Flexible small cavity seal for gas turbine engines
A seal assembly, comprising a first segment, a second segment, and a seal incorporated between the first segment and the second segment, the seal comprising a mesh. The first segment may comprise a blade outer air seal and the second segment may comprise a vane. In various embodiments, the first segment and the second segment may define a gap, and the seal may seal the gap. The seal may have a first member and a second member that enmeshes the first member. The seal may comprise a member that enmeshes a non-metallic member. The seal may comprise a ceramic fiber enmeshed by a member. The seal may comprise a non-metallic member enmeshed by a metallic member. The seal may comprise a plurality of annular connecting members, each annular connecting member extending about the seal. The seal may comprise a single annular member.
1. A seal assembly, comprising:
a first segment;
a second segment spaced from the first segment; and
a seal incorporated between the first segment and the second segment, wherein the seal comprises a first member comprising a braided fiber, a second member woven through a plurality of apertures formed through the first member to form a single annular member, and a sheath covering the first member and the second member, wherein the seal comprises a U-shaped member comprising a first leg engaged with the first segment, a second leg engaged with the second segment, and an open space extending between opposing portions of the first leg and second leg, wherein each of the first leg and the second leg comprise the first member, the second member, and the sheath.
2. The seal assembly of claim 1 , wherein the first segment comprises a blade outer air seal and the second segment comprises a vane.
3. The seal assembly of claim 1 , wherein the first segment and the second segment define a gap, and the seal seals the gap.
4. The seal assembly of claim 1 , wherein the first member comprises a non-metallic member.
5. The seal assembly of claim 1 , wherein the first member comprises a ceramic fiber.
6. The seal assembly of claim 1 , wherein the first member comprises a non-metallic member and the second member comprises a metallic member.
7. A seal for incorporation between a blade outer air seal segment and a vane segment, the seal comprising:
a first seal comprising:
a first member comprising a braided fiber:
a second member woven through a plurality of apertures formed through the first member to form a single annular member, wherein the first seal comprises a U-shaped member comprising a closed end, a first leg, and a second leg that is spaced from the first leg, wherein each of the first leg and the second leg of the first seal comprise the first member and the second member of the first seal; and
a gap located at a circumferential location on the first seal;
a second seal, separate from the first seal, and comprising:
a first member; and
a second member interwoven with the first member to form a single annular member, wherein the second seal comprises a U-shaped member comprising a closed end, a first leg, a second leg, and an open space bounded by the closed end, the first leg, and the second leg of the second seal, wherein the second seal is nested within the first seal such that the closed end of the second seal engages the closed end of the first seal, such that the first leg of the second seal engages the first leg of the first seal, and such that the second leg of the second seal engages the second leg of the first seal, wherein each of the first leg and the second leg of the second seal comprise the first member and the second member of the second seal, wherein a first portion of the first seal is fixed to a first portion of the second seal near the gap and wherein a second portion of the first seal is slidably coupled to a second portion of the second seal near the gap.
8. The seal of claim 7 , wherein the first member comprises a non-metallic member.
9. The seal of claim 7 , wherein the second member comprises a metallic member.
10. The seal of claim 7 , wherein the second member comprises a nickel-chromium based austenitic alloy.
11. A seal assembly, comprising a blade outer air seal segment, a vane segment, and the seal of claim 7 , wherein the first leg of the first seal engages the blade outer air seal segment, and the second leg of the first seal engages the vane segment.
12. The seal of claim 7 , wherein the second seal is located radially outward of the first seal.