Modulated turbine cooling system

Patent metadata

Field	Value
Publication number	US-11092013-B2
Application number	US-201816236018-A
Country	US
Kind code	B2
Filing date	Dec 28, 2018
Priority date	Mar 15, 2013
Publication date	Aug 17, 2021
Grant date	Aug 17, 2021

Abstract

A flow transfer apparatus for transferring cooling flow from a primary gas flowpath to a turbine rotor. The apparatus includes a first supply plenum communicating with the primary gas flowpath and first inducers, the first inducers configured to accelerate a first fluid flow from the first supply plenum and discharge it toward the rotor with a tangential velocity; a second supply plenum communicating with the primary gas flowpath and second inducers, the second inducers configured to accelerate a second fluid flow from the second supply plenum towards the rotor with a tangential velocity; and a cooling modulation valve operable to selectively permit or block the second fluid flow from the primary gas flowpath to the second supply plenum. The valve includes a flow control structure disposed in the primary gas flowpath and an actuation structure extending to a location radially outside of a casing defining the primary gas flowpath.

First claim

What is claimed is:

1. A method of transferring a cooling flow from a primary gas flowpath to a turbine rotor of a gas turbine engine that has at least two different operating conditions, the method comprising:
during all conditions of engine operation, flowing a first fluid flow from the primary gas flowpath through a first supply plenum to a plurality of first inducers, each of the first inducers configured to accelerate the first fluid flow and discharge the first fluid flow toward the turbine rotor with a tangential velocity component; and
during some but not all of the operating conditions, flowing a second fluid flow from the primary gas flowpath through a cooling modulation valve and a second supply plenum to a plurality of second inducers, each of the second inducers configured to accelerate the second fluid flow and discharge the second fluid flow towards the turbine rotor with a tangential velocity component;
wherein the cooling modulation valve comprises a flow control structure disposed in the primary gas flowpath and a valve actuation structure extending from the flow control structure to a location radially outside of a casing defining the primary gas flowpath; and
wherein the flow control structure comprises a valve body with a cylindrical bore and a window formed through the body, communicating with the bore and a piston received in the bore and translatable between a closed position in which it blocks flow between the window and the bore, and an open position in which it permits flow from the window to the bore.

2. The method of claim 1 wherein the first supply plenum is defined in part by an annular space between an inner combustor liner and an annular inner nozzle support.

3. The method of claim 1 wherein the second supply plenum is disposed immediately axially upstream of the first supply plenum.

4. The method of claim 1 wherein the second fluid flow is transferred from the second supply plenum to each of the second inducers by an axially-extending transfer tube disposed within the first supply plenum.

5. The method of claim 1 wherein an operating rod is disposed in the valve body and has a lower end connected to the piston and an upper end extending outside of the casing.

6. The method of claim 5 wherein an actuator is disposed outside the casing and coupled to the upper end of the operating rod.

7. The method of claim 1 wherein:
the cooling modulation valve comprises a generally cylindrical valve body that extends in a radial direction from a collar housing of the second supply plenum to the casing; and
the valve body is moveable in a radial direction relative to the collar housing.

8. The method of claim 7 wherein a ring-like collar is disposed within the collar housing surrounding an inner end of the valve body.

Assignees

• Gen Electric

Inventors

• Rahaim John Joseph
• Fusinato Daniel John
• Hunter Scott David
• Kirk Joel Francis
• Melzak Michael Robert
• Stover Curtis Walton

Classifications

• F01D5/082 Primary

  on the side of the rotor disc · CPC title

• F01D5/081

  Cooling fluid being directed on the side of the rotor disc or at the roots of the blades (F01D5/087 takes precedence) · CPC title

• F02C7/125

  by partial arc admission of the working fluid or by intermittent admission of working and cooling fluid · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F05D2270/3062

  of the auxiliary fluid for heating or cooling purposes · CPC title