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Blade tip clearance control apparatus using bellcrank mechanismA clearance control apparatus has a positioning mechanism for controlling clearance between rotor blade tips and a shroud segment of a gas turbine engine casing. The positioning mechanism is supported by the casing, coupled to the shroud segment, and actuatable for moving the shroud segment toward and away from the rotor blade tips to reach a position at which a desired clearance is established. The mechanism includes a shaft and a bellcrank actuating assembly. The shaft is mounted through a passage defined by a mounting structure on the casing for radial movement along a longitudinal axis of the shaft toward and away from the rotor axis and is coupled at its inner end to the shroud segment. The bellcrank actuating assembly is coupled to an outer end of the shaft and mounted to the casing adjacent the shaft for pivotal movement about an axis spaced from and extending transverse to the longitudinal axis of the shaft. The pivotal movement of the bellcrank actuating assembly produces radial movement of the shaft and shroud segment therewith toward and away from the rotor blade tips.
Document ID
20080004253
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Corsmeier, Robert J.
Petsche, Joseph
Date Acquired
August 24, 2013
Publication Date
October 8, 1991
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-440633
Patent Number: US-PATENT-5,054,997
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-5,054,997
Patent Application
US-PATENT-APPL-SN-440633
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