High aspect ratio flying wing drone
CN309885467SActive Publication Date: 2026-03-31INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT
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Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Designs(China)
- Current Assignee / Owner
- Filing Date
- 2025-04-28
- Publication Date
- 2026-03-31
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Figure 000001_ABST
Abstract
1. The name of the design product: large aspect ratio flying wing model. 2. The use of the design product: mainly used for wind tunnel test, providing support for the development of large aspect ratio flying wing layout aircraft. 3. The design points of the design product: in shape. 4. The picture or photo that best indicates the design points: perspective view. 5. The design points are embodied in the perspective view, the right view is omitted; the bottom view is symmetrical with the top view, and the bottom view is omitted.
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