首页> 外国专利> Improvements introduced in which they can be suspended by groups in a launching ingenio (Machine-translation by Google Translate, not legally binding)

Improvements introduced in which they can be suspended by groups in a launching ingenio (Machine-translation by Google Translate, not legally binding)

机译:引入了一些改进,可以在启动的genio中按组将它们暂停(由Google Translate进行机器翻译,没有法律约束力)

摘要

Improvements introduced in the rockets that must be able to be incorporated in a cluster of rockets suspended from a launching device that have, on the one hand, means of union called "inferior" with a rocket called "previous" (which must be fired before) and , on the other hand, means of union called "superior" with a rocket called "posterior" (which must be fired afterwards), with the upper joining means of each rocket being applied, when placing the rockets in place on the engine that must ensure its launch, with lower joining means carried by the rear rocket (or by the launching device), the assembly of said joining means being such as to allow axial displacement at the time of the rocket yield. , then the release of said rocket in relation to the rear rocket, characterized by, on the one hand, one by which the two genera of joining means (upper and lower) considered to have appropriate retaining means for securing in the axial direction the cooperating connecting means of different genera carried by two rockets attached to each other, as long as the force tending to separate said rockets from each other by an axial displacement remains less than a predetermined critical value and, on the other hand, said rocket is provided with a screen having dimensions and an active position such that the screen of each subsequent rocket penetrates the propellant jet of the supposedly ignited fore-round rocket and undergoes a push "p "directed backward, whose intensity is such that the conjugate effect, on these two rockets, of this thrust" p "and the propellant thrust" p "that the forward rocket requests forward, subject said retention means to a superior force at said critical value, while the conjugated effect of said forces on the subsequent rocket gives rise, on the means of retention that they connect the latter and its own subsequent rocket, at a force lower than the critical value in question. (Machine-translation by Google Translate, not legally binding)
机译:火箭中引入的改进措施必须能够纳入从发射装置悬挂的一组火箭中,这些火箭一方面具有被称为“劣等”的联合方式与被称为“先前”的火箭的结合方式(必须在发射之前),并在另一方面将称为“高级”的火箭与称为“后部”的火箭的联合(随后必须发射),并且在将火箭放置在发动机上的位置时应用每个火箭的上部连接装置必须通过后火箭(或由发射装置)携带的下部连接装置来确保其发射,所述连接装置的组装应允许在火箭屈服时轴向移动。然后相对于后部火箭释放所述火箭,其特征在于,一方面,两个连接装置(上部和下部)被认为具有适当的保持装置,以沿轴向固定协作装置。只要两个趋向于通过轴向位移将所述火箭彼此分离的力保持小于预定的临界值,并且另一方面,所述火箭具有具有一定尺寸和有效位置的屏幕,使得随后的每枚火箭的屏幕都穿透所谓的被点燃的前轮火箭的推进剂射流,并向后推“ p”,其强度使得对这两个火箭的共轭效应前进火箭要求向前推力“ p”和推进剂推力“ p”的火箭,使所述保持装置承受处于所述临界值的力,所述力对后继火箭的共轭作用,通过保持力将后者与它自己的后继火箭连接,从而产生的作用力低于所讨论的临界值。 (通过Google翻译进行机器翻译,没有法律约束力)

著录项

  • 公开/公告号ES240510A1

    专利类型

  • 公开/公告日1958-11-01

    原文格式PDF

  • 申请/专利权人 BREVETS AERO-MECANIQUES SOCIETE ANONYME;

    申请/专利号ES19590240510

  • 发明设计人

    申请日1959-03-06

  • 分类号1F16A;

  • 国家 ES

  • 入库时间 2022-08-23 21:50:40

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号