JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
タイトル切削加工より製作されるクアッドコプター用小径プロペラの騒音解析
その他のタイトルDevelopment of quiet propellers for a vertical takeoff and landing-type quadcopter
著者(日)鈴木, 翔平; 菅, 洋志
著者(英)Suzuki, Shouhei; Suga, Hiroshi
著者所属(日)千葉工業大学; 千葉工業大学
著者所属(英)Chiba Institute of Technology; Chiba Institute of Technology
発行日2017-01-01
発行機関など千葉工業大学
Chiba Institute of Technology
刊行物名千葉工業大学研究報告
Report of Chiba Insitute of Technology
64
開始ページ23
終了ページ28
刊行年月日2017-01-01
言語jpn
eng
抄録The quadcopter has been spotlighted in recent years as an unmanned aircraft used for aerially transporting goods to remote areas during disasters. An advantage of the quadcopter is that it can be used in a narrower flight airspace than a fixed-wing aircraft, as the quadcopter has a vertical rise and vertical drop. However, there are a number of issues associated with quadcopters, such as safety and noise. Noise is generated by the propeller. Especially, for small quadcopters, the noise generated by rotation is serious because of the high-speed rotation of the small propeller. However, there are few reports on reducing the noise by small propellers. Conventional small propellers are made using parameters such as size and twist angle, but sufficient consideration has not been given to the propeller’s surface roughness. Therefore, we cleared the surface-roughness dependence and size-dependence on the noise. Propellers of various sizes and surface roughnesses were fabricated by NC machining, and their resulting noise was measured. We found that the surface roughness of the propeller blade influences the rotation noise of the small propeller.
内容記述形態: カラー図版あり
Physical characteristics: Original contains color illustrations
キーワードクアッドコプター; プロペラ; 騒音
資料種別Departmental Bulletin Paper
NASA分類Aircraft Design, Testing and Performance
SHI-NOAA1640293000
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/586822


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