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Power generation rocket engine fan and power generation rocket engine

机译:发电火箭发动机风扇和发电火箭发动机

摘要

PROBLEM TO BE SOLVED: To provide a hydrogen-fueled engine suitable for an aircraft engine which did not exist before as conventional aircraft jet engines use petroleum fossil fuel and discharge air pollutants and carbon dioxide and there is an issue of depletion of oil.;SOLUTION: A turbine 15 which operates by a jet flow by the combustion inside a liquid hydrogen-fueled rocket engine 14 is installed. A turbine shaft 16 that is connected to the turbine 15 is penetrated through a hole 33 installed at a combustion chamber 17 of the liquid hydrogen-fueled rocket engine 14 by a drilling work and a power generator 18 which generates power by the rotation of the turbine 15 and the turbine shaft 16 is installed anterior to and outside of the combustion chamber 17. Water inside a water electrolysis apparatus 19 is decomposed by electricity generated by the power generator 18. Hydrogen and oxygen obtained by the water electrolysis apparatus 19 are liquefied and stored by a liquefier and a storing tank 20 and supplied as the fuel for the liquid hydrogen-fueled rocket engine 14 and an oxidant of liquefied hydrogen.;COPYRIGHT: (C)2011,JPO&INPIT
机译:要解决的问题:提供一种适用于飞机发动机的氢燃料发动机,因为传统的飞机喷气发动机使用石油化石燃料并排放空气污染物和二氧化碳,所以这种燃料不存在,并且存在油耗的问题。 :安装有涡轮15,该涡轮15通过液态氢燃料火箭发动机14内的燃烧而通过射流而运转。连接至涡轮15的涡轮轴16通过钻孔作业穿过安装在液态氢燃料火箭发动机14的燃烧室17处的孔33以及通过涡轮的旋转而发电的发电机18。如图15所示,涡轮轴16安装在燃烧室17的前方和外部。在水电解装置19内的水被发电机18产生的电力分解。由水电解装置19得到的氢和氧被液化并储存。由液化器和储罐20构成,并作为液态氢燃料火箭发动机14的燃料和液化氢的氧化剂供应。;版权所有:(C)2011,JPO&INPIT

著录项

  • 公开/公告号JP5113230B2

    专利类型

  • 公开/公告日2013-01-09

    原文格式PDF

  • 申请/专利权人 伊東 貴之;

    申请/专利号JP20100197116

  • 发明设计人 伊東 貴之;

    申请日2010-08-16

  • 分类号F01K25;F02C3/22;F01D15/08;F02K9/42;

  • 国家 JP

  • 入库时间 2022-08-21 16:53:34

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