Back to results
US 12,584,444 B2Granted
Suction enabled post shutdown combustor cooling and core ventilation
AssigneeRtx Corporation
InventorsMurat Yazici, Jeffrey T. Morton, Konstantinos P. Giannakopoulos
Life of this patent
Estimating the term…
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.
Claims18
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.
5 more elements
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.
6 more elements
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.
10 more elements
Dependencies are inferred from the claim text.