Experimental Study on Relation of Small UAV Propeller Thrust Generation and The Mouth-Ring

International Conference on Advanced Manufacturing and Industry Applications

机械制造;工业技术

Othman, M.N.K.^1 ; Razlan, Z.M.^1 ; Muhamad Azmi, M.S.^1 ; Zunaidi, I.^1 ; Wan, W.K.^1 ; Shahriman, A.B.^1 ; Hashim, M.S.M.^1 ; Faizi, M.K.^1 ; Ibrahim, I.^1 ; Kamarrudin, N.S.^1

School of Mechatronic Engineering, Universiti Malaysia Perlis, Pauh Putra Campus, Perlis, Arau

02600, Malaysia^1

关键词: Propeller blades;    Propeller thrusts;    Small UAV;    Thrust generation;    Value of velocity;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/429/1/012079/pdf
DOI  :  10.1088/1757-899X/429/1/012079

学科分类：工业工程学

来源: IOP

【 摘 要 】

In this study, the main focus is to study the thrust generation of various propeller blade width-spans with the mouth-ring application. By using the parameter, the thrust were calculated based on the value of velocity, voltage and RPM. The testing was performing in three different width-span that are; 10mm, 8mm and 5mm. There are also variable that be tested that cover the reducing the diameter of mouth-ring from 36 mm to 32mm. In addition, if compared the gaps and different position proved that centre position gives better thrust. Furthermore, the application of mouth-ring is evaluated to be good base on this study