ARRANGEMENT OF DAMS IN AIR DATA PROBE
    2.
    发明申请

    公开(公告)号:US20190041421A1

    公开(公告)日:2019-02-07

    申请号:US16158793

    申请日:2018-10-12

    Abstract: An air data probe is provided. The air data probe includes a pitot probe having a mounting base or flange, support strut, and tube with a forward facing inlet that is configured to capture a total pressure of the surrounding air, at least three dams placed within the tube of the pitot probe for blocking the ballistic trajectory of water droplets or ice crystals from passing directly through the tube to a downstream pressure sensing element, and a heater element integrated into the tube of the pitot probe on the outside of the dams. The at least three dams are oriented within the tube of the pitot probe in such a way that the dam locations are configured for two or more installations of the air data probe.

    ARRANGEMENT OF DAMS IN AIR DATA PROBE
    5.
    发明申请

    公开(公告)号:US20180259548A1

    公开(公告)日:2018-09-13

    申请号:US15457912

    申请日:2017-03-13

    CPC classification number: G01P5/165

    Abstract: An air data probe is provided. The air data probe includes a pitot probe having a mounting base or flange, support strut, and tube with a forward facing inlet that is configured to capture a total pressure of the surrounding air, at least three dams placed within the tube of the pitot probe for blocking the ballistic trajectory of water droplets or ice crystals from passing directly through the tube to a downstream pressure sensing element, and a heater element integrated into the tube of the pitot probe on the outside of the dams. The at least three dams are oriented within the tube of the pitot probe in such a way that the dam locations are configured for two or more installations of the air data probe.

    Arrangement of dams in air data probe

    公开(公告)号:US10126320B2

    公开(公告)日:2018-11-13

    申请号:US15457912

    申请日:2017-03-13

    Abstract: An air data probe is provided. The air data probe includes a pitot probe having a mounting base or flange, support strut, and tube with a forward facing inlet that is configured to capture a total pressure of the surrounding air, at least three dams placed within the tube of the pitot probe for blocking the ballistic trajectory of water droplets or ice crystals from passing directly through the tube to a downstream pressure sensing element, and a heater element integrated into the tube of the pitot probe on the outside of the dams. The at least three dams are oriented within the tube of the pitot probe in such a way that the dam locations are configured for two or more installations of the air data probe.

    Auxiliary power unit inlet door having openings formed therein
    7.
    发明授权
    Auxiliary power unit inlet door having openings formed therein 有权
    辅助动力单元入口门,其中形成有开口

    公开(公告)号:US09145214B2

    公开(公告)日:2015-09-29

    申请号:US14063324

    申请日:2013-10-25

    Abstract: An inlet door system includes a duct, an inlet door, and a plurality of openings. The duct is configured to extend from the auxiliary power unit (APU) to an intake opening formed in an outer surface of an aircraft. The duct includes an inlet port, an outlet port, and a duct sidewall extending between the inlet port and the outlet port. The inlet door includes an inner surface, an outer surface, and an outer peripheral edge between the inner and outer surfaces. The door is rotationally coupled to the duct, and is configured to selectively rotate between a closed position and a plurality of open positions. The openings extend through the inlet door between the inner surface and outer surface, and each opening is disposed adjacent to the outer peripheral edge.

    Abstract translation: 入口门系统包括管道,入口门和多个开口。 管道构造成从辅助动力单元(APU)延伸到形成在飞行器的外表面中的进气口。 管道包括入口,出口和在入口和出口之间延伸的管道侧壁。 入口门包括内表面,外表面和内表面和外表面之间的外周边缘。 门旋转地联接到管道,并且构造成选择性地在关闭位置和多个打开位置之间旋转。 开口在内表面和外表面之间延伸穿过入口门,并且每个开口邻近外围边缘设置。

    AUXILIARY POWER UNIT INLET DOOR HAVING OPENINGS FORMED THEREIN
    8.
    发明申请
    AUXILIARY POWER UNIT INLET DOOR HAVING OPENINGS FORMED THEREIN 有权
    辅助动力单元入口门具有形成的开口

    公开(公告)号:US20150115099A1

    公开(公告)日:2015-04-30

    申请号:US14063324

    申请日:2013-10-25

    Abstract: An inlet door system includes a duct, an inlet door, and a plurality of openings. The duct is configured to extend from the auxiliary power unit (APU) to an intake opening formed in an outer surface of an aircraft. The duct includes an inlet port, an outlet port, and a duct sidewall extending between the inlet port and the outlet port. The inlet door includes an inner surface, an outer surface, and an outer peripheral edge between the inner and outer surfaces. The door is rotationally coupled to the duct, and is configured to selectively rotate between a closed position and a plurality of open positions. The openings extend through the inlet door between the inner surface and outer surface, and each opening is disposed adjacent to the outer peripheral edge.

    Abstract translation: 入口门系统包括管道,入口门和多个开口。 管道构造成从辅助动力单元(APU)延伸到形成在飞行器的外表面中的进气口。 管道包括入口,出口和在入口和出口之间延伸的管道侧壁。 入口门包括内表面,外表面和内表面和外表面之间的外周边缘。 门旋转地联接到管道,并且构造成选择性地在关闭位置和多个打开位置之间旋转。 开口在内表面和外表面之间延伸穿过入口门,并且每个开口邻近外围边缘设置。

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