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Methods of the spacesuits flexibility improvement

机译:提高航天服柔韧性的方法

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Spacesuit is one of crucial elements of the human spaceflight. It protects astronauts not only from harmful effects of low barometric pressure in case of depressurization, but also from overheating and hypothermia. However, to create a small weight spacesuit with a good flexibility is complicated. This paper is dedicated to flexibility of spacesuits with a special attention to inflatable spacesuit and its design. Spacesuits resist the movement of a body and this is one of the main problems of inflatable spacesuits design as to satisfy necessary requirements on this parameter is technically difficult. The flexibility of the spacesuit is provided by movable joints of its shell (hinges), located in accordance with the main human joints. In modern spacesuits the flexibility of extremities is limited and demands additional efforts. Ideally the level of flexibility of a spacesuit has to correspond to the level of flexibility in usual clothes. The hinge has to provide the movement in a corresponding joint in the required range of corners with minimum moments for its bending. Moving parts of a cover should be designed to meet following conditions: hinges have to be combined with joints of the human (whenever it is possible); a gap between a human body and the cover has to be provided in case of impossibility of their matching by movement in hinges. This article analyses soft hinges which are providing bending of parts of a body as well as the way to reduce efforts required for bending. The main idea is in transfer of longitudinal efforts to the power elements located in the neutral surface or the plane of the hinge. Articulations of the skeleton allow two types of movements: rotation and bending (corresponds to technical connections: shaft with sleeve and ball joint). In addition to the kinematic flexibility of the spacesuit, it is also characterized by energy (power) factors. To assess the flexibility of any hinge, the information on limiting angles of its deviation should
机译:宇航服是载人航天的关键部件之一。它不仅可以保护宇航员在减压时免受低气压的有害影响,还可以防止过热和低温。然而,要制造一件具有良好柔韧性的轻量航天服是很复杂的。本文致力于研究宇航服的柔韧性,特别关注充气宇航服及其设计。宇航服能抵抗物体的运动,这是充气式宇航服设计的主要问题之一,因为满足对该参数的必要要求在技术上是困难的。航天服的灵活性是由其外壳的活动关节(铰链)提供的,这些关节与人体的主要关节一致。在现代宇航服中,四肢的灵活性是有限的,需要额外的努力。理想情况下,宇航服的柔韧性水平必须与普通服装的柔韧性水平相对应。铰链必须在要求的转角范围内,以最小的弯曲力矩,在相应的接头中提供运动。盖子的活动部件应设计为满足以下条件:铰链必须与人体关节结合(只要可能);人体和盖子之间必须有间隙,以防铰链中的运动无法匹配。本文分析了为车身零件提供弯曲的软铰链,以及减少弯曲所需力的方法。其主要思想是将纵向作用力转移到位于中性表面或铰链平面的动力元件上。骨骼的关节允许两种类型的运动:旋转和弯曲(对应于技术连接:带套筒的轴和球头)。除了宇航服的运动灵活性外,它还具有能量(功率)因素。为了评估任何铰链的灵活性,应提供有关其偏差极限角度的信息

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