Patent ID: 8826942

Claim:
A sleeve and leak detection assembly for an aircraft, comprising: a hose ( 50 ) that connects and channels pressurized air from a pressurized air source to a system with pressurized air requirements; a sleeve ( 52 ) that delimits an annular chamber around said hose ( 50 ), said sleeve ( 52 ) comprising at least one opening ( 54 ) delimited by an edge ( 58 ), said at least one opening ( 54 ) providing a link between said annular chamber and an outside of the sleeve ( 52 ); and a leak detection system that comprises i) at least one loop (A, B) in the form of a threadlike element ( 56 ), and ii) a connecting device that comprises a ring ( 60 ) connected at at least one connecting point ( 64 ) with the loop (A, B), and a flexible wall that delimits a channel hose ( 68 ) forming a pressurized air channel that extends from the edge ( 58 ) of the opening ( 54 ) up to the ring ( 60 ).