FUEL/OIL MANIFOLD
    1.
    发明申请
    FUEL/OIL MANIFOLD 审中-公开
    燃油/油管

    公开(公告)号:US20160208708A1

    公开(公告)日:2016-07-21

    申请号:US15022653

    申请日:2014-09-26

    Abstract: A fuel/oil manifold includes first and second manifold flanges and a manifold tube. The first and second manifold flanges are located in non-parallel planes with respect to one another. The manifold tube is connected at a first end to the first manifold flange and at a second end to the second manifold flange and includes at least one turn between the first and the second end that includes a non-zero tube bend radius defined as the ratio of a turn radius to a diameter of the manifold tube.

    Abstract translation: 燃料/油歧管包括第一和第二歧管凸缘和歧管管。 第一和第二歧管凸缘相对于彼此位于非平行平面中。 歧管在第一端连接到第一歧管凸缘,第二端连接到第二歧管凸缘,并且包括在第一和第二端之间的至少一个匝,其包括非零管弯曲半径,其定义为比率 的转弯半径相对于歧管管的直径。

    SEAL PLATE WITH FLUID BYPASS CONTROL
    7.
    发明申请
    SEAL PLATE WITH FLUID BYPASS CONTROL 审中-公开
    具有流体旁路控制的密封板

    公开(公告)号:US20160356220A1

    公开(公告)日:2016-12-08

    申请号:US14623309

    申请日:2015-02-16

    Abstract: The present disclosure relates generally to a manifold including a plurality of manifold channels disposed therethrough, each manifold channel including a manifold channel opening, and a seal plate, including a plurality of seal plate apertures disposed thereon, operably coupled to the manifold, wherein the seal plate includes at least one seal plate channel extending between at least two of the plurality of seal plate apertures.

    Abstract translation: 本公开总体上涉及一种包括多个歧管通道的歧管,每个歧管通道设置在其中,每个歧管通道包括歧管通道开口和密封板,密封板包括可操作地联接到歧管的多个密封板孔,其中密封件 板包括在多个密封板孔中的至少两个之间延伸的至少一个密封板通道。

    Retention assembly for gas turbine engine

    公开(公告)号:US11111821B2

    公开(公告)日:2021-09-07

    申请号:US16574562

    申请日:2019-09-18

    Abstract: A retention assembly for a gas turbine engine is provided. The retention assembly may include a bolt, a spacer, a housing, a fitting component, and a conduit assembly. The housing may define at least one receiving aperture sized to receive a second portion of the shaft. The fitting component may define a first through-hole and a second through-hole sized for a first portion of the shaft and the second portion of the shaft to extend therethrough. The conduit assembly may include a conduit for securing to the fitting component such that the first through-hole is open to the conduit. The bolt, the spacer, the fitting component, and the housing may be arranged with one another to define a captive clearance fit such that a first clearance space is defined between a first surface of the second through-hole and the first portion of the bolt.

    RETENTION ASSEMBLY FOR GAS TURBINE ENGINE

    公开(公告)号:US20210079812A1

    公开(公告)日:2021-03-18

    申请号:US16574562

    申请日:2019-09-18

    Abstract: A retention assembly for a gas turbine engine is provided. The retention assembly may include a bolt, a spacer, a housing, a fitting component, and a conduit assembly. The housing may define at least one receiving aperture sized to receive a second portion of the shaft. The fitting component may define a first through-hole and a second through-hole sized for a first portion of the shaft and the second portion of the shaft to extend therethrough. The conduit assembly may include a conduit for securing to the fitting component such that the first through-hole is open to the conduit. The bolt, the spacer, the fitting component, and the housing may be arranged with one another to define a captive clearance fit such that a first clearance space is defined between a first surface of the second through-hole and the first portion of the bolt.

Patent Agency Ranking