发明名称 Ground running test facility for aircraft having jet engines
摘要 A ground running test facility for aircraft having jet engines is arranged in a sound-insulated hall (1). The engine exhaust gases are led away through a silencer (6). A device (4) for decelerating the flow of the exhaust gas jet is arranged upstream of the silencer (6). The jet inlet area (7) of this device (4) extends over the majority of the hall width. Resistance bodies (8) are arranged in a plurality of successive groups, which resistance bodies (8) are in the form of bars, extend transversely with respect to the flow direction and are offset with respect to one another in successive groups. The exhaust gas jet is decelerated by the resistance bodies (8) to a flow speed which is acceptable for the silencer (6), without any reverse flow occurring in this case. <IMAGE>
申请公布号 DE4326891(A1) 申请公布日期 1995.02.16
申请号 DE19934326891 申请日期 1993.08.11
申请人 DEUTSCHE LUFTHANSA AG, 50679 KOELN, DE 发明人 RIES, WALTER, PROF. DIPL.-ING., 30880 LAATZEN, DE;KRAUS, SIEGMUND, DIPL.-ING., 64331 WEITERSTADT, DE
分类号 B64F1/26;E04H6/44;(IPC1-7):B64F5/00;G01M15/00 主分类号 B64F1/26
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