Power lever apparatus for a turbine engine

F - Mech Eng,Light,Heat,Weapons – 02 – C

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F02C 9/16 (2006.01) F02C 9/28 (2006.01)

Patent

CA 1217064

ABSTRACT OF THE DISCLOSURE In a turbine engine having a compressor with a bleed valve and a variable geometry apparatus responsive to an operational control member for regulating the flow rate of fuel supplied the turbine engine as a function of atmospheric pressure and the temperature of air supplied to the compressor corresponding to movement of a power lever by an operator to a desired operation of the turbine engine. The power lever has an indicator member fluidtcally connected to a follower member linked to the operational control member. The fluidic connection is responsive to operational parameters of the turbine engine and limits the rotational input to the follower member when the rate of fuel flow could cause stal- ling and the development of an unacceptable operating temperature or overspeed condition in the turbine engine.

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