发明名称 TEST DEVICE FOR THE FAN OF AN AIRCRAFT ENGINE
摘要 <p>The device has outer housing modules (18-24) detachably and sealably connected with each other. The housing modules are supported on a floor side and adjustable in X, Y and Z directions. Bypass flow and core flow guide vanes (41, 42) and inner and outer pipe elements (43,44) are exchangeably arranged in interior of an outer housing for transferring air flow produced by a fan (17) to a bypass flow channel (45) and a core flow channel (46). Measuring devices (38, 39) and a microphone (40) are connected to a modularly formed telemetry unit and exchangeably arranged in the bypass channel.</p>
申请公布号 EP2326822(B1) 申请公布日期 2015.09.09
申请号 EP20090780515 申请日期 2009.07.13
申请人 ANECOM AEROTEST GMBH 发明人 SAND, STEFAN;AHLERS, EDMUND;HEYDORN, CARSTEN;DAUM, CARSTEN;STEINBORN, ANDRÉ;HOBSON, IAN;RIEPE, AXEL
分类号 F02K3/04;F01D25/00 主分类号 F02K3/04
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