专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

71. 发明申请

WO2014168743A1 INTEGRALLY BLADED ROTOR 审中-公开
标题翻译：整体叶片转子
公开(公告)号：WO2014168743A1
公开(公告)日：2014-10-16
申请号：PCT/US2014/031163
申请日：2014-03-19
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： AIELLO, Nicholas
IPC分类号： F01D5/02 , F01D11/00 , F02C7/20 , F02C7/28 , F02C7/04
CPC分类号： F01D11/006 , F01D5/02 , F01D5/3007 , F01D5/34 , F04D29/322 , F04D29/329 , F05D2220/32 , F05D2240/20 , F05D2240/55 , F05D2260/941 , Y02T50/671
摘要： An integrally bladed rotor for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a radially inner hoop extending circumferentially about an axis, a plurality of circumferentially spaced, axially extending slots, separated by respective blade supports, and a seal system that includes seal fingers extending axially through the slots.
摘要翻译：根据本公开的示例性方面的用于燃气涡轮发动机的整体叶片转子包括径向内环，其围绕轴线周向延伸，多个沿周向间隔开的轴向延伸的槽，由相应的叶片支撑件分开，以及密封系统，其包括轴向延伸穿过狭槽的密封指。

72. 发明申请

WO2014137577A1 RING-SHAPED COMPLIANT SUPPORT 审中-公开
标题翻译：环形合规支持
公开(公告)号：WO2014137577A1
公开(公告)日：2014-09-12
申请号：PCT/US2014/016761
申请日：2014-02-18
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： ROMANOV, Dmitriy A.
IPC分类号： F01D11/08 , F01D25/24 , F02C7/28
CPC分类号： F01D11/16 , F01D11/18 , F01D25/14 , F01D25/24 , F01D25/243 , F01D25/246 , F01D25/26 , F01D25/265 , F01D25/28 , F05D2220/32 , F05D2240/10 , F05D2240/20 , F05D2240/55 , Y02T50/675
摘要： A ring-shaped compliant support for a gas turbine engine includes, among other things, an annular case, and an adjustment member that will turn relative to the annular case if exposed to thermal energy.
摘要翻译：用于燃气涡轮发动机的环形适应支撑件尤其包括环形壳体和调节构件，其如果暴露于热能则相对于环形壳体转动。

73. 发明申请

WO2014133706A1 EDGE TREATMENT FOR GAS TURBINE ENGINE COMPONENT 审中-公开
标题翻译：气体涡轮发动机部件的边缘处理
公开(公告)号：WO2014133706A1
公开(公告)日：2014-09-04
申请号：PCT/US2014/013792
申请日：2014-01-30
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： FARRIS, John R. , STROCK, Christopher W. , LUTJEN, Paul M.
IPC分类号： F01D5/02 , F01D5/00 , F02C7/00
CPC分类号： F01D11/24 , F01D5/14 , F01D9/023 , F05D2240/11 , F05D2250/00 , F05D2250/182 , F05D2250/294
摘要： A gas turbine engine component according to an exemplary aspect of the present disclosure includes, among other things, a body having a first outer face meeting a second outer face at an intersection, the body having a plurality of apertures extending from an opening in the first outer face to an opening on the second outer face; and a coating filling at least a portion of the plurality of apertures.
摘要翻译：根据本公开的示例性方面的燃气涡轮发动机部件尤其包括具有在交叉点处与第二外表面相交的第一外表面的本体，该主体具有从第一外表面到第二外表面上的开口; 以及填充所述多个孔的至少一部分的涂层。

74. 发明申请

WO2014126696A1 GAS TURBINE ENGINE GEARED ARCHITECTURE 审中-公开
标题翻译：气体涡轮发动机齿轮架构
公开(公告)号：WO2014126696A1
公开(公告)日：2014-08-21
申请号：PCT/US2014/012957
申请日：2014-01-24
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： ROBERGE, Gary D.
IPC分类号： F02C7/36 , F01D25/00
CPC分类号： F02C7/36 , F02C3/073
摘要： A gas turbine engine assembly according to an exemplary aspect of the present disclosure includes, among other things, a geared architecture configured to rotatably couple a turbine and a compressor of an engine to rotate the compressor at a different speed than the turbine and a fan.
摘要翻译：根据本公开的示例性方面的燃气涡轮发动机组件包括构造成可旋转地连接发动机的涡轮机和压缩机的齿轮架构，其以与涡轮机和风扇不同的速度旋转压缩机。

75. 发明申请

WO2014052061A1 TURBOMACHINE THRUST REVERSER 审中-公开
公开(公告)号：WO2014052061A1
公开(公告)日：2014-04-03
申请号：PCT/US2013/059878
申请日：2013-09-16
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： GUKEISEN, Robert L. , MERCIER, Claude , MALECKI, Robert E.
IPC分类号： F02K1/62 , B64D33/04
CPC分类号： F02K1/58 , B64D29/06 , F02C7/20 , F02K1/64 , F05D2250/34
摘要： An example thrust reverser of a gas turbine engine is configured to connect to an aircraft wing via a pylon via one or more thrust reverser mounts located adjacent to a top circumferential apex of the engine according to an exemplary aspect of the present disclosure includes, among other things, a first cowl moveable between a stowed position and a deployed position relative to a second cowl. The first cowl in the deployed position configured to permit thrust to be redirected from an engine to slow the engine. The first cowl forming a portion of a substantially annular encasement of the engine. The first cowl directly interfaces with second cowl of the encasement at a cowl interface position that is more than 18 degrees circumferentially offset from the top circumferential apex when the first cowl is in the stowed position.
摘要翻译：燃气涡轮发动机的示例推力反向器被构造成根据本公开的示例性方面经由经由一个或多个相对于发动机的顶部圆周顶点定位的一个或多个推力反向器安装座经由塔架连接到飞机机翼，事物，第一整流罩可相对于第二整流罩在收起位置和展开位置之间移动。在展开位置的第一个整流罩配置成允许从发动机重新引导推力以减慢发动机。第一整流罩形成发动机的大致环形的壳体的一部分。当第一整流罩处于收起位置时，第一整流罩直接与外壳的第二整流罩接合在整流罩接口位置，该顶盖接口位置与顶部圆周顶点周向偏移大于18度。

76. 发明申请

WO2014052039A1 TURBOMACHINE ROTOR GROOVE 审中-公开
标题翻译：涡轮转子槽
公开(公告)号：WO2014052039A1
公开(公告)日：2014-04-03
申请号：PCT/US2013/059597
申请日：2013-09-13
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： AIELLO, Nicholas , MALI, Raji
IPC分类号： F01D5/30 , F02C7/00 , F02K3/00
CPC分类号： F01D5/3038 , Y10T29/49332
摘要： An example turbomachine rotor provides a groove that is annular and is configured to receive a root of an airfoil, the groove having a radial cross-sectional area. A ratio of the radial cross-sectional area of the groove to a radial cross-sectional area of the root received within the annular groove is from 2 to 5.
摘要翻译：涡轮机转子的一个实例提供了一个环形槽，并被构造为容纳翼型的根部，该槽具有径向横截面积。槽的径向横截面积与在环形槽内容纳的根部的径向横截面积的比为2〜5。

77. 发明申请

WO2014051657A1 TURBOMACHINE BEARING SUPPORT STRUCTURE 审中-公开
标题翻译：涡轮轴承支撑结构
公开(公告)号：WO2014051657A1
公开(公告)日：2014-04-03
申请号：PCT/US2013/022011
申请日：2013-01-18
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： AMADOR, Armando , MCCUTCHAN, Sean
IPC分类号： F01D25/16
CPC分类号： F16C27/00 , F01D25/164 , F16C19/06 , F16C27/04 , F16C27/045 , F16C2360/23
摘要： A centering spring assembly of a turbomachine according to an exemplary aspect of the present disclosure includes, among other things, a damper beam, a bearing support, and a spanner nut. At least a portion of the damper beam axially overlaps at least a portion of the spanner nut relative to a rotational axis of the turbomachine.
摘要翻译：根据本公开的示例性方面的涡轮机的定心弹簧组件尤其包括阻尼器梁，轴承支撑件和扳手螺母。阻尼器梁的至少一部分相对于涡轮机的旋转轴线轴向重叠至少一部分扳手螺母。

78. 发明申请

WO2014008005A1 TURBOMACHINE THERMAL ENERGY EXCHANGE 审中-公开
标题翻译：涡轮机热能交换
公开(公告)号：WO2014008005A1
公开(公告)日：2014-01-09
申请号：PCT/US2013/046962
申请日：2013-06-21
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： WINTER, Michael
IPC分类号： F02C7/00 , F02C9/00 , F02C7/12
CPC分类号： F02C3/30 , F02C7/18 , F02C7/185 , F05D2260/212 , F05D2260/213 , Y02T50/675
摘要： An example method of thermal energy exchange within a turbomachine includes heating a liquid using thermal energy from compressed air, injecting the liquid into a first portion of a turbomachine, and using the compressed air to cool a second portion of the turbomachine.
摘要翻译：在涡轮机内的热能交换的一个示例性方法包括使用来自压缩空气的热能加热液体，将液体注入涡轮机的第一部分，并使用压缩空气来冷却涡轮机的第二部分。

79. 发明申请

WO2013180928A1 RETAINING RING REMOVAL TOOL 审中-公开
标题翻译：保持环拆卸工具
公开(公告)号：WO2013180928A1
公开(公告)日：2013-12-05
申请号：PCT/US2013/040507
申请日：2013-05-10
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： MARIANO, Thomas A. , JUH, Christopher M. , VEZZETTI, Ronnie J.S.
IPC分类号： B25B27/20 , B25B27/02 , B25B27/14
CPC分类号： B25B27/28 , F01D25/285 , Y10T29/49815 , Y10T29/49824 , Y10T29/53 , Y10T29/53613 , Y10T29/53996
摘要： An example retaining ring removal tool includes a shaft extending along an axis from a first end to a second end, and at least one tapered tab extending axially from the first end of the shaft at a radially outer perimeter of the shaft.
摘要翻译：示例性保持环拆除工具包括沿轴线从第一端延伸到第二端的轴，以及在轴的径向外周缘处从轴的第一端轴向延伸的至少一个锥形突出部。

80. 发明申请

WO2013173097A1 COMPONENT FINISHING METHOD AND ASSEMBLY 审中-公开
标题翻译：组件整理方法和组装
公开(公告)号：WO2013173097A1
公开(公告)日：2013-11-21
申请号：PCT/US2013/039595
申请日：2013-05-04
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： RIZZO, JR., John P.
IPC分类号： C25F3/00 , C25F3/16
CPC分类号： B23K26/00 , B23K26/1224 , B23K26/361 , B23K2201/001 , C25F3/16 , Y10T428/12993 , Y10T428/24355
摘要： An example component finishing method includes immersing a surface of a component within a fluid during a finishing process. The method heats fluid near the surface during the finishing to create a convection current within the fluid that carries a byproduct of the finishing away from the surface.
摘要翻译：示例性部件整理方法包括在精加工过程中将部件的表面浸入流体内。该方法在精加工期间加热表面附近的流体，以在流体内产生对流，该流体将整理的副产物远离表面。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式