Diametrically expandable/collapsible piston seal
A gas turbine engine includes a rotor that has a seal surface and a shaft that is rotatable about an engine central axis. The shaft has an annular seal channel that opens to the seal surface. There is a seal for sealing against the seal surface. The seal has channels formed therein that define a tortuous seal wall with interconnected spring ligaments such that the seal is elastically diametrically expandable for installation clearance around the shaft and, once on the shaft, elastically diametrically collapsible into the annular seal channel.
1. A gas turbine engine comprising:
a rotor having a seal surface;
a shaft rotatable about an engine central axis, the shaft having an annular seal channel that opens to the seal surface;
a seal for sealing against the seal surface, the seal having first and second opposed axial faces, the seal having channels formed therein, radially inner and outer faces, and an annular groove that opens at the radially inner face, the channels are axial through-channels that open at each of the first and second opposed axial faces, and the channels define a tortuous seal wall with interconnected spring ligaments such that the seal is elastically diametrically expandable for installation clearance around the shaft and, once on the shaft, elastically diametrically collapsible into the annular seal channel; and
a flexible sealant disposed in the channels and the annular groove, the flexible sealant sealing the channels with respect to flow between the first and second opposed axial faces.
2. The gas turbine engine as recited in claim 1 , wherein the seal is metallic.
3. The gas turbine engine as recited in claim 1 , wherein the seal is a full hoop.
4. The gas turbine engine as recited in claim 1 , wherein the flexible sealant includes silicone or fluoropolymer.
5. The gas turbine engine as recited in claim 1 , wherein the channels are unbranched.
6. A gas turbine engine comprising:
a rotor having a seal surface;
a shaft rotatable about an engine central axis, the shaft having an annular seal channel that opens to the seal surface; and
a seal for sealing against the seal surface, the seal having channels formed therein that define a tortuous seal wall with interconnected spring ligaments such that the seal is elastically diametrically expandable for installation clearance around the shaft and, once on the shaft, elastically diametrically collapsible into the annular seal channel, wherein the channels are helical.
7. The gas turbine as recited in claim 1 , wherein the channels are branched.
8. A seal for a gas turbine engine, comprising:
a metallic tortuous seal wall having first and second opposed axial faces, channels formed in the metallic tortuous seal wall, radially inner and outer faces, and an annular groove that opens at the radially inner face, the channels are axial through-channels that open at each of the first and second opposed axial faces, and the metallic tortuous seal wall having interconnected spring ligaments such that the seal is elastically diametrically expandable and elastically diametrically collapsible, and a flexible sealant disposed in the channels and the annular groove, the flexible sealant sealing the channels with respect to flow between the first and second opposed axial faces.
9. The seal as recited in claim 8 , wherein the channels are unbranched.
10. The seal as recited in claim 9 , wherein the channels are helical.
11. The seal as recited in claim 8 , wherein the channels are branched.
12. A method of assembling a seal into a gas turbine engine, the method comprising:
providing a metallic tortuous seal wall with interconnected spring ligaments such that the seal is elastically diametrically expandable and elastically diametrically collapsible, the metallic tortuous seal wall having first and second opposed axial faces, channels formed in the metallic tortuous seal wall, radially inner and outer faces, and an annular groove that opens at the radially inner face, the channels are axial through-channels that open at each of the first and second opposed axial faces, and the metallic tortuous seal wall having interconnected spring ligaments such that the seal is elastically diametrically expandable and elastically diametrically collapsible, and a flexible sealant disposed in the channels and the annular groove, the flexible sealant sealing the channels with respect to flow between the first and second opposed axial faces;
applying an expanding force to the seal to elastically diametrically expand the seal, and then moving the seal over a shaft and into an annular seal channel of the shaft; and
releasing the expanding force from the seal such that the seal elastically diametrically collapses into the annular seal channel.