Rapid Calibration of Nanoliter per Second Flow Rate by Image Processing Technology

Author:

Luo Jiawei12,Yang Cheng12ORCID,Shen Yan12

Affiliation:

1. School of Aeronautics and Astronautics, Sun Yat-sen University (Shenzhen Campus), Shenzhen 518107, China

2. Shenzhen Key Laboratory of Intelligent Microsatellite Constellation, Shenzhen 518107, China

Abstract

The need for high-precision microflow control is increasingly evident across various fields. For instance, microsatellites employed in gravitational wave detection require flow supply systems with a high accuracy of up to 0.1 nL/s to achieve on-orbit attitude control and orbit control. However, conventional flow sensors are unable to provide the necessary precision in the nanoliter per second range, and thus, alternative methods are required. In this study, we propose the use of image processing technology for rapid microflow calibration. Our method involves capturing images of the droplets at the outlet of the flow supply system to rapidly obtain the flow rate, and we used the gravimetric method to verify the accuracy of our approach. We conducted several microflow calibration experiments within the 1.5 nL/s range and demonstrated that image processing technology can achieve the desired accuracy of 0.1 nL/s while saving more than two-thirds of the time required to obtain the flow rate within an acceptable margin of error compared to the gravimetric method. Our study presents an efficient and innovative approach to addressing the challenges of measuring microflows with high precision, particularly in the nanoliter per second range, and has the potential for widespread applications in various fields.

Funder

National Key R&D Program of China

Shenzhen Science and Technology Program

Publisher

MDPI AG

Subject

Electrical and Electronic Engineering,Mechanical Engineering,Control and Systems Engineering

Reference19 articles.

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5. Bock, D., Bethge, M., and Tajmar, M. (2014, January 19–22). Highly miniaturized feep thrusters for cubesat applications. Proceedings of the 4th Spacecraft Propulsion Conference, Cologne, Germany.

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