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COMBUSTION CHAMBER OF GAS TURBINE ENGINE WITH FRONT CAP FOR DIVISION OF GAS FLOW, ANNULAR WALL FORMING PEAK OF FRONT CAP OF CHAMBER, GAS TURBINE ENGINE CONTAINING ABOVE CHAMBER
COMBUSTION CHAMBER OF GAS TURBINE ENGINE WITH FRONT CAP FOR DIVISION OF GAS FLOW, ANNULAR WALL FORMING PEAK OF FRONT CAP OF CHAMBER, GAS TURBINE ENGINE CONTAINING ABOVE CHAMBER
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机译:带前盖的燃气轮机发动机燃烧室,用于划分气流,腔室前盖的环形壁形成峰,上方装有燃气轮机发动机
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摘要
FIELD: heating systems.;SUBSTANCE: annular combustion chamber of gas turbine engine with external annular wall and internal annular wall includes front cap dividing gas flow at chamber inlet into operating flow and flow of chamber inlet. Cap includes annular wall forming a peak which includes rear attachment section to wall of chamber and front section forming an edge of section of channel for passing the operating flow. Front section is continued at least with one additional rear attachment section to chamber wall.;EFFECT: development of cap which is strong enough in relation to vibration impacts.;11 cl, 7 dwg
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