A system and method for debugging and calibrating landing lights and taxiing lights

A technology for calibrating systems and taxiing lights, which is applied in the direction of electrical components, etc., can solve the problems of difficult calibration, meteorological conditions such as high wind speed requirements, and high risk of falling

A technology for calibrating systems and taxiing lights, which is applied in the direction of electrical components, etc., can solve the problems of difficult calibration, meteorological conditions such as high wind speed requirements, and high risk of falling

CN109548250BActive Publication Date: 2020-05-15中航通飞华南飞机工业有限公司
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  • A system and method for debugging and calibrating landing lights and taxiing lights
  • A system and method for debugging and calibrating landing lights and taxiing lights

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Embodiment Construction

[0029] Such as figure 1 As shown, a system for debugging and calibrating landing lights and taxiing lights includes an interface mounting base 1, a laser generator and a main control device. On the fuselage, the adjusting member 2 is used to adjust the position of the interface mounting seat relative to the fuselage. The adjusting member 2 of this embodiment adopts a mounting screw, and a spring washer is arranged between the mounting screw and the fuselage structure, and the screw head There is a lock wire safety hole, which is used to fix the screw after the adjustment is completed with a fuse. The interface mounting base 1 is provided with screw holes, and the interface mounting base 1 is movably connected with the landing light, the taxi light lampshade, the spring washer and the fuselage through mounting screws. The adjustment member 2 can also be adjustable in height or length by bolts, etc., and can be adjusted by adding gaskets with a predetermined thickness to achiev...

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Abstract

The invention discloses a landing lamp and taxi light debugging and calibration system and method. The system comprises an interface mounting seat, a laser generator and a main control device. The interface mounting seat is mounted on a landing lamp and sliding lamp cover through an adjusting member, and the laser generator comprises a first microprocessor, a driver, a laser generator, an angle measuring module and a first communication module, wherein the driver, the laser generator, the angle measuring module and the first communication module are each connected to the first microprocessor.The laser generator is connected with the driver, and the main control device comprises a second microprocessor, a second communication module and a human-machine interaction module, wherein the second communication module and the human-machine interaction module are connected with the second microprocessor. The angle measuring module and the laser generator are fixedly arranged. The system makesit unnecessary for a calibration worker to select the night and to be able to perform the lighting debugging and calibration of a landing light and a taxi light without turning on the landing light and the taxi light, and also avoids the disadvantages of an operator being burned by the landing light and the taxi light.

Description

technical field [0001] The invention relates to the technical field of aircraft maintenance debugging support equipment in aviation manufacturing and aviation operation, and in particular to a system and method for debugging and calibrating landing lights and taxiing lights. Background technique [0002] In the prior art, when debugging and calibrating landing lights and taxiing lights, it is necessary to manually calibrate and adjust the installation angles of landing lights and taxiing lights so as to meet the requirements of design and installation indicators. The debugging and calibration method is to choose to drag the aircraft out of the hangar at night, keep the aircraft parked on land, and place a screen perpendicular to the plane of symmetry of the aircraft at a distance of 10 meters in front of the nose of the aircraft (indoor debugging can be done with a white wall as screen), check that the central beam of the landing light or taxiing light should be irradiated i...

Claims

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Application Information

Patent Timeline
15 May 2020
Publication
CN109548250B
IPC
H05B47/10
CPC
H05B47/10
Inventors
韩琳琳; 韩永良