Composite landing gear fairing structure and integrated rapid forming method thereof
By using carbon fiber composite materials and integrated molding technology, the problems of complicated landing gear fairing manufacturing process and easy metal corrosion have been solved, achieving lightweight, durable and efficient production, and is suitable for the manufacturing of fairings with complex shapes.
Patent Information
- Application Number
- CN202610780610.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2026-06-02
- Publication Date
- 2026-07-17
AI Technical Summary
The existing landing gear fairing manufacturing process is cumbersome, time-consuming, and inefficient, and the metal materials are easily corroded, making it difficult to meet the requirements of lightweight and durability.
The support ribs, side strips, and skin structure are designed using carbon fiber composite materials. Combined with an integrated rapid molding method, the support ribs, reinforcing ribs, and skin are formed in one step by using a combination of fragmented prepreg and continuous fiber prepreg.
It significantly reduces the weight of the fairing, improves production efficiency, enhances corrosion resistance and impact resistance, simplifies the manufacturing process, reduces costs, and improves the environmental adaptability and structural stability of the fairing.
Smart Images
Figure CN122402773A_ABST
Abstract
Citation Information
Patent Citations
Carbon fiber composite fairing, forming mold and forming method thereof
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