<p>A recuperated gas turbine engine fuel control valve and method which controls fuel flow during engine acceleration as a preselected empirical function of combustor gauge pressure and combustor inlet temperature, and which can also control fuel flow during deceleration without interruption of the combustion process.</p>
申请公布号
CA1168880(A)
申请公布日期
1984.06.12
申请号
CA19830425260
申请日期
1983.04.05
申请人
GARRETT CORPORATION (THE)
发明人
JANSEN, HARVEY B.;ADAMS, MILTON R.;SUMEGI, ROBERT B.;HUBER, KLAUS K. G.;SALISBURY, JOHN A., (DECEASED)
