Abstract
This paper describes the design of a miniature air suction system to house a chemical sensor. It has been designed to improve the aerodynamic chemical sensing efficiency and to have a low weight since it is meant to be mounted on a micro air vehicle. The design is done around a readily available miniature axial flow fan by computational methods. A converging-diverging shape for the air suction system with the sensor disc having a central hole and mounted at the throat is proposed as good design concept. The systematic approach has led to a light weight system with high aerodynamic efficiency even under extreme flow conditions that may be caused by MAV manoeuvre or cross winds.
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Abbreviations
- D 1, D 2, D 3, L 1, L 2 :
- d :
-
diameter of the hole in the sensor disc plate (mm)
- L :
-
total length of the air suction duct = 30 mm
- p :
-
pressure (Pa)
- Q :
-
volumetric flow rate (lpm)
- T :
-
torque (N-m)
- v :
-
velocity (m/s)
- V ∞ :
-
velocity of the MAV carrying the air suction device (m/s)
- z :
-
fan axis and also flow direction
- α :
-
angle of attack of air suction device with freestream (deg)
- ρ :
-
density of air (kg/m3)
- τ w :
-
wall shear stress (Pa)
- ω :
-
fan rotational speed (rad/s)
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Acknowledgements
We thank the Department of Science and Technology (DST), New Delhi for funding this project; the Programme Office, National Programme on Micro Air Vehicles (NP-MICAV), Aeronautical Development Establishment, Bengaluru for sanctioning and monitoring the project; and the National Design and Research Forum (NDRF), Bengaluru of the Institution of Engineers (India) for coordinating the project.
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Deshpande, M.D., Sivapragasam, M. & Umesh, S. An efficient miniature air suction system for chemical sensors for micro air vehicle application. Sādhanā 45, 116 (2020). https://doi.org/10.1007/s12046-020-01352-y
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DOI: https://doi.org/10.1007/s12046-020-01352-y