Adjustable clearance control for rotor blade tips in a gas turbi

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Between blade edge and static part

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Details

4151733, 4151741, 4151734, F01D 1108

Patent

active

053442849

ABSTRACT:
In a gas turbine engine having rotor blades which rotate with the blade tips in proximity with a surrounding rub strip in the engine shroud, an improvement is provided in the form of a radially adjustable rub strip-air bladder assembly. That is, an air bladder is mounted between the rub strip and the shroud and compressed air is fed to or withdrawn from the bladder to radially displace the rub strip so it can follow changes in the rotor blade length and maintain a close clearance with the tips of such blades under varying engine conditions, e.g. accels and decels, while minimizing contact of blade tips and rub-strip. The rub strip-bladder assembly is flexible and can react automatically to radially withdraw in advance of extending rotor blades as a pressure surge suddenly backs through such blades.

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