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    • 2. 发明申请
    • PTO ASSEMBLY FOR A GAS TURBINE ENGINE
    • 燃气涡轮发动机PTO装配
    • US20070022735A1
    • 2007-02-01
    • US11161338
    • 2005-07-29
    • John HenryRaymond Patt
    • John HenryRaymond Patt
    • F02C7/32
    • F02K3/04F02C7/36F05D2260/4031F05D2260/85
    • A PTO apparatus for a gas turbine engine having first and second drive shafts includes a first ring gear for being coupled to the first drive shaft and a first bevel gear engaged with the first drive gear and coupled to a PTO shaft. A second ring gear is provided for being coupled to the second drive shaft. A second bevel gear is engaged with the second drive gear and coupled to the PTO shaft through a one-way clutch. A method of operating a gas turbine engine includes operatively coupling a PTO shaft to first and second drive shafts and providing a starting torque to the first and second drive shafts through the PTO shaft. After the engine is started, power is transferred from the first drive shaft to the PTO shaft; and the second shaft is decoupled from the PTO shaft.
    • 一种用于具有第一和第二驱动轴的燃气涡轮发动机的PTO装置包括用于联接到第一驱动轴的第一环形齿轮和与第一驱动齿轮接合并联接到PTO轴的第一锥齿轮。 第二齿圈提供用于联接到第二驱动轴。 第二锥齿轮与第二驱动齿轮接合并通过单向离合器联接到PTO轴。 操作燃气涡轮发动机的方法包括将PTO轴可操作地联接到第一和第二驱动轴并且通过PTO轴向第一和第二驱动轴提供启动扭矩。 发动机启动后,动力从第一驱动轴传递到PTO轴; 并且第二轴与PTO轴分离。