Aircraft digital flight-control: Airplane elevons & aircraft rudder 04/10Aviation & Business, Saturday 28 December 2013, 18:41 GMT
The use of composites in the LCA resulted in a 40% reduction in the total number of parts compared to using a metallic frame. Furthermore, the number of fasteners has been reduced by half in the composite structure from the 10,000 that would have been required in a metallic frame design. The composite design also helped to avoid about 2,000 holes being drilled into the airframe. Overall, the aircraft’s weight is lowered by 21%. LATEST UPDATES
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LATEST UPDATES
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