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X-wing helicopter-scout attack configuration

机译:X翼直升机侦察兵攻击配置

摘要

The present invention provides a single seat aircraft having the capabilities of vertical takeoff, landing and hovering operations utilizing the X-Wing as a conventional helicopter rotating wing. After transition to forward flight following takeoff, the rotating wing is stopped and becomes a fixed wing of "X" configuration. The aircraft utilizes two engines within the fuselage, one engine being positioned vertically above the other along the longitudinal axis of the aircraft, the particular arrangement of engines allowing aircraft size and weight to be substantially reduced.
机译:本发明提供了一种单座飞机,其具有利用X翼作为常规直升机旋转机翼的垂直起飞,着陆和悬停操作的能力。起飞后过渡到前向飞行后,旋转的机翼停止转动并变成“ X”型固定翼。飞机在机身内使用了两个发动机,一个发动机沿着飞机的纵轴垂直放置在另一个发动机上方,发动机的特殊布置使飞机的尺寸和重量大大减小。

著录项

  • 公开/公告号US4711415A

    专利类型

  • 公开/公告日1987-12-08

    原文格式PDF

  • 申请/专利权人 NORTHROP CORPORATION;

    申请/专利号US19850696604

  • 发明设计人 JOHN A. BINDEN;

    申请日1985-01-30

  • 分类号B64C27/82;

  • 国家 US

  • 入库时间 2022-08-22 06:49:45

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