Gas turbine engine cooling apparatus

Details Gas turbine engine cooling apparatus Gas turbine engine cooling apparatus

1998-05-05

2000-07-18

Look, Edward K.

Rotary kinetic fluid motors or pumps

With passage in blade, vane, shaft or rotary distributor...

415116, 415175, 415178, F01D 1108

Patent

active

060898216

ABSTRACT:
A gas turbine engine has an assembly of circumferentially spaced rotor blades each having a radial tip. A plurality of seal segments mounted for radial movement circumscribe the rotor blades. Each segment is connected to the casing through a seal carrier provided with a flexible membrane which divides high pressure air from low pressure into two channels.

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