초록 ▼

An aircraft 1 comprising interchangeable wings 5 detachedly connected to a fuselage 3 , each wing 5 containing the fuel and flight systems 13,15 for engines 7 mounted to the wings 5 , so that the fuselage 3 need contain no flight systems, simply a “bus” 23 for communication and the tra

An aircraft 1 comprising interchangeable wings 5 detachedly connected to a fuselage 3 , each wing 5 containing the fuel and flight systems 13,15 for engines 7 mounted to the wings 5 , so that the fuselage 3 need contain no flight systems, simply a “bus” 23 for communication and the transfer of data between the wings.

대표청구항 ▼

1. An aircraft comprising:at least one pair of wings, each wing comprising means for propelling the aircraft in flight and control means for controlling the propulsion means and for controlling the aircraft in flight; anda fuselages; whereineach wing is separately detachably connected to the fuselag

1. An aircraft comprising:at least one pair of wings, each wing comprising means for propelling the aircraft in flight and control means for controlling the propulsion means and for controlling the aircraft in flight; anda fuselages; whereineach wing is separately detachably connected to the fuselage;the control means are located within the wings; andthe fuselage comprises means connecting the control means and the propulsion means in the associated wings of each pair of wings, thereby to enable controlled flight of the aircraft. 2. An aircraft as claimed in claim 1 wherein the wings contain fuel tanks for the associated propulsion means. 3. An aircraft as claimed in claim 1 wherein the propulsion means are rotatable about an axis perpendicular to the direction of forward flight of the aircraft, thereby selectively to provide propulsion for forward flight or for vertical take off and landing of the aircraft. 4. An aircraft as claimed in claim 1, wherein means are provided selectively to divert efflux from the propulsion means, thereby selectively to provide propulsion for forward flight or for vertical take off and landing of the aircraft. 5. An aircraft as claimed in claim 1 wherein the fuselage comprises at least two container modules detachably connected together. 6. An aircraft as claimed in claim 1 comprising an undercarriage adapted to facilitate take-off and landing of the aircraft, the undercarriage being integral with the fuselage. 7. An aircraft comprising:a fuselage;a pair of wings;propulsion means mounted on each wing of said pair of wings, for propelling the aircraft in flight;control means contained within each wing of said pair of wings, for controlling the propulsion means and for controlling the aircraft in flight; and means contained within the fuselage, for connecting the control means and the propulsion means in the respective wings of said pair of wings, to control flight of the aircraft; whereineach wing of said pair of wings is separately and detachably connected to the fuselage; andsaid pair of wings is coupled to the fuselage in such a manner that it is interchangeable with another pair of wings.