发明名称 COMBUSTOR LINER ARRANGEMENT
摘要 <p>When second shell section (18) diverges with respect to first shell section (16), the second liner panel (50) is located with a changing spacing from the shell. The liner is close to the shell at the upstream edge (68), and farther from the liner at the downstream end (57). The downstream end of the first liner panel (64) overlaps the second liner panel (50) on the gas side.</p>
申请公布号 WO1996018849(A1) 申请公布日期 1996.06.20
申请号 US1995015077 申请日期 1995.11.17
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