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method for the use of airships without solid or liquid p olttoaineita.

机译:使用无固体或液体的飞艇的方法

摘要

1348408 Airships H PAPST 19 April 1971 [26 Feb 1970] 22802/71 Heading B7W A method of operating an airship comprises employing, as both lifting gas and fuel supply stored in a storage bag or bags, an inflammable lighter-than-air gas selected from hydrogen, methane and hydrocarbon-containing gas, generating power to drive said airship by consuming said inflammable gas, and employing as lifting gas at least a part of the product gas obtained by consumption of said inflammable gas. An airship comprises a double walled outer envelope 1 enclosing flexible invertable walls 3a, 3b, 3c forming chambers 37, 43, 41, 45. The chambers 37 contain said inflammable gas; chambers 43 contain saturated water vapour; chambers 41 contain cold or heated air and are used as compensation chambers, and chambers 45 store a gas, e.g. carbon dioxide and/or nitrogen and air for filling the space between the two walls of envelope 1. A centre chamber 39 contains buoyant gas. The airship is propelled by a main blower 33 which discharges a propulsion jet through nozzle 9 and a blower 31 provides propulsion under slow speed conditions, directional control being provided by vanes 13a. In operation inflammable gas from chambers 37 and water vapour from chamber 43 are delivered to a catalyst apparatus 60 where they are reacted and the product gas is supplied to chamber 39. Exhaust gas in duct 47 from blower 33 is passed through apparatus 60 where it is heated and then passed to condenser 57 to condense out water vapour. Any waste gas can be conducted to a channel 15 to discharge through nozzle 9.
机译:1348408飞艇H PAPST 1971年4月19日[1970年2月26日]标题B7W一种操作飞艇的方法包括,使用一种易燃的轻于空气的气体作为提升气体和储存在一个或多个储存袋中的燃料供应。由氢气,甲烷和含碳氢化合物气体产生的气体,通过消耗所述可燃气体来产生动力来驱动所述飞艇,并且将至少一部分通过消耗所述可燃气体而获得的产物气体用作提升气体。飞艇包括双层壁外壳1,其包围柔性的可翻转壁3a,3b,3c,形成腔室37、43、41、45。腔室37容纳所述可燃气体;所述腔室37容纳所述可燃气体。腔室43容纳饱和水蒸气;腔室41容纳冷或热空气,并用作补偿腔室,腔室45储存气体,例如气体。二氧化碳和/或氮气和空气以填充外壳1的两个壁之间的空间。中心腔室39容纳浮力气体。飞艇由主鼓风机33推动,主鼓风机33通过喷嘴9排出推进射流,而鼓风机31在低速条件下提供推进力,由叶片13a提供方向控制。在操作中,来自腔室37的可燃气体和来自腔室43的水蒸气被输送到催化剂装置60,在其中它们发生反应,并且产物气体被供应到腔室39。来自鼓风机33的管道47中的排气通过装置60在该处进行。加热,然后送入冷凝器57以冷凝出水蒸气。任何废气可被引导至通道15以通过喷嘴9排出。

著录项

  • 公开/公告号HU170614B

    专利类型

  • 公开/公告日1977-07-28

    原文格式PDF

  • 申请/专利权人

    申请/专利号HU1971PA01095

  • 发明设计人

    申请日1971-02-26

  • 分类号B64B1/58;B64B1/62;

  • 国家 HU

  • 入库时间 2022-08-23 00:52:35

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