LANDING GEAR FOR AN AIRCRAFT COMPRISING AN OBSTACLE DETECTOR

摘要

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).

主权项

1. A landing gear for an aircraft comprising:
a casing, having a main direction extending along a longitudinal axis, said casing comprising a first end configured to be mounted on the aircraft, and a second end opposite to the first end, a rod, slidably mounted on the second end of the casing, said rod being movable in translation with respect to the casing along the longitudinal axis, at least one obstacle detector attached to the landing gear,the landing gear wherein the obstacle detector is attached in an area adjacent to the second end of the casing.