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Elliptical aircraft with movable ballast - has adjustable pods slung under fuselage and contg. water ballast

机译:带有可移动压载物的椭圆形飞机-在机身下方和上端悬挂有可调节的吊舱。水压载

摘要

The aircraft has an elliptical cross section, like a flying saucer, with the cockpit in the front half of the upper section. A centrally mounted ducted turbofan provides lift and movable flaps direct the thrust. Steering is by flaps and steering jets around the periphery. Stability is controlled by three pods slung under the fuselage and filled with water ballast from a control pump. The aircraft is made from glass fibre on light alloy frames for strength and lightness. The efficient turbofan has a good power to weight ratio while the ballast control, with the pods not only linked to pumps, but also extending from the fuselage, enables the craft to be steered in any direction.
机译:飞机的横截面为椭圆形,就像飞碟一样,驾驶舱位于上部的前半部分。中央安装的管道涡轮风扇提供升力,可移动的襟翼引导推力。转向是通过襟翼和周围的转向射流进行的。稳定性由悬挂在机身下方的三个吊舱控制,并装有来自控制泵的压载水。该飞机由玻璃纤维制成,并在轻合金框架上具有强度和轻便性。高效的涡扇发动机具有良好的功率重量比,而压载控制装置(吊舱不仅连接至泵,而且还从机身延伸)使船舶可以在任何方向上操纵。

著录项

  • 公开/公告号DE2540659A1

    专利类型

  • 公开/公告日1977-03-17

    原文格式PDF

  • 申请/专利权人 CONTEHEINZ PHILIPP;

    申请/专利号DE19752540659

  • 发明设计人

    申请日1975-09-12

  • 分类号B64C27/20;

  • 国家 DE

  • 入库时间 2022-08-23 00:04:39

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