DocumentCode
1890901
Title
The Calibration Technical Investigation on Helicopter Rotor Standard Blade
Author
Liang Yun ; Liang Tingwei ; Jiao Jian
Author_Institution
Hong Kong Polytech. Univ., Kowloon, China
fYear
2013
fDate
16-17 Jan. 2013
Firstpage
1153
Lastpage
1156
Abstract
The rotor system is the most important part for helicopter, the helicopter flight quality depends tightly on the rotor blade. The parameters of primary standard rotor bland had been identified by analyzing its parameters systematically basing on dynamic balance test. A new method is proposed to calibrate the parameters of primary standard rotor blade with designing series of calibration equipments. Some of verification test and simulation results indicate that the method is valid, the uncertainty of measurement accord with the technical requirements. It can solve the calibration problem of standard rotor blade, finish the metrological transfer process, and maintain the consistency and stability of helicopter rotor blades.
Keywords
blades; calibration; dynamic testing; helicopters; rotors; stability; calibration equipment; calibration technical investigation; dynamic balance test; helicopter flight quality; helicopter rotor blade stability; helicopter rotor standard blade; metrological transfer process; rotor bland; verification testing; Aerodynamics; Blades; Calibration; Helicopters; Position measurement; Rotors; Standards; Dynamic Balance Test; Flapping Measurement and Calibration; Rotor Flapping;
fLanguage
English
Publisher
ieee
Conference_Titel
Measuring Technology and Mechatronics Automation (ICMTMA), 2013 Fifth International Conference on
Conference_Location
Hong Kong
Print_ISBN
978-1-4673-5652-7
Type
conf
DOI
10.1109/ICMTMA.2013.282
Filename
6493935
Link To Document