Modular fuselage sections for vertical take off and landing distributed airframe aircraft
An aircraft capable of vertical takeoff and landing and stationary flight includes a distributed airframe coupled to a modular fuselage. The modular fuselage has a longitudinal axis substantially parallel to a rotational axis of three or more propellers. The modular fuselage includes a rear module substantially disposed within a perimeter of the distributed airframe, a front module removably connected to the rear module and substantially aligned with the longitudinal axis. One or more engines or motors are disposed within or attached to the distributed airframe or fuselage. The three or more propellers are proximate to a leading edge of the distributed airframe, distributed along the distributed airframe, and operably connected to the one or more engines or motors to provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight.
1. An aircraft capable of vertical takeoff and landing and stationary flight, comprising:
a distributed airframe comprising a closed wing;
a modular fuselage coupled to the distributed airframe, the modular fuselage having a longitudinal axis substantially parallel to a rotation axis of three or more propellers, the modular fuselage comprising a rear module substantially disposed within a perimeter of the distributed airframe, a front module removably connected to the rear module and substantially aligned with the longitudinal axis;
one or more engines or motors disposed within or attached to the distributed airframe, modular fuselage;
the three or more propellers proximate to a leading edge of the distributed airframe, distributed along the distributed airframe, and operably connected to the one or more engines or motors to provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight in a hover mode in which the longitudinal axis is substantially vertical;
the closed wing provides lift whenever the aircraft is in forward flight in an airplane mode in which the longitudinal axis is substantially in a direction of the forward flight, and one or more engines or motors provide thrust whenever the aircraft is in forward flight in the airplane mode; and
the one or more engines or motors provide lift and thrust whenever the aircraft is in vertical takeoff and landing, and stationary flight in the hover mode.
2. The aircraft of claim 1 , wherein:
the front module comprises a cockpit module, a cabin module, an escape module, a payload module, a sensor module or a surveillance module; and
the rear module comprises a cabin module, a payload module, a sensor module, a surveillance module, a power source module or a fuel module.
3. The aircraft of claim 1 , further comprising one or more middle modules removably connected between the front module and the rear module.
4. The aircraft of claim 3 , wherein the one or more middle modules comprise a cabin module, an escape module, a payload module, a sensor module, a surveillance module, a power source module or a fuel module.
5. The aircraft of claim 1 , wherein the front module detaches, pivots, or retracts at least partially into the rear module for storage or transport of the aircraft.
6. The aircraft of claim 1 , wherein the rear module is substantially disposed at a center of the distributed airframe.
7. The aircraft of claim 1 , wherein the aircraft is manned or unmanned.
8. The aircraft of claim 1 , wherein the distributed airframe comprises a closed wing that is circular-shaped, oval-shaped, triangular-shaped, or polygonal-shaped.
9. The aircraft of claim 1 , further comprising one or more parachutes operably disposed within a nose of the front module.
10. The aircraft of claim 1 , further comprising one or more ballast disposed within the front module or the rear module that selectively change a center of gravity of the aircraft by moving the one or more ballast within the modular fuselage.
11. The aircraft of claim 1 , further comprising two or more fuel tanks disposed within the front module or the rear module that selectively change a center of gravity of the aircraft by transferring a fuel between the two or more fuel tanks.
12. The aircraft of claim 1 , wherein a size or weight of the front module is selected to provide a specified center of gravity for the aircraft.
13. The aircraft of claim 1 , further comprising one or more flight control surfaces disposed on or extending from the modular fuselage.
14. The aircraft of claim 13 , wherein the one or more flight control surfaces comprise one or more airfoils, winglets, elevators or ailerons.
15. The aircraft of claim 14 , wherein the one or more airfoils or winglets are retractable, removable, stowable or variable swept.
16. The aircraft of claim 1 , wherein the distributed airframe further comprising one or more doors or removable sections that provide access to the modular fuselage when the aircraft is in a landed position.