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Aircraft with combined aerofoils and control surfaces has annulus on each side of fuselage and formed by aerofoils and control surfaces together with side walls of fuselage, and annulus accommodates propeller
Aircraft with combined aerofoils and control surfaces has annulus on each side of fuselage and formed by aerofoils and control surfaces together with side walls of fuselage, and annulus accommodates propeller
The aerofoils(2,3) and control surfaces together with the fuselage side walls form an annulus on both sides of the fuselage(1). At least one propeller(9,10) is located in each annulus and positioned between the rear upper section of the aerofoil and forward lower section of the elevator surface(4). Each annulus has additional load bearing surfaces(7,8) for suspension of the propeller shaft and for guiding of the propulsion force transmission or engine suspension.
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