Systems and methods for assembling containerized aircraft

Patent metadata

Field	Value
Publication number	US-11807397-B2
Application number	US-202217724278-A
Country	US
Kind code	B2
Filing date	Apr 19, 2022
Priority date	Jan 6, 2020
Publication date	Nov 7, 2023
Grant date	Nov 7, 2023

Abstract

Methods and systems for assembling containerized aircraft as complete aircraft. The methods comprise removing aircraft components from shipping container(s), unloading the aircraft components from shipping fixture(s), removing tooling comprising aircraft component positioning structure(s) from the shipping container(s), loading aircraft component(s) onto aircraft component positioning structure(s), positioning the aircraft components in aircraft component installation positions, positioning the aircraft component(s) using the aircraft component positioning structure(s), and attaching the aircraft components to assemble the complete aircraft. The systems comprise aircraft components configured to be loaded into shipping container(s) in a shipping arrangement, unloaded from the shipping arrangement and attached to at least one other aircraft component to assemble the complete aircraft; shipping fixture(s) configured to support the aircraft components in the shipping arrangement, and tooling configured to facilitate assembly of the aircraft components and comprising aircraft component positioning structure(s) configured to position aircraft component(s) in aircraft component installation position(s).

First claim

The invention claimed is:

1. A system for assembling a containerized aircraft as a complete aircraft, the system comprising:
a plurality of aircraft components that are configured to be loaded into a shipping arrangement, and wherein each aircraft component of the plurality of aircraft components is configured to be unloaded from the shipping arrangement and attached to at least one other aircraft component of the plurality of aircraft components to assemble the plurality of aircraft components into the complete aircraft;
one or more shipping fixtures configured to support the plurality of aircraft components in the shipping arrangement; and
tooling configured to facilitate assembly of the plurality of aircraft components into the complete aircraft, wherein the tooling is configured to be loaded into and unloaded from the shipping arrangement, wherein the tooling comprises one or more aircraft component positioning structures, wherein each aircraft component positioning structure of the one or more aircraft component positioning structures is configured to position at least one respective aircraft component of the plurality of aircraft components in at least one corresponding aircraft component installation position during assembly of the complete aircraft, wherein the tooling is configured to facilitate the assembly of the plurality of aircraft components into the complete aircraft in a plurality of assembly environments, wherein each assembly environment of the plurality of assembly environments comprises an assembly surface, and wherein the assembly surface comprises one or more of an uneven assembly surface, a dirt assembly surface, a grassy assembly surface, an unfinished assembly surface, and a wet assembly surface.

2. The system of claim 1 , wherein the plurality of aircraft components comprises a fuselage assembly, one or more wings, one or more engine assemblies, a vertical tailfin assembly, a horizontal stabilizer assembly, and a landing gear assembly.

3. The system of claim 1 , wherein at least a subset of the plurality of aircraft components comprises interconnectable preinstalled portions of one or more aircraft systems, and wherein the interconnectable preinstalled portions of each aircraft system of the one or more aircraft systems are configured to be interconnected to form a complete aircraft system.

4. The system of claim 1 , wherein each aircraft component of at least a subset of the plurality of aircraft components comprises one or more predrilled installation interfaces configured to permit a drilling-free attachment of each aircraft component of the subset of the plurality of the aircraft components.

5. The system of claim 1 , wherein one or more aircraft components of the plurality of aircraft components comprises one or more handling fittings configured to releasably engage with a conveying mechanism.

6. The system of claim 5 , wherein the tooling comprises one or more conveying mechanism handles, wherein each conveying mechanism handle is configured to associate with the conveying mechanism and releasably engage with one or more respective handling fittings, and wherein the one or more handling fittings are configured to releasably engage with at least one conveying mechanism handle of the one or more conveying mechanism handles.

7. The system of claim 1 , further comprising one or more shipping containers, wherein the plurality of aircraft components are configured to be loaded into the one or more shipping containers in the shipping arrangement, and wherein the tooling is configured to be loaded into and unloaded from the one or more shipping containers.

8. The system of claim 1 , wherein the plurality of aircraft components comprises a fuselage assembly, wherein the fuselage assembly comprises an open internal volume, and wherein one or more aircraft components of the plurality of aircraft components are configured to be received within the open internal volume of the fuselage assembly when the plurality of aircraft components are arranged in the shipping arrangement.

9. The system of claim 8 , wherein the one or more aircraft components comprises a horizontal stabilizer assembly and one or more engine assemblies, and wherein the horizontal stabilizer assembly is supported by an empennage shipping fixture, and wherein the one or more engine assemblies are supported by an engine shipping fixture.

10. The system of claim 1 , wherein the plurality of aircraft components comprises a fuselage assembly, wherein the one or more shipping fixtures comprises a fuselage shipping fixture that is configured to support and arrange the fuselage assembly in the shipping arrangement.

11. The system of claim 7 , wherein the plurality of aircraft components comprises one or more wings, wherein the one or more shipping fixtures comprises a wing shipping fixture that is configured to support and arrange the one or more wings in the one or more shipping containers.

12. The system of claim 11 , wherein the plurality of aircraft components further comprises a nose assembly, and wherein the wing shipping fixture further is configured to support and arrange the nose assembly in the shipping arrangement.

13. The system of claim 11 , wherein the wing shipping fixture comprises a hinged wing support member that is configured to operatively support a wing of the one or more wings, wherein the hinged wing support member is configured to pivot between a shipping orientation and an unloading orientation, wherein the hinged wing support member is configured to support the wing with a chord of the wing oriented upwardly in the shipping orientation, and wherein the hinged wing support member is configured to support the wing with the chord of the wing oriented outwardly in the unloading orientation.

14. The system of claim 13 , wherein the wing is configured to be unloaded from the wing shipping fixture in the unloading orientation.

15. The system of claim 1 , wherein the tooling is configured to be manually operated, and wherein the tooling is configured to be operated independent of computer aided systems.

16. The system of claim 1 , wherein the system further comprises a conveying mechanism configured to convey one or more aircraft components of the plurality of aircraft components from a respective shipping fixture of the one or more shipping fixtures to a respective aircraft component positioning structure of the one or more aircraft component positioning structures, and wherein the conveying mechanism comprises a forklift.

17. The system of claim 1 , wherein at least one of the one or more aircraft component positioning structures comprises a base structure and a vertical rise structure, wherein the base structure is configured to support the vertical rise structure on an assembly surface and comprises a laterally extending track, wherein the vertical rise structure extends upwardly from the laterally extending track and is configured to operatively support the at least one respective aircraft component.

18. The system of claim 1 , wherein at least one of the one or more aircraft component positioning structures is configured to facilitate one or more positional adjustments of the at least one respective aircraft component of the plurality of aircraft components, wherein the one or more positional adjustments comprise one or more of a pitch adjustment, a yaw adjustment, a roll adjustment, an X positional adjustment, a Y positional adjustment, and a Z positional adjustment.

19. A system for assembling a containerized aircraft as a complete aircraft, the system

Assignees

• Boeing Co

Inventors

• Anderson Joseph D
• Russell Don
• Moore Matthew B
• Warner Jason
• Herman David Jon
• Stone Patrick B
• Collier Sr Michael David

Classifications

• B64C1/26

  Attaching the wing or tail units or stabilising surfaces · CPC title

• B64C1/068

  Fuselage sections · CPC title

• B64F5/10 Primary

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B64F5/50

  Handling or transporting aircraft components · CPC title

• B64C2211/00

  Modular constructions of airplanes or helicopters · CPC title