Suction enabled post shutdown combustor cooling and core ventilation

Patent metadata

Field	Value
Publication number	US-12584444-B2
Application number	US-202418818853-A
Country	US
Kind code	B2
Filing date	Aug 29, 2024
Priority date	Aug 29, 2024
Publication date	Mar 24, 2026
Grant date	Mar 24, 2026

Abstract

A suction enabled post shutdown combustor cooling and ventilation system including a pump fluidly coupled with a suction line, wherein the suction line is fluidly coupled with suction ports proximate a fuel system component near the combustor; a pump suction valve positioned in the suction line upstream of the pump; a pump discharge line fluidly coupled with the pump, an outlet fluidly coupled with the pump discharge line; and an engine core flow path fluidly coupled with the suction ports.

First claim

What is claimed is:

1 . A suction enabled post shutdown combustor cooling and ventilation system comprising:
a pump fluidly coupled downstream of a suction line, wherein the suction line is fluidly coupled downstream of suction ports proximate a fuel system component near a combustor; a pump suction valve positioned in the suction line upstream of the pump and downstream from the suction ports; a pump discharge line fluidly coupled downstream from the pump, an outlet fluidly coupled downstream from the pump discharge line; an engine core flow path fluidly coupled with the suction ports; a core compartment supply line fluidly coupled upstream from a turbine cooling air port, the core compartment supply line comprising a core compartment inlet located within a core compartment and fluidly coupled the core compartment, the core compartment supply line comprising a core compartment supply valve located in the core compartment supply line upstream of the turbine cooling air port; a turbine cooling air supply line fluidly coupled to the core compartment supply line and the turbine cooling air port, the turbine cooling air supply line comprising a turbine cooling air valve upstream of the core compartment supply line; wherein the pump is structurally configured to remove air from the core compartment through the core compartment inlet and through the core compartment supply line and through the turbine cooling air port and through the engine core flow path and the pump is structurally configured to discharge the air from the core compartment through the outlet.

2 . The suction enabled post shutdown combustor cooling and ventilation system according to claim 1 , wherein the turbine cooling air valve is configured as closed responsive to an engine shutdown condition; and
the pump suction valve and the core compartment supply valve are configured as opened responsive to the engine shutdown condition.

3 . The suction enabled post shutdown combustor cooling and ventilation system according to claim 1 , further comprising:
a blower fluidly coupled with the core compartment supply line.

4 . The suction enabled post shutdown combustor cooling and ventilation system according to claim 1 , wherein the turbine cooling air valve is configured as opened responsive to an engine operating condition; and
the pump suction valve and the core compartment supply valve are configured as closed responsive to the engine operation condition.

5 . The suction enabled post shutdown combustor cooling and ventilation system according to claim 1 , wherein the outlet is fluidly coupled with a fan bypass duct and/or the outlet is fluidly coupled with an air dump section.

6 . The suction enabled post shutdown combustor cooling and ventilation system according to claim 1 , wherein the engine core flow path is in fluid communication between the compressor, the combustor and the turbine.

7 . A gas turbine engine having a suction enabled post shutdown combustor cooling and ventilation system comprising:
a gas turbine engine core flow path extending through a compressor, a combustor and a turbine, the turbine comprising turbine cooling air ports; a pump fluidly coupled downstream of a suction line, wherein the suction line is fluidly coupled downstream of suction ports proximate a fuel system component near the combustor; a pump suction valve positioned in the suction line upstream of the pump and downstream from the suction ports; a pump discharge line fluidly coupled downstream from the pump, an outlet fluidly coupled downstream from the pump discharge line; a core compartment supply line fluidly coupled upstream of the turbine cooling air ports, the core compartment supply line comprising a core compartment inlet located within a core compartment and fluidly coupled the core compartment, the core compartment fluidly coupled upstream of the core compartment inlet and the core compartment fluidly coupled upstream of the pump, the core compartment supply line comprising a core compartment supply valve located in the core compartment supply line upstream of the turbine cooling air ports; a turbine cooling air supply line fluidly coupled to the core compartment supply line and the turbine cooling air ports, the turbine cooling air supply line comprising a turbine cooling air valve; and the gas turbine engine core flow path fluidly coupled the suction ports and the turbine cooling air ports.

8 . The gas turbine engine having a suction enabled post shutdown combustor cooling and ventilation system according to claim 7 , wherein the turbine cooling air valve is configured as closed responsive to an engine shutdown condition; and
the pump suction valve and the core compartment supply valve are configured as opened responsive to the engine shutdown condition.

9 . The gas turbine engine having a suction enabled post shutdown combustor cooling and ventilation system according to claim 7 , wherein the turbine cooling air valve is configured as opened responsive to an engine operating condition; and the pump suction valve and the core compartment supply valve are configured as closed responsive to the engine operation condition.

10 . The gas turbine engine having a suction enabled post shutdown combustor cooling and ventilation system according to claim 7 , wherein the outlet is fluidly coupled with a fan bypass duct.

11 . The gas turbine engine having a suction enabled post shutdown combustor cooling and ventilation system according to claim 7 , wherein multiple sets of core compartment air supply lines are configured in an array about a centerline of the gas turbine engine; and
multiple sets of suction lines and at least one pump are plumbed in the gas turbine engine.

12 . The gas turbine engine having a suction enabled post shutdown combustor cooling and ventilation system according to claim 7 , further comprising:
a blower fluidly coupled with the core compartment supply line.

13 . A process for post shutdown combustor cooling and ventilation in a gas turbine engine having a suction enabled post shutdown system comprising:
a gas turbine engine core flow path extending through a compressor, a combustor and a turbine, the compressor comprising suction ports, the turbine comprising turbine cooling air ports; fluidly coupling a pump with a suction line; fluidly coupling the suction line suction ports proximate a fuel system component near the combustor; positioning a pump suction valve in the suction line upstream of the pump; fluidly coupling a pump discharge line with the pump, fluidly coupling an outlet with the pump discharge line; fluidly coupling a core compartment supply line with the turbine cooling air ports, the core compartment supply line comprising a core compartment inlet located within a core compartment; and fluidly coupling the core compartment inlet with the core compartment, the core compartment supply line comprising a core compartment supply valve located in the core compartment supply line upstream of the turbine cooling air ports; fluidly coupling a turbine cooling air supply line to the core compartment supply line and the turbine cooling air ports, the turbine cooling air supply line comprising a turbine cooling air valve; fluidly coupling the gas turbine engine core flow path with the suction ports and the turbine cooling air ports; and closing the turbine cooling air valve responsive to an engine shutdown condition; and opening the pump suction valve and the core compartment supply valve responsive to the engine shutdown condition.

14 . The process of claim 13 , further comprising:
opening the turbine

Assignees

• Rtx Corp

Inventors

• Yazici Murat
• Morton Jeffrey T
• Giannakopoulos Konstantinos P

Classifications

• F05D2260/90

  Braking · CPC title

• F05D2260/20

  Heat transfer, e.g. cooling · CPC title

• F02C9/18

  by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages {(F02C3/113 takes precedence)} · CPC title

• F01D25/12

  Cooling · CPC title

• F01D21/00

  Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for · CPC title