首页> 外国专利> SELF-PROPELLED LAUNCHER FOR TRANSPORTATION AND LAUNCH OF MISSILES FROM TRANSPORTATION-LAUNCHING PACKS WITH THE AID OF SOLID-PROPELLANT GAS GENERATORS

SELF-PROPELLED LAUNCHER FOR TRANSPORTATION AND LAUNCH OF MISSILES FROM TRANSPORTATION-LAUNCHING PACKS WITH THE AID OF SOLID-PROPELLANT GAS GENERATORS

机译:自推进发射器,在固体推进剂的帮助下,从运输发射包中发射导弹

摘要

FIELD: self-propelled launchers for transportation and launch of missiles from transportation - launching packs with the aid of solid-propellant gas generators.;SUBSTANCE: the launcher is provided at least with two supports made in the form of double-rod hydraulic cylinders of double-sided action. The upper rod of each hydraulic cylinder is linked with a movable frame, and the lower rod - with a hinge-mounted supporting plate and a supports driving mechanism having levers and tie-rods. The levers are hinge-mounted on one side on the body frame, and on the other - on the double-rod hydraulic cylinders of double-sided action. The tie-rods are hinge-mounted on a boom, and on the other - on the mentioned levers.;EFFECT: reduced time of deployment and closure of the self-propelled launcher and considerably reduced loads on the self-propelled launcher at launching.;4 dwg
机译:领域:用于运输和从运输中发射导弹的自行式发射器-借助固体推进剂气体发生器发射的发射包;物质:发射器至少配备有两个支撑,以双杆液压缸的形式制成双面动作。每个液压缸的上杆与可移动框架连接,下杆-与铰链安装的支撑板以及具有杠杆和拉杆的支撑驱动机构相连。杠杆的一侧铰接安装在车身框架上,另一侧铰接安装在具有双向作用的双杆液压缸上。拉杆铰链安装在动臂上,另一个铰接式安装在上述杠杆上。效果:减少了自行式发射器的展开和关闭时间,并大大降低了自动发射器在发射时的负荷。 ; 4 dwg

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