Hydrostatic annular seal

Abstract

A seal for an aircraft turbine engine includes a plurality of seal segments distributed circumferentially about a longitudinal axis, each seal segment having a radially outer annular wall segment and a radially inner annular wall segment which are connected to each other by an elastically deformable member. Pairs of circumferentially adjacent seal segments have their respective elastically deformable member implemented monolithically as a common deformable elastic member, the common deformable elastic member connecting together two radially inner annular wall segments of circumferentially-adjacent seal segments such that the radially outer annular wall segments of the seal segments form a monolithic outer shroud.

Dependencies are inferred from the claim text.