首页> 外国专利> TAIL CONE OF FLYING VEHICLE AND MECHANISM FOR CONNECTION OF TAIL CONE FLAPS WITH ENGINE NOZZLE SHUTTERS

TAIL CONE OF FLYING VEHICLE AND MECHANISM FOR CONNECTION OF TAIL CONE FLAPS WITH ENGINE NOZZLE SHUTTERS

机译:飞行器尾锥和尾锥襟翼与发动机喷嘴挡板连接的机理

摘要

FIELD: aeronautical engineering; construction of aircraft fuselage tail sections. SUBSTANCE: tail cone is provided with rigid flaps deflected in synchronous with engine flaps. Each movable rigid flap connected with engine nozzle shutter is additionally provided with flexible member mounted over outer contour of tail cone and fitted with three support points; first point is mounted on fixed housing of tail cone and two other supports are mounted on tiltable rigid flap for motion along it. Provision is made for flexible member and mechanism for connecting the tail cone flaps and engine nozzle shutters. EFFECT: improved aerodynamic quality of form. 4 cl, 9 dwg
机译:领域:航空工程;飞机机身尾部的构造。实质:尾锥配有与发动机襟翼同步偏转的刚性襟翼。与发动机喷嘴百叶窗相连的每个可移动的刚性襟翼还设有柔性件,该柔性件安装在尾锥的外轮廓上并装有三个支撑点。第一点安装在尾锥的固定外壳上,另外两个支撑件安装在可倾斜的刚性翻盖上,以便沿其移动。提供了用于连接尾锥阀瓣和发动机喷嘴百叶窗的柔性构件和机构。效果:改善了空气动力学形式的质量。 4厘升,9载重吨

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