Hybrid vertical takeoff and landing aircraft (large)
CN310147311SActive Publication Date: 2026-08-14CHINA HELICOPTER RES & DEV INST
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Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Designs(China)
- Current Assignee / Owner
- Filing Date
- 2025-12-11
- Publication Date
- 2026-08-14
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Figure 000001_ABST
Abstract
1. Name of the product in this design: Hybrid Vertical Take-Off and Landing Aircraft (Large). 2. Intended use of this design: for flight. 3. The key design feature of this product is its shape. 4. The image or photograph that best illustrates the design's key points: a 3D model. 5. Other situations requiring explanation are illustrated in the following diagrams: The perspective view, front view, rear view, right view, left view, top view, and bottom view represent the helicopter state of the large hybrid vertical takeoff and landing aircraft; the perspective view, front view, rear view, right view, left view, top view, and bottom view of state change 1 represent the fixed-wing state of the large hybrid vertical takeoff and landing aircraft; the perspective view, front view, rear view, right view, left view, top view, and bottom view of state change 2 represent the 45° tilt transition state of the large hybrid vertical takeoff and landing aircraft.
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