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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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2.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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3.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：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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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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6.发明授权Variable section nozzle for a turbo-jet engine and an aircraft comprising such equipment 失效用于涡轮喷气发动机的可变截面喷嘴和包括这种设备的飞机
公开(公告)号：US4577814A
公开(公告)日：1986-03-25
申请号：US554301
申请日：1983-11-22
CPC分类号： F02K1/10 , F02K1/006 , Y02T50/671
摘要： The invention relates to a variable area nozzle for a turbo-jet engine. This nozzle comprises a convergent portion, formed by a fixed semi-shell (2) and a semi-shell (3) pivotal about a diametral axis (4a-4b); the fluid-tightness of the convergent portion is ensured by a substantially semi-circular seal (6) and by two longitudinal seals (7a, 7b). The nozzle can be used for example with an engine comprising a partial re-heat system of moderate output.
摘要翻译： 本发明涉及一种用于涡轮喷气发动机的可变区域喷嘴。 该喷嘴包括由固定的半壳体（2）和围绕径向轴线（4a-4b）枢转的半壳体（3）形成的会聚部分; 收敛部分的流体密封性通过基本上为半圆形的密封件（6）和两个纵向密封件（7a，7b）来确保。 喷嘴可以例如用于包括中等输出的局部再热系统的发动机。
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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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8.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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9.发明授权Sealing ring for a turbine rotor of a turbo machine and turbo machine installations provided with such rings 失效用于涡轮机的涡轮转子的密封环和具有这种环的涡轮机装置
公开(公告)号：US4596116A
公开(公告)日：1986-06-24
申请号：US575988
申请日：1984-02-01
CPC分类号： F01D11/24 , F01D11/08 , Y02T50/672
摘要： The rotor of each stage of a turbine is surrounded, with a clearance by a fixed ring, formed by a metal ring supporting internally an annular thermal screen, in the form of ceramic segments. Expansions and contractions of the metal ring under the action of air which is supplied thereto in order to control the said clearance are transformed into displacements of radial faces of the ring in contact with radial flanges rigid with the turbine casing and seals serve to ensure fluidtightness of the ring.
摘要翻译： 涡轮机每级的转子由陶瓷段形式围绕着由固定环形成的间隙，其由内部支撑环形热筛的金属环形成。 在为了控制所述间隙而被供应到其中的空气作用下金属环的膨胀和收缩转变成与涡轮机壳体刚性的径向凸缘接触的环的径向面的位移，并且用于确保液体密封性 戒指。
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公开(公告)号：US4543039A
公开(公告)日：1985-09-24
申请号：US547711
申请日：1983-11-01
CPC分类号： F01D25/26 , F01D11/24 , F01D9/041 , F04D29/542
摘要： A device for attaching the stator vanes of an axial compressor to an external housing is disclosed. The attachment utilizes an inner casing, having the vanes mounted on it, and an outer casing surrounding the inner casing in such a manner that differential thermal expansion between the various elements is minimized. This allows more accurate control of the clearances between the rotor and the stator.
摘要翻译： 公开了一种用于将轴向压缩机的定子叶片连接到外部壳体的装置。 该附件利用具有安装在其上的叶片的内壳和围绕内壳的外壳，使得各种元件之间的不同热膨胀最小化。 这允许更精确地控制转子和定子之间的间隙。
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