Composite control surfaces for aircraft
Composite control surface (1) for aircraft comprising a monolithic upper skin (2), a monolithic lower skin (3) and an inner structure (4) between them, all these elements being made of composite material, wherein the inner structure (4) has a corrugated shape, comprising side members (5) acting as s...
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| Hauptverfasser: | , , , |
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| Format: | Patent |
| Sprache: | eng ; fre ; ger |
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| Online-Zugang: | Volltext bestellen |
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| Zusammenfassung: | Composite control surface (1) for aircraft comprising a monolithic upper skin (2), a monolithic lower skin (3) and an inner structure (4) between them, all these elements being made of composite material, wherein the inner structure (4) has a corrugated shape, comprising side members (5) acting as spars and lower (6) and upper (7) members, the lower (6) and upper (7) members contacting the inner surfaces of the lower skin (3) and the upper skin (2) respectively. A method to manufacture the control surface (1) is also provided. |
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