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High speed rotor assembly shroud
   
Document Number
US Patent 7066714
Issued Date
June 27, 2006
Link
Inventors
Miller; Jeff H. (Simi Valley, CA)
Grota; Steven P. (Thousand Oaks, CA)
Map
Abstract
An improved rotor assembly shroud includes at least one reinforcing flange on the upper surface of the shroud. The strength provided by the reinforcing flange allows for a smaller shroud thickness resulting in a net reduction of shroud mass. The lower shroud mass reduces the centrifugal stress on the rotor assembly blade during operation. The strength provided by the reinforcing flanges also significantly reduces the centrifugal bending stress on the shroud during operation. The shroud mass may be further reduced by tapering the shroud leading and trailing edges or, for shrouds incorporating a damper, by providing a damper cavity with a lower diameter surface defining an opening therethrough.
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Number of Claims:
22
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Owner
Published
June 27, 2006
Application Number
10/811,359
Filed
March 26, 2004
US Classification
415/173.6   416/192
Int'l Classification
F04D   29/08   (20060101)  
Examiner
Assistant Examiner
USPTO Field of Search
415/173.6   415/173.1   415/173.4   415/173.3   416/190   416/191   416/192   416/194   416/195  
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