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公开(公告)号：US4974638A
公开(公告)日：1990-12-04
申请号：US260775
申请日：1988-10-21
CPC分类号： F01D25/30 , F02K1/82 , Y02T50/672
摘要： A transition pipe for location between an afterburner pipe and a jet nozzle in a jet pipe assembly for a turbojet engine comprises a funnel shaped inner casing tapering downstream from a circular section at its upstream end to a quadrangular section at its downstream end, a horn shaped outer casing surrounding the inner casing and flared downstream from a circular upstream end section to a downstream end section formed of four joined segments of generally parabolic shape, and a plurality of peripherally spaced, longitudinally extending stiffeners interconnecting the inner and outer casings in the space therebetween.
摘要翻译： 在用于涡轮喷气发动机的喷射管组件中的用于位于加力管和喷嘴之间的过渡管包括漏斗形内壳，其在其上游端处的圆形截面的下游锥形，在其下游端处具有四边形部分， 外壳围绕内壳并且从圆形上游端部分向下游延伸到由四个大致抛物线形状的连接部分形成的下游端部分，以及多个周向间隔开的纵向延伸的加强件，其将内壳体和外壳体之间的空间相互连接 。
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2.发明授权Heat protective lining for an afterburner or transition duct of a turbojet engine 失效涡轮发动机燃烧器或过渡管的保护衬里
公开(公告)号：US5069034A
公开(公告)日：1991-12-03
申请号：US521036
申请日：1990-05-08
CPC分类号： F23R3/002 , F02K1/822 , F23R3/60 , F05D2250/34 , Y02T50/672 , Y02T50/675
摘要： A heat protective lining for the afterburner or transition duct of a turbojet engine comprises an assembly of tiles overlapping laterally and longitudinally to form overlapping rings of tiles in which the tiles of each ring are offset laterally from those of each adjacent ring by half a tile width. The tiles are held together by eyelets projecting from the overlapped downstream portions of the tiles through apertures in the overlapping upstream portions, and locking members engaging through the eyelets. Fastening yokes for fixing the assembly to the duct casing are secured to the outside of the tiles.
摘要翻译： 用于涡轮喷气发动机的后燃器或过渡管道的保护衬里包括横向和纵向重叠的瓦片组合，以形成瓦片的重叠环，其中每个环的瓦片横向偏离每个相邻环件的瓦片半块宽度 。 瓦片通过在重叠的上游部分中的孔从突出的瓦片的下游部分突出的孔眼保持在一起，并且锁定构件通过孔眼接合。 用于将组件固定到管壳的紧固轭被固定到瓦的外部。
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3.发明授权
公开(公告)号：US4907743A
公开(公告)日：1990-03-13
申请号：US269725
申请日：1988-11-10
CPC分类号： F23R3/60 , F02K1/04 , F02K1/80 , F05D2230/642
摘要： Two coaxial bodies of revolution made of materials having distinctly different expansion coefficients are joined together to form an assembly by fixing means comprising at least three resilient brackets of trapezoidal shape, the larger end of each bracket having a flanged edge secured at at least two points by hollow rivets to a metal ring and by bolts extending through the rivets to the body with the higher expansion coefficient, and the smaller end of each bracket being secured by at least one bolt to the body with the lower expansion coefficient in a manner which imposes a cold prestress on the bracket.
摘要翻译： 由具有明显不同的膨胀系数的材料制成的两个旋转同轴体连接在一起，以通过包括至少三个梯形形状的弹性支架的固定装置形成组件，每个支架的较大端具有通过在至少两个点处固定的凸缘 空心铆钉到金属环，并且以螺栓延伸穿过铆钉到具有较高膨胀系数的主体，并且每个支架的较小端部以至少一个螺栓固定到具有较低膨胀系数的体系，其方式为施加 支架上的冷预应力。
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公开(公告)号：US4778109A
公开(公告)日：1988-10-18
申请号：US133886
申请日：1987-12-16
CPC分类号： F02K1/006 , F02K1/1223 , F02K1/1292 , F02K1/62
摘要： An adjustable two-dimensional nozzle is disclosed in which simplified control means are located away from the flow of gasses through the nozzle. The nozzle includes a movable frame located outside of fixed sidewalls and has pivotally attached thereto a pair of upstream or converging nozzle flaps. Upstream edges of the upstream flaps are attached to the movable frame such that the flaps pivot about axes extending substantially perpendicular to the longitudinal axis of the nozzle. Downstream or diverging flaps are attached to the downstream edges of the upstream flaps such that these flaps also pivot about axes extending substantially perpendicular to the longitudinal axis of the nozzle. A cam member extends between each of the movable frames and each downstream flap to control the angular variations of the flaps during movement of the frame. The flap arrangements are symmetrically arranged with respect to a plane passing through the longitudinal axis of the nozzle, such that translational movement of the frames will alter the cross-section of the nozzle in a symmetrical manner with respect to the plane. If the frame is rotated about its pivot attachment, the nozzle flaps will be asymmetrically adjusted and may be utilized to vector the thrust of the gasses emanating from the nozzle.
摘要翻译： 公开了一种可调节的二维喷嘴，其中简化的控制装置位于远离气体流经喷嘴的位置。 喷嘴包括位于固定侧壁外侧的可移动框架，并且可旋转地附接有一对上游或会聚的喷嘴襟翼。 上游翼片的上游边缘附接到可移动框架，使得翼片围绕基本上垂直于喷嘴的纵向轴线延伸的轴线枢转。 下游或发散的翼片附接到上游翼片的下游边缘，使得这些翼片也围绕基本上垂直于喷嘴的纵向轴线延伸的轴线枢转。 凸轮构件在每个可移动框架和每个下游翼片之间延伸以在框架移动期间控制翼片的角度变化。 翼片装置相对于穿过喷嘴的纵向轴线的平面对称地布置，使得框架的平移运动将相对于平面以对称的方式改变喷嘴的横截面。 如果框架绕其枢轴附件旋转，则喷嘴挡板将被不对称地调节，并且可以用于对从喷嘴发出的气体的推力进行矢量化。
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公开(公告)号：US5305600A
公开(公告)日：1994-04-26
申请号：US025780
申请日：1993-03-03
摘要： The rotor of a fan disposed in the annular noncombusted air flow duct of aurbojet propulsion engine of the bypass type is carried by a rotary body which includes the rotor assembly of a multi-stage turbine driven by noncombusted air supplied thereto by an axisymmetrical auxiliary duct which diverts noncombusted air from the primary duct of the engine just downstream of the compressor.
摘要翻译： 设置在旁路型涡轮喷气推进发动机的环形未燃气流管道中的风扇的转子由旋转体承载，旋转体包括由轴对称辅助管道向其供应的非燃气的驱动的多级涡轮的转子组件 其在紧邻压缩机下游的发动机的主管道上转移未燃空气。
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6.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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