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 characterized in that the obstacle detector (2) is secured in a zone adjacent to the second end (10b) of the strut assembly (10).
ATTERRISSEUR POUR UN AERONEF COMPRENANT UN DETECTEUR D'OBSTACLES
LANDING GEAR FOR AN AIRCRAFT, COMPRISING AN OBSTACLE DETECTOR
FAHRWERK MIT EINEM HINDERNISDETEKTOR FÜR EIN FLUGZEUG
2018-01-31
Patent
Electronic Resource
French
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