FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering. Integral composite top panel of aircraft wing torsion box comprises skin (1) and set of stringers (2) made from polymer composite material based on carbon fibre formed as a solid structure by vacuum infusion. Packing of polymer composite material includes from 1 to N packets consisting of 1 to n layers with laying angles 0/±45/90° with percentage of layers in laying: 50% in direction 0°, 40% in directions ±45°, 10% in direction 90°.
EFFECT: reduction in the weight of the product is achieved.
5 cl, 4 dwg
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|---|---|---|---|
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|
RU2839492C1 |
| AIRCRAFT WING TIP | 2024 |
|
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| AIRCRAFT WING TORSION BOX COMPOSITE REAR SPAR | 2024 |
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| AIRCRAFT WING BOX WING COMPOSITE FRONT SPAR | 2024 |
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| WIDE-BODY LONG-RANGE AIRCRAFT WING | 2024 |
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| AIRCRAFT COMPOSITE RUDDER | 2024 |
|
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| AIRCRAFT WING | 2014 |
|
RU2557638C1 |
| TORSION BOX OF WING FROM COMPOSITE | 2013 |
|
RU2532255C1 |
| POWER STRESS BOXES AND METHODS TO OBTAIN THEM | 2014 |
|
RU2641026C2 |
