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公开(公告)号：US06892526B2
公开(公告)日：2005-05-17
申请号：US10361511
申请日：2003-02-11
IPC分类号： B64D29/00 , F01D11/00 , F02C7/04 , F02C7/045 , F02K1/80 , F04D29/16 , F04D29/54 , F04D29/68 , B64D29/06 , F02K3/06
CPC分类号： B64D33/02 , B64D29/00 , B64D2033/0206 , B64D2033/0286 , F01D11/005 , F02C7/04 , F02C7/045 , F02K1/80 , F02K1/805 , F04D29/164 , F04D29/547 , F04D29/681 , Y10T137/0536
摘要： A cowl structure (18) for a gas turbine engine (10) comprises an outer skin (26) defining a first path for a load applied to the engine (10). The cowl structure (18) includes an inner skin (24) defining a second path for the load. The inner and outer skins (24, 26) are constructed such that a major proportion of the load is transmitted along the first path.
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公开(公告)号：US20050097892A1
公开(公告)日：2005-05-12
申请号：US10703272
申请日：2003-11-07
申请人： Douglas Carper , Michael Millard
发明人： Douglas Carper , Michael Millard
IPC分类号： F02C7/28 , B32B7/02 , B32B7/04 , B32B15/02 , C04B37/02 , F02C7/00 , F02K1/12 , F02K1/80 , F02K1/06
CPC分类号： F02K1/12 , B23P6/002 , B23P6/045 , F02K1/805 , F05D2240/55 , F05D2300/21 , Y02T50/672
摘要： An inseparable assembly includes a body having a plurality of plies stacked in face to face relation and bonded together, wherein each of the plurality of plies includes a ceramic matrix composite material having a first predetermined ductility. The assembly further includes a reinforcement including a metallic wire mesh bonded to said body so that at least a portion of the metallic wire mesh is positioned between two adjacent plies in the body. The metallic wire mesh has a second predetermined ductility greater than the first ductility.
摘要翻译： 不可分离的组件包括具有面对面地堆叠的多个层的主体并且结合在一起，其中多个层中的每一个包括具有第一预定延展性的陶瓷基复合材料。 组件还包括加强件，其包括结合到所述主体的金属丝网，使得金属丝网的至少一部分位于主体的两个相邻层之间。 金属丝网具有大于第一延展性的第二预定延展性。
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公开(公告)号：US20050022532A1
公开(公告)日：2005-02-03
申请号：US10885479
申请日：2004-07-07
申请人： Emmanuel Mandet
发明人： Emmanuel Mandet
CPC分类号： F02K1/1207 , F02K1/80 , F02K1/805
摘要： In a variable-section turbomachine nozzle, a plurality of flexible follower flaps are provided that are interposed between adjacent controlled flaps against which the follower flaps are held by fastener means, each follower flap comprising a plurality of independent transverse boxes mounted side by side in a support sheet, the boxes contacting one another via their longitudinal edges and being held in the support sheet via their lateral edges which are engaged in the longitudinal edges of the support sheet, which longitudinal edges define respective bearing zones for bearing against the adjacent controlled flaps.
摘要翻译： 在可变截面涡轮机喷嘴中，设置有多个柔性随动翼片，其插入相邻的受控翼片之间，随动翼片通过紧固装置保持，每个从动翼片包括并排安装的多个独立横向箱体 支撑片通过其纵向边缘彼此接触并且通过它们的侧边缘固定在支撑片中，所述侧边缘接合在支撑片的纵向边缘中，该纵向边缘限定相应的轴承区域以抵靠相邻的受控翼片。
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公开(公告)号：US20030159430A1
公开(公告)日：2003-08-28
申请号：US10379633
申请日：2003-03-05
发明人： Jean-Pierre Lair
IPC分类号： F02K001/00
CPC分类号： B64C15/02 , F02K1/002 , F02K1/006 , F02K1/04 , F02K1/11 , F02K1/1261 , F02K1/15 , F02K1/54 , F02K1/60 , F02K1/70 , F02K1/76 , F02K1/805 , F05D2240/55 , Y02T50/672
摘要： A jet engine nozzle having a pair of pivoting extension arms and a pair of pivoting shells connected to a jet pipe is provided. The first extension arm is pivotally connected to the jet pipe at a first location, while the second extension arm is pivotally connected to the jet pipe at a second location. Each shell is pivotally connected at both the first and second locations. An axis of rotation associated with the first location is coaxial to an axis of rotation associated with the second location. Independent actuation means are provided to rotate the extension arms and the shells, thereby enabling adjustment of the thrust-vector angle or the exhaust area of the nozzle.
摘要翻译： 提供具有一对枢转延伸臂和连接到喷射管的一对枢转壳体的喷气发动机喷嘴。 第一延伸臂在第一位置处枢转地连接到喷射管，而第二延伸臂在第二位置枢转地连接到喷射管。 每个壳体在第一和第二位置处枢转地连接。 与第一位置相关联的旋转轴线与与第二位置相关联的旋转轴线共轴。 提供独立的致动装置以旋转延伸臂和壳体，由此能够调节喷嘴的推力矢量角或排气区域。
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35.发明授权公开(公告)号：US06471469B2
公开(公告)日：2002-10-29
申请号：US09728030
申请日：2000-11-30
IPC分类号： F01D1716
CPC分类号： F02K1/805 , F01D11/003 , F02K1/1207 , F05D2240/55 , F05D2300/21 , F05D2300/603 , Y10T29/49297
摘要： A gas turbine engine variable geometry exhaust nozzle including a seal system that facilitates extending a useful life of the engine variable geometry system is described. The seal system includes a backbone and an attachment assembly. The attachment assembly frictionally engages the backbone to secure the attachment assembly to the backbone. The attachment assembly includes a plurality of clamp sub-assemblies and base sheet fabricated from a ceramic matrix composite material. The clamp sub-assemblies are clamped through openings extending through the base sheet, such that a predetermined amount of preload force is applied to the base sheet.
摘要翻译： 描述了包括有助于延长发动机可变几何系统的使用寿命的密封系统的燃气涡轮发动机可变几何形状排气喷嘴。 密封系统包括骨架和附接组件。 附接组件摩擦地接合骨架以将附接组件固定到骨架上。 附接组件包括由陶瓷基复合材料制成的多个夹紧子组件和基片。 夹紧子组件通过延伸穿过基片的开口夹紧，使得预定量的预载力施加到基片上。
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公开(公告)号：US20020064455A1
公开(公告)日：2002-05-30
申请号：US09728030
申请日：2000-11-30
IPC分类号： F01D005/00
CPC分类号： F02K1/805 , F01D11/003 , F02K1/1207 , F05D2240/55 , F05D2300/21 , F05D2300/603 , Y10T29/49297
摘要： A gas turbine engine variable geometry exhaust nozzle including a seal system that facilitates extending a useful life of the engine variable geometry system is described. The seal system includes a backbone and an attachment assembly. The attachment assembly frictionally engages the backbone to secure the attachment assembly to the backbone. The attachment assembly includes a plurality of clamp sub-assemblies and base sheet fabricated from a ceramic matrix composite material. The clamp sub-assemblies are clamped through openings extending through the base sheet, such that a predetermined amount of preload force is applied to the base sheet.
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公开(公告)号：US6065756A
公开(公告)日：2000-05-23
申请号：US988013
申请日：1997-12-10
CPC分类号： F01D11/005 , F02K1/805 , F16J15/0887 , Y10S277/903 , Y10S285/917
摘要： An expansion joint seal between a gas turbine exhaust duct and an axially adjacent exhaust ductwork comprising plural layers of axially adjacent layers of flexible seal plates, each layer comprising a plurality of arcuate segments which together form a 360.degree. annulus; and further wherein the plural layers of flexible seal plates are secured at one end to the gas turbine exhaust duct, with opposite ends of the seal plates slidably engaged with at least one surface of the exhaust ductwork.
摘要翻译： 在燃气轮机排气管和轴向相邻的排气管道系统之间的膨胀接头密封件，其包括多个相邻的柔性密封层层，每个层包括多个弓形段，它们一起形成360°环; 并且其中所述多层柔性密封板的一端固定到所述燃气轮机排气管道，所述密封板的相对端与所述排气管道系统的至少一个表面可滑动地接合。
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公开(公告)号：US5348252A
公开(公告)日：1994-09-20
申请号：US36873
申请日：1993-03-25
申请人： Julian G. Balsdon
发明人： Julian G. Balsdon
CPC分类号： F01D25/125 , F02K1/004 , F02K1/805 , Y02T50/675
摘要： A vectorable nozzle mounting for an engine installation in a VSTOL aircraft in which hot gas nozzles are mounted on the airframe is described. A swivelable nozzle is mounted by means of a bearing on an intermediate fixed member such as a mounting ring on the airframe. The hot exhaust gas is discharged into the nozzle through a stub duct carried by the engine casing. Misalignment and movement between the duct and the nozzle is accommodated by movable sealing rings carried in the intermediate member which engage the outer surface of the duct. The sealing rings are spaced apart to form an annular chamber which is supplied with cooling air at a higher pressure than the pressure in the exhaust duct. The cooling air is arranged to cool the nozzle bearing and leakage passed the seals is of cooling air into the nozzle thus excluding hot exhaust gas from the engine bay.
摘要翻译： 描述了用于在VSTOL飞行器中的发动机安装的可向导喷嘴安装，其中热气喷嘴安装在机身上。 可旋转喷嘴通过轴承安装在诸如机身上的安装环的中间固定构件上。 热废气通过由发动机壳体承载的短管排出到喷嘴中。 管道和喷嘴之间的不对准和移动由在中间构件中承载的可移动密封环容纳，该密封环与管道的外表面接合。 密封环间隔开以形成环形室，其以比排气管道中的压力更高的压力供应冷却空气。 冷却空气被布置成冷却喷嘴轴承，并且通过密封件的泄漏将冷却空气进入喷嘴，从而排除来自发动机舱的热废气。
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公开(公告)号：US5115979A
公开(公告)日：1992-05-26
申请号：US706537
申请日：1991-05-28
CPC分类号： F02K1/805
摘要： A seal assembly is provided between an exhaust flap and a nozzle sidewall of a gas turbine engine exhaust nozzle. The assembly includes a housing fixedly joined to the exhaust flap and a plurality of adjoining plungers slidably disposed in the housing and each including a top extending outside a housing opening for defining a seal line for contacting the nozzle sidewall for sealing the exhaust gases from flowing therebetween. The seal lines collectively define a seal first contour being complementary to a first contour of the nozzle sidewall. A tie rod extends through the plungers and joins the plungers to the housing. The tie rod is flexible for allowing the plungers to rotate perpendicularly to the tie rod so that the seal lines collectively form a seal second contour, different than the seal first contour, to conform to a second contour of the nozzle sidewall which is different than the nozzle sidewall first contour.
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公开(公告)号：US5078412A
公开(公告)日：1992-01-07
申请号：US637847
申请日：1991-01-07
申请人： Charles F. Baumgarth
发明人： Charles F. Baumgarth
CPC分类号： F16J15/3284 , F02K1/805 , F16J15/0887 , F16J15/3212 , Y10S277/921
摘要： Disclosed is a continuous fluid pressure seal for use between two members that move relative to each other, that can withstand high temperatures, and that is separately loaded so as not to rely solely on a pressure differential across the seal for correct seating and orientation. The present invention further provides a seal which is effective between to movable members despite the presence of an obstruction therebetween.
摘要翻译： 公开了一种连续的流体压力密封件，用于两个构件之间的相对运动，其可承受高温，并且被单独加载，以便不仅仅依靠密封件上的压差来正确地固定和定向。 本发明还提供一种密封件，尽管在它们之间存在阻碍物，该密封件在可移动部件之间是有效的。
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