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1.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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2.发明授权Turbomachine casing with containment structure intended to contain fractured rotating parts 失效涡轮机外壳，带有包含断裂旋转部件的遏制结构
公开(公告)号：US4705454A
公开(公告)日：1987-11-10
申请号：US883845
申请日：1986-07-09
CPC分类号： F01D21/045 , Y02T50/672
摘要： Retaining structure for a turbo-machine forming an annulus having a complexircumferential construction comprising a cylindrical sector of a high mechanical strength material protecting a member secured on the casing of the machine. The complementary sector of the annulus is a honeycomb structure mounted between an internal and an external skin. The cylindrical sector is formed by a thickening of the internal skin. A strap of a material with a high elastic modulus serves to secure at least the complementary sector.
摘要翻译： 用于形成具有复杂周向构造的环的涡轮机的保持结构包括高机械强度材料的圆柱形部分，其保护固定在机器壳体上的构件。 环的互补部分是安装在内部和外部皮肤之间的蜂窝状结构。 圆柱形部分由内部皮肤增厚形成。 具有高弹性模量的材料的带子用于至少确保互补部分。
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公开(公告)号：US4558564A
公开(公告)日：1985-12-17
申请号：US543047
申请日：1983-10-18
CPC分类号： F16C27/04 , F01D25/162 , F01D5/025 , F16C2360/23 , Y02T50/673
摘要： In a multi-spool turbo machine, a first shaft of the low pressure spool is supported for rotation with respect to a second shaft of the high pressure spool and is located with respect to the second shaft by means of a roller bearing. Rollers of the bearing are inserted between an internal ring mounted on the second shaft and an outer ring mounted by a ring support assembly carried by the first shaft. The ring support assembly includes a ring support member which comprises, at its outer periphery, a first toothed element cooperating with a second toothed element carried by retaining means. The ring support member is held axially by a channel-section member.
摘要翻译： 在多阀芯涡轮机中，低压阀芯的第一轴被支撑成相对于高压阀芯的第二轴转动，并通过滚子轴承相对于第二轴定位。 轴承的滚子插入安装在第二轴上的内圈和由第一轴承载的环形支撑组件安装的外圈之间。 环支撑组件包括环支撑构件，该环支撑构件在其外周处包括与由保持装置承载的第二带齿元件配合的第一齿形元件。 环支撑构件由通道截面构件轴向保持。
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公开(公告)号：US4521160A
公开(公告)日：1985-06-04
申请号：US529938
申请日：1983-09-08
CPC分类号： F01D21/045 , F01D5/282 , F16C15/00 , Y02T50/672
摘要： Device for the containment of fragments of a fan ring in the event of burng of the ring.The fan ring comprises two cylindrical surfaces spaced axially and located radially inside of two containment rings of high tensile strength in the circumferential direction, engaged respectively in grooves of two parts of the rotor, located on either side of the fan ring.
摘要翻译： 用于在发生环的情况下容纳风扇环的碎片的装置。 风扇环包括轴向间隔开的两个圆柱形表面，并且位于沿周向方向具有高抗拉强度的两个容纳环的径向内侧，分别接合在位于风扇环两侧的转子的两个部分的槽中。
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5.发明授权
公开(公告)号：US4415310A
公开(公告)日：1983-11-15
申请号：US309210
申请日：1981-10-06
CPC分类号： F04D27/0215 , F01D5/087 , F02C6/08 , F02C7/18 , F04D29/321 , F01D5/3038 , F05D2250/14 , Y02T50/676
摘要： A system for cooling a gas turbine by bleeding air from the compressor and channeling the air at the center of the engine towards the turbine in order to cool it. The air is bled from the plane of the disc bearing the blades of the compressor, said disc having radial ducts for the flow of the air. The invention is utilized in gas turbine engines to cool the turbine.
摘要翻译： 一种用于通过从压缩机排出空气并将发动机中心的空气引向涡轮以冷却燃气轮机的系统。 空气从承载压缩机叶片的盘的平面排出，所述盘具有用于空气流动的径向管道。 本发明用于燃气涡轮发动机以冷却涡轮机。
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6.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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7.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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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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