Research on morphing wing structure using extremely anisotropic composites
| Project/Area Number |
24560970
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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 |
Aerospace engineering
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| Research Institution | The University of Tokyo |
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Principal Investigator |
YOKOZEKI Tomohiro 東京大学, 工学(系)研究科(研究院), 准教授 (50399549)
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| Project Period (FY) |
2012-04-01 – 2015-03-31
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| Project Status |
Completed (Fiscal Year 2014)
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| Budget Amount *help |
¥4,940,000 (Direct Cost: ¥3,800,000、Indirect Cost: ¥1,140,000)
Fiscal Year 2014: ¥1,560,000 (Direct Cost: ¥1,200,000、Indirect Cost: ¥360,000)
Fiscal Year 2013: ¥1,820,000 (Direct Cost: ¥1,400,000、Indirect Cost: ¥420,000)
Fiscal Year 2012: ¥1,560,000 (Direct Cost: ¥1,200,000、Indirect Cost: ¥360,000)
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| Keywords | Morphing wing / Composites / 航空工学 / 構造力学 / モーフィング翼 / 複合材 / 航空宇宙工学 / 構造・機能材料 |
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| Outline of Final Research Achievements |
The present study proposed morphing wing structures using ultra-anisotropic composites for the feasible morphing technology enabling us to improve flight efficiency and aerodinamic performance of the future aircraft. Based on the real aircraft wing, airfoil structures with morphing trailing edge was structurally analyzed, and morphing wing with wire-driven actuation mechanism was designed. Morphng wing prototype was manufactured using the ultra-anisotropic composites, and wind tunnel test was performed to demonstrate the driving of morphing under aerodynamic forces. Successful driving of morphing wing under 30m/s airstream was presented in this study. The present study successfully indicated a useful insight for the feasibility of morphing wing and establishment of design methodology of morphing wing.
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Report
(4 results)
Research Products
(4 results)
