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公开(公告)号：US5566884A
公开(公告)日：1996-10-22
申请号：US336491
申请日：1981-12-30
IPC分类号： F02K1/12
CPC分类号： F02K1/1223 , F05D2250/323 , F05D2250/324 , Y02T50/671
摘要： Convergent flaps of a jet engine nozzle are controlled by actuating cylinders through actuating levers hinged to the fixed structure of the engine and by connecting rods. Divergent flaps are slaved to the convergent flaps by connecting rods themselves driven by the actuating levers. Cold flaps not hinged to the divergent flaps are slaved to the convergent flaps by further connecting rods connected to the first-named connecting rods.
摘要翻译： 喷气发动机喷嘴的收敛翼片通过致动液压缸通过铰链到发动机的固定结构的致动杆和通过连接杆来控制。 通过由致动杆驱动的连接杆本身，不同的翼片从收敛的翼片中被切割。 通过连接到第一个连接杆的另外的连接杆，不铰接到发散的翼片的冷襟翼被奴隶到收敛的襟翼。
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公开(公告)号：US5542607A
公开(公告)日：1996-08-06
申请号：US448528
申请日：1982-11-24
IPC分类号： F02K1/12
CPC分类号： F02K1/1223 , F05D2250/323 , F05D2250/324 , Y02T50/671
摘要： A turbojet engine has an outlet duct to which an annular array of actuating cylinders for nozzle flaps are hinged. The housings for the cylinders are connected together by transverse members to form a rigid structure coaxial with the outlet duct. The arrangement includes convergent flaps and slaving devices for divergent flaps, all hinged to the rigid structure and particularly to the housings.
摘要翻译： 涡轮喷气发动机具有出口管道，用于喷嘴襟翼的致动气缸的环形阵列被铰接在该出口管道上。 用于气缸的壳体通过横向构件连接在一起以形成与出口管同轴的刚性结构。 该装置包括用于发散襟翼的会聚翼片和从动装置，其全部铰接于刚性结构，特别是铰接到外壳上。
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3.发明授权Nozzle for a jet engine containing an adjustable convergent-divergent portion 失效用于喷气发动机的喷嘴，其包含可调节的收敛 - 发散部分
公开(公告)号：US5520336A
公开(公告)日：1996-05-28
申请号：US237399
申请日：1981-01-13
IPC分类号： F02K1/12
CPC分类号： F02K1/12 , F02K1/1223 , F05D2250/323 , F05D2250/324 , Y02T50/671
摘要： A nozzle comprises: a set of first flaps articulated to a rigid structure, and forming a convergent; a set of second flaps each articulated to a corresponding first flap, and forming a divergent; a set of third flaps each of which is connected at a position between two adjacent second flaps and which is, on the one hand, articulated to the rigid structure and, on the other hand, linked to each of the two adjacent second flaps by carrier linked to the aforesaid third flap by a ball joint.
摘要翻译： 喷嘴包括：一组铰接到刚性结构的第一翼片，并且形成会聚; 一组第二翼片，每个第二翼片铰接到相应的第一翼片，并形成发散; 一组第三翼片，每个翼片连接在两个相邻的第二翼片之间的位置，并且一方面铰接到刚性结构，另一方面通过载体连接到两个相邻的第二翼片中的每一个 通过球形接头连接到上述第三挡板。
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4.发明授权
公开(公告)号：US4674951A
公开(公告)日：1987-06-23
申请号：US770247
申请日：1985-08-28
IPC分类号： F04D27/02
CPC分类号： F02K7/075 , F04D27/0215 , F04D27/023 , Y02T50/672
摘要： A ring of an annular valve assembly is movable in the direction of its longitudinal axis and is intended for an axial compressor blow-off arrangement. The ring takes the form of an axially orientated channel-section member having a first annular skin of concave section nested in a second annular skin also of concave section. A cavity filled with a synthetic resin filler is defined by the two skins. The blow-off arrangement for an axial-flow compressor of a turbo-jet engine, which incorporates this ring, comprises an annular opening with which the ring cooperates to re-form the wall of the air flow when the blow-off arrangement is inoperative.
摘要翻译： 环形阀组件的环可以在其纵向轴线的方向上移动，并且用于轴向压缩机吹出装置。 该环采取轴向定向的通道截面构件的形式，其具有嵌在第二环形表皮中的凹部的第一环形表皮，也是凹形部分。 填充有合成树脂填料的空腔由两个表皮限定。 涡轮喷气发动机的轴流式压缩机的排放装置，其结合了该环，包括环形开口，当排放装置不起作用时，该环与该空气合流以重新形成空气流的壁 。
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公开(公告)号：US4541567A
公开(公告)日：1985-09-17
申请号：US502203
申请日：1983-06-08
CPC分类号： F02K1/12 , Y10S60/905
摘要： A vane for a convergent-divergent nozzle is constituted by a central body d a base plate. The central body comprises a reinforcement substantially in the shape of an isoceles triangle and of channel section, the reinforcement having internal and external edge flanges and a cover plate of the same shape and dimensions as the reinforcement, the reinforcement being secured to the flanges of the latter.The base plate is rectangular and has a triangular opening of a contour corresponding to that of the reinforcement. The central body is secured to the base plate by securing means constituted by a profiled member of a shape corresponding to that of the opening.The central body is of a composite carbon-carbon material; the base plate and securing means, of steel.
摘要翻译： 收敛发散喷嘴的叶片由中心体和基板构成。 中心体包括基本上等间距三角形和通道部分形状的加强件，该加强件具有内部和外部边缘凸缘以及与加强件相同形状和尺寸的盖板，该加强件固定到该凸缘的凸缘上 后者。 基板是矩形的，具有与加强件相对应的轮廓的三角形开口。 中心体通过由与开口相对应的形状的成形构件构成的固定装置固定在基板上。 中心体为复合碳 - 碳材料; 基板和固定装置。
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公开(公告)号：US5593278A
公开(公告)日：1997-01-14
申请号：US568223
申请日：1983-12-30
申请人： Gerard E. A. Jourdain , Jean-Paul Lagrange , Gerard M. F. Mandet , Jacques H. Mouchel , Jean-Philippe E. Richard , Marcel R. Soligny
发明人： Gerard E. A. Jourdain , Jean-Paul Lagrange , Gerard M. F. Mandet , Jacques H. Mouchel , Jean-Philippe E. Richard , Marcel R. Soligny
CPC分类号： F01D11/18 , F01D25/246 , Y02T50/67 , Y02T50/671
摘要： The disclosed invention relates to a sealing device for the rotor blades of a gas turbine engine which permits real time adjustment to be made of the clearances between the rotor blade tips and the sealing structure. The sealing shroud around the turbine wheel is formed of sectors, each sector being attached to a monolithic short response time ring and a monolithic long response time ring. Ventilating air from upstream of the turbine wheel is directed onto the rings such that the sectors are caused to radially expand or contract in compliance with the expansion or contraction of the tips of the rotor blades during stabilized and transient engine operational modes. A small positive clearance between the sealing sectors and the blade tips is maintained throughout the range of the engine's operation.
摘要翻译： 所公开的本发明涉及一种用于燃气涡轮发动机的转子叶片的密封装置，其允许由转子叶片尖端和密封结构之间的间隙进行实时调节。 涡轮机轮周围的密封罩由扇形部分组成，每个扇形部分连接到单片短响应时间环和单片长响应时间环。 涡轮机叶轮上游的通风空气被引导到环上，使得在稳定和瞬态的发动机操作模式期间，这些扇区在转子叶片的尖端的膨胀或收缩下被引起径向膨胀或收缩。 在发动机运行的整个范围内，保持密封扇区和叶片尖端之间的小的正间隙。
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公开(公告)号：US4409791A
公开(公告)日：1983-10-18
申请号：US212748
申请日：1980-12-04
CPC分类号： F23R3/60 , F02C7/222 , F23R3/283 , F23D2211/00
摘要： A fuel intake tube passes radially through an engine casing. It is surrounded between the casing and an injector head by a second tube attached to the casing. Guidance means and a sealing element are provided between the fuel intake tube and the second tube. The device is equipped with one or more injector heads. The guidance means consist of two elements: a cap and cylindrical projections.
摘要翻译： 燃料吸入管径向通过发动机壳体。 通过附接到壳体的第二管将其包围在壳体和喷射头之间。 引导装置和密封元件设置在燃料进入管和第二管之间。 该装置装备有一个或多个喷射头。 导向装置由两个元件组成：盖和圆柱形突起。
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8.发明授权Device for connecting a burner ring or flame holder to an afterburner duct of a turbojet engine 失效用于将燃烧器环或火焰保持器连接到涡轮喷气发动机的后燃器管的装置
公开(公告)号：US4724671A
公开(公告)日：1988-02-16
申请号：US903250
申请日：1986-09-03
CPC分类号： F23R3/20
摘要： A connection device is disclosed for connecting a burner ring or flame holder made of a composite material and having a "V"-shaped cross-section, to an afterburner chamber duct of a turbojet engine. The connecting device has a cylindrical portion and a trapezoidal portion. The cylindrical portion extends through hollow projections formed from the composite ring material and extending from the ring in an upstream direction. The converging, opposite sides of the trapezoidal portion bear against inner surfaces of the converging flanges forming the "V" cross-section of the ring. The cylindrical portion is then attached to the afterburner duct via a link-bar mechanism.
摘要翻译： 公开了一种连接装置，用于将由复合材料制成并具有“V”形横截面的燃烧器环或火焰保持器连接到涡轮喷气发动机的后燃室室管道。 连接装置具有圆筒形部分和梯形部分。 圆柱形部分延伸穿过由复合环材料形成的中空凸起，并沿着上游方向从环延伸。 梯形部分的会聚的相对侧面抵靠形成环的“V”横截面的会聚凸缘的内表面。 圆柱形部分然后通过连杆机构连接到后燃器管道。
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公开(公告)号：US4353516A
公开(公告)日：1982-10-12
申请号：US169151
申请日：1980-07-15
摘要： Two groups of half shells capable of being retracted from the jet flow, in a position closing the jet pipe. The thrust reverser and the silencer are concentric and their axes of rotation are upstream with respect to their position in the jet flow.
摘要翻译： 两组半壳能够在关闭喷射管的位置中从喷射流中缩回。 推力反向器和消音器是同心的，并且它们的旋转轴线相对于它们在喷射流中的位置是上游的。
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公开(公告)号：US5700130A
公开(公告)日：1997-12-23
申请号：US474526
申请日：1983-03-09
IPC分类号： F01D5/08
CPC分类号： F01D5/081 , F05D2300/502 , F05D2300/603 , Y02T50/672 , Y02T50/676
摘要： This device embodies a centrifugal compressor secured to a joint-carrier disk secured to an upstream flange of the rotor disk to be cooled. The recompressed air is ejected through channels near the roots of the blades of the disk.
摘要翻译： 该装置体现了一种离心式压缩机，该离心式压缩机被固定到固定到要冷却的转子盘的上游凸缘上的联合承载盘。 再压缩的空气通过靠近盘的叶片根部的通道排出。
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