CABIN BLOWER SYSTEM
    1.
    发明申请

    公开(公告)号:US20230132101A1

    公开(公告)日:2023-04-27

    申请号:US18045857

    申请日:2022-10-12

    申请人: ROLLS-ROYCE plc

    IPC分类号: B64D13/06 F02C7/36 F02C7/32

    摘要: A cabin blower system, for an aircraft, comprising: a cabin blower compressor, for compressing air for delivery to a cabin of an aircraft, comprising a compressor drive shaft running on a contactless bearing system; and a transmission comprising an input and an output, the input being arranged to receive power from an engine of the aircraft and the output being arranged to mechanically drive the cabin blower compressor, wherein the output of the transmission is mechanically coupled with the compressor drive shaft via a flexible drive coupling.

    ROTARY ASSEMBLY
    2.
    发明公开
    ROTARY ASSEMBLY 审中-公开

    公开(公告)号:US20240151154A1

    公开(公告)日:2024-05-09

    申请号:US18379976

    申请日:2023-10-13

    申请人: ROLLS-ROYCE plc

    IPC分类号: F01D17/16

    摘要: A rotary assembly for driving spool rotation includes a rotor and a flow modifier. The rotor is mechanically coupled to a spool of a gas turbine engine. The flow modifier receives flow from and/or direct flow to the rotor. The rotary assembly permits relative movement between the rotor and the flow modifier to move between: a turbine configuration wherein the rotor receives air from an external air source to drive the spool to rotate; and a compressor configuration wherein the rotor is driven to rotate by the spool and to receive and compress air from the gas turbine engine, and discharge the compressed air for supply to the airframe system. The rotary assembly also includes controller to control relative movement between the rotor and the flow modifier through a range of turbine positions of the turbine configuration to vary a torque applied to the rotor for driving the spool.