发明名称 GENERATEUR DE GAZ POUR TURBINES A GAZ
摘要 <p>The gas generator for a gas turbine engine has a combustion chamber (3) inside the inner wall (8) of a double walled outer cylinder (2). Gas is fed into the combustion chamber by a tube (7) at one end, and is discharged from its open end (4) towards the blades of the turbine (10). Fresh air enters the outer tube through a connection (1) behind the gas supply tube. This air flows forwards around the inner wall to pass through holes (9) at the gas discharge end, then flow in the reverse direction to pass through holes through the combustion chamber to mix with the burning gases with a swirling action. Part of the air also cools the combustion chamber while circulating over its outside.</p>
申请公布号 FR2510238(A1) 申请公布日期 1983.01.28
申请号 FR19820012951 申请日期 1982.07.23
申请人 HEUNG DUK DAN 发明人
分类号 F23R3/54;(IPC1-7):23R3/54 主分类号 F23R3/54
代理机构 代理人
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