VENTILATION SYSTEM AND METHOD OF ASSEMBLY
    1.
    发明申请
    VENTILATION SYSTEM AND METHOD OF ASSEMBLY 有权
    通风系统和组装方法

    公开(公告)号:US20130115868A1

    公开(公告)日:2013-05-09

    申请号:US13288796

    申请日:2011-11-03

    IPC分类号: B64D13/00 B23P11/00

    摘要: A ventilation system for ventilating a passenger compartment of an aircraft is disclosed herein. The ventilation system includes, but is not limited to, a nozzle that is adapted to be mounted proximate an interior of the aircraft and that is configured to direct a stream of air into the passenger compartment. The ventilation system further includes a valve that is spaced apart from the nozzle and positioned upstream of the nozzle, the valve configured to control a flow of air to the nozzle. The ventilation system still further includes a conduit that fluidly couples the valve to the nozzle. The conduit is configured to convey the flow of air from the valve to the nozzle.

    摘要翻译: 本文公开了一种用于通风飞机乘客舱的通风系统。 通风系统包括但不限于适于安装在飞行器内部附近并且被配置成将空气流引导到乘客舱中的喷嘴。 通风系统还包括与喷嘴间隔开并定位在喷嘴上游的阀,阀构造成控制到喷嘴的空气流。 通风系统还包括将阀流体地连接到喷嘴的导管。 导管构造成将空气流从阀传送到喷嘴。

    Ventilation system and method of assembly
    2.
    发明授权
    Ventilation system and method of assembly 有权
    通风系统及组装方法

    公开(公告)号:US09550574B2

    公开(公告)日:2017-01-24

    申请号:US13288796

    申请日:2011-11-03

    IPC分类号: B64D13/00 B60H1/34

    摘要: A ventilation system for ventilating a passenger compartment of an aircraft is disclosed herein. The ventilation system includes, but is not limited to, a nozzle that is adapted to be mounted proximate an interior of the aircraft and that is configured to direct a stream of air into the passenger compartment. The ventilation system further includes a valve that is spaced apart from the nozzle and positioned upstream of the nozzle, the valve configured to control a flow of air to the nozzle. The ventilation system still further includes a conduit that fluidly couples the valve to the nozzle. The conduit is configured to convey the flow of air from the valve to the nozzle.

    摘要翻译: 本文公开了一种用于通风飞机乘客舱的通风系统。 通风系统包括但不限于适于安装在飞行器内部附近并且被配置成将空气流引导到乘客舱中的喷嘴。 通风系统还包括与喷嘴间隔开并定位在喷嘴上游的阀,阀构造成控制到喷嘴的空气流。 通风系统还包括将阀流体地连接到喷嘴的导管。 导管构造成将空气流从阀传送到喷嘴。