Removable copying cutter
    1.
    发明授权
    Removable copying cutter 失效
    可拆卸复印机

    公开(公告)号:US5833402A

    公开(公告)日:1998-11-10

    申请号:US446894

    申请日:1995-05-17

    IPC分类号: B23C5/10 B24B3/06 B23C5/02

    摘要: The present invention relates to a copying cutter provided with a cylindrical or conical body having a spherical end, constituting the active portion of the cutter, said end including a plurality of flutes inclined at a determined angle .theta. relative to the longitudinal axis of the cutter and formed along circular arcs at a determined distance x from the midplane P of the cutter, an inside face and an outside face of each of the flutes constituting, after machining, respectively a cutting face and clearance faces of each tooth of the cutter. The clearance faces comprise a first clearance face and an additional clearance face presenting at least a first facet. The cutting face has a cutting angle .gamma. given by the following equation: ##EQU1## where R is the radius of the cutter. The present invention also relates to a method of manufacturing the cutter.

    摘要翻译: 本发明涉及一种复制刀具,其具有构成切割器活动部分的具有球形端部的圆柱形或锥形体,所述端部包括相对于切割器的纵向轴线以确定的角度θ倾斜的多个槽纹,以及 以与切割器的中平面P相距的确定距离x的圆弧形成,每个凹槽的内表面和外表面分别在机械加工后构成切割器的每个齿的切割面和间隙面。 间隙面包括呈现至少第一面的第一间隙面和附加间隙面。 切割面具有由以下等式给出的切割角度γ:本发明还涉及一种制造切割器的方法。

    Method of densifying porous substrates by chemical vapor infiltration of
silicon carbide
    3.
    发明授权
    Method of densifying porous substrates by chemical vapor infiltration of silicon carbide 失效
    通过化学气相渗透碳化硅致密化多孔基材的方法

    公开(公告)号:US5738908A

    公开(公告)日:1998-04-14

    申请号:US656347

    申请日:1996-06-14

    摘要: A reaction gas containing methyltrichlorosilane (MTS) and hydrogen is injected into the infiltration chamber (30) in which the substrate is placed and where predetermined infiltration temperature and pressure conditions obtain. The gas entering the infiltration chamber is preheated (by plates 46) so as to bring it up to temperature before coming into contact with the substrate. The residual gas containing the remainder of the reaction gas together with gaseous reaction products is extracted from the chamber. Infiltration is performed at a temperature lying in the range 960.degree. C. to 1050.degree. C., and preferably in the range 1000.degree. C. to 1030.degree. C., under a total pressure of not more than 25 kPa, and preferably equal to 7 kPa to 12 kPa, and the concentration of silicon-containing species in the residual gas is lowered at the outlet from the infiltration chamber, e.g. by injecting an inert gas (via 70).

    摘要翻译: PCT No.PCT / FR94 / 01453第 371日期1996年6月14日第 102(e)1996年6月14日PCT 1994年12月13日PCT PCT。 WO95 / 16803 PCT出版物 日期:1995年6月22日将含有甲基三氯硅烷(MTS)和氢的反应气体注入到其中放置基材的浸渗室(30)中并且获得预定的渗透温度和压力条件。 进入渗透室的气体被预热(通过板46),以便在与基底接触之前使其达到温度。 将含有剩余反应气体的残余气体与气体反应产物一起从室中提取出来。 渗透在960℃至1050℃的温度下进行,优选在1000℃至1030℃的范围内,总压力不超过25kPa,优选等于 7kPa至12kPa,并且残留气体中的含硅物质的浓度在渗透室的出口处降低,例如 通过注入惰性气体(通孔70)。

    Optimized system for feeding a reignitable rocket engine
    4.
    发明授权
    Optimized system for feeding a reignitable rocket engine 失效
    优化的系统用于喂养一个可再生火箭发动机

    公开(公告)号:US5531067A

    公开(公告)日:1996-07-02

    申请号:US556631

    申请日:1995-11-13

    申请人: Christophe Koppel

    发明人: Christophe Koppel

    IPC分类号: B64G1/26 B64G1/40 F02K9/44

    CPC分类号: B64G1/402 B64G1/26 B64G1/401

    摘要: The present invention relates to a system for feeding the engines of a space vehicle with at least one liquid propellant, the system comprising for the purpose of storing said liquid propellant under a pressure greater than the feed pressure, firstly a main tank having no liquid expulsion device, and secondly an auxiliary tank that is smaller than the main tank and that is provided with a device for separating the liquid phase from the gas phase, switching means enabling the auxiliary tank to be selectively refilled with liquid propellant from the main tank; such that liquid propellant that is free from pressurization gas bubbles can always be delivered regardless of the flight conditions of the vehicle, and in particular when it is not possible to take said liquid propellant from the main tank.

    摘要翻译: 本发明涉及一种用于向空间车辆的发动机供给至少一种液体推进剂的系统,该系统包括用于在大于进给压力的压力下储存所述液体推进剂,首先是没有液体排出的主罐 装置,其次是比主油箱小的辅助油箱,并设置有用于从气相中分离液相的装置,使辅助罐能够从主油箱中选择性地重新填充液体推进剂的切换装置; 使得无论车辆的飞行条件如何,并且特别是当不可能从主油箱中取出所述液体推进剂时,总是能够输送没有加压气泡的液体推进剂。

    Rocket engine nozzle with an engine diffuser
    5.
    发明授权
    Rocket engine nozzle with an engine diffuser 失效
    火箭发动机喷嘴与发动机扩散器

    公开(公告)号:US5490629A

    公开(公告)日:1996-02-13

    申请号:US248968

    申请日:1994-05-25

    IPC分类号: F02K9/97

    CPC分类号: F02K9/978

    摘要: The downstream portion of the diverging part of the nozzle of the rocket engine is extended by an ejectable diffuser which, downstream from the zone where it is connected to the diverging part, presents a zone of smaller cross-section that acts during a first stage of flight in the presence of significant outside pressure to recompress the flow of hot gases and to prevent a flow separation from appearing along with the wall of the diverging part. The ejectable diffuser may have a streamlined throat which constitutes the zone of smaller cross-section.

    摘要翻译: 火箭发动机的喷嘴的发散部分的下游部分通过可喷射的扩散器延伸,该扩散器在其与其分开的部分连接的区域的下游具有较小横截面的区域,该区域在第一阶段 在存在显着的外部压力的情况下飞行,以重新压缩热气体的流动并防止流动分离与分流部分的壁一起出现。 可喷射扩散器可以具有流线型的喉部,其构成较小横截面的区域。

    Rocket engine nozzle with selectively smaller outlet cross-section
    6.
    发明授权
    Rocket engine nozzle with selectively smaller outlet cross-section 失效
    火箭发动机喷嘴具有选择性较小的出口横截面

    公开(公告)号:US5481870A

    公开(公告)日:1996-01-09

    申请号:US249159

    申请日:1994-05-25

    IPC分类号: F02K9/97 F02K1/06

    CPC分类号: F02K9/978

    摘要: In a rocket engine nozzle with a selectively smaller outlet cross-section, the nozzle comprising a converging portion which receives the gases produced in a combustion chamber, a nozzle throat of small cross-section and a diverging part connected to the nozzle throat and terminating at its downstream portion in a gas jet outlet cross-section defining a high cross-section ratio, a releasable annular obstacle is connected to the downstream end of the diverging part so as to define at the outlet of the diverging part a zone of selectively smaller cross-section which ensures stability of the separation of the flow of hot gases relative to the wall of the diverging part during a first phase of flight.

    摘要翻译: 在具有选择性较小的出口横截面的火箭发动机喷嘴中,喷嘴包括会聚部分,其接收在燃烧室中产生的气体,具有小横截面的喷嘴喉部和与喷嘴喉部连接的发散部分, 其在气体喷射出口横截面中的下游部分限定了高横截面比,可释放的环形障碍物连接到发散部分的下游端,以便在发散部分的出口处限定选择性较小的交叉的区域 确保在第一飞行阶段期间热气体相对于分流部分的壁分离的稳定性。

    High performance centrifugal pump having an open-faced impeller
    7.
    发明授权
    High performance centrifugal pump having an open-faced impeller 失效
    具有敞开式叶轮的高性能离心泵

    公开(公告)号:US5427498A

    公开(公告)日:1995-06-27

    申请号:US157746

    申请日:1993-11-24

    摘要: The centrifugal pump with an open-faced impeller comprises at least one open-faced impeller having blades placed inside a casing defining both a delivery pipe and a suction pipe facing the base of the blades situated in the vicinity of a central shaft for driving the impeller. An active axial balancing system for the rotary assembly is integrated in the impeller and comprises a balancing chamber interposed between the rear face of the body of the impeller and an outer rear portion of the casing, the impeller itself acting as the balancing turntable. A shroud-forming intermediate part is prevented from rotating relative to the casing and is interposed between an outer front portion of the casing and the impeller, a cavity is formed between the outer front portion of the casing and the intermediate part to receive a back pressure of predetermined value serving, in operation, to maintain small clearance without contact between the intermediate part that is prevented from rotating and the blades of the impeller.

    摘要翻译: 具有敞开式叶轮的离心泵包括至少一个敞开的叶轮,其具有放置在壳体内的叶片,所述叶片限定输送管和面向位于中心轴附近的叶片的基部的吸入管,用于驱动叶轮 。 用于旋转组件的主动轴向平衡系统集成在叶轮中,并且包括设置在叶轮主体的后表面和壳体的外后部之间的平衡室,叶轮本身用作平衡转台。 护罩形成中间部件被防止相对于壳体旋转并且被插入在壳体的外前部和叶轮之间,在壳体的前前部和中间部之间形成空腔以接收背压 在操作中,为了保持小间隙而不会在防止旋转的中间部分与叶轮的叶片之间接触,其具有预定值。

    Apparatus for preheating a flow of gas in an installation for chemical
vapor infiltration, and a densification method using the apparatus
    8.
    发明授权
    Apparatus for preheating a flow of gas in an installation for chemical vapor infiltration, and a densification method using the apparatus 失效
    用于预热用于化学气相渗透的装置中的气体流的装置,以及使用该装置的致密化方法

    公开(公告)号:US5362228A

    公开(公告)日:1994-11-08

    申请号:US967817

    申请日:1992-10-28

    申请人: Serge Vaudel

    发明人: Serge Vaudel

    摘要: The gas is preheated by means of at least one screen disposed transversely relative to the flow of gas penetrating into the enclosure. The screen is provided with passages for the flow of gas and is fixed inside a peripheral wall to define a channel to enable the gas to flow through the preheating apparatus, it is also provided with fins which project from its surface, the screen and the fins being made of a refractory sheet material, in particular a sheet of laminated graphite.

    摘要翻译: 气体通过至少一个相对于渗透到外壳中的气体流横向设置的筛网进行预热。 屏幕上设置有用于气体流动的通道,并固定在周围壁内,以形成通道,使气体能够流过预热装置,同时还设有从其表面,屏幕和翅片突出的翅片 由耐火片材制成,特别是层压石墨片。

    Electrically controlled valve having a totally leakproof valve plug
    9.
    发明授权
    Electrically controlled valve having a totally leakproof valve plug 失效
    电控阀具有完全防漏阀塞

    公开(公告)号:US5356112A

    公开(公告)日:1994-10-18

    申请号:US84756

    申请日:1993-06-29

    摘要: The present invention relates to an electrically controlled leakproof valve having a fluid feed channel and at least one channel for delivering said fluid, rotary displacement of a distributor plug in said valve being under the control of an actuator. The actuator comprises an axially pierced rotor through which the fluid from the feed channel flows without headloss, the actuator being connected to the valve body in leakproof manner without using dynamic sealing devices. The present leakproof valve is particularly suitable for use in corrosive environments, and in particular under cryogenic conditions.

    摘要翻译: 本发明涉及一种电控防漏阀,其具有流体供给通道和用于输送所述流体的至少一个通道,所述阀中的分配器插头在致动器的控制下的旋转位移。 致动器包括轴向穿透的转子,来自进料通道的流体通过该转子流动而没有头部损失,致动器以防漏的方式连接到阀体,而不使用动态密封装置。 本泄漏阀特别适用于腐蚀性环境,特别是在低温条件下。

    Retractable-gasket valve having two stiffnesses
    10.
    发明授权
    Retractable-gasket valve having two stiffnesses 失效
    具有两个刚度的可伸缩垫片阀

    公开(公告)号:US5253843A

    公开(公告)日:1993-10-19

    申请号:US990331

    申请日:1992-12-10

    申请人: Patrick Garceau

    发明人: Patrick Garceau

    IPC分类号: F16K5/20

    CPC分类号: F16K5/201

    摘要: The retractable-gasket ball valve includes sealing means fixed on the valve body, and including, in particular, a gasket for providing sealing between the shutter member and the valve body when the shutter member is in a closed position, and further including a slide for causing said sealing means to move between a retracted position which is also a rest position in which the sealing means is spaced spart from the spherical shutter member, and a contact position in which the gasket is pressed against the shutter member. The valve includes a first resilient element of low stiffness which tends to separate the sealing means from the shutter member when the valve is brought to its open position, and a second resilient element of relatively greater stiffness which is put under tension by the slide a few degrees before the mechanical closure position of the valve when the gasket is in contact with the shutter member, and which exerts control pressure on said gasket in contact with the shutter member.

    摘要翻译: 可伸缩垫圈球阀包括固定在阀体上的密封装置,特别是包括用于当活门构件处于关闭位置时在挡板构件和阀体之间提供密封的衬垫,还包括用于 使得所述密封装置在缩回位置之间移动,所述缩回位置也是所述密封装置与所述球形快门部件间隔开的静止位置,以及所述垫圈被压靠在所述挡板部件上的接触位置。 该阀包括低刚度的第一弹性元件,当阀门处于其打开位置时,其倾向于将密封装置与闸板部件分开,并且具有相对较大刚度的第二弹性元件,该第二弹性元件被滑块张紧 在垫圈与闸门构件接触时,阀的机械闭合位置之前的程度,并且在与挡板构件接触的所述垫圈上施加控制压力。