Design and Application of Database System for Dynamic Balancing Test of Helicopter Main Rotor Blade

被引:1
|
作者
Yoon, Byung-Il [1 ]
Paek, Seung-Kil [1 ]
Song, Keun-Woong [1 ]
Kim, Deog-Kwan [1 ]
机构
[1] Korea Aerosp Res Inst, Daejeon, South Korea
关键词
Helicopter; Dynamic Balancing(RTB); Relational Database(RDB); Main Rotor Blade; Whirl Tower; TRACK;
D O I
10.5139/JKSAS.2019.47.8.582
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The dynamic balancing test of helicopter main rotor blades is a blade rotation test conducted on the ground to make the track of each blade and the load on each pitch rod to a similar level before the flight tests. The purpose of the test is to reduce the vibration occurring on main rotor system as a result of dissimilarity of each blade. The RTB test has been performed for a long period at Whirl Tower Test Facility located in Goheung Flight Centre, accumulating its data. As the amount of the results has become increasingly enormous the needs for the development of database system has been raised to manage the data with effective method. This research aimed to describe the development of Dynamic-Balancing Database System for the RTB test results. For the design of the database system the informations of RTB test results have been categorized into properties, connecting each others according to its logical meaning, and comprised into a database system with relational elements. It has been shown in this paper that the Dynamic Balancing database system enables to effectively accumulate the RTB test data and to be utilized for the data analysis.
引用
收藏
页码:582 / 589
页数:8
相关论文
共 50 条
  • [1] Failure of a helicopter main rotor blade
    Amura, Mikael
    Aiello, Lorenzo
    Colavita, Mario
    De Paolis, Fabrizio
    Bernabei, Manuele
    20TH EUROPEAN CONFERENCE ON FRACTURE, 2014, 3 : 726 - 731
  • [2] APPLICATION OF OPTIMIZATION METHODS TO HELICOPTER ROTOR BLADE DESIGN
    CHATTOPADHYAY, A
    WALSH, JL
    STRUCTURAL OPTIMIZATION, 1990, 2 (01): : 11 - 22
  • [3] Stability analysis on dynamic balance test for helicopter rotor blade
    Liang, Ting-Wei
    Wang, Qi
    Dong, Liang
    Xue, Wei-Song
    Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2009, 41 (01): : 24 - 30
  • [4] The Dynamic Characteristics Design of Rotor Blade about Unmanned Helicopter
    Jiang, Nianzhao
    Xie, Qinwei
    Dai, Yong
    Zhang, Zhiqing
    Wang, Kexuan
    Song, Jun
    Yin, Han
    PROCEEDINGS OF FIRST INTERNATIONAL CONFERENCE OF MODELLING AND SIMULATION, VOL I: MODELLING AND SIMULATION IN SCIENCE AND TECHNOLOGY, 2008, : 35 - 40
  • [5] Helicopter Main Rotor Conceptual Design - Application to a Westland Lynx Helicopter
    Novak, Doris
    Bucak, Tino
    Domitrovic, Anita
    STROJARSTVO, 2008, 50 (03): : 169 - 173
  • [6] Helicopter main rotor conceptual design - Application to a Westland Lynx helicopter
    University of Zagreb, Faculty of Traffc and Transportation Sciences, Department of Aeonautics, Vukeličeva 4, HR - 10000 Zagreb, Croatia
    Strojarstvo, 2008, 3 (169-173):
  • [7] Static and Dynamic Balancing of Helicopter Tail Rotor Blade Using Two- Plane Balancing Method
    bin Ammoo, Mohd Shariff
    Awal, Ziad Bin Abdul
    Sangiti, Norhidayah binti Mat
    JURNAL TEKNOLOGI, 2014, 71 (02):
  • [8] Recent Experiences of Helicopter Main Rotor Blade Damage
    Weber, Simone
    Lone, Mudassir
    Cooke, Alastair
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2019, 64 (03)
  • [9] Effect of surface roughness on helicopter main rotor blade
    Rohizan, W. N. W.
    Rafie, A. S. M.
    Harmin, M. Y.
    Ciang, C. C.
    AEROTECH VI - INNOVATION IN AEROSPACE ENGINEERING AND TECHNOLOGY, 2016, 152
  • [10] On the dynamic response of a hingeless helicopter rotor blade
    Sarker, Pratik
    Chakravarty, Uttam K.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 115