Gas turbine shroud seal and corresponding gas turbine engine

摘要

A blade outer air seal system includes a body (38) that extends between two circumferential sides (44), a leading edge (42a) and a trailing edge (42b), and a radially inner side (40a) and a radially outer side (40b). An attachment section (46) is associated with the body (38) and includes at least one engagement surface(48a,48b) that is transverse to the radially outer side (40b).