Invention Grant
US08172514B2 Rim seal for a gas turbine engine 有权
燃气轮机的轮辋密封

Rim seal for a gas turbine engine
Abstract:
The rim seal is positioned in an annular space between blades and a non-rotating adjacent structure in a gas turbine engine. The rim seal is connectable to the non-rotating structure and is made of an abradable material.
Public/Granted literature
Information query
Patent Agency Ranking
0/0