Patent ID: 9718539
Date: 2017-08-01
CPC Classifications: B60T,B64C,B64D,F16C,G01P

Claim:
1. An aircraft landing gear comprising an axle ( 3 ) intended to receive a wheel ( 4 ) comprising a rim ( 6 ) mounted to rotate on the axle ( 3 ) by means of at least one rolling bearing ( 8 ), said rolling bearing ( 8 ) comprising an inner ring ( 11 ) mounted around the axle ( 3 ) and an outer ring ( 12 ) rotationally secured to the rim ( 6 ) of the wheel ( 4 ), the landing gear further comprising measurement means ( 21 ) intended to perform measurements of at least one operating parameter of the landing gear, characterized in that the measurement means ( 21 ) are incorporated in the rolling bearing ( 8 ) by being secured to one of the inner and outer rings of the rolling bearing ( 8 ).