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FUSELAGE STRUCTURE FOR ACCOMMODATING TAILS AND CANARDS OF DIFFERENT SIZES AND SHAPES
FUSELAGE STRUCTURE FOR ACCOMMODATING TAILS AND CANARDS OF DIFFERENT SIZES AND SHAPES
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机译:适应不同大小和形状的尾巴和机匣的机身结构
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摘要
An aircraft includes a fuselage with structural interfaces for connection to any one or more of a variety of vertical tails, horizontal tails and canards. Vertical tails, horizontal tails and/or canards of different sizes, shapes, sweep angles, box chords, and/or root chords may connect to the fuselage without changing the structural layout or configuration of the fuselage structural interfaces.
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