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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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