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