COMPOSITION TYPE PRESSURE SPRAYING NOZZLE FOR GAS TURBINE BURNER

    公开(公告)号:JPH11159757A

    公开(公告)日:1999-06-15

    申请号:JP26027598

    申请日:1998-09-14

    Abstract: PROBLEM TO BE SOLVED: To provide a composition type pressure spraying nozzle for a gas turbine to improve suitability of spray characteristics of liquid to each load condition and realize excellent premixture throughout a total load range. SOLUTION: This composition type pressure spraying nozzle comprises a nozzle body 1 having at least two different feed passages 7 and 12 for at least one kind of liquid to be sprayed. Besides, a first feed passage 7 is partially surrounded with a second feed passage 12 and communicates in a spot situated downstream with an outer chamber 5 through one injection orifice 11 and a second feed passage 12 is also connected to an outer chamber 5. In a composition type pressure spraying nozzle for a so formed type gas turbine burner, the second feed passage 12 is provided with at least two injection orifices 13 communicating with the outer chamber 5.

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