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公开(公告)号:US10794211B2
公开(公告)日:2020-10-06
申请号:US16090893
申请日:2017-04-10
Applicant: United Technologies Corporation
Inventor: Paul M. Sheedy , Changsheng Guo
Abstract: A turbomachine sealing component has: a substrate having circumferential surface; and a coating on the circumferential surface. The coating or a layer thereof is patterned to form circumferential sealing ridges.
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公开(公告)号:US20190275627A1
公开(公告)日:2019-09-12
申请号:US15916683
申请日:2018-03-09
Applicant: United Technologies Corporation
Inventor: Zhigang Wang , Changsheng Guo , Daniel V. Viens
Abstract: A system includes a machine tool that includes a cutting tool, a fluid subsystem that provides fluid to the cutting tool, and at least one processor that executes instructions that cause the at least one processor to: obtain a signal indicative of a load on the cutting tool, establish a first value of at least one parameter of the fluid based on the signal, obtain a second value of the at least one parameter that is based on a simulation, determine a difference between the first value and the second value, and adjust a state of a device of the fluid subsystem based on the determined difference.
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公开(公告)号:US20180223677A1
公开(公告)日:2018-08-09
申请号:US15943431
申请日:2018-04-02
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Changsheng Guo , Christopher W. Strock
CPC classification number: F01D5/20 , F01D11/122 , F05D2220/32 , F05D2230/10 , F05D2230/25 , F05D2230/90 , F05D2300/2112 , F05D2300/22 , F05D2300/2282 , F05D2300/2284 , F05D2300/30 , F05D2300/506 , Y10T29/49337
Abstract: A blade includes a blade body extending from a blade root to an opposed blade tip surface along a longitudinal axis. The blade body defines a pressure side and a suction side. The blade body includes a cutting edge defined where the tip surface of the blade body meets the pressure side of the blade body. The cutting edge is configured to abrade a seal section of an engine case. A method for manufacturing a blade includes forming an airfoil with a root and an opposed tip surface along a longitudinal axis, wherein the airfoil defines a pressure side and a suction side. The method also includes forming a cutting edge where the tip surface of the airfoil meets the pressure side of the airfoil.
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公开(公告)号:US10036402B2
公开(公告)日:2018-07-31
申请号:US14709721
申请日:2015-05-12
Applicant: UNITED TECHNOLOGiES CORPORATION
Inventor: Shahram Amini , Christopher W Strock , Changsheng Guo
CPC classification number: F04D29/526 , F01D5/28 , F01D11/12 , F01D11/122 , F01D21/045 , F02K3/06 , F04D19/002 , F04D29/023 , F04D29/164 , F05B2220/302 , F05B2230/90 , F05B2280/107 , F05B2280/40 , F05B2280/5011 , Y02T50/672 , Y02T50/673
Abstract: A turbine engine system comprising a turbine engine component, such as a fan includes a fan casing and a fan blade rotatable within the fan casing. An abradable seal coupled to the fan casing proximate the fan blade. The abradable seal comprising an abradable composite layer including a MAX phase solid and a polymer based abradable composition.
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公开(公告)号:US09932839B2
公开(公告)日:2018-04-03
申请号:US14725052
申请日:2015-05-29
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Changsheng Guo , Christopher W. Strock
CPC classification number: F01D5/20 , F01D11/122 , F05D2220/32 , F05D2230/10 , F05D2230/25 , F05D2230/90 , F05D2300/2112 , F05D2300/22 , F05D2300/2282 , F05D2300/2284 , F05D2300/30 , F05D2300/506 , Y10T29/49337
Abstract: A blade includes a blade body extending from a blade root to an opposed blade tip surface along a longitudinal axis. The blade body defines a pressure side and a suction side. The blade body includes a cutting edge defined where the tip surface of the blade body meets the pressure side of the blade body. The cutting edge is configured to abrade a seal section of an engine case. A method for manufacturing a blade includes forming an airfoil with a root and an opposed tip surface along a longitudinal axis, wherein the airfoil defines a pressure side and a suction side. The method also includes forming a cutting edge where the tip surface of the airfoil meets the pressure side of the airfoil.
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公开(公告)号:US20150322809A1
公开(公告)日:2015-11-12
申请号:US14761496
申请日:2013-01-29
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Christopher W. Strock , Changsheng Guo
CPC classification number: F01D11/122 , B82Y30/00 , F01D5/02 , F01D5/288 , F01D11/125 , F01D25/24 , F05D2300/224 , F05D2300/437
Abstract: One aspect of the disclosure involves a nib material comprising a polymeric matrix and carbon nanotubes in the matrix. In one or more embodiments of any of the foregoing embodiments, the matrix comprises a silicone. In one or more embodiments of any of the foregoing embodiments, the rub material is at least 1.0 mm thick. In one or more embodiments of any of the foregoing embodiments, the silicone is selected from the group consisting of dimethyl- and fluoro-silicone rubbers and their copolymers. In one or more embodiments of any of the foregoing embodiments, the carbon nanotubes at least locally have a concentration of 1-20% by weight.
Abstract translation: 本公开的一个方面涉及一种在基质中包含聚合物基体和碳纳米管的笔尖材料。 在任何前述实施方案的一个或多个实施方案中,基质包含硅氧烷。 在任何前述实施例的一个或多个实施例中,摩擦材料至少为1.0mm厚。 在任何前述实施方案的一个或多个实施方案中,硅氧烷选自二甲基和氟硅橡胶及其共聚物。 在任何前述实施方案的一个或多个实施方案中,碳纳米管至少局部地具有1-20重量%的浓度。
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公开(公告)号:US20150204347A1
公开(公告)日:2015-07-23
申请号:US14509780
申请日:2014-10-08
Applicant: United Technologies Corporation
Inventor: Christopher W. Strock , Changsheng Guo
CPC classification number: F04D29/388 , F01D5/20 , F01D5/286 , F01D5/288 , F01D11/122 , F04D19/002 , F05D2220/36 , F05D2240/307 , F05D2240/31 , F05D2300/211 , F05D2300/2282 , F05D2300/43 , F05D2300/434 , F05D2300/44 , Y10T156/10
Abstract: A fan blade for a gas turbine engine is disclosed. The disclosed fan blade includes an airfoil having a leading edge, a trailing edge, a convex side, a concave side and a distal tip. The leading edge, trailing edge, convex side and concave side of the airfoil is at least partially coated with an erosion resistant coating. The distal tip of the airfoil is coated with a bonded abrasive coating. The bonded abrasive coating engages the abradable coating disposed on the fan liner and, because of its low thermal conductivity, reduces heat transfer to the distal tip of the fan blade. The reduction in heat transfer to the distal tip of the fan blade preserves the integrity of erosion resistant coatings that may be applied to the body or the airfoil of the fan blade.
Abstract translation: 公开了一种用于燃气涡轮发动机的风扇叶片。 所公开的风扇叶片包括具有前缘,后缘,凸侧,凹侧和远端的翼型。 翼型件的前缘,后缘,凸侧和凹面至少部分地涂覆有抗侵蚀涂层。 机翼的远端通过粘合的磨料涂层涂覆。 粘合磨料涂层与布置在风扇衬套上的可磨损涂层接合,并且由于其低导热性,减少了传递到风扇叶片的远端的热传递。 传递到风扇叶片的远端的传热的减少保持了可施加到风扇叶片的主体或翼型上的耐腐蚀涂层的完整性。
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公开(公告)号:US20150114074A1
公开(公告)日:2015-04-30
申请号:US14492507
申请日:2014-09-22
Applicant: United Technologies Corporation
Inventor: Changsheng Guo
IPC: B24B39/00
CPC classification number: B24B39/006 , B23P9/04 , C21D7/04
Abstract: A method for controlled peening includes forming a surface layer on a workpiece by impacting a surface with a tool wherein the tool is under control to form compressive residual stresses in the surface layer. A system for peening a workpiece includes a tool configured to vibrate and an effector operatively connected to control the tool. The tool includes a peening surface. The tool is configured to cause controlled impact between the peening surface and a surface of a workpiece to form a surface layer of the workpiece with compressive residual stresses. The effector is configured to move the tool in multiple axes.
Abstract translation: 用于可控喷丸的方法包括通过用工具进行冲击而在工件上形成表面层,其中该工具受到控制以在表面层中形成压缩残余应力。 用于硬化工件的系统包括构造成振动的工具和可操作地连接以控制工具的效应器。 该工具包括一个喷丸表面。 该工具被配置成引起喷丸表面和工件表面之间的受控冲击,以形成具有压缩残余应力的工件的表面层。 效应器被配置为在多个轴上移动刀具。
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公开(公告)号:US20150086283A1
公开(公告)日:2015-03-26
申请号:US14472804
申请日:2014-08-29
Applicant: United Technologies Corporation
Inventor: Raja Kountanya , Changsheng Guo
IPC: B23C5/10
CPC classification number: B23C5/1009 , B23C2215/44 , B23C2265/08 , Y10T407/1946
Abstract: A tool is disclosed that has an elongated tool body defining a longitudinal axis and includes a ball-end section having a positive taper angle relative to the longitudinal axis of the tool body, and a relief section that extends rearwardly from the ball-end section and has a negative taper angle relative to the positive taper angle of the ball-end section.
Abstract translation: 公开了一种具有限定纵向轴线的细长工具主体的工具,并且包括相对于工具主体的纵向轴线具有正锥角的球头部分和从球头部分向后延伸的浮雕部分,以及 具有相对于球端部的正锥角的负锥角。
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公开(公告)号:US11090772B2
公开(公告)日:2021-08-17
申请号:US16238167
申请日:2019-01-02
Applicant: United Technologies Corporation
Inventor: Changsheng Guo , Zhigang Wang , Eric Fromerth
Abstract: A method and apparatus for machining parts with variable stiffness includes determining, by a controller, a chatter-lobe plot of a cutter assembly. A preliminary tool path is developed by the controller. Virtual machining of a blank part using the preliminary tool path is performed by the controller. A chatter-lobe plot of the virtually machined part is determined by the controller. A dynamic chatter-lobe plot using the chatter-lobe plot of the cutting tool assembly and the chatter-lobe plot of the virtually machined part is determined by the controller. A chatter-free rotational speed of the cutting tool from the dynamic chatter-lobe plot is determined by the controller. A machining apparatus, controlled by the controller, uses the determined chatter-free rotational speed of the cutting tool to machine a blank part.
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