Composite component, method of manufacturing a composite component, aircraft wing and vehicle
By laying a composite layer on the surface of the mold and curing it to form a composite component with ridges and channels, the problem of wrinkles in the composite component during manufacturing is solved, and the efficient and reliable manufacturing of the composite component and the improvement of its aerodynamic performance are achieved.
CN122186379APending Publication Date: 2026-06-12AIRBUS DEFENCE AND SPACE(GB)
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Patent Information
- Application Number
- CN202511836992.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Priority Date
- 2024-12-11
- Filing Date
- 2025-12-08
- Publication Date
- 2026-06-12
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Figure CN122186379A_ABST
Abstract
The present disclosure provides composite components, methods of manufacturing composite components, aircraft wings, and vehicles. The composite components have a first surface and an opposite second surface, wherein at least a portion of the first surface forms an outer aerodynamic surface of the vehicle. A region of the component has a curvature in two orthogonal directions. The component has a relief that defines a channel in one of the first surface or the second surface and a corresponding ridge in the other of the first surface and the second surface.
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