The invention relates to a landing gear (1) of an aircraft (5), comprising: a strut assembly (10) including a first end (10a) designed to be mounted on the aircraft (5) and a second end (10b) opposite the first end (10a); a rod (14) slidably mounted on the second end (10b) of the strut assembly (10), said rod (14) being translationally movable in relation to the strut assembly (10); and at least one obstacle detector (2) secured to the landing gear (1), the landing gear (1) being characterised in that the obstacle detector (2) is secured in a zone adjacent to the second end (10b) of the strut assembly (10).
LANDING GEAR FOR AN AIRCRAFT COMPRISING AN OBSTACLE DETECTOR
09.02.2017
Patent
Elektronische Ressource
Englisch
Landing gear for an aircraft comprising an obstacle detector
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