Abstract: The utility model provides a kind of change sweepforward twin-fuselage configuration aircraft, is related to a kind of multipurpose air fighting platform layout scheme.The utility model becomes sweepforward twin-fuselage configuration aircraft, it can be achieved that subsonic flight state is to the conversion of supersonic flight state, and becoming sweepforward twin-fuselage configuration aircraft includes：Anterior centrosome (1), two variable sweepback front wings (2), two fuselages (4), variable buzzard-type wing (6) and undercarriage.Becoming sweepforward twin-fuselage configuration aircraft can realize subsonic speed state to the mode conversion of supersonic speed state by becoming body mechanism, become sweepforward, the design of boxlike wing layout takes into account Asia/supersonic speed lift resistance ratio, and it can realize retrofocus amount more smaller than conventional airplane, supersonic speed state both sides fuselage is combined into one, increase slenderness ratio, longitudinal cross-section area distribution is gentle, twin fuselage and anterior centrosome fuselage arrangement, add the delivered payload capability of body, compatible kinetic energy and directional energy antipersonnel weapon.
Another transformer plane, sort of. The illustration is obviously based on a J-20 fuselage, although this by itself doesn't mean the concept or idea necessarily has a connection with J-20 or has to be confined to J-20. Note the movable surfaces have been greatly modified to allow for flexible aerodynamic configurations. The link below contains a full English translation.
Abstract: The invention proposes a kind of variant invisible plane and its changing method and applications.The aircraft is designed by stealthy requirement, moves canard and two deflectable formula slab tails entirely using lifting body strake wing allosteric type aerodynamic arrangement scheme, including two deployable and collapsibles. Deployable and collapsible canard takes in fuselage when aircraft cruises or high speed is flat winged, to reduce radar cross section, improves stealth. Deflectable formula slab tail is then deflectable to different angle under different flight state, thus as V-arrangement tail, horizontal tail or abdomeinal fin.The transformation of the aircraft aerodynamic arrangement, including canard configuration, anury formula layout and three-surface configuration are realized with this.The switching of three kinds of aerodynamic arrangements can combine the advantage of this three, preferably meet the requirement under each flight profile, mission profile and state of flight to air maneuver and stealth.The variant aircraft can be used as a kind of high lift-drag ratio, high maneuverability, the good someone of new generation of stealth and unmanned air fighting platform, for executing air superiority combat duty.