Tail fin of an aircraft
CN309351757SActive Publication Date: 2025-06-24SICHUAN AEROFUGIA TECH DEV CO LTD
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Patent Information
- Application Number
- CN202430145602.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Designs(China)
- Current Assignee / Owner
- Filing Date
- 2024-03-20
- Publication Date
- 2025-06-24
- Estimated Expiration
- 2039-03-20
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Figure 000007_ABST
Abstract
1. Name of the design product: Tail fin of an aircraft. 2. Use of the design product: This design product is used for manned flight, cargo flight, etc. The local appearance of the product is mainly used to assist the flight of the aircraft, playing roles such as balancing torque, controlling direction, and maintaining stability. 3. Design key points of the design product: Lies in the local shape. 4. Picture or photograph that best shows the design key points: Perspective view 1 of Design 1. 5. Design 1 is designated as the basic design. 6. Other situations that need to be explained: Other explanations: This design is a partial design. The partial appearance claimed is the appearance shown by the solid lines in the views. The dashed lines are used to indicate the boundary between the claimed appearance and the non-claimed appearance. The appearances shown by the dashed lines and the dotted lines are not claimed. Reference views of Design 1-3 and 10 are used to assist in expressing the solid line appearance shape of the occluded parts.
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