{TAIL ~ The method} 8 wherein the cooling air is supplied to a first annular cavity formed by said annular seal structure and then to a second annular cavity within {HEAD ~ said aft end} of said combustor liner 
{ TAIL ~ The method } 8 wherein the cooling air is supplied to a first annular cavity formed by said annular seal structure and then to a second annular cavity within { HEAD ~ said aft end } of said combustor liner
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