Design and Validation of Sensor Balance for Propeller Experiment

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Abstract:

This paper proposes a new two-component sensor balance to measure the thrust and torque of the propeller. Its principles of measuring force were derived and the procedures of balance measuring system were also provided according to the virtual instruments. The sensor balance was calibrated through the ground static calibration bench to verify its accuracy. And a ground static thrust experiment on a one-meter sized propeller model was carried out. By comparison, the experimental results of adopting the designed sensor balance basically tally with those of wind tunnel experiment, which proves that this sensor balance can be used in propeller experiments.

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652-656

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January 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] Liu, P. Q., Ma, R., Duan, Z. Z., & Ma, L. C. (2011). Ground wind tunnel test study of the propeller of stratospheric airships. Journal of Aerospace Power, 26(8), 1775–1781.

Google Scholar

[2] Nie, Y., Wang, S., & Yang. Y. C. (2009). Comparative Analysis of Propeller Static Thrust Simulation and Experiment. Computer Simulation, 26(3), 103-107.

Google Scholar

[3] Wang, L. G., Song, B. F., Shao, L. M., & Yuan, C. S. (2008). Flapping-wing Testing System Based on Virtual Instrument. Science Technology and Engineering, 8(5), 1224–1228.

Google Scholar

[4] Morris, M., Callicoat, J., Arena A., Gaeta, R., & Jacob, J. (2013). Engine and Propeller Testing for Small to Mid-Size UAVs, AIAA-13-1134.

Google Scholar

[5] Liu, P. Q. (2006). Theory and Application of Air Propellers, Beijing: Beihang University Publication, (2006).

Google Scholar