TURBINE ENGINE TIP CLEARANCE CONTROL SYSTEM WITH LATERAL TRANSLATABLE SLIDE BLOCK

摘要

An assembly is provided for a turbine engine with an axial centerline. This turbine engine assembly may include a blade outer air seal segment 66, a linkage 70 and an actuation device 68. The linkage 70 may include a shaft 136 and a head 138, where the shaft 136 is connected to the blade outer air seal segment 66 and extends radially outward to the head 138. The actuation device 68 may include a sloped slide block 78 located radially within and engaged with the head 138. The actuation device 68 may be configured to laterally translate the sloped slide block 78 and thereby radially move the blade outer air seal segment 66.