FIELD: transport.
SUBSTANCE: invention relates to winged aircraft. Proposed aircraft comprises wings (10), control surfaces (11, 12) on said wings, transducer to measure actual load on wing at whatever preset flit time interval and control device connected with said transducer and wing control surfaces. Note here that said wing control surface are arranged to reduce maximum lift of wings.
EFFECT: reduced weight of aircraft.
10 cl, 2 dwg
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