초록 ▼

The invention is a flying wing aircraft having a forward fuselage; an aft fuselage segment; a propulsion segments adapted to mate to the fuselage segments; a pair of wing segments adapted to mate with the propulsion segments. The invention further includes a center section adapted to fit between the

The invention is a flying wing aircraft having a forward fuselage; an aft fuselage segment; a propulsion segments adapted to mate to the fuselage segments; a pair of wing segments adapted to mate with the propulsion segments. The invention further includes a center section adapted to fit between the forward and aft fuselage sections; the center section adapted to receive multiple compartment systems.

대표청구항 ▼

1. A flying wing aircraft having an exterior surface, the aircraft comprising: an airframe including a forward fuselage segment and an aft fuselage segment;left and right propulsion segments adapted to mate to said fuselage segments;left and right wing segments adapted to mate with said left and rig

1. A flying wing aircraft having an exterior surface, the aircraft comprising: an airframe including a forward fuselage segment and an aft fuselage segment;left and right propulsion segments adapted to mate to said fuselage segments;left and right wing segments adapted to mate with said left and right propulsion segments respectively; anda center section formed to define a recess for receiving one of a plurality of compartment systems, each compartment system being insertable within the recess, the center section further being engagable to the forward fuselage segment and to the aft fuselage segment;each compartment system defining a lower surface, side surfaces, a front surface, a rear surface, and a top surface such that, upon insertion within the center section recess, the lower surface defines a portion of the aircraft exterior surface, and the side surfaces and top surface are disposed within the recess. 2. The aircraft as set forth in claim 1 further comprising a compartment system connected to the center section, the compartment system being formed as one of the group consisting of a bomb bay, a cargo compartment system and a tanker compartment system. 3. The flying wing aircraft as set forth in claim 2 wherein when said compartment system is said cargo bay, said aircraft further comprises: right and left retractable canards mounted to said forward fuselage section; andan air system supply to provide pressurized air from said propulsion system for blowing pressurized air over said canards. 4. The flying wing aircraft as set forth in claim 3 wherein the aircraft includes trailing edge flaps and said air supply system provides air over the flaps. 5. The flying wing aircraft as set forth in claim 2 wherein each oldie compartment systems are interchangeable, while maintaining substantially the same external dimensions of the flying wing aircraft. 6. The flying wing aircraft as set forth at claim 2 wherein when the flying wing aircraft receives the bomb bay or the tanker compartment system, the external configuration of the aircraft remains substantially the same. 7. The flying wing aircraft as set forth in claim 2 wherein each of the compartment systems defines an exterior surface portion formed to substantially conform to the adjacent exterior surface of the aircraft. 8. The flying wing aircraft as set forth in claim 7 wherein said cargo compartment system defines cargo bay doors formed in the aircraft exterior surface portion. 9. The flying wing aircraft as set forth in claim 7 wherein the tanker compartment system includes a plurality of fuel tanks. 10. The flying wing aircraft as set forth in claim 1 wherein the center section recess defines a recess top surface and recess side surfaces, and wherein, upon insertion within the center section recess, the compartment system top surface and side surfaces are disposed adjacent the recess top surface and side surfaces, respectively. 11. The flying wing aircraft as set forth in claim 1 wherein upon insertion within the center section recess, the compartment system top surface, side surfaces, front surface and rear surface are each disposed with the aircraft exterior surface.