发明名称 AEROMECHANICAL INJECTION SYSTEM WITH PRIMARY ANTIRETURN SWIRLER
摘要 PROBLEM TO BE SOLVED: To provide an injection system for a turbomachine combustion chamber where a defect seen in conventional arts is relieved. SOLUTION: The injection system is provided with a fuel injection nozzle for vaporizing fuel in the combustion chamber, and a mixer/deflector assembly. The assembly is provided with a primary swirler (40) and a secondary swirler (42), the swirlers are coaxially at a determined distance from each other, and the turbomachine combustion chamber is separated by a Venturi device (44) disposed coaxially with an injection nozzle. The primary swirler is firmly mounted on the injection nozzle and situated separately from the injection nozzle by a constant radial distance. The radial distance is determined such that fuel vaporized by the injection nozzle can under no circumstances collide with the primary swirler.
申请公布号 JP2003042452(A) 申请公布日期 2003.02.13
申请号 JP20020203572 申请日期 2002.07.12
申请人 SNECMA MOTEURS 发明人 BAUDOIN CHRISTOPHE;COMMARET PATRICE-ANDRE;VIGUIER CHRISTOPHE
分类号 F23R3/14;F23R3/28;(IPC1-7):F23R3/14 主分类号 F23R3/14
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