2005
Patent primary examiner
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