公开(公告)号：US20110079020A1

公开(公告)日：2011-04-07

申请号：US12571987

申请日：2009-10-01

申请人： Eric DUROCHER ,  Pierre-Yves LEGARE

发明人： Eric DUROCHER ,  Pierre-Yves LEGARE

IPC分类号： F02C7/20

CPC分类号： F01D11/18 ,  F02C7/28

摘要： An air metering apparatus for a secondary air system of gas turbine engine includes a metering gap defined between surfaces comprised of one or more metals having one of similar coefficients of thermal expansion or similar thermal expansions at an operating temperature. Provided is an air metering gap which undergoes thermal growth in a way which provides a suitable air metering gap during engine running conditions.

摘要翻译： 用于燃气涡轮发动机的二次空气系统的空气计量装置包括限定在由一种或多种金属构成的表面之间的计量间隙，所述金属具有在工作温度下具有相似的热膨胀系数或相似的热膨胀系数之一。 提供了一种空气计量间隙，其在发动机运行条件下以提供合适的空气计量间隙的方式进行热生长。

公开(公告)号：US20100071208A1

公开(公告)日：2010-03-25

申请号：US12236128

申请日：2008-09-23

申请人： Eric DUROCHER ,  Anca Mateescu

发明人： Eric DUROCHER ,  Anca Mateescu

IPC分类号： B23P11/00

CPC分类号： F01D25/285 ,  F01D9/04 ,  F05D2230/60 ,  F05D2230/68 ,  Y10T29/49245 ,  Y10T29/49321 ,  Y10T29/49323 ,  Y10T29/53613 ,  Y10T29/53635

摘要： The vane assembly has mating vane support and vane ring, the vane ring having a plurality of annularly interspaced radial loading elements which, when the vane ring is assembled to the vane support, are in a resiliently flexed state and exert corresponding annularly interspaced and outward-oriented radial loads against the vane support, thereby restraining relative radial movement between the vane ring and the vane support during operation of the gas turbine engine. The method includes flexing each of the radial loading elements into the resiliently flexed state simultaneously by sliding the radial loading elements against corresponding lead-in tapers. This can be achieved using a guide tool which includes a plurality of segments bearing the lead-in tapers and which is previously assembled to the vane support.

摘要翻译： 叶片组件具有配合叶片支撑件和叶片环，叶片环具有多个环形间隔的径向加载元件，当叶片环组装到叶片支撑件上时，叶片环处于弹性弯曲状态并施加相应的环形间隔和向外 - 相对于叶片支撑件的定向径向载荷，从而在燃气涡轮发动机的操作期间抑制叶片环和叶片支撑件之间的相对径向运动。 该方法包括通过相对于引入锥度滑动径向加载元件，将每个径向加载元件同时弯曲成弹性弯曲状态。 这可以使用引导工具来实现，该引导工具包括多个带有引入锥形部分并且预先组装到叶片支撑件的部分。

公开(公告)号：US20080232963A1

公开(公告)日：2008-09-25

申请号：US12131403

申请日：2008-06-02

申请人： Eric DUROCHER ,  Assaf FARAH

发明人： Eric DUROCHER ,  Assaf FARAH

IPC分类号： F01D5/18

CPC分类号： F01D11/08 ,  F01D9/04 ,  F01D25/12 ,  F05D2230/21 ,  F05D2240/11 ,  F05D2250/51 ,  F05D2250/52 ,  F05D2260/20

摘要： A shroud segment of a turbine shroud of a gas turbine engine comprises a platform with front and rear legs. The platform defines a plurality of axially extending holes with individual inlets on an outer surface of the platform for transpiration cooling of the platform of the turbine shroud segment.

摘要翻译： 燃气涡轮发动机的涡轮机护罩的护罩部分包括具有前腿和后腿的平台。 平台在平台的外表面上限定了多个具有单独入口的轴向延伸的孔，用于涡轮机护罩段的平台的蒸发冷却。

公开(公告)号：US20130223982A1

公开(公告)日：2013-08-29

申请号：US13404347

申请日：2012-02-24

申请人： Eric DUROCHER ,  Guy LEFEBVRE

发明人： Eric DUROCHER ,  Guy LEFEBVRE

IPC分类号： F02C7/00 ,  B23P11/00 ,  F16B5/04

CPC分类号： F16B5/0241 ,  F16B5/04 ,  Y10T29/4932 ,  Y10T403/217

摘要： A thermal expansion joint suited for metal sheet component assemblies and method of connection is described. The expansion joint connection is formed by overlapping edge portions of components which are subject to different temperatures. Slot apertures are formed in the edge portion of a first component at predetermined locations and hole apertures are formed in the edge portion of the second component and disposed for confronting alignment with the slot apertures. A connecting sleeve is disposed in each hole aperture and projects through the hole and associated slot and a retention washer is secured over an end of the connecting sleeve on the other side of the second component. A fastener extends through the retention washer and the connecting sleeve to clampingly interconnect the overlapped edge portions of the first and second components.

摘要翻译： 描述适用于金属片组件组件的热膨胀接头和连接方法。 膨胀接头连接部由经受不同温度的部件的重叠边缘部分形成。 槽孔在第一部件的边缘部分形成在预定位置处，并且在第二部件的边缘部分中形成孔孔，并且设置成与槽孔对准。 连接套筒设置在每个孔孔中并突出穿过孔和相关联的槽，并且保持垫圈固定在第二部件另一侧的连接套筒的一端上。 紧固件延伸穿过保持垫圈和连接套筒夹紧地互连第一和第二部件的重叠的边缘部分。

公开(公告)号：US20110079019A1

公开(公告)日：2011-04-07

申请号：US12572066

申请日：2009-10-01

申请人： Eric DUROCHER ,  Pierre-Yves LEGARE

发明人： Eric DUROCHER ,  Pierre-Yves LEGARE

IPC分类号： F02C7/12 ,  F02C7/20

CPC分类号： F01D5/082 ,  F01D9/065 ,  F01D11/001 ,  F01D11/02 ,  F01D25/125 ,  F01D25/162 ,  F02C7/12 ,  F02C7/18

摘要： A mid turbine frame is disposed between high and low pressure turbine assemblies. A cooling air system defined in the mid turbine frame of a gas turbine engine includes internal cavities for containing pressurized cooling air to cool the inter-turbine duct and the hollow struts, and discharges the used cooling air to further cool respective high and low pressure turbine assemblies.

摘要翻译： 中间涡轮机框架设置在高压和低压涡轮机组件之间。 限定在燃气涡轮发动机的中间涡轮机框架中的冷却空气系统包括用于容纳加压冷却空气以冷却涡轮机间管道和中空支柱的内部空腔，并且排放所使用的冷却空气以进一步冷却相应的高压和低压涡轮机 装配。

公开(公告)号：US20100275572A1

公开(公告)日：2010-11-04

申请号：US12433163

申请日：2009-04-30

申请人： Eric DUROCHER ,  Pierre-Yves LEGARE

发明人： Eric DUROCHER ,  Pierre-Yves LEGARE

IPC分类号： F01D25/18 ,  F02C7/20 ,  F02C7/24

CPC分类号： F01D9/065 ,  F01D25/18 ,  F05D2260/231

摘要： A gas turbine engine having a mid turbine frame comprising an annular outer case providing a portion of an engine casing; an interturbine duct (ITD) disposed within the outer case, the ITD including outer and inner rings radially spaced apart one from another and being interconnected by a plurality of radially extending and circumferentially spaced hollow strut fairings, the inner and outer rings co-operating to provide a portion of a hot gas path through the engine; a tube for delivering or discharging a lubricant fluid to or from a bearing housing, the tube extending radially through one of the hollow struts; and an insulation structure radially extending through one said hollow strut fairing, the insulation structure surrounding the tube and being spaced apart from the tube and from a hot internal surface of the one hollow strut fairing for shielding the tube from heat radiated from the hot internal surface of the one hollow strut fairing and for preventing the lubricant fluid from contacting the hot internal surface of said one hollow strut fairing when lubricant fluid leakage occurs.

摘要翻译： 一种具有中间涡轮机框架的燃气涡轮发动机，其包括提供发动机壳体的一部分的环形外壳; 设置在外壳内的涡轮管（ITD），ITD包括彼此径向间隔开的并由多个径向延伸和周向间隔开的中空支柱整流罩互连的外环和内环，内环和外环与 提供通过发动机的热气路径的一部分; 用于将润滑剂流体输送到轴承壳体或从轴承壳体排出的管，该管径向延伸穿过其中一个中空支柱; 以及径向延伸穿过一个所述中空支柱整流罩的绝缘结构，所述绝缘结构围绕所述管并且与所述管和所述一个中空支柱整流罩的热内表面间隔开，用于屏蔽所述管免受从所述热内表面辐射的热 的一个空心支柱整流罩，并且用于在发生润滑剂流体泄漏时防止润滑剂流体接触所述一个中空支柱整流罩的热内表面。

公开(公告)号：US20090110548A1

公开(公告)日：2009-04-30

申请号：US11928512

申请日：2007-10-30

申请人： Eric DUROCHER ,  Guy LEFEBVRE

发明人： Eric DUROCHER ,  Guy LEFEBVRE

IPC分类号： F04D29/08

CPC分类号： F01D11/001 ,  F05D2240/122 ,  F05D2240/304 ,  F05D2240/80

摘要： An abradable rim seal arrangement for a turbine stage of a gas turbine engine, which includes an abradable rim seat attached to a leading edge of an annular inner duct of a turbine exhaust case, causing a trailing edge platform of each rotor blade to overlap the abradable rim seal, and allowing rubbing with the trailing edge platform during engine operation.

摘要翻译： 一种用于燃气涡轮发动机的涡轮级的可磨损轮辋密封装置，其包括附接到涡轮机排气箱的环形内部管道的前缘的可磨损轮辋座，使得每个转子叶片的后缘平台与可磨损的 轮辋密封，并且在发动机操作期间允许与后缘平台摩擦。

公开(公告)号：US20080085183A1

公开(公告)日：2008-04-10

申请号：US11538863

申请日：2006-10-05

申请人： Eric DUROCHER ,  Rene Paquet

发明人： Eric DUROCHER ,  Rene Paquet

IPC分类号： F04D29/08

CPC分类号： F04D29/102 ,  F01D11/001 ,  F01D11/02

摘要： The air seal arrangement is for a disc wheel in a gas turbine engine. The disc wheel comprises a sleeve portion having an outer surface. The arrangement comprises a static knife edge seal in registry with the outer surface. The static knife edge seal has a free end adjacent to the outer surface.

摘要翻译： 空气密封装置用于燃气涡轮发动机中的盘轮。 盘轮包括具有外表面的套筒部分。 该装置包括与外表面对准的静态刀边密封件。 静态刀刃密封件具有邻近外表面的自由端。

公开(公告)号：US20080060344A1

公开(公告)日：2008-03-13

申请号：US11530529

申请日：2006-09-11

申请人： Eric DUROCHER ,  Guy LEFEBVRE

发明人： Eric DUROCHER ,  Guy LEFEBVRE

IPC分类号： F02K1/38

CPC分类号： F02K1/04 ,  F05D2260/30

摘要： An annular exhaust duct of a gas turbine engine includes inner and outer cases co-axially disposed, and radially spaced apart by a plurality of airfoils radially extending therebetween. The outer case includes a connection apparatus for supportably connecting the exhaust duct to the gas turbine engine and the inner case includes an axial end portion at a rear end thereof for connection with a tail cone. The axial end portion bends radially and inwardly at a rear extremity thereof to stiffen the rear end of the inner ease.

摘要翻译： 燃气涡轮发动机的环形排气管包括同轴地设置的内壳体和外壳体，并且由在其间径向延伸的多个翼型件径向隔开。 外壳包括用于将排气管可支撑地连接到燃气涡轮发动机的连接装置，并且内壳在其后端包括用于与尾锥连接的轴向端部。 轴向端部在其后端处径向向内弯曲并使其内侧的后端变硬。

公开(公告)号：US20130051989A1

公开(公告)日：2013-02-28

申请号：US13222022

申请日：2011-08-31

申请人： Eric DUROCHER ,  Guy LEFEBVRE

发明人： Eric DUROCHER ,  Guy LEFEBVRE

IPC分类号： F01D25/24 ,  B23P17/00

CPC分类号： F01D11/005 ,  B22F3/225 ,  B22F5/009 ,  B22F7/08 ,  F01D9/04 ,  F05D2220/32 ,  F05D2240/57 ,  Y10T29/4998

摘要： A feather seal is positioned in a mold and a shroud body is metal injection molded about a proximal end of the feather seal to provide a shroud segment with an integrated feather seal. A seal groove is provided in an opposite lateral side of the shroud body to receive the feather seal of a circumferentially adjacent shroud segment.

摘要翻译： 羽毛密封件定位在模具中，并且护罩主体围绕羽毛密封件的近端金属注射模制，以提供具有集成的羽毛密封件的护罩区段。 密封槽设置在护罩主体的相对的侧面上，以容纳周向相邻护罩区段的羽毛密封。