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    FUEL/OIL MANIFOLD
    2.
    发明申请
    FUEL/OIL MANIFOLD 审中-公开
    燃油/油管

    公开(公告)号：WO2015048374A1

    公开(公告)日：2015-04-02

    申请号：PCT/US2014/057593

    申请日：2014-09-26

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： BUTCHER, Evan ,  FISK, Benjamin, T. ,  TWELVES, Wendell, V. ,  OSWALD, Caitlin ,  TROUGHTON, Andre, Herman ,  CONWAY, Bryan, P.

    IPC: F16L9/18 ,  F28F1/00 ,  F02C7/22

    CPC classification number: F02C7/222 ,  B22F3/1055 ,  B22F5/10 ,  B33Y80/00 ,  F02C7/06 ,  F05D2230/31 ,  F16L41/03 ,  Y02P10/295

    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。

    A NONMETALLIC AIRFOIL WITH A COMPLIANT ATTACHMENT
    3.
    发明申请
    A NONMETALLIC AIRFOIL WITH A COMPLIANT ATTACHMENT 审中-公开

    公开(公告)号：WO2015047450A3

    公开(公告)日：2015-04-02

    申请号：PCT/US2014/034497

    申请日：2014-04-17

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： COOK, Grant, O. ,  FISK, Benjamin, T.

    IPC: F01D5/30 ,  F01D5/14 ,  F02C7/20

    Abstract: An airfoil is disclosed. The airfoil may comprise a body portion having a leading edge, a trailing edge, a pressure side, and a suction side. The airfoil may further comprise a compliant attachment bonded to the body portion and the compliant attachment may be configured to connect to a support structure. The compliant attachment may have a coefficient of thermal expansion intermediate between a coefficient of the thermal expansion of the body portion of the airfoil and a coefficient of thermal expansion of the support structure.

    FUEL/OIL MANIFOLD
    4.
    发明公开
    FUEL/OIL MANIFOLD 审中-公开
    燃油/机油歧管

    公开(公告)号：EP3049703A1

    公开(公告)日：2016-08-03

    申请号：EP14849740.7

    申请日：2014-09-26

    Applicant: United Technologies Corporation

    Inventor： BUTCHER, Evan ,  FISK, Benjamin, T. ,  TWELVES, Wendell, V. ,  OSWALD, Caitlin ,  TROUGHTON, Andre, Herman ,  CONWAY, Bryan, P.

    IPC: F16L9/18 ,  F28F1/00 ,  F02C7/22

    CPC classification number: F02C7/222 ,  B22F3/1055 ,  B22F5/10 ,  B33Y80/00 ,  F02C7/06 ,  F05D2230/31 ,  F16L41/03 ,  Y02P10/295

    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/油歧管包括第一歧管凸缘和第二歧管凸缘以及歧管。 第一歧管凸缘和第二歧管凸缘相对于彼此位于不平行的平面中。 歧管管在第一端连接到第一歧管凸缘并且在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转弯，其包括非零管弯曲半径，该弯曲半径被定义为比值 的转弯半径与歧管的直径之和。

    AIRFOIL INCLUDING LOOSE DAMPER
    6.
    发明公开
    AIRFOIL INCLUDING LOOSE DAMPER 有权
    包含松散阻尼器的机翼

    公开(公告)号：EP2841705A1

    公开(公告)日：2015-03-04

    申请号：EP13782220.1

    申请日：2013-04-20

    Applicant: United Technologies Corporation

    Inventor： FISK, Benjamin, T. ,  PROPHETER-HINCKLEY, Tracy, A. ,  HOUSTON, David, P. ,  TRACY, Anita, L.

    IPC: F01D5/12 ,  F01D5/18 ,  F02C7/00 ,  F02K3/00

    Abstract: An airfoil includes an airfoil body that has a leading edge and a trailing edge and a first sidewall and a second sidewall that is spaced apart from the first sidewall. The first sidewall and the second sidewall join the leading edge and the trailing edge and at least partially define a cavity in the airfoil body. A damper member is enclosed in the cavity and is loose within the cavity.

    Abstract translation: 翼型包括具有前缘和后缘以及第一侧壁和与第一侧壁间隔开的第二侧壁的翼型体。 第一侧壁和第二侧壁连接前缘和后缘并且至少部分地限定翼型体中的空腔。 阻尼器构件被封闭在空腔中并且在空腔内松动。

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