Clearance control system

Rotary kinetic fluid motors or pumps – With control means responsive to non-cyclic condition... – Temperature or fluid force responsive member

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415116, F01D 1700

Patent

active

048939846

ABSTRACT:
A system for controlling rotor blade tip clearances in a gas turbine engine supplies both heating air and cooling air to the rotor bore. The heating air flow is controlled by a valve and the cooling air flow is not controlled.

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CF6 Jet Engine Diagnostics Program, by M. A. Radomski, Jan. 1982.
CFM56-5 Technical Review-Oct. 1986.

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