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188 条记录 (耗时 0.024 秒)

    Particle traps for turbo-prop engine
    61.
    发明授权
    Particle traps for turbo-prop engine 有权
    用于涡轮增压发动机的颗粒捕集器

    公开(公告)号：US6129509A

    公开(公告)日：2000-10-10

    申请号：US342730

    申请日：1999-06-29

    申请人： Antoine Emmanuel Cousin ,  Georges Mazeaud

    发明人： Antoine Emmanuel Cousin ,  Georges Mazeaud

    IPC分类号： B64D33/02 ,  F02C7/052 ,  F02C7/20 ,  F02G3/00

    CPC分类号： F02C7/052 ,  B64D33/02 ,  F02C7/20 ,  B64D2033/0246 ,  B64D2033/0293 ,  Y02T50/671

    摘要： The particle trap (15) that extends behind an elbow in the air flow stream (6) in a turbo-prop engine is delimited at the back by an end plate (12) to which intake housing suspension rods (10) supporting the front of the rotating shaft (2), are fastened. It is divided by suspension arms (11) which may be drilled (21) to restore the continuity of the annular chamber forming the trap. Therefore the intake housing suspension device extends through the trap. This type of trap makes use of the inertia of solid bodies carried by the air drawn in, and which could damage the engine blades, and to collect them.

    摘要翻译： 在涡轮驱动发动机中在空气流（6）中延伸到弯头后面的颗粒捕集器（15）在后面由端板（12）界定，入口壳体悬架杆（10）支撑在 旋转轴（2）被紧固。 它被悬挂臂（11）分开，可以钻（21）以恢复形成陷阱的环形室的连续性。 因此，进气室悬挂装置延伸穿过疏水阀。 这种陷阱利用被吸入的空气携带的固体的惯性，并且可能损坏发动机叶片并收集它们。

    Gas containment box used with a welding head
    66.
    发明授权
    Gas containment box used with a welding head 失效
    气体收容箱用于焊接头

    公开(公告)号：US5950904A

    公开(公告)日：1999-09-14

    申请号：US877557

    申请日：1997-06-17

    申请人： Florent Camy ,  Gerard Louis Zanolin

    发明人： Florent Camy ,  Gerard Louis Zanolin

    IPC分类号： B23K9/16 ,  B23K37/00 ,  B23K1/00 ,  B23K37/02

    CPC分类号： B23K9/162

    摘要： This invention concerns a containment box disposed around a welding head (1) and including a fixed frame carrying a fairing (16) modeled to the shape of the element (3) to be welded, a cover (9) sliding on the frame (10), and a bell with spherical boss (7) integral with the welding head (1) which slides and rotates in a vertical sleeve (8) traversing the cover (9). All the movements of the welding head (1) are therefore permitted which makes it possible to have complicated welding trajectories. Gaskets (15, 17) are provided.

    摘要翻译： 本发明涉及一种围绕焊接头（1）设置的容纳箱，其包括固定框架，该固定框架承载着待被焊接的元件（3）的形状的整流罩（16），在框架（10）上滑动的盖 ）和具有与焊接头（1）成一体的球形凸台（7）的钟形件，其在穿过盖（9）的垂直套筒（8）中滑动并旋转。 焊接头（1）的所有运动因此被允许，这使得可以具有复杂的焊接轨迹。 垫圈（15,17）。

    Process for the manufacture of a hollow turbomachine blade and apparatus for use in said process
    67.
    发明授权
    Process for the manufacture of a hollow turbomachine blade and apparatus for use in said process 失效
    用于制造中空涡轮机叶片的方法和用于所述方法的装置

    公开(公告)号：US5946802A

    公开(公告)日：1999-09-07

    申请号：US909874

    申请日：1997-08-12

    申请人： Gilles Michel George Louis Calle ,  Gilles Charles Klein

    发明人： Gilles Michel George Louis Calle ,  Gilles Charles Klein

    IPC分类号： B23P15/02 ,  B21D26/02 ,  B21D26/027 ,  B21D26/055 ,  B21D53/78 ,  C22F1/00 ,  C22F1/18 ,  F01D5/18 ,  F02C7/00 ,  B23P15/00

    CPC分类号： B21D26/027 ,  B21D26/055 ,  B21D53/78 ,  Y10T29/49339 ,  Y10T29/49341

    摘要： In a process for the manufacture of a hollow turbomachine blade in which die-forged and machined sheets are assembled and diffusion welded face to face after applying an antidiffusion coating to areas of the sheets where the assembly is to be expanded in forming the hollow blade, the welded assembly is subjected to a step of unsticking the coated areas of the sheets which are pressed together during the diffusion welding step, the unsticking step including subjecting the assembly to localized heating in a region where the intermediate sheet is provided with intercavity communication holes, and injecting pressurized gas into the welded assembly in a controlled manner to hot form a gas distribution duct in the locally heated region of the assembly to facilitate unsticking of the remainder of the coated areas. Apparatus for use in carrying out the unsticking step is also described.

    摘要翻译： 在制造中空涡轮机叶片的方法中，其中组装模锻和加工的片材并且在将组合件在形成中空叶片中的片材的区域上施加抗扩散涂层之后面对面地扩散焊接， 对焊接组件进行剥离在扩散焊接步骤期间被压在一起的片材的涂覆区域的步骤，该脱模步骤包括使组件在中间片材设置有腔间连通孔的区域中进行局部加热， 并且以受控的方式将加压气体注入焊接组件中以在组件的局部加热区域中热形成气体分配管道，以促进其余涂覆区域的剥离。 还描述了用于执行脱胶步骤的装置。

    Fuel injection system with improved air/fuel homogenization
    68.
    发明授权
    Fuel injection system with improved air/fuel homogenization 失效
    具有改善空气/燃料均质化的燃油喷射系统

    公开(公告)号：US5941075A

    公开(公告)日：1999-08-24

    申请号：US912815

    申请日：1997-08-19

    申请人： Denis Roger Henri Ansart ,  Gilles Gerard Claude Lepretre ,  Denis Jean Maurice Sandelis

    发明人： Denis Roger Henri Ansart ,  Gilles Gerard Claude Lepretre ,  Denis Jean Maurice Sandelis

    IPC分类号： F02C7/232 ,  F23R3/12 ,  F23R3/14 ,  F23R3/28 ,  F23R3/30 ,  F02C1/00

    CPC分类号： F23R3/14

    摘要： A system is disclosed for injecting air and fuel into a combustion chamber of a turbojet engine in which the system includes a fuel injector having an axis A, a first radial swirler located rearwardly of the fuel injector having a plurality of first air passages to direct air into the fuel emanating from the fuel injector in a first plane generally perpendicular to the axis A, a housing located rearwardly of the first radial swirler and forming a pre-mixing chamber bounded by a converging-diverging wall forming a venturi with a throat, the housing having a plurality of second air passages forming a second radial swirler to direct air into the pre-mixing chamber forwardly of the venturi throat in a second plane generally perpendicular to the axis A. The housing also has a plurality of third air passages forming an axial swirler, the second passages and the third passages alternating in a circumferential direction around the housing. A bowl member has a flanged portion connected to the housing and is located rearwardly of the housing such that fuel and air emanating from the premixing chamber and air emanating from the axial swirler pass into the bowl member and are subsequently mixed and passed into the combustion chamber, to which the bowl member is attached.

    摘要翻译： 公开了一种用于将空气和燃料喷射到涡轮喷气发动机的燃烧室中的系统，其中系统包括具有轴线A的燃料喷射器，位于燃料喷射器后方的第一径向旋流器具有多个第一空气通道以引导空气 在大致垂直于轴线A的第一平面中从燃料喷射器排出的燃料，位于第一径向旋流器后方的壳体，并形成由汇合发散壁限定的预混合室，其形成文丘里管与喉部， 壳体具有形成第二径向旋流器的多个第二空气通道，以在大致垂直于轴线A的第二平面中将空气引导到文丘里喉部的前方。前壳体还具有多个第三空气通道，其形成 轴向旋流器，第二通道和第三通道在围绕壳体的圆周方向上交替。 碗形部件具有连接到壳体的凸缘部分并且位于壳体的后方，使得从预混合室发出的燃料和空气以及从轴向旋流器发出的空气进入碗形部件，并随后混合并且进入燃烧室 ，碗构件附接到其上。

    Layout and process for adjusting the diameter of a stator ring
    70.
    发明授权
    Layout and process for adjusting the diameter of a stator ring 失效
    用于调节定子环直径的布局和过程

    公开(公告)号：US5915919A

    公开(公告)日：1999-06-29

    申请号：US893521

    申请日：1997-07-11

    申请人： Jean-Claude Taillant ,  Laurent Palmisano ,  Marc Marchi ,  Patrick Rossi

    发明人： Jean-Claude Taillant ,  Laurent Palmisano ,  Marc Marchi ,  Patrick Rossi

    IPC分类号： F01D11/18 ,  F01D11/24

    CPC分类号： F01D11/18 ,  F01D11/24

    摘要： Layout for adjusting the diameter of a turbine engine ring (5) positioned facing mobile rotor blades (4) and connected to a case element (7). The latter is provided with a cavity (16) communicating with chambers (21, 23) around a gas flow stream (31). A limited air current traverses the cavity (16) and is sufficiently reduced to ensure the development of a heat convection, which renders uniform the temperature of the case element (7) and the ring (5) and consequently the diameter of the latter.

    摘要翻译： 用于调节面向移动转子叶片（4）并连接到壳体元件（7）的涡轮发动机环（5）的直径的布置。 后者设置有围绕气流（31）与腔室（21,23）连通的空腔（16）。 有限的气流穿过空腔（16）并被充分地减小以确保热对流的发展，这使得壳体元件（7）和环（5）的温度均匀，并因此导致热对流的直径。