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Application filed by Національний Авіаційний УніверситетfiledCriticalНаціональний Авіаційний Університет
Priority to UAU201201617UpriorityCriticalpatent/UA73711U/en
Publication of UA73711UpublicationCriticalpatent/UA73711U/en
A superlight aircraft with an integrated wing, which consists of a fuselage with a power unit located in its forward part, a rectangular wing and a classical empennage located in the rear part of fuselage. A wing is integrated with a constant chord, it consists of two main structural parts. The first part is made in the form of a rectangular sweepback wing, which center wing section is located directly above the bow of normal fuselage and is attached thereto by means of footings. The second part is made in the form of a rectangular sweepforward wing with a positive transverse angle V, which is attached to the underside of the fuselage.
UAU201201617U2012-02-142012-02-14Superlight aircraft with integrated wing
UA73711U
(en)