Method and Apparatus for Loadable Aircraft Software Parts Distribution

• US 20090138873A1
• Filed: 11/24/2008
• Published: 05/28/2009
• Est. Priority Date: 11/27/2007
• Status: Abandoned Application

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Beck, Walter R., Walker, Olga C., Reid, Travis Stephen, Gould, Todd William
• Application Number:
  US12/277,174
• Publication Number:
  US 20090138873A1
• Time in Patent Office: Days
• US Class Current: 717/173
• CPC Class Codes: G06F 8/61 Installation
• CPC Class Codes: G06Q 10/087 Inventory or stock management, e.g. order filling, procurement or balancing against orders

Abstract

A computer implemented method and apparatus for managing aircraft software parts. An aircraft software part management apparatus comprises a library, a receiving module, a proxy server, an onboard electronic distribution system on an aircraft, and a portable software maintenance tool. The library on the ground data processing system stores and manages aircraft software parts for aircraft. The receiving module is capable of receiving the aircraft software parts from suppliers and sending the aircraft software parts to the library. The proxy server is in communication with the library and is capable of distributing software to a plurality of aircraft clients. The onboard electronic distribution system is an aircraft client and is capable of receiving aircraft software parts for the aircraft from the library through the proxy server. The portable software maintenance tool provides an alternate route to send the aircraft software part to the onboard electronic distribution system for the aircraft.

Claims

1. An aircraft software part management apparatus, comprising:

a library associated with a data processing system, the library being configured to manage a set of aircraft software parts for a set of aircraft;

a receiving module capable of receiving the plurality of aircraft software parts and sending the set of aircraft software parts to the library;

a proxy server in communication with the library, wherein the proxy server is capable of serving a set of aircraft clients;

an onboard electronic distribution system for an aircraft in the set of aircraft, wherein the onboard electronic distribution system is an aircraft client in the set of aircraft clients and is capable of receiving an aircraft software part for the aircraft from the library through the proxy server; and

a portable software maintenance tool, wherein the portable software maintenance tool provides an alternate route to send the aircraft software part to the onboard electronic distribution system of the aircraft.

2. The aircraft software part management apparatus of claim 1, wherein the library being configured to create a crate containing the aircraft software part and wherein the aircraft software part is sent to the onboard electronic distribution system in the crate.

3. The aircraft software part management apparatus of claim 1, wherein the proxy server is associated with the data processing system.

4. The aircraft software part management apparatus of claim 1, wherein the portable software maintenance tool connects to the proxy server to receive the aircraft software part, is moved onto the aircraft containing the onboard electronic distribution system with the aircraft software part, and connects to the onboard software distribution system to transfer the aircraft software part to the onboard electronic distribution system.

5. The aircraft software part management apparatus of claim 1, wherein the onboard electronic distribution system downlinks data from a set of line replaceable units on the aircraft to the proxy server to form downlink data, and wherein the proxy server sends the downlink data to the library for storage.

6. The aircraft software part management apparatus of claim 1, wherein the aircraft software part is moved from the library to the onboard electronic distribution system in a crate.

7. A computer implemented method for managing a plurality of aircraft software parts, the computer implemented method comprising:

storing an aircraft software part in a library;

identifying an aircraft for the aircraft software part to form an identified aircraft;

sending the aircraft software part from the library to a proxy server; and

sending the aircraft software part from the proxy server to an onboard electronic distribution system on the identified aircraft.

8. The computer implemented method of claim 7, wherein the step of sending the aircraft software part from the proxy server to an onboard electronic distribution system on the identified aircraft comprises:

sending the aircraft software part from the proxy server to the onboard electronic distribution system on the identified aircraft using a communications link.

9. The computer implemented method of claim 7, wherein the step of sending the aircraft software part from the proxy server to an onboard electronic distribution system on the identified aircraft comprises:

sending the aircraft software part from the proxy server to the onboard electronic distribution system on the identified aircraft using a portable software maintenance tool.

10. The computer implemented method of claim 7, wherein the storing step comprises:

receiving the aircraft software part from a supplier to form a received aircraft software part;

processing the aircraft software part to from a processed aircraft software part; and

storing the processed aircraft software part in the library.

11. The computer implemented method of claim 7 further comprising:

sending a command to the onboard electronic distribution system from the library through the proxy server to download data from the aircraft; and

receiving the data at the library through the proxy server in response to sending the command.

12. The computer implemented method of claim 7 further comprising:

sending the aircraft software part from the library to a software maintenance tool on a portable computer;

moving the portable computer with the aircraft software part to the aircraft;

establishing a communications link between the software maintenance tool with the onboard electronic distribution system on the aircraft after moving the portable computer to the aircraft to form an established communications link; and

sending the aircraft software part from the software maintenance tool to the onboard electronic distribution system through the established communications link.