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公开(公告)号：US20080134667A1
公开(公告)日：2008-06-12
申请号：US11782631
申请日：2007-07-24
Applicant: Thomas Clayton Pavia , James Robert Grote
Inventor： Thomas Clayton Pavia , James Robert Grote
IPC: F02K9/97
CPC classification number: F02K9/64 , F02K9/972 , F02K9/974 , F05D2260/202 , F05D2260/205 , F05D2300/121 , F05D2300/171 , F05D2300/1721 , F05D2300/1723
Abstract: In some embodiments a propulsion system includes a thrust chamber having an inside wall, an expansion nozzle mounted to the thrust chamber and having an interior and having an exterior, a main propellant injector mounted to the thrust chamber to inject a fluid in the interior of the thrust chamber, the fluid comprising oxidizer, fuel and internal film coolant, the internal film coolant ranging from about 1% to about 5% of the fluid, limited coolant tubing circumscribing the exterior of the expansion nozzle to circulate an external coolant, and an injector mounted to the expansion nozzle to inject the external coolant in the interior of the expansion nozzle, the external convective coolant about 2.5% of the fluid. The system operates at lower temperatures while having conventional amounts of thrust, in which the thrust chamber can be made of thin walls of lower cost conventional metals with simple coolant tube construction.
Abstract translation: 在一些实施例中，推进系统包括具有内壁的推力室，安装到推力室的膨胀喷嘴，并且具有内部并具有外部，主推进剂喷射器安装到推进室以将流体注入到内部 推进室，包括氧化剂，燃料和内部薄膜冷却剂的流体，内部薄膜冷却剂的范围为流体的约1％至约5％，限制膨胀喷嘴外部的限制冷却液管以使外部冷却剂循环，以及喷射器 安装到膨胀喷嘴以将外部冷却剂注入膨胀喷嘴的内部，外部对流冷却剂约为流体的2.5％。 该系统在较低温度下工作，同时具有常规的推力，其中推力室可由具有简单冷却剂管构造的较低成本常规金属的薄壁制成。
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公开(公告)号：US20040150164A1
公开(公告)日：2004-08-05
申请号：US10693524
申请日：2003-10-27
Applicant: ROLLS ROYCE PLC
Inventor： Jonathan J. Morgan
IPC: F16J009/00
CPC classification number: F01D11/001 , F01D11/02 , F04D29/023 , F04D29/083 , F05D2240/55 , F05D2300/1721 , F05D2300/1723 , F05D2300/2112 , F05D2300/2118 , F05D2300/224 , F05D2300/2261 , F05D2300/2283 , F16J15/442 , F16J15/443
Abstract: A sealing arrangement for sealing a leakage gap between relatively moveable parts in a flow path between a region of high-fluid pressure and a region of low fluid pressure comprises a sealing member having an upstream surface, a downstream surface, a radially outer surface and a radially inner surface, said sealing member being in communication with a housing via resilient means. The resilient means is fixedly joined to the upstream surface of the sealing member such that during operation both the radial force induced on the sealing member by fluid flowing axially into and circumferentially over the radially inner surface and the axial force induced on the sealing member because of a pressure difference across the sealing member is resisted by the resilient means.
Abstract translation: 用于密封高流体压力区域和低流体压力区域之间的流动路径中相对移动部件之间的泄漏间隙的密封装置包括具有上游表面，下游表面，径向外表面和 径向内表面，所述密封构件通过弹性装置与壳体连通。 弹性装置固定地连接到密封构件的上游表面，使得在操作期间，通过流体轴向地流入径向内表面并周向地在径向内表面上引起的径向力和在密封构件上引起的轴向力，由于 通过弹性装置抵抗密封构件两端的压力差。
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公开(公告)号：US07997510B2
公开(公告)日：2011-08-16
申请号：US11782631
申请日：2007-07-24
Applicant: Thomas Clayton Pavia , James Robert Grote
Inventor： Thomas Clayton Pavia , James Robert Grote
IPC: B64D33/04
CPC classification number: F02K9/64 , F02K9/972 , F02K9/974 , F05D2260/202 , F05D2260/205 , F05D2300/121 , F05D2300/171 , F05D2300/1721 , F05D2300/1723
Abstract: In some embodiments a propulsion system includes a thrust chamber having an inside wall, an expansion nozzle mounted to the thrust chamber and having an interior and having an exterior, a main propellant injector mounted to the thrust chamber to inject a fluid in the interior of the thrust chamber, the fluid comprising oxidizer, fuel and internal film coolant, the internal film coolant ranging from about 1% to about 5% of the fluid, limited coolant tubing circumscribing the exterior of the expansion nozzle to circulate an external coolant, and an injector mounted to the expansion nozzle to inject the external coolant in the interior of the expansion nozzle, the external convective coolant about 2.5% of the fluid. The system operates at lower temperatures while having conventional amounts of thrust, in which the thrust chamber can be made of thin walls of lower cost conventional metals with simple coolant tube construction.
Abstract translation: 在一些实施例中，推进系统包括具有内壁的推力室，安装到推力室的膨胀喷嘴，并且具有内部并具有外部，主推进剂喷射器安装到推进室以将流体注入到内部 推进室，包括氧化剂，燃料和内部薄膜冷却剂的流体，内部薄膜冷却剂的范围为流体的约1％至约5％，限制膨胀喷嘴外部的限制冷却液管以使外部冷却剂循环，以及喷射器 安装到膨胀喷嘴以将外部冷却剂注入膨胀喷嘴的内部，外部对流冷却剂约为流体的2.5％。 该系统在较低温度下工作，同时具有常规的推力，其中推力室可由具有简单冷却剂管构造的较低成本常规金属的薄壁制成。
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公开(公告)号：US07320468B2
公开(公告)日：2008-01-22
申请号：US10693524
申请日：2003-10-27
Applicant: Jonathan J. Morgan
Inventor： Jonathan J. Morgan
IPC: F16J15/44
CPC classification number: F01D11/001 , F01D11/02 , F04D29/023 , F04D29/083 , F05D2240/55 , F05D2300/1721 , F05D2300/1723 , F05D2300/2112 , F05D2300/2118 , F05D2300/224 , F05D2300/2261 , F05D2300/2283 , F16J15/442 , F16J15/443
Abstract: A sealing arrangement for sealing a leakage gap between relatively moveable parts in a flow path between a region of high fluid pressure and a region of low fluid pressure comprises a sealing member having an upstream surface, a downstream surface, a radially outer surface and a radially inner surface, the sealing member being in communication with a housing via a resilient element. The resilient element is fixedly joined to the upstream surface of the sealing member such that during operation both the radial force induced on the sealing member by fluid flowing axially into and circumferentially over the radially inner surface and the axial force induced on the sealing member because of a pressure difference across the sealing member is resisted by the resilient element.
Abstract translation: 用于密封高流体压力区域和低流体压力区域之间的流动路径中的相对可移动部件之间的泄漏间隙的密封装置包括具有上游表面，下游表面，径向外表面和径向外表面的密封件 所述密封构件通过弹性元件与壳体连通。 弹性元件固定地连接到密封构件的上游表面，使得在操作期间，通过流体轴向地流入径向内表面并在周向上在径向内表面上引起的径向力和在密封构件上引起的轴向力，由于 密封构件两端的压力差由弹性元件抵抗。
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5.发明授权公开(公告)号：US11754115B1
公开(公告)日：2023-09-12
申请号：US17722863
申请日：2022-04-18
Applicant: Pratt & Whitney Canada Corp.
Inventor： Jean-Francois Belanger
CPC classification number: F16C17/02 , F01D25/166 , F16C33/06 , F16C35/02 , F05D2240/54 , F05D2300/121 , F05D2300/125 , F05D2300/171 , F05D2300/1721 , F05D2300/50212 , F16C2202/22
Abstract: An assembly is provided for a gas turbine engine. This assembly includes a rotating structure, a stationary structure and a bushing. The rotating structure extends axially along and is rotatable about a centerline. The stationary structure extends circumferentially about the rotating structure. The stationary structure is configured from or otherwise includes stationary structure material with a coefficient of thermal expansion between 10 μin/in-° F. and 15 μin/in-° F. The bushing is radially between the rotating structure and the stationary structure. The bushing includes a mount and a bearing within the mount. The mount is configured from or otherwise includes mount material with a coefficient of thermal expansion between 9 μin/in-° F. and 10 μin/in-° F. The mount material contacts the stationary structure material. The bearing is configured from or otherwise includes bearing material, where the bearing material is engaged with and rotatably supports the rotating structure. The bearing material is or otherwise includes copper.
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Patent Agency Ranking
6.发明授权Method and system of increasing wear resistance of a part of a rotating mechanism exposed to fluid flow therethrough 有权增加暴露于流体流动的旋转机构的一部分的耐磨性的方法和系统公开(公告)号：US09488184B2
公开(公告)日：2016-11-08
申请号：US13461816
申请日：2012-05-02
Applicant: Vladimir Petrovich Selkin , Sergei Vasilvevich Sosnovsky , Turki Saud Mohammed Al-Saud , Mohammed A Binhussain , Vladimir Enokovich Agabekov
Inventor： Vladimir Petrovich Selkin , Sergei Vasilvevich Sosnovsky , Turki Saud Mohammed Al-Saud , Mohammed A Binhussain , Vladimir Enokovich Agabekov
CPC classification number: F04D29/026 , F04D7/04 , F04D29/167 , F04D29/2294 , F05D2230/313 , F05D2300/1721 , F05D2300/173 , F05D2300/611 , Y10T428/12903
Abstract: A method of increasing wear resistance of one or more part(s) of a rotating mechanism includes manufacturing the one or more part(s) with a portion thereof configured to be exposed to wear during fluid flow associated with the rotating mechanism having a dimension different from that of a desired dimension, applying a protective coating of an aluminum bronze alloy to the portion through welding deposition, and mechanically treating the protective coating. The method also includes applying one or more layer(s) of solid-alloy over the protective coating through electro-erosion deposition, and continuing the mechanical treatment of the protective coating and/or the one or more layer(s) of solid-alloy after the solid-alloy deposition to obtain the desired dimension of the portion.
Abstract translation: 增加旋转机构的一个或多个部分的耐磨性的方法包括制造一个或多个部分，其中一个或多个部分被配置为在与具有不同尺寸的旋转机构相关联的流体流动期间暴露于磨损 从期望的尺寸，通过焊接沉积将铝青铜合金的保护涂层施加到该部分，以及机械处理保护涂层。 该方法还包括通过电蚀蚀沉积在保护涂层上施加一层或多层固体合金，并继续对保护涂层和/或一个或多个固体合金层进行机械处理 在固体合金沉积之后，获得该部分的所需尺寸。
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公开(公告)号：US07448856B2
公开(公告)日：2008-11-11
申请号：US10950267
申请日：2004-09-24
Applicant: Xavier Girod , Eric Icarre , Michel El Baz
Inventor： Xavier Girod , Eric Icarre , Michel El Baz
IPC: F04D29/20
CPC classification number: F04D29/023 , F04D29/329 , F05D2300/172 , F05D2300/1721 , F05D2300/43 , Y10T29/49318
Abstract: A fan assembly has a central metallic element and a polymeric fan. The polymeric fan has a hub carrying the central metallic element and has a plurality of blades extending from the hub. The central metallic element has a central longitudinal aperture and a lateral surface. The central metallic element lateral surface is of substantially uniform substantially square section along a majority of a length of the central metallic element.
Abstract translation: 风扇组件具有中心金属元件和聚合风扇。 聚合物风扇具有承载中心金属元件的毂，并且具有从轮毂延伸的多个叶片。 中心金属元件具有中心纵向孔和侧面。 中心金属元件侧表面沿着中心金属元件的大部分长度具有基本均匀的基本上正方形的截面。
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公开(公告)号：US20170107999A1
公开(公告)日：2017-04-20
申请号：US14886904
申请日：2015-10-19
Applicant: ROLLS-ROYCE CORPORATION
Inventor： Bradley T. Fanton , Roy David Fulayter
CPC classification number: B23P15/006 , F01D5/3007 , F01D5/3092 , F04D29/322 , F05D2300/1721 , Y02T50/672
Abstract: According to one aspect, a rotating structure comprises a hub having a mounting slot defined by a cavity surface and a body having an anchor structure disposed in the mounting slot. A wear member is disposed between the anchor structure and the cavity surface and the wear member has at least first and second portions of first and second material characteristics, respectively.
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9.发明申请METHOD AND SYSTEM OF INCREASING WEAR RESISTANCE OF A PART OF A ROTATING MECHANISM EXPOSED TO FLUID FLOW THERETHROUGH 有权增加暴露于流体流动的旋转机构的一部分的耐磨性的方法和系统公开(公告)号：US20130294896A1
公开(公告)日：2013-11-07
申请号：US13461816
申请日：2012-05-02
Applicant: VLADIMIR PETROVICH SELKIN , Sergei Vasilvevich Sosnovsky , Turki Saud Mohammed Al-Saud , Mohammed A. Binhussain , Vladimir Enokovich Agabekov
Inventor： VLADIMIR PETROVICH SELKIN , Sergei Vasilvevich Sosnovsky , Turki Saud Mohammed Al-Saud , Mohammed A. Binhussain , Vladimir Enokovich Agabekov
CPC classification number: F04D29/026 , F04D7/04 , F04D29/167 , F04D29/2294 , F05D2230/313 , F05D2300/1721 , F05D2300/173 , F05D2300/611 , Y10T428/12903
Abstract: A method of increasing wear resistance of one or more part(s) of a rotating mechanism includes manufacturing the one or more part(s) with a portion thereof configured to be exposed to wear during fluid flow associated with the rotating mechanism having a dimension different from that of a desired dimension, applying a protective coating of an aluminum bronze alloy to the portion through welding deposition, and mechanically treating the protective coating. The method also includes applying one or more layer(s) of solid-alloy over the protective coating through electro-erosion deposition, and continuing the mechanical treatment of the protective coating and/or the one or more layer(s) of solid-alloy after the solid-alloy deposition to obtain the desired dimension of the portion.
Abstract translation: 增加旋转机构的一个或多个部分的耐磨性的方法包括制造一个或多个部分，其中一个或多个部分被配置为在与具有不同尺寸的旋转机构相关联的流体流动期间暴露于磨损 从期望的尺寸，通过焊接沉积将铝青铜合金的保护涂层施加到该部分，以及机械处理保护涂层。 该方法还包括通过电蚀蚀沉积在保护涂层上施加一层或多层固体合金，并继续对保护涂层和/或一个或多个固体合金层进行机械处理 在固体合金沉积之后，获得该部分的所需尺寸。
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公开(公告)号：US20060073018A1
公开(公告)日：2006-04-06
申请号：US10950267
申请日：2004-09-24
Applicant: Xavier Girod , Eric Icarre , Michel El Baz
Inventor： Xavier Girod , Eric Icarre , Michel El Baz
IPC: B64C27/00
CPC classification number: F04D29/023 , F04D29/329 , F05D2300/172 , F05D2300/1721 , F05D2300/43 , Y10T29/49318
Abstract: A fan assembly has a central metallic element and a polymeric fan. The polymeric fan has a hub carrying the central metallic element and has a plurality of blades extending from the hub. The central metallic element has a central longitudinal aperture and a lateral surface. The central metallic element lateral surface is of substantially uniform substantially square section along a majority of a length of the central metallic element.
Abstract translation: 风扇组件具有中心金属元件和聚合风扇。 聚合物风扇具有承载中心金属元件的毂，并且具有从轮毂延伸的多个叶片。 中心金属元件具有中心纵向孔和侧面。 中心金属元件侧表面沿着中心金属元件的大部分长度具有基本均匀的基本上正方形的截面。
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