Jet engine fan and compressor bearing support

Details Jet engine fan and compressor bearing support Jet engine fan and compressor bearing support

F - Mech Eng,Light,Heat,Weapons

02

C

60/91

F02C 7/06 (2006.01) F01D 25/16 (2006.01) F04D 29/64 (2006.01)

Patent

CA 1308924

A bypass turbofan jet engine subassembly. A row of structural fan stators and a row of structural compressor guide vanes have their outer ends attached to the engine outer duct. The structural stator inner ends are attached by an inner support cone to the outer race of the fan rolling element bearing and the structural guide vana inner ends are attached by another inner support cone to the outer race of the compressor rolling element bearing. The fan and compressor outer races are interconnected by a tie bar. The subassembly eliminates the engine fan and compressor frames.

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