CONFORMAL SEAL
    11.
    发明申请
    CONFORMAL SEAL 有权
    一致密封

    公开(公告)号:US20160115811A1

    公开(公告)日:2016-04-28

    申请号:US14830771

    申请日:2015-08-20

    Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an adjacent second seal section, each including a base and two extending legs defining respective first and second ends of the seal. At least the first seal section includes a first plurality of slots extending from the first end to the base and a second plurality of slots extending from the second end to the base.

    Abstract translation: 本公开总体上涉及两个部件之间的滑动密封。 滑动密封件包括第一密封部分和相邻的第二密封部分,每个密封部分包括基部和限定密封件的相应的第一和第二端的两个延伸的腿。 至少第一密封部分包括从第一端部延伸到基部的第一多个狭槽以及从第二端部延伸到基部的第二多个槽。

    HINGED SEAL
    12.
    发明申请
    HINGED SEAL 有权
    铰链密封

    公开(公告)号:US20160115808A1

    公开(公告)日:2016-04-28

    申请号:US14830665

    申请日:2015-08-19

    Inventor: Timothy M. Davis

    Abstract: The present disclosure relates generally to a seal between two components. The seal includes a first substantially frustoconical seal section including a first seal section radially outer end and a first seal section radially inner end. The seal also includes a second substantially frustoconical seal section including a second seal section radially outer end and a second seal section radially inner end, wherein the second seal section radially inner end is supported by the first seal section radially inner end to create a hinge joint allowing an angle defined between the first and second seal sections to change.

    Abstract translation: 本公开一般涉及两个部件之间的密封。 密封件包括第一基本截头圆锥形密封部分,其包括第一密封部分径向外端和第一密封部分径向内端。 密封件还包括第二基本截头圆锥形密封部分,其包括第二密封部分径向外端和第二密封部径向内端,其中第二密封部径向内端由第一密封部径向内端支撑以形成铰链接头 允许在第一和第二密封部分之间限定的角度改变。

    GAS TURBINE ENGINE RAMPED RAPID RESPONSE CLEARANCE CONTROL SYSTEM

    公开(公告)号:US20200025020A1

    公开(公告)日:2020-01-23

    申请号:US16399254

    申请日:2019-04-30

    Abstract: An active clearance control system of a gas turbine engine includes a multiple of blade outer air seal assemblies and a multiple of rotary ramps. Each of the multiple of rotary ramps is associated with one of the multiple of blade outer air seal assemblies. A method of active blade tip clearance control for a gas turbine engine is provided. The method includes rotating a multiple of rotary ramps to control a continuously adjustable radial position for each of a respective multiple of blade outer air seal assemblies.

    Bifurcated sliding seal
    19.
    发明授权

    公开(公告)号:US10344609B2

    公开(公告)日:2019-07-09

    申请号:US14830689

    申请日:2015-08-19

    Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the first seal section and/or the second seal section, are disposed between the first and second seal sections, and bias the first and second seal sections away from one another.

    SLIDING SEAL
    20.
    发明申请
    SLIDING SEAL 审中-公开

    公开(公告)号:US20190170007A1

    公开(公告)日:2019-06-06

    申请号:US16271323

    申请日:2019-02-08

    Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section, a second seal section, and (in some embodiments) a third seal section. Two or three of the seal sections are uncoupled, which allows the uncoupled seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the second seal section and bias the first and third (or in some embodiments, the first and second) seal sections away from one another.

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