首页> 外国专利> SYSTEM OF WINGLETS AND METHOD OF IMPROVING THE FLYING-TECHNICAL CHARACTERISTICS OF AN AIRCRAFT PLANE

SYSTEM OF WINGLETS AND METHOD OF IMPROVING THE FLYING-TECHNICAL CHARACTERISTICS OF AN AIRCRAFT PLANE

机译:小翼系统和改进飞机飞机飞行技术特性的方法

摘要

FIELD: aviation.;SUBSTANCE: winglet system for a wing contains an upper winglet and a lower winglet mounted on the wing tip. The lower winglet has a static position when the wing is subject to static loading when parking on the ground. The lower end flap is designed so that the wing deflection upward with a flight load of approximately 1g causes the lower winglet to move from the static position to the flight position, resulting in a relative increase in the span of the wing. The aircraft contains a system of winglets that are located at the intersection of the gate gap and the lumen line at pitch and roll. Method of the aircraft operation is characterized by the movement of the winglets.;EFFECT: reduction of inductive drag of the wing.;20 cl, 15 dwg
机译:领域:航空;实体:机翼的小翼系统包括安装在机翼尖端的上小翼和下小翼。当机翼停放在地面上时,如果机翼承受静载荷,则下小翼将处于静态位置。下端襟翼的设计使得机翼在大约1g的飞行载荷作用下向上偏转,导致下小翼从静态位置移动到飞行位置,从而导致机翼跨度相对增加。该飞机包含一个小翼系统,这些小翼系统位于栅隙和管腔线的交点处,俯仰和滚动。飞机操作方法的特征在于小翼的运动;效果:减小了机翼的感应阻力; 20 cl,15 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