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    Fully integrated environmental and secondary power system
    6.
    发明授权
    Fully integrated environmental and secondary power system 失效
    全面整合环境和二次电力系统

    公开(公告)号：US5490645A

    公开(公告)日：1996-02-13

    申请号：US164491

    申请日：1993-12-09

    申请人： Geoffrey D. Woodhouse

    发明人： Geoffrey D. Woodhouse

    IPC分类号： B64D13/06 ,  B64D41/00

    CPC分类号： B64D41/00 ,  B64D13/06 ,  B64D2013/0611 ,  F05B2220/50 ,  Y02T50/44 ,  Y02T50/56

    摘要： An aircraft subsystem provides the aircraft with all its electrical and conditioned air requirements without requiring the extraction of either shaft power and/or pressurized air from the aircraft's main engines. At the core of this subsystem are two rotating assemblies journaled on non-oil lubricated bearings to a housing. One assembly includes a cooling turbine, a starter/generator, a core compressor, and a high pressure stage of a two stage axial turbine, all mounted on a single shaft. A combustor is disposed between the core compressor and the turbine. The other assembly is comprised of the low pressure stage of the axial turbine coupled to a load compressor via a second shaft. The high pressure turbine stage and cooling turbine are sized to drive the core compressor and starter/generator which provides all the aircraft's electrical needs both on the ground and inflight. The low pressure turbine stage drives the load compressor, which produces pressurized air that is conditioned through heat exchange components and then expanded and cooled across the cooling turbine before being delivered to the aircraft cabin.

    摘要翻译： 飞机子系统为飞机提供其所有电气和调节空气需求，而不需要从飞机的主发动机提取轴功率和/或加压空气。 在这个子系统的核心是两个旋转组件在非油润滑轴承轴颈轴承到外壳。 一个组件包括全部安装在单个轴上的冷却涡轮机，起动器/发电机，核心压缩机和两级轴向涡轮机的高压级。 燃烧器设置在核心压缩机和涡轮机之间。 另一组件包括通过第二轴联接到负载压缩机的轴向涡轮机的低压级。 高压涡轮级和冷却涡轮机的尺寸适于驱动核心压缩机和起动器/发电机，其在地面和机动车上提供所有飞机的电力需求。 低压涡轮机级驱动负载压缩机，其产生通过热交换部件调节的加压空气，然后在被输送到飞机机舱之前在冷却涡轮机上膨胀和冷却。