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An improved instrument for indicating the attitude and behaviour of aircraft in flight

机译:用于指示飞行中的飞机的姿态和行为的改进的仪器

摘要

517,563. Level indicators for aircraft. LANGLEY, T. W., and TECALEMIT, Ltd. May 9, 1938, No. 13866. [Class 97 (ii)] An indicator for the attitude and behaviour of aircraft during flight comprises a casing 1 having a translucent front screen 3 upon which a representation of the aircraft is depicted, two tubes 6 whereby light from bulbs 7 passing through aperture 8 are reflected by mirrors 11, 11', to a mirror 13 mounted for universal movement and to remain perpendicular to gravitational force or to. the resultant of gravitational and centrifugal forces acting on the aircraft and thence by mirrors 15, 151 to the screen. When the aircraft is flying level the light beams H, H1 are projected on to the screen to coincide with the marks 16, 161 on the aircraft representation, deviation of the beams indicating the mechanism of the aircraft other than level. The mirror 13 in frame 17 is mounted in a gimbal ring 18 mounted universally and is provided with a pendulum dipping into an oil receptacle 28. A " rate of turn indicator may be provided comprising a pointer 32 mounted on a shaft 31 attached to a frame 34 in which a shaft 38 is mounted having a gyroscope 35 driven by air jet nozzles 39. A restoring spring 37 for the frame 34 is provided and the pointer 32 is responsive to any gyroscopic couples set up. Modifications of the mirror 13 and also of the mirrors 11, 111, 15, 151 as described.
机译:517,563。飞机的液位指示器。 TW。LANGLEY和TECALEMIT,Ltd.,1938年5月9日,编号13866。[等级97(ii)]用于指示飞机在飞行过程中的姿态和行为的指示器包括机壳1,该机壳具有半透明的前屏幕3,在该屏幕上显示描绘了飞机的平面图中的两个管6,来自灯泡7的穿过孔8的光被反射镜11、11'反射到安装用于普遍运动并保持垂直于重力或垂直于重力的反射镜13。重力和离心力作用在飞机上的合力,然后由反射镜15、15 1投射到屏幕上。当飞机在水平飞行时,光束H,H <1>投射到屏幕上,与飞机图示上的标记16、16 <1>重合,光束的偏离表明飞机不在水平面上。镜架17中的镜子13安装在万向节环18中,该万向节环18被普遍地安装,并且具有被浸入到油容器28中的摆。可提供“转速指示器”,其包括安装在附接到镜架的轴31上的指示器32。在图34中,轴38被安装,轴38具有由空气喷嘴39驱动的陀螺仪35。提供用于框架34的复位弹簧37,并且指针32响应于所建立的任何陀螺仪对。如上所述,反射镜11、11 1,15、15 1。

著录项

  • 公开/公告号GB517563A

    专利类型

  • 公开/公告日1940-02-02

    原文格式PDF

  • 申请/专利权人 THOMAS WINSMORE LANGLEY;TECALEMIT LIMITED;

    申请/专利号GB19380013866

  • 发明设计人

    申请日1938-05-09

  • 分类号G01C9/12;

  • 国家 GB

  • 入库时间 2022-08-24 04:40:03

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