Process for making a composite material assembly and aircraft wing and stabilizing element obtained by this process
    1.
    发明申请
    Process for making a composite material assembly and aircraft wing and stabilizing element obtained by this process 失效
    通过该方法制备复合材料组件和飞机机翼和稳定元件的方法

    公开(公告)号:US20060076102A1

    公开(公告)日:2006-04-13

    申请号:US11147011

    申请日:2005-06-07

    申请人: Franck Bequet

    发明人: Franck Bequet

    IPC分类号: B29C53/58 B65H81/00

    摘要: Process for manufacturing an assembly made of a composite material and wing and stabilizing element obtained by this process. The junction zone for a part (P) made of a composite material comprising two parts (A1, A2) in which the principal directions intersect at a non-singular angle, is made in a single operation by continuous lay-up. The 0° directions of the lay-up coordinate systems (R1, R2) of the parts (A1, A2) are oriented such that these directions make an angle of close to 180°-θ°, where ±θ° represents the other directions of the lay-up coordinate systems (R1, R2). Thus, the layers of fibers oriented at 0° in one of the coordinate systems correspond approximately to a lay-up direction of ±θ° in the other coordinate system.

    摘要翻译: 用于制造由该方法获得的复合材料和翼和稳定元件制成的组件的方法。 由包括两个主要方向以非奇异角相交的两部分(A 1,A 2)的复合材料制成的部分(P)的连接区域通过连续叠层进行单次操作。 部件(A 1,A 2)的叠层坐标系(R 1,R 2)的0°方向取向为使得这些方向成为接近180°-θ°的角度,其中±θ° 表示叠层坐标系(R 1,R 2)的其他方向。 因此,在一个坐标系中以0°取向的纤维层大致对应于另一坐标系中±θ°的叠层方向。

    Brake corrector subject to the load of a vehicle
    2.
    发明授权
    Brake corrector subject to the load of a vehicle 失效
    制动校正器受车辆的负载

    公开(公告)号:US4828330A

    公开(公告)日:1989-05-09

    申请号:US93856

    申请日:1987-09-04

    IPC分类号: B60G15/06 B60T8/18 B60T8/30

    摘要: Assembly consisting of a suspension element (20) and of a brake corrector (10) intended to be subject to the load of a vehicle, the corrector (10) comprising a body in which slides a piston (12) forming a shutter element capable of opening or closing a hydraulic passage between an inlet (14) and an outlet (16) of the corrector, the piston (12) being connected by a connection mechanism to a spring mechanism (23) of the suspension element (20), characterized in that the connection mechanism comprises a lever (24) mounted on the suspension element (20) between two pivoting elements (28; 32) which are subjected to the force exerted by the suspension element (20) and which are arranged so as to transmit some of the force to the lever (24).

    摘要翻译: 由悬挂元件(20)和旨在承受车辆负载的制动器校正器(10)组成的组件,所述校正器(10)包括主体,所述主体在所述主体中滑动形成活门(12),所述活塞 在校正器的入口(14)和出口(16)之间打开或关闭液压通道,活塞(12)通过连接机构连接到悬挂元件(20)的弹簧机构(23),其特征在于 所述连接机构包括安装在所述悬挂元件(20)上的杠杆(24),所述杠杆(24)经受所述悬挂元件(20)施加的力的两个枢转元件(28; 32)之间,并被布置成传递一些 的力到杠杆(24)。

    Device for joining a panel and a structure, able to transmit significant forces
    3.
    发明授权
    Device for joining a panel and a structure, able to transmit significant forces 有权
    用于连接面板和结构的装置,能够传递显着的力

    公开(公告)号:US06663314B2

    公开(公告)日:2003-12-16

    申请号:US10052258

    申请日:2002-01-23

    申请人: Franck Bequet

    发明人: Franck Bequet

    IPC分类号: B64C328

    摘要: A device for joining a panel and another structure. The device (10) includes a plurality of mounts (16) evenly distributed along the interface (I) between the panel (12) and the structure (14). Each mount (16) comprises a tension screw approximately perpendicular to the interface (I) and a nut embedded in the panel (12), close to the latter. To allow the transmission of more significant forces, the nuts are arranged in at least two different rows (R1, R2, R3), parallel to the interface (I). Moreover, the nuts of the adjacent mounts are located in different rows.

    摘要翻译: 一种用于连接面板和另一结构的装置。装置(10)包括沿面板(12)和结构(14)之间的界面(I)均匀分布的多个安装件(16)。 每个安装件(16)包括大致垂直于接口(I)的张紧螺钉和嵌入在面板(12)中的螺母,靠近后者。 为了允许传递更重要的力,螺母被布置成平行于界面(I)的至少两个不同的行(R1,R2,R3)。 此外,相邻安装座的螺母位于不同的行中。

    Brake booster with a hinged positioning member
    4.
    发明授权
    Brake booster with a hinged positioning member 失效
    具有铰链定位构件的制动助力器

    公开(公告)号:US4765226A

    公开(公告)日:1988-08-23

    申请号:US39555

    申请日:1987-04-16

    CPC分类号: B60T13/244 B60T13/57

    摘要: The booster comprises, in a radial opening (21) of the valve body (6), a first positioning member (22) fastened in the valve body and a second positioning member (23) interposed between the first positioning member and an interacting shoulder (19) of the valve plunger (14), the second positioning member (23) internally associated in a hinged connection with the first positioning member and having an outer end zone (30) interacting, in a rest position of the booster, with a stationary surface (31), with which the piston structure (2-5) also interacts by coming up against it, to assign to the valve plunger (14) a specific rest position relative to the valve body (6).

    摘要翻译: 增压器在阀体(6)的径向开口(21)中包括紧固在阀体中的第一定位构件(22)和插入在第一定位构件和相互作用肩部之间的第二定位构件(23) 所述第二定位构件(23)内部与所述第一定位构件铰接连接并具有在所述助推器的静止位置相互作用的外端区域(30),所述外端区域与所述第二定位构件 表面(31),活塞结构(2-5)也通过抵靠它而相互作用,以将阀柱塞(14)分配给相对于阀体(6)的特定静止位置。

    Process for making a composite material assembly and aircraft wing and stabilizing element obtained by this process
    5.
    发明授权
    Process for making a composite material assembly and aircraft wing and stabilizing element obtained by this process 失效
    通过该方法制备复合材料组件和飞机机翼和稳定元件的方法

    公开(公告)号:US07874517B2

    公开(公告)日:2011-01-25

    申请号:US11147011

    申请日:2005-06-06

    申请人: Franck Bequet

    发明人: Franck Bequet

    IPC分类号: B64C5/00 B64C3/00

    摘要: Process for manufacturing an assembly made of a composite material and wing and stabilizing element obtained by this process.The junction zone for a part (P) made of a composite material comprising two parts (A1, A2) in which the principal directions intersect at a non-singular angle, is made in a single operation by continuous lay-up. The 0° directions of the lay-up coordinate systems (R1, R2) of the parts (A1, A2) are oriented such that these directions make an angle of close to 180°−θ°, where ±θ° represents the other directions of the lay-up coordinate systems (R1, R2). Thus, the layers of fibers oriented at 0° in one of the coordinate systems correspond approximately to a lay-up direction of ±θ° in the other coordinate system.

    摘要翻译: 用于制造由该方法获得的复合材料和翼和稳定元件制成的组件的方法。 由包括主要方向以非奇异角相交的两个部分(A1,A2)的复合材料制成的部分(P)的接合区域通过连续叠层进行单次操作。 部件(A1,A2)的叠层坐标系(R1,R2)的0°方向取向为使得这些方向形成接近180°的角度,其中±& 叠层坐标系(R1,R2)的其他方向。 因此,在一个坐标系中以0°取向的纤维层大致对应于另一个坐标系中的±&Thetas;°的叠层方向。

    Process for making a composite material assembly and aircraft wing and stabilizing element obtained by this process
    6.
    发明授权
    Process for making a composite material assembly and aircraft wing and stabilizing element obtained by this process 失效
    通过该方法制备复合材料组件和飞机机翼和稳定元件的方法

    公开(公告)号:US06908526B2

    公开(公告)日:2005-06-21

    申请号:US10304654

    申请日:2002-11-25

    申请人: Franck Bequet

    发明人: Franck Bequet

    IPC分类号: B29C70/30 B65H81/00

    摘要: Process for manufacturing an assembly made of a composite material and wing and stabilizing element obtained by this process.The junction zone for a part (P) made of a composite material comprising two parts (A1, A2) in which the principal directions intersect at a non-singular angle, is made in a single operation by continuous lay-up. The 0° directions of the lay-up coordinate systems (R1, R2) of the parts (A1, A2) are oriented such that these directions make an angle of close to 180°−θ°, where ±θ° represents the other directions of the lay-up coordinate systems (R1, R2). Thus, the layers of fibers oriented at 0° in one of the coordinate systems correspond approximately to a lay-up direction of ±θ° in the other coordinate system.

    摘要翻译: 用于制造由该方法获得的复合材料和翼和稳定元件制成的组件的方法。 由包括两个主要方向以非奇异角相交的两部分(A 1,A 2)的复合材料制成的部分(P)的连接区域通过连续叠层进行单次操作。 部件(A 1,A 2)的叠层坐标系(R 1,R 2)的0°方向取向为使得这些方向成为接近180°-θ°的角度,其中±θ° 表示叠层坐标系(R 1,R 2)的其他方向。 因此,在一个坐标系中以0°取向的纤维层大致对应于另一坐标系中±θ°的叠层方向。