BIDIMENSIONAL AND ASYMMETRICAL SUPERSONIC AIR INTAKE FOR THE COMBUSTION AIR OF AN AIRCRAFT ENGINE
摘要
<p>The bidimensional supersonic air intake for the combustion air of an aircraft engine comprises on the one hand a front flap (3) forming a visor and on the other hand a hull (4). The front flap (3) is movable about a pivot axis (5) situated opposite the hull (4). The front flap (3) is integral with a movable hull mouth (6) situated at the front of the hull (4) and moving in front of the latter when the front flap (3) moves in the direction which increases the cross-section of the air intake. …<IMAGE>… </p>
申请公布号
EP0354103(B1)
申请公布日期
1992.01.08
申请号
EP19890402144
申请日期
1989.07.28
申请人
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES (ONERA)
发明人
FALEMPIN, FRANCOIS;SANS, CLAUDE;CHAMPIGNY, PATRICK;LARUELLE, GERARD;GARREL, JEAN-MARIE