Hybrid vertical takeoff and landing aircraft (large)

CN310147311SActive Publication Date: 2026-08-14CHINA HELICOPTER RES & DEV INST
View PDF 0 Cites 0 Cited by

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Designs(China)
Current Assignee / Owner
Filing Date
2025-12-11
Publication Date
2026-08-14

Smart Images

  • Figure 000001_ABST
    Figure 000001_ABST
Patent Text Reader

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.
Need to check novelty before this filing date? Find Prior Art