Abstract: A system for cooling at least one gas turbine liquid fuel component located in a high temperature environment to eliminate coking in the component is disclosed. The system includes a sleeve surrounding the liquid fuel component, a device for providing a current of cool air, and a conduit connected between the cool air device and the sleeve to direct the current of cool air into the sleeve to cool the liquid fuel component. The system can also include a manifold connected to the conduit and a plurality of second conduits for connecting the manifold to a plurality of sleeves surrounding a plurality of liquid fuel components, each sleeve being connected to a corresponding second conduit. Each sleeve includes a plurality of spacing devices for centering the sleeve around the at least one liquid fuel component so as to form an annulus between the sleeve and the liquid fuel component through which the current of cool air flows.

Abstract: A system for cooling at least one gas turbine liquid fuel component located in a high temperature environment to eliminate coking in the component is disclosed. The system includes a sleeve surrounding the liquid fuel component, a device for providing a current of cool air, and a conduit connected between the cool air device and the sleeve to direct the current of cool air into the sleeve to cool the liquid fuel component. The system can also include a manifold connected to the conduit and a plurality of second conduits for connecting the manifold to a plurality of sleeves surrounding a plurality of liquid fuel components, each sleeve being connected to a corresponding second conduit. Each sleeve includes a plurality of spacing devices for centering the sleeve around the at least one liquid fuel component so as to form an annulus between the sleeve and the liquid fuel component through which the current of cool air flows.

Abstract: A system for cooling at least one gas turbine liquid fuel component located in a high temperature environment to eliminate coking in the component is disclosed. The system includes a sleeve surrounding the liquid fuel component, a device for providing a current of cool air, and a conduit connected between the cool air device and the sleeve to direct the current of cool air into the sleeve to cool the liquid fuel component. The system can also include a manifold connected to the conduit and a plurality of second conduits for connecting the manifold to a plurality of sleeves surrounding a plurality of liquid fuel components, each sleeve being connected to a corresponding second conduit. Each sleeve includes a plurality of spacing devices for centering the sleeve around the at least one liquid fuel component so as to form an annulus between the sleeve and the liquid fuel component through which the current of cool air flows.

Abstract: The invention is embodied in a closed-cycle lubrication oil system used during turbine start-up to provide both lift oil and hydraulic oil from one system using a single variable volume pump that supplies fluid at a high pressure for lift oil requirements. The pump discharge pressure is reduced, through a pressure regulating/reducing valve, down to hydraulic system demands. During steady-state gas turbine operation, the system provides only a flow of hydraulic oil to position the inlet guide vanes and gas valves as required by the gas turbine controls logic. During gas turbine shut-down, the system again meets both lift oil and hydraulic oil requirements. A second pump is advantageously incorporated in the preferred embodiments of the system to provide 100% redundancy in providing either lift or hydraulic oil.

Abstract: The invention is embodied in a closed-cycle lubrication oil system used during turbine start-up to provide both lift oil and hydraulic oil from one system using a single variable volume pump that supplies fluid at a high pressure for lift oil requirements. The pump discharge pressure is reduced, through a pressure regulating/reducing valve, down to hydraulic system demands. During steady-state gas turbine operation, the system provides only a flow of hydraulic oil to position the inlet guide vanes and gas valves as required by the gas turbine controls logic. During gas turbine shut-down, the system again meets both lift oil and hydraulic oil requirements. A second pump is advantageously incorporated in the preferred embodiments of the system to provide 100% redundancy in providing either lift or hydraulic oil.

Abstract: The invention is embodied in a closed-cycle lubrication oil system used during turbine start-up to provide both lift oil and hydraulic oil from one system using a single variable volume pump that supplies fluid at a high pressure for lift oil requirements. The pump discharge pressure is reduced, through a pressure regulating/reducing valve, down to hydraulic system demands. During steady-state gas turbine operation, the system provides only a flow of hydraulic oil to position the inlet guide vanes and gas valves as required by the gas turbine controls logic. During gas turbine shut-down, the system again meets both lift oil and hydraulic oil requirements. A second pump is advantageously incorporated in the preferred embodiments of the system to provide 100% redundancy in providing either lift or hydraulic oil.