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Scanning Laser Doppler Vibrometer Measurements Inside Helicopter Cabins in Running Conditions: Problems and Mock-up Testing

机译:在运行条件下扫描直升机舱内的激光多普勒振动计测量:问题和模拟测试

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The present work deals with the analysis of problems and potentials of laser vibrometer measurements inside helicopter cabins in running conditions. The paper describes the results of a systematic measurement campaign performed on an Agusta A109MKII mock-up. The aim is to evaluate the applicability of Scanning Laser Doppler Vibrometer (SLDV) for tests in simulated flying conditions and to understand how performances of the technique are affected when the laser head is placed inside the cabin, thus being subjected to interfering inputs. Firstly a brief description of the performed test cases and the used measuring set-ups are given. Comparative tests between SLDV and accelerometers are presented, analyzing the achievable performances for the specific application. Results obtained measuring with SLDV placed inside the helicopter cabin during operative excitation conditions are compared with those performed with the laser lying outside the mock-up, these last being considered as "reference measurements". Finally, in order to give an estimate of the uncertainty level on measured signals, a study linking the admitted percentage of noise content on vibrometer signals due to laser head vibration levels will be introduced.The research has been carried out within the Framework of the EU project CREDO (Cabin Noise Reduction by Experimental and Numerical Design Optimisation), funded by the European Commission in the 6~(th) Framework Programme (Thematic Priority: AERONAUTICS AND SPACE, AST5-CT-2006-030814).
机译:目前的工作涉及的运行条件下问题和直升机车厢内激光测振仪测量的潜力分析。本文介绍上阿古A109MKII实体模型进行了系统的测量活动的结果。的目的是评估扫描激光多普勒振动计(SLDV)的用于测试在模拟飞行条件的适用性,并了解如何当激光头被放置在机舱内,因此受到的干扰输入的技术的性能会受到影响。首先的执行测试用例的简要描述和使用的测量的调校中给出。 SLDV和加速度计之间的对比试验被呈现,分析针对特定应用的可实现的性能。获得具有SLDV测量结果期间可操作激发条件与那些与激光躺在实体模型,这些最后被认为是“基准测量”外部执行相比放置在直升机机舱内。最后,为了给不确定性水平的估计,对测量信号,对测振仪信号中的噪声内容的比例录取连接由于激光头的一项研究振动水平将被娘家人的研究已经在欧盟的框架内进行项目CREDO(机舱降噪通过实验和数值优化设计),由欧盟委员会在6〜(TH)资助的框架计划(优先主题:航空航天,AST5-CT-2006-030814)。

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