초록 ▼

A blended wing body cargo aircraft is disclosed. A body section defines a cargo volume, where an outer surface of the body section is shaped to provide an aerodynamic lifting surface. A cargo door and ramp structure is located in an aft end of the body section and is shaped to conform to an outer sh

A blended wing body cargo aircraft is disclosed. A body section defines a cargo volume, where an outer surface of the body section is shaped to provide an aerodynamic lifting surface. A cargo door and ramp structure is located in an aft end of the body section and is shaped to conform to an outer shape of the aerodynamic lifting surface when in a closed position. A control surface has a slightly cambered downward shape, and is positioned substantially near an aft end of the cargo door and ramp structure.

대표청구항 ▼

1. A blended wing body cargo aircraft comprising: a body section defining a cargo volume, an outer surface of the body section shaped to provide an aerodynamic lifting surface comprising a lift coefficient increasing smoothly near a center of the body section;a cargo door and ramp structure located

1. A blended wing body cargo aircraft comprising: a body section defining a cargo volume, an outer surface of the body section shaped to provide an aerodynamic lifting surface comprising a lift coefficient increasing smoothly near a center of the body section;a cargo door and ramp structure located in an aft end of the body section and an outer shape of the aerodynamic lifting surface is shaped to conform with the cargo door and ramp structure and to form a steep upsweep preserving an aerodynamic efficiency of the blended wing body cargo aircraft when the cargo door and ramp structure is in a closed position; andat least one pitch control surface having a slightly cambered downward shape, and positioned near an aft end of the cargo door and ramp structure such that an efficient lift distribution is maintained while providing pitch control. 2. The blended wing body cargo aircraft according to claim 1, further comprising a plurality of wing sections coupled to the body section. 3. The blended wing body cargo aircraft according to claim 1, wherein the cargo door and ramp structure comprises substantially parallel contour lines forming a substantially planar surface through at least one of the group consisting of: about 92.6%, about 85.2%, about 77.8%, about 70.4%, about 63%, and about 55.6% of a length of the blended wing body cargo aircraft. 4. The blended wing body cargo aircraft according to claim 1, wherein the upsweep on the aft end of the body section provides cargo clearance. 5. The blended wing body cargo aircraft according to claim 1, wherein the at least one pitch control surface is cambered downward by about two degrees relative to a level line. 6. The blended wing body cargo aircraft according to claim 1, wherein: an angle of a cargo ramp of the cargo ramp and door structure is about 9 degrees from a ground line when deployed, anda toe extension of the cargo ramp of the cargo door and ramp structure is about 13 degrees from the ground line when deployed. 7. The blended wing body cargo aircraft according to claim 1, wherein the outer shape of the aerodynamic lifting surface is conformed to the cargo door and ramp structure by shaping a plurality of airfoil sections that form the blended wing body cargo aircraft. 8. The blended wing body cargo aircraft according to claim 7, wherein: the airfoil sections are located at about ±6.2%, about ±12.4%, about ±18.7%, about ±24.9% and about ±31.1% of a span of the blended wing body cargo aircraft, andthe airfoil sections have chord line angles to a level line of about 3.5, about 2.4, about 0.8, about 1.63, and about 2.62 degrees respectively. 9. The blended wing body cargo aircraft according to claim 7, wherein the cargo door and ramp structure is bounded by the airfoil sections located at about ±6.2% of a span of the blended wing body cargo aircraft. 10. The blended wing body cargo aircraft according to claim 7, wherein the at least one pitch control surface comprising the slightly cambered downward shape is provided by an addition of slender extensions at trailing edges of the airfoil sections over a width of the cargo door and ramp structure plus a smooth transition region outboard. 11. An aerodynamic lifting body comprising: a plurality of airfoil sections located at respective span locations of the aerodynamic lifting body and enclosing a cargo volume, the airfoil sections shaped to provide an aerodynamic lifting surface comprising a lift coefficient increasing smoothly near a center of the aerodynamic lifting body;a cargo door and ramp structure located in aft ends of the airfoil sections, outer contours of the airfoil sections shaped to conform with the cargo door and ramp structure forming a steep upsweep preserving an aerodynamic efficiency of the aerodynamic lifting body when the cargo door and ramp structure is in a closed position; andat least one pitch control surface having a slightly cambered downward shape, and comprising trailing edges of the airfoil sections and operable to provide pitch control such that an efficient lift distribution is maintained. 12. The aerodynamic lifting body according to claim 11, wherein a width of the cargo door and ramp structure is within about ±6.2% of a span of the aerodynamic lifting body. 13. The aerodynamic lifting body according to claim 11, wherein: the airfoil sections are located on at least one of the group consisting of: about ±6.2%, about ±12.4%, about ±18.7%, about ±24.9%, and about ±31.1% of a span of the aerodynamic lifting body, andthe airfoil sections have chord line angles to a level line of about 3.5, about 2.4, about 0.8, about 1.63, and about 2.62 degrees respectively. 14. The aerodynamic lifting surface according to claim 11, wherein the aft ends of the airfoil sections are upswept at substantially parallel lateral contour lines located at at least one of the group consisting of: about 92.6%, about 85.2%, about 77.8%, about 70.4%, about 63% and about 55.6% of a length of the aerodynamic lifting body. 15. The aerodynamic lifting surface according to claim 11, wherein: an angle of a cargo ramp of the cargo door and ramp structure is about 9 degrees from a ground line when deployed, anda toe extension of a cargo ramp of the cargo door and ramp structure is about 13 degrees from the ground line when deployed. 16. A method of forming a blended wing body cargo aircraft, the method comprising: providing a body section defining a cargo volume, an outer surface of the body section shaped to provide an aerodynamic lifting surface comprising a lift coefficient increasing smoothly near a center of the body section;providing a cargo door and ramp structure located in an aft end of the body section, an outer shape of the aerodynamic lifting surface shaped to conform with the cargo door and ramp structure and to form a steep upsweep when the cargo door and ramp structure is in a closed position; andpositioning at least one control surface having a slightly cambered downward shape near an aft end of the cargo door and ramp structure. 17. The method of claim 16, further comprising coupling a plurality of wing sections to the body section. 18. The method of claim 16, further comprising conforming a shape of the cargo door and ramp structure with the outer shape of the aerodynamic lifting surface by shaping a plurality of airfoil sections that form the blended wing body cargo aircraft to provide a nearly elliptical lift distribution. 19. The method of claim 18, further comprising providing an upsweep angle of the steep upsweep at aft ends of the airfoil sections located at substantially parallel lateral section lines at at least one of the group consisting of: about 92.6%, about 85.2%, about 77.8%, about 70.4%, about 63% and about 55.6% of a length of the body section, wherein the aft ends of the airfoil sections form a substantially planar surface. 20. The method of claim 18, wherein: the airfoil sections are located at one of the group consisting of: about ±6.2%, about ±12.4%, about ±18.7%, about ±24.9%, and about ±31.1% of a span of the blended wing body, andthe airfoil sections have chord line angles to a level line of about 3.5, about 2.4, about 0.8, about 1.63, and about 2.62 degrees respectively. 21. An aerodynamic lifting body comprising: a plurality of airfoil sections located at respective span locations of the aerodynamic lifting body and enclosing a cargo volume;a cargo door and ramp structure located in aft ends of the airfoil sections and shaped to conform with outer contours of the airfoil sections when in a closed position, the airfoil sections are located on at least one of the group consisting of: about ±6.2%, about ±12.4%, about ±18.7%, about ±24.9% and about ±31.1% of a span of the aerodynamic lifting body, and the airfoil sections have chord line angles to a level line of about 3.5, about 2.4, about 0.8, about 1.63 and about 2.62 degrees respectively; andat least one pitch control surface having a slightly cambered downward shape, and comprising trailing edges of the airfoil sections and operable to provide pitch control.