首页> 外国专利> EXTENDIBLE BELL-SHAPED PROPULSION NOZZLE FOR ROCKET PROPULSION MECHANISM

EXTENDIBLE BELL-SHAPED PROPULSION NOZZLE FOR ROCKET PROPULSION MECHANISM

机译:火箭推进机构的可扩展钟形推进喷嘴

摘要

PROBLEM TO BE SOLVED: To provide an extendible bell-shaped propulsion nozzle simply structured to minimize mass, and having an extendible mechanism operating with high precision.;SOLUTION: The bell-shaped propulsion nozzle includes a first part with a small diameter disposed to be fixed to an engine of a rocket propulsion mechanism and having a generally conical shape, and a second part with a large diameter movably disposed and having a generally conical shape. The mechanism extending the second part of the bell-shaped propulsion nozzle from a loading position I to an operating position II includes a plurality of extension arms distributed around and disposed between the first part and the second part. A first end portion is hinged to a supporting structure portion provided on an outer peripheral surface of the first part, and a second end portion is movably arranged on an inner peripheral surface of the second part so as to turn while decreasing a radial clearance of the second end portion of the extension arm to the first part of the bell-shaped propulsion nozzle. The second part of the bell-shaped propulsion nozzle can be extended in a direction toward a rear operating position II so as to continue to the generally conical shape of the second part of the bell-shaped propulsion nozzle, when turning so as to make the extension arm close to the first part of the bell-shaped propulsion nozzle.;COPYRIGHT: (C)2005,JPO&NCIPI
机译:解决的问题:提供一种可伸缩的钟形推进喷嘴,其结构简单,以最大程度地减少质量,并具有可高精度操作的可伸缩机构。解决方案:钟形推进喷嘴包括第一部分,该第一部分的小直径设置为固定到火箭推进机构的发动机上并具有大体上圆锥形的形状,并且具有大直径的第二部分可移动地布置并且具有大体上圆锥形的形状。钟形推进喷嘴的第二部分从装载位置I延伸到操作位置II的机构包括围绕第一部分和第二部分分布并设置在第一部分和第二部分之间的多个延伸臂。第一端部铰接到设置在第一部分的外周表面上的支撑结构部分,第二端部可移动地布置在第二部分的内周表面上,从而在减小其径向间隙的同时转动。延伸臂的第二端部到钟形推进喷嘴的第一部分。钟形推进喷嘴的第二部分可以在朝向后操作位置II的方向上延伸,以便在转动时继续钟形推进喷嘴的第二部分的大致圆锥形。延长臂靠近钟形推进喷嘴的第一部分。;版权所有:(C)2005,JPO&NCIPI

著录项

  • 公开/公告号JP2004286031A

    专利类型

  • 公开/公告日2004-10-14

    原文格式PDF

  • 申请/专利权人 EADS ASTRIUM GMBH;

    申请/专利号JP20040083320

  • 发明设计人 ROTH MARTIN;SPERBER FRANZ;

    申请日2004-03-22

  • 分类号F02K9/97;

  • 国家 JP

  • 入库时间 2022-08-21 23:36:11

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