Remote control structural exciters for structural data acquisition system calibrations

被引:0
作者
Banaszak, D [1 ]
机构
[1] USAF, Res Lab, Air Vehicles Directorate, Wright Patterson AFB, OH 45433 USA
来源
PROCEEDINGS OF THE IEEE 2000 NATIONAL AEROSPACE AND ELECTRONICS CONFERENCE: ENGINEERING TOMORROW | 2000年
关键词
calibration; vibration; structures; exciters; statistics; experimental design; remote control;
D O I
10.1109/NAECON.2000.894897
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The Air Force invented a new calibration technique, which allows one person to perform multiple end-to-end mechanical calibrations of structural dynamics measurement systems. An end-to-end calibration means a full calibration of instrumentation from the physical input to the transducer to the output where the analog or digital signal is normally analyzed. It is difficult to stimulate mounted and embedded transducers with known physical inputs. Normally two people calibrate-one at the transducer holds or attaches the exciter and one operates the recorder. This new technique uses remote control structural exciters to stimulate measurement transducers contained in structures, with a measurable input level, and the output signal is communicated to a data recorder. The Air Force demonstrated this patented technique by using accelerometers in the laboratory. A commercial off-the-shelf vibration paging system sends a signal from a master control unit to individual exciters that stimulate accelerometers mounted on structures. A reference accelerometer measures the input. Engineers validated the technique using eight different exciters in a completely randomized block design experiment consisting of three 2-level factors: material, structural thickness and excitation mode. The engineers measured amplitude, frequency and transfer function between the accelerometers. This paper describes the invention and looks at potential field applications to insure data integrity in structural data acquisition systems on aging commercial and military vehicles.
引用
收藏
页码:95 / 104
页数:10
相关论文
共 8 条
[1]  
[Anonymous], JMP INTR GUID VERS 3
[2]  
Banaszak D, 1998, INSTITUTE OF ENVIRONMENTAL SCIENCES AND TECHNOLOGY - 1998 PROCEEDINGS, P172
[3]  
BANASZAK D, 1998, Patent No. 5804697
[4]  
BANASZAK D, 1996, SOUND VIBRATION
[5]  
DEAN A, 1999, DESIGN ANAL EXPT, P295
[6]  
HIMELBLAU H, 1990, HDB DYNAMIC DATA ACQ, P148
[7]  
MONTGOMERY DC, 1991, DESIGN ANAL EXPT, P128
[8]  
NUETER J, 1990, APPL LINEAR STAT MOD, P1032