Invention Grant
US08573942B2 Axial retention of a platform seal 有权
轴向保持平台密封

Axial retention of a platform seal
Abstract:
A gas turbine engine component having an axial pin stop assembly that reduces stress around a seal pin damper slot between a platform and a buttress is disclosed. The seal pin damper slot is extended to the leading edge of the buttress and an axial pin stop seal extends into the pin damper slot to limit movement of the seal pin damper while relieving stress concentration at the interface between the buttress and platform.
Public/Granted literature
Information query
Patent Agency Ranking
0/0