Patent ID: 8550398
Filing Date: 2013-10-08
Classification: B64C

Abstract:
1. Fairing ( 10 ) for aircraft horizontal stabilizer ( 3 ) comprising a front part ( 11 ) and a rear part ( 12 ), wherein the front part ( 11 ) is the part of the fairing ( 10 ) receiving hot air stream ( 6 ) coming from the aircraft engines ( 4 ), this front part ( 11 ) being made of an anti-erosion material, the rear part ( 12 ) being made of a material resisting the aerodynamic loads existing on the fairing ( 10 ), wherein the rear part ( 12 ) is a single unitary piece enlarged in order to allow the front part ( 11 ) to overlap said rear part ( 12 ), wherein the front part ( 11 ) and the rear part ( 12 ) are further joined by rivets.