Turbine engine shroud segment, featherseal for a shroud segment and corresponding assembly

摘要

An air seal assembly (10) includes a featherseal (76) engaged between adjacent turbine engine components (54) to close a gap therebetween. The featherseal (76) includes a first lateral tab (80) and a second lateral tab (82) which defines a tab space (84) therebetween. The tab space (84) locks the featherseal (76) into the turbine engine component (54) to prevent fore-aft movement thereof.