ABSTRACT A method and system for installing a software aircraft part on an aircraft involves receiving an independent command to initiate installation of a software aircraft part already stored on the aircraft. If the software part was already stored before the = command was received, a verification message identifying the stored software part is sent to a third party to verify that the software part should be installed. A response message, including at least an identification of the software part and an indication as to whether or not the software part should be installed, is received from the third party. When the response message indicates that the software part should be installed, the software part stored on the aircraft is installed such that the processor onboard the aircraft can execute functions provided by the software part. A confirmation message to the third party indicating whether or not the software part has been installed on the aircraft. CA 2903634 2019-12-16
SOFTWARE AIRCRAFT PART INSTALLATION SYSTEM
SYSTEME D'INSTALLATION DE LOGICIEL DE PIECE D'AERONEF
2021-04-13
Patent
Electronic Resource
English
IPC: | G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Aircraft fuselage part, aircraft and installation method
European Patent Office | 2021
|Emerald Group Publishing | 1972
A Camera Installation in a Pressurized Part 23 Aircraft
SAE Technical Papers | 2004
|