Air-start assembly and method
AssigneeGeneral Electric Company
InventorsJohn J. Ciokajlo, Michael T. O'Brien
Life of this patent
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AssigneeGeneral Electric Company
InventorsJohn J. Ciokajlo, Michael T. O'Brien
Estimating the term…
A method and assembly are effective for air-starting an aircraft gas turbine engine having a fan powered by a low pressure turbine through a first shaft, and a compressor powered by a high pressure turbine through a second shaft disposed coaxially therewith. A gear train is selectively operatively joined between the first and second shafts by selectively engaging a first clutch for transmitting torque through the first clutch only in one direction from the first shaft to the second shaft when the fan is windmilling for driving the second shaft to allow an air-start of the gas turbine engine during flight. In a preferred embodiment, a second clutch is operatively joined to the gear train and is selectively engageable at speeds of the second shaft below a predetermined release speed, and disengageable at the release speed and above for disconnecting the air-start assembly once the engine has been started.
An air-start assembly for an aircraft gas turbine engine having a fan powered by a low pressure turbine through a first shaft, and a compressor powered by a high pressure turbine through a second shaft disposed coaxially around said first shaft comprising:
An air-start assembly for an aircraft gas turbine engine having a fan powered by a low pressure turbine through a first shaft, and a compressor powered by a high pressure turbine through a second shaft disposed coaxially around said first shaft comprising;
An assembly according to claim 5 wherein said first clutch is operatively joined between said third gear and said first shaft for transmitting torque only from said first shaft to said third gear, and for preventing torque transmission from said third gear to said first shaft.
Dependencies are inferred from the claim text.