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    • 1. 发明授权
    • Low-vulnerability solid-propellant motor
    • 低脆弱性固体推进剂电机
    • US06148606A
    • 2000-11-21
    • US96613
    • 1998-06-12
    • Augustin GrossiPatrick Fiandesio
    • Augustin GrossiPatrick Fiandesio
    • F42B39/20F02K9/38
    • F42B39/20
    • The present invention relates to a low-vulnerability solid-propellant motor (1) comprising a charge (11) of solid propellant, a heat shield (2) covering the inside of a metal structure with a front end wall (3) and a rear end wall (4) which carries at least one nozzle (10), the said front and rear end walls being fastened to a cylindrical shell (5) having wide apertures which are circumferentially distributed and temporarily sealed by sealing plugs (8). The object of the present invention is to provide a motor which has a simple structure and avoids the use of detection and actuation means for freeing the plugs. The motor according to the invention is such that the sealing plugs (8) are held in the apertures between the heat shield and a composite winding (7) of fibres impregnated in a matrix which surrounds the cylindrical shell (5).
    • 本发明涉及一种低脆弱性固体推进剂电动机(1),其包括固体推进剂的电荷(11),覆盖金属结构的内部的隔热罩(2),其具有前端壁(3)和后端 端壁(4),其承载至少一个喷嘴(10),所述前端和后端壁紧固到具有宽孔的圆柱形外壳(5),所述圆形壳体周向分布并通过密封塞(8)临时密封。 本发明的目的是提供一种具有简单结构并避免使用用于释放插头的检测和致动装置的电动机。 根据本发明的电动机使得密封塞(8)保持在隔热件和浸渍在围绕圆柱形壳体(5)的矩阵中的纤维的复合绕组(7)之间的孔中。
    • 2. 发明授权
    • Device for actuating a mechanical member, in particular for the force
guidance of a missile, and missile equipped with said device
    • 用于致动机械构件的装置,特别是用于导弹的力引导和装备有所述装置的导弹的装置
    • US5405103A
    • 1995-04-11
    • US167416
    • 1993-12-14
    • Jean-Louis GirardeauAugustin GrossiJoel FargesPatrick Fiandesio
    • Jean-Louis GirardeauAugustin GrossiJoel FargesPatrick Fiandesio
    • B64C15/12F15B11/08F15B13/044F42B10/60F42B10/66F42B15/01
    • F42B10/663
    • A device for actuating a movable mechanical member, using a fluid source such as a gas generator of a missile, of the type having a controllable distributor connected to the source. The device includes a body (11) provided with a distributor (12), the body being coupled, via an inlet orifice (17), to a fluid source; a first conduit (15) capable of connecting the inlet orifice to a chamber (16) of the distributor; an actuator cylinder (14) arranged in the body and including a first chamber (19A) and a second chamber (19B) which are coaxial and separated from each other by a sliding piston (31) connected to a rod (31B) which projects externally in relation to the body in order to be linked to a mechanical member. A second conduit (18) connects the chamber (16) of the distributor to the first chamber (19A) of the actuator cylinder, it being possible for the second conduit (18) to be brought into communication, via the chamber (16) of the distributor, either with the first conduit (15) or with an outlet orifice (20) outside the body, depending on the position of the distributor. A third conduit (21) connects the second chamber (19B) of the actuator cylinder to the inlet orifice (17) of the body.
    • 使用诸如导弹的气体发生器的流体源来致动可移动机械构件的装置,该装置具有连接到源的可控分配器。 该装置包括设置有分配器(12)的本体(11),该主体经由入口孔(17)联接到流体源; 能够将入口孔连接到分配器的腔室(16)的第一导管(15); 布置在主体中的致动器气缸(14),其包括通过连接到外部突出的杆(31B)的滑动活塞(31)彼此共轴并分离的第一室(19A)和第二室(19B) 相对于身体,以便与机械构件相关联。 第二导管(18)将分配器的腔室(16)连接到致动器气缸的第一腔室(19A),可以使第二导管(18)经由腔室(16)连通 分配器,具有第一导管(15)或与主体外部的出口孔(20),这取决于分配器的位置。 第三导管(21)将致动器气缸的第二腔室(19B)连接到主体的入口孔(17)。