DocumentCode
3514487
Title
Research on operation cost of helicopter components based on flight condition
Author
Jia, Zhonghu ; Liu, Wenlin ; Hou, Zhiqiang ; Lv, Weimin
Author_Institution
Dept. of Airborne Vehicle Eng., Naval Aeronaut. & Astronaut. Univ., Yantai, China
fYear
2009
fDate
20-24 July 2009
Firstpage
274
Lastpage
277
Abstract
Operation and support cost occupy large proportion of life-cycle cost. The operation cost prediction is difficult due to the complex helicopter flight conditions. Based on the fatigue damage by flight conditions, an analytical model is presented for the calculation of influence of flight time proportion changes on the operation cost of helicopter components by introduced influence factor. Two influence factors for the cases where only one flight condition is modified at a time and all flight conditions except one are modified can provide qualitative ordering and quantitative assessment of flight condition changes on operation cost. Some results are obtained by the analysis to helicopter main rotors based on flight spectrum. For the helicopter main rotors only two of the forty-eight flight conditions would have any significant effect that a 0.1 time fraction change leads to operation cost change more than 0.01. The results indicate this method can be used practically in operation cost prediction of helicopter components.
Keywords
aerospace components; fatigue; helicopters; life cycle costing; maintenance engineering; rotors; fatigue damage; flight spectrum; helicopter components; helicopter flight condition; life-cycle costing; operation cost prediction; rotors; Aerodynamics; Aerospace engineering; Analytical models; Automotive engineering; Costs; Failure analysis; Fatigue; Helicopters; Large-scale systems; Vehicle dynamics; fatigue damage; flight condition; influence analysis; operation cost;
fLanguage
English
Publisher
ieee
Conference_Titel
Reliability, Maintainability and Safety, 2009. ICRMS 2009. 8th International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4244-4903-3
Electronic_ISBN
978-1-4244-4905-7
Type
conf
DOI
10.1109/ICRMS.2009.5270193
Filename
5270193
Link To Document