Common flight deck module for family of commercial aircraft

• US 6,497,388 B1
• Filed: 08/31/2001
• Issued: 12/24/2002
• Est. Priority Date: 08/31/2001
• Status: Expired due to Fees

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Eakins, Mark E., Friend, Michael G., Huffington, Jay R.
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US09/944,967
• Time in Patent Office: 480 Days
• Field of Search: 244/117.R, 244/119, 244/120, 244/140, 244/141
• US Class Current: 244/120
• CPC Class Codes: B64C 2001/0045 Fuselages characterised by special shapes
• CPC Class Codes: B64C 2211/00 Modular constructions of airplanes or helicopters
• CPC Class Codes: B64D 11/00 Passenger or crew accommodation; Flight-deck installations not otherwise provided for
• CPC Class Codes: B64D 2011/0046 Modular or preassembled units for creating cabin interior structures
• CPC Class Codes: Y02T 50/10 Drag reduction

Abstract

A common flight deck module for use with a plurality of aircraft platforms. The common flight deck module includes a discrete structure that is independent of the structure of the aircraft fuselage and may includes an avionics system and other hardware, controls and equipment. The common flight deck module is configured to “plug into” the fuselage from each of the aircraft platforms. The “plug in” modularity of the common flight deck module permits the standardization of various components and procedures to thereby make possible efficiency-based cost reductions for both aircraft manufacturers and aircraft consumers.

Claims

1. A method for fabricating an aircraft, the method comprising the steps of:

providing a flight deck module having a module structure that defines an avionics suite and at least one exterior window aperture;

generating a build order for an aircraft, the aircraft being selected from a plurality of aircraft platforms, each of the aircraft platforms having a fuselage with a predetermined capacity, wherein each of the fuselages is sized with a different cross-sectional area and wherein the flight deck module is compatible with each of the plurality of aircraft platforms;

fabricating at least a portion of an associated fuselage of the aircraft; and

fixedly coupling the flight deck module and the associated fuselage to one another to integrate the flight deck module into the aircraft.

2. The method of claim 1, wherein each of the fuselages has a generally hollow cylindrical shape and each of the fuselages is defined by a different exterior diameter.

3. The method of claim 1, wherein the flight deck module includes a pair of sidewalls, at least a portion of the sidewalls extending vertically upwardly from the associated fuselage.

4. The method of claim 3, wherein the flight deck module includes a top surface that tapers rearwardly and upwardly from a leading edge of the flight deck module to a transition point between the leading edge and a trailing edge of the flight deck module.

5. The method of claim 4, wherein the top surface of the flight deck module tapers rearwardly and downwardly from the transition point to the trailing edge.

6. The method of claim 1, wherein the flight deck module includes a cab floor and a forward pressure bulkhead.

7. The method of claim 1, wherein prior to the step of fixedly coupling the flight deck module and the fuselage, the method includes the steps of:

providing a set of flight deck avionics; and

incorporating the set of flight deck avionics into the flight deck module.

8. A commercial transport aircraft comprising:

a flight deck module having a discrete module structure defining an avionics suite and at least one exterior window aperture; and

a fuselage having a discrete fuselage structure with a flight deck aperture configured to receive the flight deck module;

wherein the flight deck module is configured to be fixedly coupled to the fuselage so as to be non-removable therefrom during flight; and

wherein the flight deck module is configured to be employed in a plurality of discrete aircraft platforms wherein each aircraft platform includes a uniquely sized fuselage that has a cross-sectional area that is different from the fuselage of each other aircraft platform.

9. The commercial transport aircraft of claim 8, wherein the fuselage has a generally hollow cylindrical shape.

10. The commercial transport aircraft of claim 8, wherein the flight deck module includes a pair of sidewalls, at least a portion of the sidewalls extending vertically upwardly from the fuselage.

11. The commercial transport aircraft of claim 10, wherein the flight deck module includes a top surface that tapers rearwardly and upwardly from a leading edge of the flight deck module to a transition point between the leading edge and a trailing edge of the flight deck module.

12. The commercial transport aircraft of claim 11, wherein the top surface of the flight deck module tapers rearwardly and downwardly from the transition point to the trailing edge.

13. The commercial transport aircraft of claim 8, wherein the flight deck module includes a cab floor and a forward pressure bulkhead.

14. The commercial transport aircraft of claim 8, wherein the flight deck module includes a set of flight deck avionics.