Patent ID: 11945063
Assignee: RTX CORPORATION
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 0:
1. A gas turbine engine, comprising:
a compressor section configured to compress a gas;
a combustor section aft of the compressor section and configured to combust the gas; and
a piston seal assembly comprising:
a worked seal groove, wherein the worked seal groove is generated between a forward seal wall and an aft seal wall of the piston seal groove, wherein the forward seal wall and the aft seal wall extend radially from a case comprising the piston seal assembly, wherein after removing the worn material, one of the seal walls comprises a first thickness and the other seal wall comprises a second thickness, wherein the first thickness is smaller relative the second thickness;
a groove buildup member secured to the worked seal groove, wherein the groove buildup member is a guard type member, wherein the guard type member comprises an inner guard and an outer guard joined at a distal end by an orthogonal web, wherein the outer guard is shorter relative the inner guard, wherein the inner guard is disposed within the worked seal groove, wherein the guard type member is configured to interface with the seal wall having the first thickness, wherein the orthogonal web of the guard type member is disposed over the seal wall having the first thickness; and
a seal member disposed proximate the groove buildup member.