Suppression of random vibration response of optical satellite by matching honeycomb stiffened plates’ structural parameters

2016 ◽  
Vol 24 (2) ◽  
pp. 372-380
Author(s):  
谭陆洋 TAN Lu-yang ◽  
王 栋 WANG Dong ◽  
孔 林 KONG Lin ◽  
闫 勇 YAN Yong ◽  
李 林 LI Lin
1971 ◽  
pp. 87-95
Author(s):  
John D. Robson ◽  
Colin J. Dodds ◽  
Donald B. Macvean ◽  
Vincent R. Paling

1987 ◽  
Vol 30 (5) ◽  
pp. 42-49
Author(s):  
Allen Curtis ◽  
Richard McKain

This paper presents a rational method by which an effective random vibration screen may be developed efficiently and quantitatively. In summary, a Flaw Precipitation Threshold (FPT) was derived from measurements of vibration response at known flaw locations. Responses were measured on a variety of modern electronic and electro-mechanical equipment, manufactured by five different manufacturers, during ongoing vibration screens. A vibration screen can be tailored for a piece of equipment by performing a global vibration response survey and adjusting the input spectra so that the response falls within the FPT.


2012 ◽  
Vol 226-228 ◽  
pp. 124-128
Author(s):  
Ai Lun Wang ◽  
Hui Long ◽  
Qiang Huang ◽  
Qian Jin Wang

The group number and group coupling stiffness are important structural parameters of the grouped blade-disk. This work examines how the group number and group coupling stiffness affect the vibration response localization of tuned grouped blade-disk. The lumped parameter model of the grouped blade-disk was established, and the vibration equation was derived. The vibration response localization factors of tuned grouped blade-disks were obtained at the different group number and group coupling stiffness, and the effects of group number and group coupling stiffness on vibration response localization was analyzed. The results show that the vibration localization appears in the tuned grouped blade-disk and the degree of vibration response localization reduces with the increasing of group number and group coupling stiffness. The results can help to completely reveal the localization mechanism of the grouped blade-disk


2001 ◽  
Vol 29 (2) ◽  
pp. 66-78 ◽  
Author(s):  
H. J. Yu ◽  
H. Aboutorabi

Abstract A combined tire, wheel, and suspension FE model is described. The system simulates the tire mounted on the vehicle. The natural frequencies are calculated successfully for this highly non-linear system where the tire is in the inflated and loaded condition. The random vibration response of the model to the road roughness is calculated.


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