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Common computer program for the optimal use of multiple turbine forces for all gravity helicopter flight maneuvers

机译:通用计算机程序,可在所有重力直升机飞行机动中最佳利用多个涡轮力

摘要

Common computer program for the optimal operational use of several turbine forces for all gravity helicopter flight maneuvers, whereby it is provided that all turbine forces of the gravity helicopter (SKHS) can be fully used in all flight maneuvers, whereby a first rotor turbine drive and a second large turbine plant (GTW) are provided, whereby a GTW is provided , which has an acceptable weight and construction, has strong forces and can be inserted vertically into the SKHS fuselage, the vertical GTW position being provided as the base with a GTW swivel axis arranged between the two GTW broad sides and a GTW rotation angle, adjustable by computer application programs for GTW force assignments for GTW shares in the SKHS forward movement if GTW-SKHS forces can be diverted by the SKHS lifting process, whereby jointly calculated Be for the equipment of the computer program (CP) with effective operating instructions drive inserts are provided, whereby an entire aircraft wing structure is rotatably mounted, is provided on the SKHS underbody in the longitudinal direction of the SKHS, in order to reach a flight active position with a 90 degree rotation by means of a CP operation command, CFRP material use being provided primarily
机译:通用计算机程序,用于在所有重力直升机飞行演习中最佳使用几种涡轮力,从而规定重力直升机(SKHS)的所有涡轮力可以在所有飞行演习中得到充分利用,从而实现了第一个旋翼涡轮驱动和提供第二大型涡轮机厂(GTW),从而提供GTW,该GTW具有可接受的重量和结构,具有强大的作用力,并且可以垂直插入SKHS机身中,竖直GTW位置用作GTW的基座旋转轴布置在两个GTW宽边和一个GTW旋转角度之间,如果可以通过SKHS提升过程转移GTW-SKHS力,则可以通过计算机应用程序在SKHS向前运动中为GTW份额的GTW力分配来调整该值,从而共同计算Be对于带有有效操作说明的计算机程序(CP)设备,提供了驱动插件,从而整个飞机机翼结构为了通过CP操作指令以90度的旋转到达飞行激活位置,可调节地安装在SKHS车身底部的SKHS车身上,主要使用CFRP材料

著录项

  • 公开/公告号DE102018005177A1

    专利类型

  • 公开/公告日2020-01-02

    原文格式PDF

  • 申请/专利权人 DANGER MÖRICKE;

    申请/专利号DE20181005177

  • 发明设计人 GLEICH ANMELDER;

    申请日2018-06-25

  • 分类号B64C19;B64D31;

  • 国家 DE

  • 入库时间 2022-08-21 11:02:05

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