<p>A gas turbine engine internal fuel manifold (22) has a plurality of airblast fuel nozzles (26) in communication with an air source such that nozzle core air does not pass through the manifold (22).</p>
申请公布号
EP1710500(A1)
申请公布日期
2006.10.11
申请号
EP20060251630
申请日期
2006.03.27
申请人
PRATT & WHITNEY CANADA, INC.
发明人
PROCIW, LEV ALEXANDER;SHAFIQUE, HARRIS;KOJOVIC, ALEKSANDAR
