Hydrostatic annular seal

A seal for an aircraft turbine engine, comprising a plurality of seal segments distributed circumferentially about a longitudinal axis, each seal segment comprising a radially outer annular wall segment (204) and a radially inner annular wall segment (202) which are connected to each other by an elastically deformable member a first elastically deformable member comprising:

• an inner leg (206) having a radially inner end (208) fixed to the radially inner annular wall segment (202, 205) and
• an outer leg (207) having a radially outer end (209) fixed to the radially outer annular wall segment (204), the radially outer end (210) of the inner leg (206) and the radially inner end (211) of the outer leg (207) being connected to each other by a connecting wall (215), the inner leg (206) and the outer leg (207) extending radially such that the radially inner end (211) of the outer leg (207) is arranged radially inside the radially outer end (210) of the inner leg 2. The seal according to claim 16, wherein said elastically deformable member further comprises a third elastically deformable member (215), the outer leg of the second elastically deformable member (213) being arranged axially between the inner leg of the first elastically deformable member (212) and the inner leg of the third elastically deformable member (215).