Power plants – Combustion products used as motive fluid – Using special fuel or oxidizer
Patent
1994-10-13
1996-10-08
Casaregola, Louis J.
Power plants
Combustion products used as motive fluid
Using special fuel or oxidizer
60734, F02C 7232
Patent
active
055619762
ABSTRACT:
A trip oil system automatically controls the fuel shut-off valves in an industrial gas turbine. The trip oil system applies hydraulic pressure to actuate and hold open a fuel shut-off valve so that fuel flows to the combustor of the gas turbine. When the trip oil system relieves the hydraulic pressure, the fuel shut-off valve closes and stops the fuel flow to the combustor. A bank of three solenoid valves controls the application of hydraulic pressure to each fuel shut-off valve. Hydraulic fluid conduits interconnect the three solenoid valves such that no single valve by itself can relieve the hydraulic pressure applied to the fuel shut-off valve. During normal operation of the gas turbine, all three redundant solenoid valves are activated. For the trip oil system to cause the fuel shut-off valve to close, at least two of the solenoid valves must de-energize to relieve pressure to the fuel shut-off valve.
REFERENCES:
patent: 2559814 (1951-07-01), Whittle
patent: 3168810 (1965-02-01), Gatzemeyer et al.
patent: 3805519 (1974-04-01), Plotnick et al.
patent: 4229937 (1980-10-01), Smith
patent: 4446377 (1984-05-01), Kure-Jensen et al.
patent: 4708594 (1987-11-01), Shinmei et al.
patent: 4808896 (1989-02-01), Katsuragi et al.
Annin Scott V.
Chu Henry G.
Hubschmitt George
Ray Brian P.
Casaregola Louis J.
General Electric Company
LandOfFree
Redundant trip solenoid valve shut-off for gas turbine fuel syst does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Redundant trip solenoid valve shut-off for gas turbine fuel syst, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Redundant trip solenoid valve shut-off for gas turbine fuel syst will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-50237