Invention Grant
- Patent Title: Hollow fan blade for gas turbine engine
- Patent Title (中): 用于燃气轮机的中空风扇叶片
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Application No.: US11295335Application Date: 2005-12-06
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Publication No.: US07993105B2Publication Date: 2011-08-09
- Inventor: Michael A. Weisse , William R. Graves , Stephen Bret Bonarrigo
- Applicant: Michael A. Weisse , William R. Graves , Stephen Bret Bonarrigo
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D5/14
- IPC: F01D5/14

Abstract:
A hollow fan blade for a gas turbine engine provides improved resistance to buckling without adding wall thickness. The hollow fan blade includes a pressure side wall and a suction side wall separated and supported by ribs. In the present invention, each wall segment between each adjacent pair of ribs is straight, not curved. At least some of the adjacent walls segments extend at non-parallel angles relative to one another to form the airfoil shape to the hollow fan blade. The resulting fan blade side walls have faceted surfaces, rather than a continuous smooth, curved surface. The straight wall segments between adjacent ribs can withstand higher compressive forces without buckling. As a result, the wall thickness can be reduced.
Public/Granted literature
- US20070128042A1 Hollow fan blade for gas turbine engine Public/Granted day:2007-06-07
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