
Sensitivity Analysis of Design Parameters on Fluidlastic 
Isolators Performance 
J H Deng and Q Y Cheng
*
 
Science and Technology  on Rotorcraft Aeromechanics Laboratory, China Helicopter 
Research and Development Institute, Jingdezhen  333001,  China 
 
Corresponding  author and e-mail:  Q Y Cheng, qy_cheng@163.com 
Abstract. Control of vibration in helicopters has always been a complex and challenging task. 
The fluidlastic isolators become more and more widely used because the fluids are non-toxic, 
non-corrosive, nonflammable, and compatible with  most elastomers and adhesives. In the 
field of the fluidlastic isolators design, the selection of design parameters is very important to 
obtain efficient vibration-suppressed. Aiming at getting sensitivity of property of fluidlastic 
isolator to design parameters, a dynamic equation is set up based on the theory of dynamics. 
The  orthogonal  experimental  method  is  used  to  analyze  the  parametric  sensitivity  of  the 
design parameters on the property of fluidlastic isolator. Two control indexes for design are 
taken as the experimental indexes, and five parameters influencing the property of the isolator 
are  taken  as  the  experimental  factors.  Arranged  for  the  tests  based  on  the  orthogonal 
experiment table, 2 indexes 6 factors orthogonal experiment is carried out. Range analysis is 
adopted  to  study  the  sensitivity.  The  results  show  that  for  the  combustion  efficiency  of 
dynamic stiffness of fluidlastic isolator, the order of significance levels in turn decreases with 
η,  K
1
,  c  ,  L,  ρ  and  K
2
 respectively. For the combustion efficiency of dynamic stiffness of 
fluidlastic isolator, the order of significance levels in turn decreases with η, K
1
, c, K
2,
 ρ and L 
respectively. 
1.  Introduction 
Helicopter vibration is a critical aspect of helicopter design and a major reason for extended lead time 
during the aircraft development phase. Control of vibration in helicopters has always been a complex 
and challenging task. Increasing demands for expanding the flight envelop of helicopters, such as nap 
of earth flying, high speed, high maneuvers, coupled with the need to improve system reliability and 
reduce maintenance costs has resulted in more stringent vibration  specifications. 
Various  methods  have  been  applied  to  vibration  control  in  the  engineering  field  [1-5]. 
Traditionally,  passive  isolators  and  dampers  are  used  to  attenuate  mechanical  vibrations.  The 
traditional approach  to  passive vibration isolation is to  install relatively soft springs or elastomeric 
isolators to provide a primary low natural  frequency [6-9]. These isolators would also  incorporate 
sufficient damping to control resonant response. Soft systems with primary natural frequencies well 
below the N/rev exciting  frequency  are required to achieve isolation. Such systems result in large 
relative  motion  between  the  pylon  and  the  airframe  due  to  static  loads.  Natural  frequencies  low 
enough to isolate N/rev vibration would have static (1G) deflections up to 0.50 inches. Since flight 
64
Deng, J. and Cheng, Q.
Sensitivity Analysis of Design Parameters on Fluidlastic Isolators Performance.
In Proceedings of the International Workshop on Materials, Chemistry and Engineering (IWMCE 2018), pages 64-70
ISBN: 978-989-758-346-9
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