Support structure for a cargo aircraft

• US 8,387,917 B1
• Filed: 03/25/2010
• Issued: 03/05/2013
• Est. Priority Date: 05/03/2007
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Grip, Robert Erik, Rawdon, Blaine Knight
• Primary Examiner(s): Alsomiri, Isam
• Assistant Examiner(s): BENEDIK, JUSTIN M
• Application Number:
  US12/731,261
• Time in Patent Office: 1,076 Days
• Field of Search: 244/118.1, 244/119, 244/137.1, 244/137.3, 244/4.A
• US Class Current: 244/119
• CPC Class Codes: B64C 1/08 Geodetic or other open-frame structures
• CPC Class Codes: B64C 1/22 Other structures integral with fuselages to facilitate loading , e.g. cargo bays, cranes

Abstract

A method and apparatus for transporting containers in an aircraft. A number of containers is loaded into the aircraft. The aircraft is comprised of first and second outer planar structures, a number of planar structures located between the first outer planar structure and the second outer planar structure, a wing, and a support structure. The first outer planar structure, the second outer planar structure, and the number of planar structures are substantially parallel to each other, are coupled to each other to form a fuselage structure, and are configured to receive the number of containers. The support structure connects the wing to a first bottom end of the first outer planar structure, a second bottom end of the second outer planar structure, and a number of bottom ends of the number of planar structures. The aircraft is operated to transport the number of containers to a destination.

Claims

1. An aircraft comprising:

a first outer planar structure;

a second outer planar structure;

wherein the first outer planar structure and the second outer planar structure each comprise a truss;

a number of planar structures located between the first outer planar structure and the second outer planar structure, wherein the first outer planar structure, the second outer planar structure, and the number of planar structures are substantially parallel to each other, are coupled to each other to form a fuselage structure, and are configured to receive a number of containers;

a second plurality of planar structures connected to the first outer planar structure, the second outer planar structure, and the number of planar structures, wherein the second plurality of planar structures is substantially parallel to each other and wherein the first plurality of planar structures and the second plurality of planar structures form a plurality of bays in the fuselage structure, wherein the plurality of bays is configured to receive the number of containers, and wherein the first outer planar structure, the second outer planar structure, the number of planar structures, and the second plurality of planar structures are each comprised of a plurality of nodes and a plurality of elements connecting the plurality of nodes;

a wing; and

a support structure connecting the wing to a first bottom end of the first outer planar structure, a second bottom end of the second outer planar structure, and a number of bottom ends of the number of planar structures.

2. The aircraft of claim 1, wherein the support structure comprises:

a first outer member extending from a first side of the wing to the first bottom end of the first outer planar structure;

a second outer member extending from a second side of the wing to the second bottom end of the second outer planar structure;

a number of members connected to the number of bottom ends of the number of planar structures and associated with the first outer member and the second outer member.

3. The aircraft of claim 2, wherein the number of members are positioned at a number of angles to provide support for the first outer planar structure, the second outer planar structure, and the number of planar structures, wherein the number of angles are different than angles at which the first outer member and the second outer member are positioned.

4. The aircraft of claim 1, wherein the support structure carries vertical loads extending through load paths through the first outer planar structure, the second outer planar structure, and the number of planar structures.

5. The aircraft of claim 4, wherein at least a portion of the load paths extend from the wing through at least one of the first outer planar structure, the second outer planar structure, and the number of planar structures to the support structure.

6. The aircraft of claim 4, wherein a portion of a load path extending from the wing through one of the number of planar structures to the support structure is through a component in a number of components connecting the number of bottom ends of the number of planar structures to a number of members in the support structure.

7. The aircraft of claim 1, wherein the wing is associated with a top of the fuselage structure.

8. The aircraft of claim 1 further comprising:

a plurality of bays formed between the first outer planar structure, the second outer planar structure, and the number of planar structures, wherein the plurality of bays is configured to receive the number of containers.

9. The aircraft of claim 1, wherein the first plurality of planar structures lies in a substantially vertical-longitudinal plane, and wherein the second plurality of planar structures lies in a substantially horizontal-longitudinal plane.

10. The aircraft of claim 1, wherein the first outer planar structure, the second outer planar structure, the number of planar structures, and the plurality of second planar structures comprise a plurality of trusses.

11. The aircraft of claim 1, wherein the first outer planar structure, the second outer planar structure, and the number of planar structures form one of a space frame and a semi-monocoque structure.

12. A method for transporting containers in an aircraft, the method comprising:

loading a number of containers into the aircraft, wherein the aircraft is comprised of a first outer planar structure;

a second outer planar structure;

wherein the first outer planar structure and the second outer planar structure each comprise a truss;

a number of planar structures located between the first outer planar structure and the second outer planar structure, wherein the first outer planar structure, the second outer planar structure, and the number of planar structures are substantially parallel to each other, are coupled to each other to form a fuselage structure, and are configured to receive the number of containers;

a wing, wherein the first outer planar structure, the second outer planar structure, and the number of planar structures are a first plurality of planar structures;

a support structure connecting the wing to a first bottom end of the first outer planar structure, a second bottom end of the second outer planar structure, and a number of bottom ends of the number of planar structures;

a second plurality of planar structures connected to the first outer planar structure, the second outer planar structure, and the number of planar structures, wherein the second plurality of planar structures is substantially parallel to each other and wherein the first plurality of planar structures and the second plurality of planar structures form a plurality of bays in the fuselage structure, wherein the plurality of bays is configured to receive the number of containers, and wherein the first outer planar structure, the second outer planar structure, the number of planar structures, and the second plurality of planar structures are each comprised of a plurality of nodes and a plurality of elements connecting the plurality of nodes; and

operating the aircraft to transport the number of containers to a destination.

13. The method of claim 12, wherein the support structure comprises:

a first outer member extending from a first side of the wing to the first bottom end of the first outer planar structure;

a second outer member extending from a second side of the wing to the second bottom end of the second outer planar structure; and

a number of members connected to the number of bottom ends of the number of planar structures and associated with the first outer member and the second outer member.

14. The method of claim 12, wherein the support structure carries vertical loads extending through load paths through the first outer planar structure, the second outer planar structure, and the number of planar structures.

15. The method of claim 14, wherein at least a portion of the load paths extend from the wing through at least one of the first outer planar structure, the second outer planar structure, and the number of planar structures to the support structure.

16. The method of claim 14, wherein a portion of a load path extending from the wing through one of the number of planar structures to the support structure is through a component in a number of components connecting the number of bottom ends of the number of planar structures to a number of members in the support structure.

17. The method of claim 12, wherein the wing is associated with a top of the fuselage structure.

18. The method of claim 12 further comprising:

a plurality of bays formed between the first outer planar structure, the second outer planar structure, and the number of planar structures, wherein the plurality of bays is configured to receive the number of containers.

19. The method of claim 12, wherein the first plurality of planar structures lies in a substantially vertical-longitudinal plane, and wherein the second plurality of planar structures lies in a substantially horizontal-longitudinal plane.

20. The method of claim 12, wherein the first outer planar structure, the second outer planar structure, the number of planar structures, and the second plurality of planar structures comprise a plurality of trusses.

21. The method of claim 12, wherein the first outer planar structure, the second outer planar structure, and the number of planar structures form one of a space frame and a semi-monocoque structure.