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公开(公告)号:WO2013180895A1
公开(公告)日:2013-12-05
申请号:PCT/US2013/039598
申请日:2013-05-04
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: CORSON, Michael, A.
CPC classification number: F01D25/24 , F01D21/045 , F05D2220/50 , F05D2250/11
Abstract: An exemplary containment structure includes an annular wall configured to receive a rotatable portion of a turbomachine. A plurality of apertures extend radially through the annular wall. The apertures have a varying circumferential width.
Abstract translation: 示例性的容纳结构包括被配置为容纳涡轮机的可旋转部分的环形壁。 多个孔径向延伸穿过环形壁。 孔具有变化的周向宽度。
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公开(公告)号:WO2013166103A1
公开(公告)日:2013-11-07
申请号:PCT/US2013/038999
申请日:2013-05-01
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: MIRONETS, Sergey , TWELVES, Wendell V. , KLUCHA, Agnes
CPC classification number: B22D27/04 , B22C9/065 , B22C9/22 , B22D23/06 , B22D25/02 , F01D25/30 , F04D29/522 , F05D2220/32 , F05D2230/21 , F05D2230/22
Abstract: A method of component forming according to an exemplary aspect of the present disclosure includes, among other things, positioning a metal powder in a mold cavity, melting the metal powder within the mold cavity, and cooling the melted metal powder to form a component.
Abstract translation: 根据本公开的示例性方面的部件形成方法包括将金属粉末定位在模具腔中,将金属粉末熔化在模腔内,以及冷却熔融的金属粉末以形成部件。
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公开(公告)号:WO2013154636A1
公开(公告)日:2013-10-17
申请号:PCT/US2013/021681
申请日:2013-01-16
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: SHERIDAN, William G. , MCCUNE, Michael E.
IPC: F02C7/36
CPC classification number: F02K3/06 , F01D25/168 , F02C7/36 , F04D29/522 , F05D2220/36 , F05D2260/40311
Abstract: A high-bypass ratio geared turbomachine according to an exemplary aspect of the present disclosure comprises a compressor section of a high-bypass ratio geared turbomachine, the compressor section providing at least a low-pressure compressor and a high-pressure compressor, wherein a rotor of the low-pressure compressor rotates together with a rotor of a fan. In a further non-limiting embodiment of any of the foregoing high-bypass ratio geared turbomachine embodiments, the rotor of the low pressure compressor and the rotor of the fan may rotate at the same speed and in the same direction. In a further non-limiting embodiment of any of the foregoing high-bypass ratio geared turbomachine embodiments, the high-bypass ratio geared turbomachine may have a fan bypass ratio greater than about 8.
Abstract translation: 根据本公开的示例性方面的高旁路比齿轮涡轮机包括高旁路比齿轮涡轮机的压缩机部分,压缩机部分至少提供低压压缩机和高压压缩机,其中转子 的低压压缩机与风扇的转子一起旋转。 在上述任何上述高旁路比齿轮涡轮机实施例的另一个非限制性实施例中,低压压缩机的转子和风扇的转子可以以相同的速度和相同的方向旋转。 在上述任何上述高旁路比齿轮涡轮机实施例的另一非限制性实施例中,高旁路比齿轮涡轮机可具有大于约8的风扇旁路比。
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公开(公告)号:WO2013130162A1
公开(公告)日:2013-09-06
申请号:PCT/US2012/068918
申请日:2012-12-11
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: RING, Mark David
IPC: F01D9/02
CPC classification number: F01D5/225 , F01D9/041 , F05D2250/31 , F05D2260/30 , F05D2260/37
Abstract: A stator vane assembly of a turbomachine according to an exemplary embodiment of the present disclosure includes, among other possible things, a shroud having a leading edge, a trailing edge, and at least one circumferential edge. The leading edge is circumferentially offset relative to the trailing edge when installed within the turbomachine. In a further embodiment of the foregoing stator vane assembly embodiment, the circumferential edge includes a portion that is aligned with an axis of the turbomachine. In a further embodiment of either of the foregoing stator vane embodiments, a vane extends radially from the shroud. In a further embodiment of any of the foregoing stator vane embodiments, the vane is a cantilevered vane.
Abstract translation: 根据本公开的示例性实施例的涡轮机的定子叶片组件除了其它可能的内容之外还包括具有前缘,后缘和至少一个周向边缘的护罩。 当安装在涡轮机内时,前缘相对于后缘周向地偏移。 在上述定子叶片组件实施例的另一实施例中,圆周边缘包括与涡轮机的轴线对准的部分。 在上述定子叶片实施例中的任一个的另一实施例中,叶片从护罩径向延伸。 在任何上述定子叶片实施例的另一实施例中,叶片是悬臂叶片。
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公开(公告)号:WO2013112331A1
公开(公告)日:2013-08-01
申请号:PCT/US2013/021690
申请日:2013-01-16
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: SHERIDAN, William, G. , MCCUNE, Michael, E.
IPC: B64D33/00
CPC classification number: F02C3/107 , F02C7/36 , F04D25/02 , F05D2260/4023
Abstract: An exemplary turbomachine clutch assembly includes a clutch that moves from a first position to a second position in response to rotation of a turbomachine fan at a speed greater than a threshold speed. The clutch permits rotation of the turbomachine fan in a first direction whether the clutch is in the first position or the second position. The clutch limits rotation of the turbomachine fan in an opposite, second direction when the clutch is in the first position.
Abstract translation: 示例性的涡轮机离合器组件包括离合器,其响应于涡轮机风扇以大于阈值速度的速度旋转而从第一位置移动到第二位置。 该离合器允许涡轮机风扇在第一方向上旋转,无论离合器是处于第一位置还是第二位置。 当离合器处于第一位置时,离合器限制涡轮机风扇在相反的第二方向上的旋转。
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公开(公告)号:WO2012134442A1
公开(公告)日:2012-10-04
申请号:PCT/US2011/030242
申请日:2011-03-29
Inventor: O'NEILL, Jonathan, Daniel , PATTERSON, JR., Timothy W.
CPC classification number: H01M8/0488 , G05F1/575 , H01M8/04589 , H01M8/0491 , H01M8/04952 , Y02E60/50
Abstract: An example method of controlling a fuel cell power plant based on provided power includes selectively varying an electrical resistance of the variable resistive device responsive to at least one of a power provided by the fuel cell power plant, a current provided by the fuel cell power plant, or a voltage decay rate.
Abstract translation: 基于提供的功率来控制燃料电池发电厂的示例性方法包括响应于由燃料电池发电厂提供的功率,由燃料电池发电厂提供的电流中的至少一个选择性地改变可变电阻装置的电阻 ,或电压衰减率。
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公开(公告)号:WO2012030324A1
公开(公告)日:2012-03-08
申请号:PCT/US2010/047202
申请日:2010-08-31
Applicant: UTC POWER CORPORATION , MITTAL, Vishal Onkarmal , DARLING, Robert Mason
Inventor: MITTAL, Vishal Onkarmal , DARLING, Robert Mason
CPC classification number: H01M8/04082 , H01M8/026 , H01M8/04097 , H01M8/04291 , H01M8/04753 , H01M8/1007 , Y02E60/50
Abstract: An example method of controlling fluid distribution within a fuel cell includes adjusting a flow of a reactant moving within a fuel cell to increase water within a portion of the fuel cell. Another example method of controlling fluid distribution within a fuel cell includes adjusting a flow of fuel entering a fuel cell, a velocity of air entering the fuel cell, or both, so that a first amount of water exiting the fuel cell in a fuel stream is about the same as a second amount of water exiting the fuel cell in an airstream.
Abstract translation: 控制燃料电池内的流体分配的示例性方法包括调节在燃料电池内移动的反应物的流动,以增加燃料电池的一部分内的水。 控制燃料电池内的流体分配的另一示例性方法包括调节进入燃料电池的燃料的流动,进入燃料电池的空气的速度或两者,使得在燃料流中离开燃料电池的第一量的水为 大约与在气流中离开燃料电池的第二量的水相同。
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18.
公开(公告)号:WO2009143415A1
公开(公告)日:2009-11-26
申请号:PCT/US2009/044962
申请日:2009-05-22
Applicant: CONTINENTAL AUTOMOTIVE SYSTEMS US, INC. , DOERR, Benjamin , KACHOUH, Patricia , OSTRANDER, Gerald , DESAI, Tejas, B. , REIMUS, David
Inventor: DOERR, Benjamin , KACHOUH, Patricia , OSTRANDER, Gerald , DESAI, Tejas, B. , REIMUS, David
CPC classification number: G07C9/00309 , B60R25/24 , G07C2209/63
Abstract: An example remote keyless entry locating method includes transmitting a signal from a fob to a first vehicle antenna and transmitting the signal from the fob to a second vehicle antenna. The example method further includes determining a position of the fob based on the signal. An example remote keyless entry locator system includes a transmitter configured to transmit a signal to a first vehicle antenna and a second vehicle antenna spaced from the first vehicle antenna. The system also includes a controller configured to determine a location of a fob relative to a vehicle. The controller uses a first distance between the first vehicle antenna and the transmitter, and uses a second distance between the second vehicle antenna and the transmitter, to determine the location.
Abstract translation: 遥控无钥匙进入定位方法的示例包括将信号从一个小物件发送到第一车辆天线,并将该信号从该货物信号发送到第二车辆天线。 该示例性方法还包括基于该信号来确定小窝的位置。 示例性远程无钥匙进入定位器系统包括被配置为向第一车辆天线发送信号的发射机和与第一车辆天线间隔开的第二车辆天线。 该系统还包括控制器,该控制器被配置为确定相对于车辆的货架的位置。 控制器使用第一车辆天线和发射机之间的第一距离,并且使用第二车辆天线和发射机之间的第二距离来确定位置。
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公开(公告)号:WO2008076133A1
公开(公告)日:2008-06-26
申请号:PCT/US2006/062467
申请日:2006-12-21
Applicant: UTC POWER CORPORATION , SKIBA, Tommy
Inventor: SKIBA, Tommy
CPC classification number: H01M8/04029 , F16K15/04 , F16K33/00 , F16K47/10 , H01M8/04059 , H01M8/04223 , H01M8/04228 , H01M8/04253 , H01M8/04303
Abstract: An exemplary valve device for controlling a flow of a fuel cell fluid includes a housing having a first opening and a second opening, and a flow control member within the housing. Flow in a first direction through the housing moves the flow control member to a first position near the first opening to restrict flow through the first opening. Flow in a second, opposite direction through the housing moves the flow control member to a second position to provide a second, greater flow through the first opening.
Abstract translation: 用于控制燃料电池流体流动的示例性阀装置包括具有第一开口和第二开口的壳体以及壳体内的流量控制构件。 通过壳体沿第一方向的流动使流动控制构件移动到第一开口附近的第一位置,以限制流过第一开口的流动。 通过壳体的相反方向的流动将流量控制构件移动到第二位置,以提供通过第一开口的第二,更大的流动。
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20.
公开(公告)号:WO2015175042A2
公开(公告)日:2015-11-19
申请号:PCT/US2015/015540
申请日:2015-02-12
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: ROMANOV, Dmitriy A. , PAULINO, Jose R. , BLANEY, Ken F.
CPC classification number: F01D11/08 , B22C9/10 , B22C9/24 , F01D11/24 , F05D2230/211 , F05D2240/11 , F05D2260/204 , F05D2260/22141 , F05D2300/13 , Y02T50/676
Abstract: A blade outer air seal according to an exemplary aspect of the present disclosure includes, among other things, a body to be distributed circumferentially about a blade array. The body has a plurality of grooves, which can, for example, improve the aerodynamic efficiency of a turbine. A fin is between a first groove and a second groove of the plurality of grooves. The fin extends radially from the body and terminates at a radially inner fin face that provides one or more cooling outlets.
Abstract translation: 根据本公开的示例性方面的叶片外部空气密封件尤其包括围绕叶片阵列周向分布的主体。 主体具有多个凹槽,其可以例如改善涡轮机的空气动力学效率。 翅片在多个凹槽的第一凹槽和第二凹槽之间。 翅片从主体径向延伸并且终止于提供一个或多个冷却出口的径向内部翅片面。
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