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    • 76. 发明公开
    • Missile launcher
    • Raketenwerfer
    • EP1857766A1
    • 2007-11-21
    • EP06114163.6
    • 2006-05-18
    • SAAB AB
    • Hällgren, Emanuel
    • F41F3/052
    • F41F3/052
    • A missile launcher comprising a forward support (501) for supporting a forward portion of a missile, and an aft support (505) for supporting an aft portion of the missile where the forward support (501) is arranged to swing clear of the aft portion of the missile during the initial period of its launching run where the forward support comprises a roll member (501) being in the shape of a segment of a circle and pivoted at the circle centre, where the perimeter of said member (501) is arranged to make frictional contact to the missile fuselage in order to confer mechanical energy to the roll member (501) to make said member to swing clear of the aft portion of the missile during the initial period of said missiles launching run.
    • 一种导弹发射器,包括用于支撑导弹前部的前支撑件(501)和用于支撑导弹的后部的后支撑件(505),其中前支撑件(501)布置成摆动离开后部部分 的导弹在其发射运行的初始阶段期间,其中前部支撑件包括圆形部分的滚动部件(501)并且在圆心处枢转,所述部件(501)的周边布置在圆心处 以使所述导弹机身摩擦接触,以便在所述导弹发射运行的初始阶段期间向所述滚动部件(501)赋予机械能以使所述部件在所述导弹的后部摆动。
    • 77. 发明公开
    • Self-contained canister missile launcher with tubular exhaust uptake ducts
    • Mehrzellige Raketenstarteinheit mitrohrförmigen,nach oben gerichtetenGasauslasskanäle
    • EP1225411A2
    • 2002-07-24
    • EP02001507.9
    • 2002-01-22
    • Lockheed Martin Corporation
    • Briggs, David ConradCiappi, Jorge IgancioKraft, William Russell, III
    • F41F3/04
    • F41F3/052F41F3/0413F41F3/042
    • A self-contained missile canister (10) includes a cylindrical shell (12) having a plenum or manifold at the breech end for receiving and deflecting missile exhaust gases. A plurality of tubular exhaust ducts (36) or uptake tubes route exhaust gases from the plenum to locations near the missile exit end of the canister. Protrusions on the missile, such as guide rails or aerodynamic control fins, extend from the missile body at locations lying between the exhaust ducts. The tubular exhaust ducts resist the exhaust pressure in hoop tension, so are lightweight. Ablative material may line the exhaust ducts. The exhaust ducts may be supported by longitudinally disposed support beams, preferably I-beams. In one embodiment, each I-beam supports two exhaust ducts.
    • 一个独立的导弹罐(10)包括一个圆柱形壳体(12),该圆柱形壳体(12)在后膛端具有一个集气室或歧管,用于接收和偏转导弹废气。 多个管状排气管道(36)或吸入管道将废气从气室引导到罐的导弹出口端附近的位置。 诸如导轨或空气动力学控制翼之类的导弹上的突起在位于排气管之间的位置处从导弹体延伸。 管状排气管阻止环向张力中的排气压力,因此轻便。 烧蚀材料可以排放排气管。 排气管可以由纵向设置的支撑梁,优选地I型梁支撑。 在一个实施例中,每个I型梁支撑两个排气管。