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Light aircraft for short-distance takeoff and landing

机译:轻型飞机,用于短距离起降

摘要

A light aircraft for short distance takeoff and landing includes an airplane having a propeller provided on a rear pedestal thereof for producing vertical propulsion and an airship having a propeller provided on a rear pedestal thereof for producing vertical propulsion and also having a flight attitude sensor provided within an operating compartment thereof. The flight attitude sensor is always directed in the vertical direction, detects forward and rearward inclinations of the airship, and transmits signals corresponding to the inclinations to the two propellers, thereby rotating the two propellers to produce downward or upward propulsion to maintain the aircraft at the normal horizontal attitude at all times.
机译:一种用于短距离起降的轻型飞机,包括:飞机,其后座上设置有螺旋桨,用于产生垂直推进;以及飞艇,其后座上设置有螺旋桨,用于产生垂直推进,并且还具有设置在其内部的飞行姿态传感器。其操作室。飞行姿态传感器始终指向垂直方向,检测飞艇的向前和向后倾斜,并将与该倾斜相对应的信号传输到两个螺旋桨,从而旋转两个螺旋桨以产生向下或向上的推进力,从而将飞机保持在始终保持正常的水平姿势。

著录项

  • 公开/公告号US4889297A

    专利类型

  • 公开/公告日1989-12-26

    原文格式PDF

  • 申请/专利权人 IKEDA;MINORU;

    申请/专利号US19880267276

  • 发明设计人 MINORU IKEDA;

    申请日1988-11-04

  • 分类号B64B1/20;B64C1/34;

  • 国家 US

  • 入库时间 2022-08-22 06:08:11

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