AIRCRAFT TOWING ROBOT AND WORKING METHOD THEREFOR

An aircraft towing robot, comprising an omnidirectional mobile chassis formed by a heavy-load frame body (1) and a Mecanum wheel (2) assembly distributed around the heavy-load frame body (1). An aircraft support plate (9), which can be lifted and lowered by a lifting assembly, is mounted on each of...

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Main Authors AI, Yuming, WANG, Chunmei, YU, Baocheng, XIONG, Li, XU, Wenxia, GUO, Ran, GUO, Kai, ZHANG, Min, WNAG, Han, WU, Jing, ZHANG, Lina
Format Patent
LanguageChinese
English
French
Published 04.08.2022
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Summary:An aircraft towing robot, comprising an omnidirectional mobile chassis formed by a heavy-load frame body (1) and a Mecanum wheel (2) assembly distributed around the heavy-load frame body (1). An aircraft support plate (9), which can be lifted and lowered by a lifting assembly, is mounted on each of the front and rear ends of the upper portion of the heavy-load frame body (1). A laser sensor (10) for detecting the distance between the aircraft support plate (9) and an aircraft connection point is disposed on an outer side of a support recess on each aircraft support plate (9). A locking connection assembly for locking an aircraft is provided on both sides of the middle of the upper portion of the heavy-load frame body (1). PSD sensors (15), which correspond one-to-one to the positions of laser transmitters at the bottom portion of the aircraft, are distributed on the upper portion of the heavy-load frame body (1). A navigation code reader (14) for collecting and parsing a two-dimensional code at a node positio
Bibliography:Application Number: WO2021CN99744