Development of elemental technology for constructing floating particle collection turbojet UAV system
| Project/Area Number |
26340047
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| Research Category |
Grant-in-Aid for Scientific Research (C)
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| Allocation Type | Multi-year Fund |
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| Section | 一般 |
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| Research Field |
Environmental impact assessment
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| Research Institution | Niigata University |
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Principal Investigator |
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| Co-Investigator(Kenkyū-buntansha) |
松原 幸治 新潟大学, 自然科学系, 教授 (20283004)
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| Co-Investigator(Renkei-kenkyūsha) |
KAWASAKI Kazumasa 新潟大学, 大学院自然科学研究科, 准教授 (50214622)
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| Research Collaborator |
SHIRAI Kenji 新潟大学, 工学部, 技術職員
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| Project Period (FY) |
2014-04-01 – 2017-03-31
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| Project Status |
Completed (Fiscal Year 2016)
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| Budget Amount *help |
¥5,070,000 (Direct Cost: ¥3,900,000、Indirect Cost: ¥1,170,000)
Fiscal Year 2016: ¥1,040,000 (Direct Cost: ¥800,000、Indirect Cost: ¥240,000)
Fiscal Year 2015: ¥1,040,000 (Direct Cost: ¥800,000、Indirect Cost: ¥240,000)
Fiscal Year 2014: ¥2,990,000 (Direct Cost: ¥2,300,000、Indirect Cost: ¥690,000)
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| Keywords | 小型ジェットエンジン / 浮遊粒子採取 / UAV / 新潟スカイプロジェクト / 小型ターボジェットエンジン / アニュラ型燃焼器 / 浮遊粒子 / 騒音 / シェブロンノズル / 燃焼の可視化 |
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| Outline of Final Research Achievements |
Research leaders have participated in the Niigata Sky Project and have been developing compact jet engines and aircraft for civilian UAV. Under such circumstances, we planned to develop a UAV system for collecting airborne particles over the Sea of Japan. Therefore, in this research, we conducted a performance test of a compact jet engine and successfully visualized the combustion by the combustor of the developed engine. Moreover, we started to silence the engine, and it was able to attenuate the engine sound. Matsubara, a co-researcher, made it possible to perform three-dimensional numerical analysis of the combustor. Furthermore, a flight test using a commercially available UAV was also obtained with permission from the Ministry of Land, Infrastructure and Transport, making it possible to collect suspended particles.
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Report
(4 results)
Research Products
(9 results)
