Method and apparatus for high altitude starting of gas turbine e

Power plants – Combustion products used as motive fluid

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60 39142, 60737, F23R 332

Patent

active

052149110

ABSTRACT:
Difficulties in starting a gas turbine engine at high altitudes may be avoided by the method of starting such an engine which includes the steps of introducing fuel into the combustor (26) of the engine through at least one fuel injector (46) having an outlet (76, 78) within the combustor (26), atomizing the fuel with a burst of oxidant at elevated pressure from a source (92) of pressurized stored oxidant until ignition is obtained, and thereafter discontinuing the burst of oxidant from the source (92).

REFERENCES:
patent: 2608054 (1952-08-01), Price
patent: 2643511 (1953-06-01), Briggs
patent: 2749023 (1956-06-01), Lewis
patent: 2992531 (1961-07-01), Hershey
patent: 3098626 (1963-07-01), Messinger
patent: 4033115 (1977-07-01), Baits
patent: 4375745 (1983-03-01), Schelp
patent: 4445532 (1984-05-01), Mitchell
Lefebvre, Arthur H. Gas Turbine Combustion, Hemisphere Publ. Corp., New York, 1983, pp. 412 and 413.

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