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91.发明授权Process for the assembly of at least two parts made from a composite material incorporating a ceramic or vitroceramic matrix reinforced by ceramic fibres 失效用于组装由包含陶瓷纤维增强的陶瓷或陶瓷基体的复合材料制成的至少两个部件的方法
公开(公告)号：US5448041A
公开(公告)日：1995-09-05
申请号：US74408
申请日：1993-06-10
CPC分类号： C04B37/005 , C03B23/20 , C03C27/06 , C04B2235/5224 , C04B2235/5244 , C04B2237/064 , C04B2237/083 , C04B2237/10 , C04B2237/341 , C04B2237/38 , C04B2237/592 , C04B2237/595 , C04B2237/708
摘要： A process for assembling at least two parts made from a composite material incorporating a ceramic or vitroceramic matrix reinforced by ceramic fibers. A continuous connection between these parts is achieved by approaching two of the parts along their respective edges to be assembled, forming a joint between the two parts by sewing with a tie or link of ceramic fibers from each of the parts to be assembled and heating the joints by a heating device employing a powerful and extremely localized heating until the two parts are welded together.
摘要翻译： 用于组装由包含陶瓷纤维增强的陶瓷或陶瓷基体的复合材料制成的至少两个部件的方法。 这些部件之间的连续连接是通过沿其相应边缘的两个部件接近组装而实现的，通过用要组装的每个部件的陶瓷纤维的连接或连接缝合来在两个部件之间形成接头，并加热 通过采用强大且非常局部化的加热的加热装置将两个部件焊接在一起。
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公开(公告)号：US5417782A
公开(公告)日：1995-05-23
申请号：US70862
申请日：1993-06-03
申请人： Jean-Marc Rongvaux
发明人： Jean-Marc Rongvaux
CPC分类号： C22F1/10
摘要： A nickel-based superalloy known by the designation "718" and having a typical composition comprising, in percentages by weight, Cr 19, Fe 18, Nb 5, and the remainder Ni, is subjected, after the usual thermo-mechanical and heat treatment steps, to an additional annealing step wherein the temperature and duration are selected from the following range as desired:800.degree. C. for between 5 and 30 hours;750.degree. C. for between 25 and 70 hours; and700.degree. C. for between 100 and 300 hours.This leads to a definite improvement in the behaviour of parts made from the superalloy, in terms of fatigue cracking, when used at temperatures over 650.degree. C.
摘要翻译： 在通常的热机械和热处理之后，经过名称为“718”的具有典型组成的镍基超级合金，其中包含以重量％计，Cr 19，Fe 18，Nb 5和余量为Ni的组合物 步骤，至另外的退火步骤，其中温度和持续时间根据需要从以下范围中选择：800℃，持续5至30小时; 750℃，持续25-70小时; 和700℃下进行100-300小时。 这导致了当在超过650℃的温度下使用时，由超耐热合金制成的部件在疲劳裂纹方面的作用有明显的改善。
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公开(公告)号：US5413270A
公开(公告)日：1995-05-09
申请号：US174403
申请日：1993-12-28
摘要： A method for removing a portion of a coating disposed on a plate, in which a nozzle having a wide jet is first utilized to remove most of the material of the portion to be removed. Successively or concurrently therewith, at least one fine jet nozzle is utilized to cut the contour of the portion of the coating being removed. The method is particularly advantageous for removing deposits of a plasma deposition, and more particularly for deposits which resist a diffusion welding or soldering of plates or substrates with one another.
摘要翻译： 一种用于去除布置在板上的涂层的一部分的方法，其中首先利用具有宽射流的喷嘴去除待除去部分的大部分材料。 连续或同时地，使用至少一个细小的喷嘴来切割被去除的涂层部分的轮廓。 该方法特别有利于去除等离子体沉积物的沉积物，更具体地说，用于抵抗板或基板彼此扩散焊接或焊接的沉积物。
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公开(公告)号：US5407322A
公开(公告)日：1995-04-18
申请号：US125753
申请日：1993-09-24
申请人： Jean-Louis Charbonnel , Jean-Luc C. Y. Goga , Gerard G. Miraucourt , Jacky S. Naudet , Denis B. Pottier
发明人： Jean-Louis Charbonnel , Jean-Luc C. Y. Goga , Gerard G. Miraucourt , Jacky S. Naudet , Denis B. Pottier
CPC分类号： F01D17/162 , F16B4/00 , F05D2300/505 , Y02T50/672
摘要： Variable phase vane provided with a composite pivot having a joining piece for receiving the control pieces. The joining piece is made of a material less dense than the actual pivot. These two elements are force-fitted without using any weld or mechanical linking device. The vane finally obtained is thus rendered lighter in weight
摘要翻译： 具有复合枢轴的可变相叶片具有用于接收控制件的接合件。 连接件由比实际枢轴密度小的材料制成。 这两个元件是强制安装的，不使用任何焊接或机械连接装置。 因此，最终获得的叶片的重量更轻
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公开(公告)号：US5383355A
公开(公告)日：1995-01-24
申请号：US56889
申请日：1993-05-05
摘要： A system for the examination or inspection of a gas turbine engine in which a computer 3 controls a series of probes by way of devices for controlling movements in different directions. Thus, there is a centralized control of the measurements for allowing faster performance. The system is applicable to tests on gas turbine engines, particularly prior to mass production.
摘要翻译： 一种用于检查或检查燃气涡轮发动机的系统，其中计算机3通过用于控制不同方向的运动的装置来控制一系列探针。 因此，对于允许更快性能的测量进行集中控制。 该系统适用于燃气涡轮发动机的试验，特别是在大规模生产之前。
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96.发明授权Variable geometry flame trap device for use in an after-burner device of a gas turbine 失效用于燃气轮机的后燃烧器装置的可变几何形状的火焰捕集装置
公开(公告)号：US5269138A
公开(公告)日：1993-12-14
申请号：US16074
申请日：1993-02-10
CPC分类号： F23R3/22
摘要： A variable geometry flame trap device for use in an after-burner device of a gas turbine, which is not exposed to deformation forces during its use in the after-burner mode. This is achieved with a plurality of flame trap plate pairs (21), positioned downstream of the turbine at the outlet of a primary air flow duct (9) and mounted so as to pivot on a plurality of diffuser arms (19) located at the outlet of a secondary air flow duct (7), characterized in that the plates (21) of each pair are made from a composite material and in that they have a cam projecting from their facing faces (42), said two cams (43) bearing on one another.
摘要翻译： 一种用于燃气轮机的后燃烧器装置的可变几何型火焰捕集装置，其在后燃烧器模式中的使用期间不会受到变形力的影响。 这是通过多个阻气板对（21）来实现的，其位于涡轮机的主要空气流动管道（9）的出口的下游，并且安装成在位于所述主要空气流动管道（9）处的多个扩散器臂 二次气流管道（7）的出口，其特征在于，每对的板（21）由复合材料制成，并且它们具有从其相对面（42）突出的凸轮，所述两个凸轮（43） 彼此相依。
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公开(公告)号：US4928483A
公开(公告)日：1990-05-29
申请号：US367627
申请日：1989-06-19
CPC分类号： F02C6/08 , F01D11/005 , F02C7/20 , F02C7/28 , F02C7/32
摘要： The present invention provides an air tapping device for tapping a portion of the air passing through the bypass duct of a fan-type turbojet engine. The device is incorporated into the engine mount and is provided with an anti-vibration mounting to minimize the transmission of engine vibrations to the air tapping device. The device is preferably incorporated into the rear engine mount which attaches the engine to the aircraft structure.
摘要翻译： 本发明提供一种用于抽出通过风扇式涡轮喷气发动机的旁路管道的空气的一部分的空气攻丝装置。 该装置结合到发动机支架中并且设置有防振安装件，以将发动机振动的传递最小化到排气装置。 该装置优选地结合到将发动机附接到飞行器结构的后部发动机支架中。
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公开(公告)号：US4899539A
公开(公告)日：1990-02-13
申请号：US295998
申请日：1989-01-12
摘要： A flow mixer and flame stabilizer structure for an afterburner of a turbofan engine is disclosed having a variable mixer to mix a portion of the cold flow with the hot flow gasses and which also forms a flame stabilizer for a secondary afterburner fuel injection manifold which injects fuel into the cold flow air during afterburner operation. The device forms a flame stabilizer around the secondary, annular fuel injection manifold and has a generally "U" shaped cross-section. One of the legs forming the "U" shape is fixed, while the opposite leg is movable so as to vary the downstream facing opening between the legs. The movable leg also blocks a portion of the cold flow duct to generate localized increases in pressure upstream of the stabilizer. An air scoop located in this upstream portion communicates with the primary afterburner flame stabilizer to direct pressurized air to cool the primary flame stabilizer.
摘要翻译： 公开了一种用于涡轮风扇发动机的后燃器的流动混合器和火焰稳定器结构，其具有可变混合器以将冷流的一部分与热流体气体混合，并且还形成用于喷射燃料的二次加力燃料喷射歧管的火焰稳定器 在后燃器运行期间进入冷流空气。 该装置在次级环形燃料喷射歧管周围形成火焰稳定器，并且具有大致“U”形的横截面。 形成“U”形状的一个腿是固定的，而相对的腿是可移动的，以便改变腿之间的下游面向开口。 可移动的腿还阻挡冷流道的一部分以产生稳定器上游压力的局部增加。 位于该上游部分的空气勺与主辅助燃烧器火焰稳定器连通，以引导加压空气冷却主火焰稳定器。
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公开(公告)号：US4899535A
公开(公告)日：1990-02-13
申请号：US229473
申请日：1988-08-08
CPC分类号： F02C7/236 , F02C7/14 , F02C7/22 , Y02T50/675
摘要： In a turbojet fuel supply system in which a controlled flow of fuel ql is diverted from between the high pressure pump and the feed flow regulator and recycled upstream of the high pressure pump in order to maintain a substantially constant pressure differential cross the feed regulator, a flow qc is tapped from the hot flow ql for return to the fuel tank and to allow a correspondingly greater portion of cold fuel from the low pressure pump to be mixed with the recycled hot fuel ql delivered to the high pressure pump. If necessary, the tapped hot flow qc is mixed with a flow of cold fuel qf tapped from the low pressure pump output to form a lukewarm mixture qr for return to the tank.
摘要翻译： 在涡轮喷气燃料供应系统中，其中控制的燃料流量q1从高压泵和进料流量调节器之间转移并在高压泵的上游再循环，以便保持基本上恒定的压力差与进料调节器交叉， 从热流q1抽出流量qc以返回到燃料箱，并允许来自低压泵的相应较大部分的冷燃料与输送到高压泵的回收热燃料q1混合。 如果需要，将轻敲的热流qc与从低压泵输出端抽出的冷燃料流混合，形成一个回流到油箱的冷热混合物qr。
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公开(公告)号：US4863354A
公开(公告)日：1989-09-05
申请号：US253760
申请日：1988-10-05
CPC分类号： B64C11/14 , F02C7/047 , F05D2200/221 , Y02T50/672
摘要： A nose cowl or spinner is provided for a fixed, non-rotatable central hub of a turbojet engine having assembly means that facilitate the attachment and detachment of the nose cowl to the central hub, and provides a readily visible indication of whether or not the nose cowl has been properly assembled to the hub. The nose cowl has a smooth outer surface to provide undisturbed air flow into the turbojet engine compressor and defines means to circulate heated air to prevent icing of the external surface. An inner cowl member is attached to a bearing cover of the central hub in a non-rotatable manner, an outer cowl member is axially locked to the central hub so as to be concentrally arranged about the inner cowl member, and a locking device is used to lock the inner and outer cowl members together to prevent inadvertent rotation of the outer cowl member.
摘要翻译： 提供了一种用于涡轮喷气发动机的固定的，不可旋转的中心轮毂的鼻罩或旋转器，其具有便于将鼻罩安装和拆卸到中心轮毂的组装装置，并且提供了鼻子 整流罩已正确组装到集线器。 鼻罩具有光滑的外表面，以提供未受干扰的空气流入涡轮喷气发动机压缩机，并且限定了循环加热空气以防止外表面结冰的装置。 内罩壳部件以不可旋转的方式附接到中心轮毂的轴承盖上，外整流罩部件轴向地锁定到中心轮毂，以便围绕内整流罩部件同心地布置，并且使用锁定装置 以将内外罩组件锁定在一起以防止外罩组件的意外旋转。
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