Software Aircraft Part Installation System

• US 20160098259A1
• Filed: 10/02/2014
• Published: 04/07/2016
• Est. Priority Date: 10/02/2014
• Status: Abandoned Application

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Mitchell, James Edward
• Application Number:
  US14/504,482
• Publication Number:
  US 20160098259A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64F 5/00 Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
• CPC Class Codes: G06F 8/61 Installation

Abstract

A method and apparatus for installing a software aircraft part in an aircraft. A command to install the software aircraft part is received. A determination is made as to whether the software aircraft part is present in the aircraft. A third party verifies that the software aircraft part is to be installed when the software aircraft part is present in the aircraft. The third party is in a location remote to the aircraft. An installation of the software aircraft part in the aircraft is performed when the software aircraft part is present in the aircraft and the software aircraft part is verified for the installation. The aircraft operates with the software aircraft part installed in the aircraft.

Claims

1. A method for installing a software aircraft part in an aircraft, the method comprising:

receiving a command to install the software aircraft part;

determining whether the software aircraft part is present in the aircraft;

verifying with a third party that the software aircraft part is to be installed when the software aircraft part is present in the aircraft, wherein the third party is in a location remote to the aircraft; and

performing an installation of the software aircraft part in the aircraft when the software aircraft part is present in the aircraft and the software aircraft part is verified for the installation, wherein the aircraft operates with the software aircraft part installed in the aircraft.

2. The method of claim 1 further comprising:

verifying whether the command is authentic.

3. The method of claim 1, wherein the verifying step comprises:

sending a verification message to the third party to confirm the command to install the software aircraft part; and

receiving a response to the verification message from the third party, wherein the response indicates whether the command to install the software aircraft part should be followed.

4. The method of claim 3, wherein the verification message includes an identification of a current version of the software aircraft part installed on the aircraft and an identification of a new version of the software aircraft part to be installed on the aircraft.

5. The method of claim 1 further comprising:

sending a confirmation message to the third party indicating that the software aircraft part has been installed after installing the software aircraft part in the aircraft.

6. The method of claim 5, wherein the confirmation message includes metadata generated in the aircraft that describes at least one of a version of the software aircraft part that was installed, a log of the installation of the software aircraft part, and a use of the software aircraft part installed in the aircraft.

7. The method of claim 1, wherein the installing step comprises:

setting a schedule to install the software aircraft part; and

installing the software aircraft part based on the schedule.

8. The method of claim 1 further comprising:

proposing an update of the software aircraft part to an operator of the aircraft; and

setting a schedule to update a group of aircraft including the aircraft when an approval is received from the operator of the aircraft.

9. The method of claim 1, wherein the installing step comprises:

determining whether the software aircraft part present in the aircraft is valid based on at least one of a cyclic redundancy check value for the software aircraft part, a certificate of authentication for the software aircraft part, a compatibility of a version of the software aircraft part with other aircraft parts in the aircraft, or an amount of time the software aircraft part has been in the aircraft; and

installing the software aircraft part when the software aircraft part is identified as valid.

10. The method of claim 9 further comprising:

adding an indication to metadata generated in the aircraft indicating that the command received to install the software aircraft part in the aircraft is not performed when the software aircraft part has been identified as invalid.

11. A method for installing a software aircraft part in an aircraft, the method comprising:

sending the software aircraft part to the aircraft;

sending a command to the aircraft to install the software aircraft part;

receiving a request from the aircraft to verify an installation of the software aircraft part;

determining whether the software aircraft part should be installed based on the request; and

sending a confirmation that the software aircraft part should be installed when the installation of the software aircraft part is verified, wherein the software aircraft part is installed on the aircraft when the confirmation is received by the aircraft.

12. The method of claim 11, wherein the determining step is performed by an operator for a third party selected from at least one of a program running on a computer system or a human operator.

13. An apparatus comprising:

a part installer that receives a command to install a software aircraft part;

determines whether the software aircraft part is present in an aircraft;

verifies with a third party that the software aircraft part is to be installed when the software aircraft part is present in the aircraft in which the third party is in a location remote to the aircraft; and

installs the software aircraft part in the aircraft when the software aircraft part is present in the aircraft and the software aircraft part is verified for installation, wherein the aircraft operates with the software aircraft part installed in the aircraft.

14. The apparatus of claim 13 further comprising:

a computer system in the aircraft, wherein the part installer is located in the computer system.

15. The apparatus of claim 13 further comprising:

verifying whether the command is authentic.

16. The apparatus of claim 13, wherein in verifying with the third party that the software aircraft part is to be installed, the part installer sends a message to the third party to confirm the command to install the software aircraft part;

and receives a response to the message from the third party, wherein the response indicates whether the command to install the software aircraft part should be followed.

17. The apparatus of claim 16, wherein the message includes an identification of a current version of the software aircraft part installed on the aircraft and an identification of a new version of the software aircraft part to be installed on the aircraft.

18. The apparatus of claim 17, wherein the message includes metadata generated in the aircraft that describes at least one of a version of the software aircraft part that was installed, a log of the installation of the software aircraft part, and a use of the software aircraft part installed in the aircraft.

19. The apparatus of claim 13, wherein the part installer sends a message to the third party indicating that the software aircraft part has been installed after installing the software aircraft part in the aircraft.

20. The apparatus of claim 13, wherein the part installer installs the software aircraft part in the aircraft when the software aircraft part is present in the aircraft and the software aircraft part is verified for installation, the part installer sets a schedule to install the software aircraft part and installs the software aircraft part based on the schedule.