• 主题
高级搜索  >
历史搜索 清空历史
首页> 外国专利> ONE TECHNOLOGY USE AND PRODUCTION AEROLETOV: AEROLET (OPTIONS), the fuselage SET fragment and WINGS, air intake, thrust reversers, CONTROL AEROLETOM, a way to create lift AEROLETA, flight mode AEROLETA, METHOD FOR TAKE-OFF AND METHOD FOR LANDING AEROLETA (RU) METHOD AEROLETOM CONTROL IN fLIGHT, METHOD FOR OPERATING REVERSE

ONE TECHNOLOGY USE AND PRODUCTION AEROLETOV: AEROLET (OPTIONS), the fuselage SET fragment and WINGS, air intake, thrust reversers, CONTROL AEROLETOM, a way to create lift AEROLETA, flight mode AEROLETA, METHOD FOR TAKE-OFF AND METHOD FOR LANDING AEROLETA (RU) METHOD AEROLETOM CONTROL IN fLIGHT, METHOD FOR OPERATING REVERSE

机译：一种技术的使用和生产航空器：航空器（选件），机身SET片段和机翼，进气口，推力反向器，控制航空器，创建升空航空器的方法，飞行模式航空器，起飞方法和着陆航空器的方法（ RU）飞行中的方法气动控制，反向操作方法

页面导航
  • 摘要
  • 著录项
  • 相似文献

摘要

FIELD: transport.;SUBSTANCE: invention relates to aircraft engineering. Proposed flight vehicle comprises power plant, fuselage and wing fragments. Set of wing fragments comprises bearing and control surfaces and their mounts. Wing fragment includes structural set including spar, stringer and ribs. Fuselage includes set of frames, spars, stringers and skin. Frames and spars have opening to fasten wing fragments. Engine reversing device comprises flap pivoted in housing to close its openings and provided with grids composed of gas flow guide vanes. Air intake with jet engine integrated in fuselage tail features variable-depth grooves arranged opposite each other on supports. Control system comprises control rod with pedals at its bottom and handle at its top. Said handle has landing gear extension/retraction knob and that of electric drive of bottom set of fragments. Methods of flight vehicle control comprise exploiting air and gas flows.;EFFECT: simplified servicing.;47 cl, 30 dwg
机译：技术领域本发明涉及飞机工程。拟议的飞行器包括发电厂，机身和机翼碎片。机翼碎片的集合包括轴承和控制表面及其底座。机翼碎片包括翼梁，桁条和肋骨在内的结构件。机身包括框架，翼梁，纵梁和皮肤。车架和撑杆已打开以固定机翼碎片。发动机换向装置包括翼片，该翼片在壳体中枢转以关闭其开口，并设有由气流导向叶片组成的格栅。集成在机身尾部的喷气发动机进气口具有可变深度的凹槽，凹槽在支架上彼此相对布置。控制系统包括控制杆，控制杆的底部为踏板，顶部为手柄。所述手柄具有起落架伸出/缩回旋钮以及底部片段组的电驱动装置。飞行器控制方法包括利用空气和气体流。效果：简化维修; 47 cl，30 dwg

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱：kefu@zhangqiaokeyan.com

京公网安备：11010802029741号 ICP备案号：京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有

  • 客服微信

  • 服务号