COMPANY:

Manufacturer and sales in Japan of all types of springs and automotive seat parts

Bachelor of aeronautical engineering and working full-time as a reliability engineer for an aircraft engine OEM. In his graduation research, he analyzed and tested the strength and weight of sandwich composite materials for unmanned aerial vehicles. Can take an interview in Japanese, and will be taking the next JLPT N2.

Profile

COUNTRY / REGION
India
SEX
Male
UNIVERSITY
Visvesvaraya Technological University
SPECIALIZATION
Aerospace
ACADEMIC LEVEL
Bachelor

MESSAGE

I would like to thank FAST OFFER International for providing me with this opportunity. I got to know about FAST OFFER International through my friends. The whole hiring process was smooth because of the fast offer staff and my mentor. They trained me to appear for the interviews without being worried or nervous. It was a joyful moment when I got the news about the selection, which cannot be explained through words. Again, I would wish all the very best for the future of FAST OFFER International.

FINAL YEAR PROJECT

工学で設計と開発するとき材料の選択は重要なことです。航空宇宙産業では強度はその材料の重量よりたかかったら最高です。重量を低くなると無人航空機(UAV)の飛ぶ時間を上げることができます。それを目標にして物資に関するプロジェクトをしました。現在無人航空機の応用範囲はいろいろな産業であります。航空宇宙工業で複合材料の使用は年々上がってきています。それはこの物資の強度のためである。やく21の色々の論文を参考にしてサンドイッチ複合について習いました。
サンドイッチ複合材料で二つ薄いラミネートの間に軽量の厚いコアラがあります。この構造の複合材料は軽量で、比較的に高い曲げ強度を持っています。私のプロジェクトでバルサ材のコアで グラスファイバー表面マットとポリエステルじゅしのラミネートを使いました。コムソール(Comsol)というソフトを使って複合材料の構造的な分析引張、圧縮、曲げのテストのシミュレーションをしました。この分析の結果とテストの結果が合いました。引張(ASTMC297)、圧縮(ASTM C365)、曲げ(ASTMC393)などのテストは、ASTM規格に従って実行されました。テストの結果は他のおなじ特徴の複合の論文と比べたら、この複合材料の強度が高かった。構造テストの結果は平均引張強度12.22MPa, 平均圧縮強度28.186MPaと平均曲げ強度15.12MPaでした。結果に満足があったのでこの複合材料で無人航空機の翼NACA2410を参考にして作って飛ばされた。手作りの方法を使ったので全体的な製造経費を減らすことができました。ついにこの複合に軽量の金属ストリップとか高強度繊維を使用すると高速UAV構造にも使います。
このプロジェクトがAmerican institute of physicsジャーナル論文に掲載されました。それに加えてチームワークの大切さとかプレゼンテションとか学びました。

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