Load distribution system for gas turbine engine

Details Load distribution system for gas turbine engine Load distribution system for gas turbine engine

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/06 (2006.01) F01D 3/04 (2006.01) F01D 25/16 (2006.01) F16C 27/08 (2006.01) F16C 39/04 (2006.01) F16C 41/02 (2006.01)

Patent

CA 2701512

There is provided an axial bearing load distribution system for a gas turbine engine of the type having a low pressure rotor supported by axial bearings. The system comprises a line having an inlet end positioned in a high-pressure compressor gas path downstream of any compressor stage provided with a variable geometry. The line is adapted to sense static pressure in the high-pressure compressor gas path. The line has an outlet end producing the static pressure. An air-tight pressure actuator is operatively connected to the outlet end and to one of the axial bearings to exert a force on the axial bearing proportionally to a pressure of the outlet end.

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