发明名称 METHOD AND DEVICE FOR PROTECTING FUEL NOZZLES OF GAS TURBINE MACHINE
摘要 FIELD: power engineering. ^ SUBSTANCE: method comprises injecting compressed air into the system for supplying fuel to the nozzle. The compressed air is injected directly to the fuel injection head downstream of the valves. The injecting is controlled by the signal characteristic for a given stage of operation of the turbine machine. The compressed air is taken at the exit of the compressor, is collected in a tank, and then is injected to the head through the internal pipeline. ^ EFFECT: enhanced reliability. ^ 12 cl, 8 dwg
申请公布号 RU2296916(C2) 申请公布日期 2007.04.10
申请号 RU20050117880 申请日期 2005.06.09
申请人 SNEKMA MOTER 发明人 KERVISTEHN ROBER;DE DZHAKOMONI MARION;RODRIG ZHOZE ROLAN;ROLLEHN ZHILL' LUI
分类号 F23D11/38;F02C7/22;F02C7/232 主分类号 F23D11/38
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