公开(公告)号：EP3092397A1

公开(公告)日：2016-11-16

申请号：EP14885222.1

申请日：2014-12-19

申请人： United Technologies Corporation

发明人： HILL, James, D. ,  CUOZZO, Michael, J.

IPC分类号： F02K7/067

CPC分类号： F02C5/02 ,  F02C5/10 ,  F23R7/00

摘要： An inlet manifold for a multi-tube pulse detonation engine includes a vaneless diffuser disposed in a first zone to collect an air discharged from a compressor; a vaned diffuser including a plurality of guide vanes disposed in a second zone to slow the air from the compressor; a plenum disposed in a third zone located next to second zone to provide the air from the compressor to chambers; and a splitter disposed in a fourth zone to split the air from the compressor into an airflow required by each pulse detonation tube for detonation.