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    • 21. 发明申请
    • AIRCRAFT PROPULSION SYSTEM
    • 飞机推进系统
    • US20110259996A1
    • 2011-10-27
    • US12768585
    • 2010-04-27
    • DANIEL KENT VETTERSRobert Wayne CedozDavid Eames
    • DANIEL KENT VETTERSRobert Wayne CedozDavid Eames
    • B64D27/10
    • B64D27/10B64D27/26B64D2027/005B64D2027/026Y02T50/44Y02T50/64Y02T50/66
    • An aircraft propulsion system is disclosed herein. The aircraft propulsion system includes a core engine having an intake, a compressor section, a combustor section, and a turbine section arranged along a centerline axis. The aircraft propulsion system also includes a nacelle surrounding the core engine. The aircraft propulsion system also includes at least one free power turbine driven to rotate by exhaust gases exiting the turbine section. The aircraft propulsion system also includes at least one rotor module driven to rotate by at least one free power turbine. The aircraft propulsion system also includes first and second pylons extending away from the nacelle and operable to mount the core engine to an aircraft. The first and second pylons are spaced from one another on opposite sides of at least one plane containing the centerline axis and mirror one another across the at least one plane.
    • 这里公开了一种飞机推进系统。 飞行器推进系统包括具有进气口的核心发动机,压缩机部分,燃烧器部分和沿中心轴线布置的涡轮部分。 飞机推进系统还包括围绕核心发动机的机舱。 飞行器推进系统还包括至少一个自由动力涡轮机,该自由动力涡轮机被排出涡轮部分的废气驱动旋转。 飞行器推进系统还包括至少一个被至少一个自由动力涡轮机驱动旋转的转子模块。 飞机推进系统还包括从机舱延伸的第一和第二塔架,并且可操作地将核心发动机安装到飞机上。 第一和第二塔在包含中心线轴线的至少一个平面的相对侧上彼此间隔开,并且跨越至少一个平面相互镜像。