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AIRCRAFT HAVING ADJUSTABLE SWEPTBACK WINGS

机译:飞机有可调节的后掠翼

摘要

Means for varying the sweepback and angle of incidence of the wings of an aircraft with respect to airspeed so as to maintain efficient operation. The axis of rotation of the wings is pivotal so as to permit adjustment of the axis and consequently variance of the sweep angle in accordance with airspeed. In the forward position of the wings which corresponds to take-off and landing, the wings are parallel to the longitudinal axis of the fuselage with a zero incidence angle. In the sweptback position, the wings rise to a negative angle of incidence for greater operational efficiency during high-speed flight.
机译:用于改变飞机机翼相对于空速的后掠角和入射角以保持有效运行的装置。机翼的旋转轴线是枢转的,以便允许调节轴线并且因此允许后掠角根据空速而变化。在机翼的对应于起飞和着陆的向前位置中,机翼以零入射角平行于机身的纵轴。在后掠位置,机翼上升到负入射角,以在高速飞行中获得更高的运行效率。

著录项

  • 公开/公告号US3795374A

    专利类型

  • 公开/公告日1974-03-05

    原文格式PDF

  • 申请/专利权人 ZECH ADT;SCHAEFER EDT;

    申请/专利号USD3795374

  • 发明设计人 SCHAEFER EDT;ZECH ADT;

    申请日1971-07-16

  • 分类号B64C3/40;

  • 国家 US

  • 入库时间 2022-08-23 05:01:10

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