Patent ID: 8800258
Filing Date: 2014-08-12
Classification: B64D,F02C,Y02T

Abstract:
1. An air intake structure mounted upstream of a mid-structure of a nacelle for an aircraft engine, said air intake structure comprising: an external wall incorporating a lip and mounted movably with respect to said mid-structure between a rear position and a front position; a partition defining a deicing component in said lip; at least one deicing manifold extending in said compartment; and at least one duct for supplying hot air to said manifold, said duct connected in a fixed manner to said mid-structure, wherein said partition is fixed in a sealed manner to said lip, and said duct is connected to said manifold by disconnectable sealed means that is non-rotatable about a longitudinal axis of said duct, wherein said disconnectable sealed means are situated in an immediate vicinity of said partition, and wherein said deicing manifold is fixedly attached to said partition.