Systems and methods for avionics software delivery

• US 20060229772A1
• Filed: 04/08/2005
• Published: 10/12/2006
• Est. Priority Date: 04/08/2005
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: McClary, Charles R.
• Application Number:
  US11/101,897
• Publication Number:
  US 20060229772A1
• Time in Patent Office: Days
• US Class Current: 701/3
• CPC Class Codes: G06F 21/629 to features or functions of an application
• CPC Class Codes: G06F 8/64 Retargetable
• CPC Class Codes: G06F 8/65 Updates security arrangements therefor G06F21/57

Abstract

Systems and methods delivering avionics software are disclosed. One method comprises equipping one or more aircraft with a computer hardware unit adapted to implement time and memory space partitioning of one or more software applications; assigning a hardware part number to the computer hardware unit; installing one or more software applications into a memory of the computer hardware unit using one or more integrity verification protocols, wherein one or more features of the one or more software applications are enabled; and assigning a software part number to a software application of the one or more software applications based on the one or more features of the one or more software applications that are enabled.

Claims

1. A software application for an on-aircraft computing system, wherein the computing system is adapted to execute one or more time and memory space partitioned software applications, the software application comprising:

a plurality of features;

wherein one or more of the plurality of features are disabled until a software key is provided to the computing system; and

a software part number, wherein the software part number identifies which of the plurality of features are enabled.

2. A system for delivering on-aircraft avionics software applications, the system comprising:

a computing system, wherein the computing system is adapted to execute one or more software applications, wherein each software application is time and memory space partitioned, wherein each software application includes one or more features;

one or more memories adapted to store the one or more software applications;

one or more delivery medium adapted to store a software code including one or more of a software application, a software upgrade for the one or more software applications, and a software key; and

one or more on-aircraft data transfer systems adapted to receive the software code from the one or more delivery systems and store the software code in the one or more memories;

wherein when the software code includes one or both of a software application and a software upgrade for the one or more software applications, the computing system and the data transfer system are further adapted to implement one or more integrity verification protocols to verify that the software code is loaded into the one or more memories correctly;

wherein when the software code is a software key, the computing system is further adapted to enable one or more features of the one or more software applications;

wherein each software application includes a software part number that identifies enabled features of the software application and software upgrades made to the software application.

3. The system of claim 2, wherein the one or more delivery medium further comprises one or more of punch cards, magnetic disk, magnetic tape, an optical disk, flash read only memory (ROM), non-volatile ROM, programmable ROM (PROM), erasable-programmable ROM (E-PROM), random access memory (RAM), electronic transmission via wire, a wireless communication link, and an optical cable.

4. The system of claim 2, wherein the computing system is further adapted to output the software part number of one or more of the one or more software applications.

5. The system of claim 2, wherein the one or more data transfer systems further comprises an input device, wherein when the software key is entered on the input device, the computing system is further adapted to enable one or more features of the one or more software applications.

6. The system of claim 2, wherein the one or more integrity verification protocols includes the ARNIC 615 protocol.

7. A method for delivering avionics software, the method comprising:

equipping one or more aircraft with a computer hardware unit adapted to implement time and memory space partitioning of one or more software applications;

assigning a hardware part number to the computer hardware unit;

installing one or more software applications into a memory of the computer hardware unit using one or more integrity verification protocols, wherein one or more features of the one or more software applications are enabled; and

assigning a software part number to a software application of the one or more software applications based on the one or more features of the one or more software applications that are enabled.

8. The method of claim 7, wherein one or more features of the one or more software applications are enabled based on an initial purchase price for the computer hardware unit.

9. The method of claim 7, wherein when one or more features of the one or more software applications are disabled, the method further comprises:

selling one or more additional features of the one or more software applications; and

providing a key to enable one or more features of the one or more software applications that are disabled.

10. The method of claim 7, wherein the one or more integrity verification protocols includes the ARNIC 615 protocol.

11. The method of claim 7 further comprising:

installing one or more updates to the one or more software applications using one or more integrity verification protocols.

12. The method of claim 11, wherein the one or more integrity verification protocols includes the ARNIC 615 protocol.

13. The method of claim 7 further comprising:

verifying a hardware unit is certified for use in an aircraft based on the hardware part number and the software part number.

14. The method of claim 7 further comprising:

interrogating the computer hardware unit to obtain the software part number of one or more of the one or more software applications; and

outputing the software part number of one or more of the one or more software applications.

15. A system for delivering on-aircraft avionics software applications, the system comprising:

means for executing one or more software applications, wherein each software application of the one or more software applications is time and memory space partitioned, wherein each software application of the one or more software applications includes one or more features;

memory means adapted to store the one or more software applications;

means for selectively enabling one or more of the one or more features of the one or more software applications, wherein each software application is adapted with a software part number that identifies the one or more enabled features;

means for delivering software code, wherein the software code includes one or more of a software application, a software upgrade for the one or more software applications, and a software key; and

means for receiving the software code, wherein the means for receiving the software code is adapted to implement one or more integrity verification protocols to verify that the software code is received correctly.

16. The system of claim 15, wherein the means for delivering software code further comprises one or more of a magnetic data storage means, an optical data storage means, a wire based data communications means, and a wireless data communication means.

17. The system of claim 15, further comprising:

means for enabling one or more of the one or more features of the one or more software applications based on the software key.

18. The system of claim 15, further comprising:

means for updating one or more of the one or more software applications based on the software patch for the one or more software applications.

19. The system of claim 15, further comprising:

means for outputting the software part number of one or more of the one or more software applications.

20. The system of claim 15, further comprising:

means for verifying certification of the system in an aircraft based on a hardware part number and the software part number for each of the one or more software applications.