首页> 外国专利> LAUNCHER carrier rocket with degeneracy of the emission spectrum of mechanical vibrations (optional) agreed with this installation method launch rocket AND METHOD OF PREPARATION OF THE IMPLEMENTATION OF THE LAST

LAUNCHER carrier rocket with degeneracy of the emission spectrum of mechanical vibrations (optional) agreed with this installation method launch rocket AND METHOD OF PREPARATION OF THE IMPLEMENTATION OF THE LAST

机译:具有退化的机械振动发射频谱的运载火箭(可选),与这种安装方法发射火箭一致,并且最后执行的方法

摘要

FIELD: transportation.;SUBSTANCE: group of inventions relates to the rocket technique field, in particular to launching ramps (LR) for rocket bearers launching (RB). Elements of LR working surfaces, interrelating while launching with currents of combustion materials (CCM) of engine unit (EU) (gas vents, pan, blast deflector, entry, checker, located in entry and under it), are made with covering, which consists of fragments made of materials, different in sound speed in them, or composed of structural components set, made of materials differ in sound speed in them or in immediate proximity to working surfaces of LR elements with fragments made of materials different in sound speed in them. Stated fragments, constructive elements or insertions can be located irregularly, or fragments, constructive elements and insertions, made of materials with similar sound speed, are located centered, or fragments, constructive elements or insertions are made of materials with different sound speed are interchange each other. After EU launching one supplies in CCM fluid flows for breakdown of supersonic CCM flow structure at the level of first wave structure. While launching of RB at the plate CCM is surrounded with gas-vapor cloud. Besides, one defines configurations of working surfaces of LR details with the usage of LR and RB models. For modeling details are made in particular of the demolishing, or not elastic deforming material, or material, melting under CCM impact.;EFFECT: decreasing of integral control action of oscillations on rocket bearers and launching ramps.;50 cl
机译:发明领域本发明涉及火箭技术领域,尤其涉及用于火箭携带者发射(RB)的发射坡道(LR)。 LR工作面的元件与发动机单元(EU)的燃烧材料(CCM)流动时相关联(排气口,锅,导风罩,入口,检查器,位于入口及其下方),这些元件的表面是覆盖的,由声速不同的材料制成的碎片,或由声速不同的材料制成的结构部件组成,或紧靠LR元件的工作表面制成的材料,由声速不同的材料制成的碎片组成。他们。陈述的片段,构造元件或插入物可以不规则地放置,或者由具有相似声速的材料制成的片段,构造元件和插入物居中放置,或者由不同声速材料制成的片段,构造元件或插入物可以互换其他。欧盟启动CCM流体供应中的一个供应后,用于在第一波结构水平上破坏超音速CCM流动结构。在板块上发射RB时,CCM被气体蒸气云包围。此外,还使用LR和RB模型定义了LR零件工作表面的配置。对于建模的细节,特别是对在CCM冲击下熔化的,已拆除或未发生弹性变形的材料或熔化的材料进行了详细说明;效果:减小了对火箭炮架和发射坡道的振荡的整体控制作用; 50 cl

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