-
公开(公告)号：WO2013123172A1
公开(公告)日：2013-08-22
申请号：PCT/US2013/026117
申请日：2013-02-14
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： MCCAFFREY, Michael G.
CPC classification number: F01D11/20 , F01D11/22 , F01D25/24 , F02C3/04 , F02C7/28 , F05D2220/32 , F05D2240/11 , F05D2240/35 , F05D2240/55 , Y10T29/49318
Abstract: An adjustable blade outer air seal apparatus includes a case structure that extends circumferentially, a support ring structure mounted radially inwards of the case structure and at least one blade outer air seal segment radially adjustably mounted relative to the support ring structure.
Abstract translation: 可调节叶片外部空气密封装置包括沿圆周延伸的壳体结构，安装在壳体结构的径向内侧的支撑环结构和至少一个叶片外部空气密封段，其相对于支撑环结构径向可调节地安装。
-
公开(公告)号：WO2015023576A1
公开(公告)日：2015-02-19
申请号：PCT/US2014/050508
申请日：2014-08-11
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： CHANG, Hoyt Y. , MCCAFFREY, Michael G.
CPC classification number: F23R3/002 , F01D11/08 , F02C7/24 , F02K1/822 , F05D2220/32 , F05D2230/60 , F05D2240/11 , F05D2240/35 , F05D2300/6033 , F23M5/04 , F23R3/007 , F23R3/60 , F23R2900/00017 , Y02T50/672
Abstract: One exemplary embodiment of this disclosure relates to a gas turbine engine including a plate, a frame attached to the plate, and a panel. The panel is supported by the frame.
Abstract translation: 本公开的一个示例性实施例涉及一种燃气涡轮发动机，其包括板，附接到板的框架和面板。 框架支持面板。
-
公开(公告)号：WO2015009388A1
公开(公告)日：2015-01-22
申请号：PCT/US2014/042848
申请日：2014-06-18
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： COOK III, Grant O. , ABBOTT, Michael G. , MCCAFFREY, Michael G.
CPC classification number: F23R3/007 , C09J5/00 , C09J2400/123 , C09J2400/163 , F01D5/284 , F01D9/02 , F01D25/246 , F05D2230/236 , F05D2230/642 , F05D2240/11 , F23R3/002 , F23R3/60 , F23R2900/00005 , F23R2900/00017 , Y02T50/672
Abstract: A gas turbine engine component assembly includes a ceramic component having a first thermal characteristic. A metallic component has a second thermal characteristic. A bonding material secures the ceramic component to the metallic component. The bonding material includes at least one of a transient liquid phase bond and a partial transient liquid phase bond. The bonding material is configured to withstand a shear stress parameter relating to a differential between the first and second thermal characteristics.
Abstract translation: 燃气涡轮发动机部件组件包括具有第一热特性的陶瓷部件。 金属部件具有第二热特性。 粘结材料将陶瓷组分固定在金属组分上。 接合材料包括瞬态液相和部分瞬态液相键中的至少一种。 接合材料被配置为承受与第一和第二热特性之间的差异相关的剪切应力参数。
-
公开(公告)号：WO2015009386A1
公开(公告)日：2015-01-22
申请号：PCT/US2014/042744
申请日：2014-06-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： COOK, Grant O. III , ABBOTT, Michael G. , MCCAFFREY, Michael G.
CPC classification number: F01D5/284 , F01D5/282 , F01D9/042 , F01D9/044 , F05D2230/23 , F05D2230/236 , F05D2300/6033 , Y02T50/672
Abstract: A gas turbine engine component assembly includes first and second portions, wherein at least one of the first and second portions is a ceramic material. The first portion includes an aperture having a first angled surface. The second portion is disposed within the aperture and includes a second angled surface adjacent to the first angled surface. The first and second angled surfaces lock the first and second portions to one another under a pulling load. A bonding material operatively secures the first and second angled surfaces to one another.
Abstract translation: 燃气涡轮发动机部件组件包括第一和第二部分，其中第一和第二部分中的至少一个是陶瓷材料。 第一部分包括具有第一倾斜表面的孔。 第二部分设置在孔内并且包括与第一倾斜表面相邻的第二倾斜表面。 第一和第二倾斜表面在牵引载荷下将第一和第二部分彼此锁定。 接合材料将第一和第二倾斜表面相互操作地固定。
-
公开(公告)号：WO2014189590A2
公开(公告)日：2014-11-27
申请号：PCT/US2014/020468
申请日：2014-03-05
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： MCCAFFREY, Michael G. , BORJA, Mark , ROUSE, Brandon T. , FARRIS, John R. , PELLETIER, Brian R. , ALMY, Thomas , GARCIA, Igor S.
CPC classification number: F01D11/18 , F01D5/02 , F01D11/22 , F01D11/24 , F01D25/24 , F05D2220/32 , F05D2240/55 , F05D2270/52 , F05D2270/62
Abstract: A control ring extends circumferentially about a central axis. A plurality of circumferentially spaced carrier portions have a cavity receiving the control ring. There are circumferential gaps between the carrier portions. A blade outer air seal is mounted on the carrier portions radially inwardly of the control ring. The control ring maintains the carrier portions at a radially outwardly expanded position when heated by an electric heater.
Abstract translation: 控制环围绕中心轴线周向延伸。 多个周向间隔的载体部分具有容纳控制环的空腔。 载体部分之间有圆周间隙。 叶片外部空气密封件安装在控制环径向向内的托架部分上。 当通过电加热器加热时，控制环将承载部分保持在径向向外扩展的位置。
-
Patent Agency Ranking
公开(公告)号：WO2014113039A1
公开(公告)日：2014-07-24
申请号：PCT/US2013/022411
申请日：2013-01-21
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： MCCAFFREY, Michael G. , SURACE, Raymond , PROPHETER-HINCKLEY, Tracy A.
IPC: F01D17/16
CPC classification number: F01D17/162 , F01D5/145 , F01D5/187
Abstract: An adjustable stator vane for a turbine engine includes a shaft, a flange and a stator vane body that pivots about a variable vane axis. The stator vane body extends axially between a first end and a second end. The stator vane body includes an airfoil, a cavity, and a body surface located at the first end. The cavity extends axially from an inlet in the body surface and into the airfoil. The shaft extends along the variable vane axis from the first end. The flange extends circumferentially around the inlet and the shaft, and radially from the stator vane body.
Abstract translation: 用于涡轮发动机的可调节定子叶片包括轴，凸缘和绕可变叶片轴线枢转的定子叶片体。 定子叶片体在第一端和第二端之间轴向延伸。 定子叶片主体包括翼型件，空腔和位于第一端的主体表面。 空腔从体表中的入口轴向延伸到翼型中。 轴从第一端沿着可变叶片轴线延伸。 凸缘围绕入口和轴周向延伸，并且从定子叶片体径向延伸。
-
公开(公告)号：WO2014014598A1
公开(公告)日：2014-01-23
申请号：PCT/US2013/046270
申请日：2013-06-18
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： MCCAFFREY, Michael G.
CPC classification number: F01D11/16 , F01D11/18 , Y02T50/672
Abstract: A radial position control assembly for a gas turbine engine stage includes a case structure. A supported structure is operatively supported by the case structure. The supported structure includes a hook providing an annular recess. A support ring is received in the recess. The supported structure and the support ring have different coefficients of thermal expansion. A sealing structure is adjacent to the supported structure. The support ring maintains the supported structure relative to the sealing structure at a clearance during thermal transients based upon a circumferential gap between adjacent supported structure and based upon a radial gap between the support ring and the supported structure.
Abstract translation: 用于燃气涡轮发动机级的径向位置控制组件包括壳体结构。 支撑结构由壳体结构可操作地支撑。 支撑结构包括提供环形凹部的钩。 一个支撑环被容纳在凹槽中。 支撑结构和支撑环具有不同的热膨胀系数。 密封结构与支撑结构相邻。 基于相邻的支撑结构之间的周向间隙，并且基于支撑环和支撑结构之间的径向间隙，支撑环在热瞬变期间的间隙处相对于密封结构保持支撑结构。
-
公开(公告)号：WO2015109292A1
公开(公告)日：2015-07-23
申请号：PCT/US2015/011963
申请日：2015-01-20
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： MCCAFFREY, Michael G.
IPC: F01D11/08
CPC classification number: F01D11/08 , F01D5/02 , F01D25/24 , F01D25/246 , F02C3/04 , F04D29/164 , F04D29/321 , F04D29/526 , F05D2220/32 , F05D2240/11 , F05D2240/35 , F05D2260/30 , F05D2300/6033 , Y02T50/672
Abstract: One exemplary embodiment of this disclosure relates to a system having a static segment with a circumferentially extending slot. The system further includes a retention clip partially received in the slot, and partially contacting a circumferential end of the static segment.
Abstract translation: 本公开的一个示例性实施例涉及具有带有周向延伸槽的静态段的系统。 所述系统还包括部分地容纳在所述槽中并且部分接触所述静态段的圆周端的保持夹。
-
公开(公告)号：WO2015069673A1
公开(公告)日：2015-05-14
申请号：PCT/US2014/063977
申请日：2014-11-05
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： MCCAFFREY, Michael G. , ALVANOS, Ioannis , ABBOTT, Michael G. , COOK, III, Grant O.
CPC classification number: F01D5/147 , F01D5/18 , F01D5/282 , F01D5/284 , F01D5/326 , F02C3/04 , F02C7/12 , F05D2220/32 , F05D2230/236 , F05D2230/51 , F05D2240/11 , F05D2240/12 , F05D2300/6033 , Y02T50/672
Abstract: An airfoil component includes a first segment that has a first piece of a mount and a first piece of an airfoil. The first segment is formed of a first ceramic-based material. A second segment includes a second piece of the mount and a second piece of the airfoil. The second segment is formed of a second ceramic-based material. The first and second segments are bonded together along a bond joint such that the first and second pieces of the mount are bonded to each other and the first and second pieces of the airfoil are bonded to each other.
Abstract translation: 机翼部件包括具有第一安装座和第一翼片的第一段。 第一段由第一陶瓷基材料形成。 第二段包括第二段安装件和第二段翼型件。 第二段由第二陶瓷基材料形成。 第一和第二段沿着接合接头结合在一起，使得第一和第二安装件彼此接合并且第一和第二翼片彼此接合。
-
公开(公告)号：WO2015057326A2
公开(公告)日：2015-04-23
申请号：PCT/US2014/055327
申请日：2014-09-12
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： MCCAFFREY, Michael G. , BERCZIK, Douglas M.
CPC classification number: C04B38/0615 , B05D3/007 , C04B35/573 , C04B35/6267 , C04B35/806 , C04B41/89 , C04B2235/3821 , C04B2235/3826 , C04B2235/3873 , C04B2235/428 , C04B2235/5248 , C04B2235/5252 , C04B2235/5256 , C04B2235/614 , C04B2235/616 , C04B35/52 , C04B38/0096
Abstract: A method of densifying a CMC article includes the steps of pyrolyzing a CMC article until a desired initial porosity is achieved, coating CMC pores within the CMC article with carbon, pyrolyzing the carbon to form carbon pores, coating the carbon pores with silicon, and heat treating the CMC article to create a silicon carbide filled pore integrated with silicon carbide of the CMC article to densify the CMC article.
Abstract translation: 使CMC制品致密化的方法包括以下步骤：热解CMC制品直至达到所需的初始孔隙率;用CMC涂覆CMC制品内的CMC孔;热解碳形成碳孔;涂覆 具有硅的碳孔以及对CMC制品进行热处理以形成与CMC制品的碳化硅整合的碳化硅填充的孔以使CMC制品致密化。
-
-
-
-
-
-
-
-
-
Search Results
102
records
(took 0.03 seconds)
