发明名称 Test device for the fan of an aircraft engine
摘要 The fundamental idea of the invention consists of the construction of the test device from a stationary inner basic structure (1, 7 to 11) that juts out from the wall of the test bench and houses the drive shaft (13) for the fan to be tested, from mobile, interchangeable external housing modules (18 to 24) which can be aligned in relation to one another by means of connected optical elements (32, 33), from interchangeable fittings (41 to 44, 48) for conducting air and noise reduction, in addition to interchangeable measuring devices (38 to 40) that are connected to a modular telemetry unit for determining performance data and aerodynamic and acoustic conditions required by the fan and the fittings. A test device that is designed on this basis permits a plurality of data that is influenced by the design of the fan and the fittings, which lie in the flow duct behind the fan, to be recorded using relatively simple structural resources and conclusions can be drawn from said data with regard to the reduction of noise, an optimal aerodynamic design and improved performance.
申请公布号 US8327698(B2) 申请公布日期 2012.12.11
申请号 US200913062837 申请日期 2009.07.13
申请人 SAND STEFAN;AHLERS EDMUND;HEYDORN CARSTEN;DAUM CARSTEN;STEINBORN ANDRE;HOBSON IAN;RIEPE AXEL;ANECOM AERO TEST GMBH 发明人 SAND STEFAN;AHLERS EDMUND;HEYDORN CARSTEN;DAUM CARSTEN;STEINBORN ANDRE;HOBSON IAN;RIEPE AXEL
分类号 G01M15/14 主分类号 G01M15/14
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