| 摘要 |
A slider seal assembly (30) for a gas turbine engine includes a housing (32), a seal plate (34) moveable relative to the housing (32) and a retaining ring (36). The housing (32) includes an outer surface (42), an inner surface (44), and a recessed opening (38) between the outer surface (42) and the inner surface (44). The seal plate (34) is received within the recessed opening (38). The inner surface (44) of the housing (32) includes a curved portion (45) which is curved in an outward direction toward the outer surface (42).
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