Aircraft Software Configuration Selection and Installation

US2016154642A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016154642-A1
Application numberUS-201313755804-A
CountryUS
Kind codeA1
Filing dateJan 31, 2013
Priority dateAug 14, 2012
Publication dateJun 2, 2016
Grant date

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

A system and method for selecting and installing a software configuration for an aircraft. A configuration tool is configured to display configuration options for aircraft software to a user and to receive configuration selections for the aircraft software from the user. The configuration selections identify selected ones of the configuration options. The configuration tool is further configured to send the configuration selections to a software installer for installation on the aircraft of the aircraft software identified by the configuration selections.

First claim

Opening claim text (preview).

1 . An apparatuses configured to execute instructions via a processor unit that comprises: a configuration tool connected to: a platform manufacturer, a platform operator, and a part supplier, such that the configuration tool comprises an access controller, a user interface generator, a configuration selector, an installation module, a report generator, and a notification generator, and configured such that in operation, the configuration tool: displays configuration options for a part for the platform on a user interface; receives a configuration selection for the part, wherein the configuration selection identifies one of the configuration options; and sends the configuration selection to an installer for installation, of the part identified by the configuration selection, on the platform. 2 . The apparatus of claim 1 , further comprising: the configuration tool configured such that in operation, the configuration options display via an Internet and receive the configuration selection via the Internet; and the part is software. 3 . The apparatus of claim 1 , wherein the configuration tool is further configured, such that in operation the installation module receives an installation authorization to install the part, identified by the configuration selection, on the platform. 4 . The apparatus of claim 3 , wherein the configuration tool is further configured such that in operation the notification generator sends a notification to the installer automatically in response to receipt of the installation authorization in the installation module. 5 . The apparatus of claim 1 , wherein the configuration tool is further configured such that in operation the configuration tool displays, installation instructions to the installer, wherein the installation instructions identify the part identified by the configuration selection. 6 . The apparatus of claim 1 , wherein the configuration tool is further configured such that in operation the configuration tool receives, from the installer, an installation confirmation that indicates the part identified by the configuration selection as being installed on the platform. 7 . The apparatus of claim 6 , wherein the configuration tool is further configured such that in operation the report generator generates, a configuration report identifying a configuration of the platform that comprises the configuration selection installed on the platform. 8 . The apparatus of claim 1 , further comprising the platform being in production, component and subassembly manufacturing. 9 . The apparatus of claim 1 , wherein the part comprises a software aircraft part. 10 . A method for selecting a configuration for a platform, comprising: receiving, in a configuration tool connected to: a network, a platform manufacturer, a platform operator, and a part supplier, such that the configuration tool comprises an access controller, a user interface generator, a configuration selector, and an installation module, via the network, configuration options; the access controller receiving, via the network, a request for access and an identification of the platform; transmitting, via the configuration selector, to a user interface, configuration options that comprise identities of parts received from a group that comprises the platform manufacturer, the platform operator, and the part supplier; receiving, in the configuration selector, a configuration selection from among the configuration options; receiving, in the configuration selector, via the network, an installation authorization for a part in the configuration selection; transmitting, from the installation module to an installer via the network, an installation instruction that comprises an identity of the part; and receiving, in the installation module, an installation confirmation of part installation in the platform in accordance with the installation instruction. 11 . The method of claim 10 , wherein the network comprises an Internet. 12 . The method of claim 10 , further comprising the configuration selection comprising: an application group of software aircraft parts to configure from a list of application groups of software aircraft parts displayed by the configuration tool; and a software aircraft part to configure from a list of software aircraft parts in the application group of software aircraft parts displayed by the configuration tool. 13 . The method of claim 10 , further comprising the configuration selection comprising: a software aircraft part number from a list of software aircraft part numbers for the aircraft software to configure. 14 . The method of claim 10 further comprising: the instruction being for installation, on an aircraft, of aircraft software. 15 . A method for installing software on an aircraft, the method comprising: connecting a configuration tool, comprising a processor unit, to a network, an aircraft manufacturer, an aircraft operator, and a software supplier, the configuration tool comprising: an access controller, a user interface generator, a configuration selector, and an installation module; receiving, in the configuration tool via the network, a configurable software and configurable options for the configurable software; the access controller receiving, via the network, a request for access and an identification of the aircraft; transmitting, via the configuration selector, to a user interface, configuration options that comprise identities of parts received from a group that comprises the aircraft manufacturer, the aircraft operator, and the software supplier; receiving, in the configuration selector, a configuration selection from among the configuration options; displaying, by the installation module via the network, installation instructions from the configuration tool for installing aircraft software on the aircraft, wherein the installation instructions identify selected aircraft software selected from configuration options for the aircraft software displayed by the configuration tool; receiving, in the installation module, an installation confirmation of part installation in the aircraft in accordance with the installation instruction; transmitting, via the network from a report generator in the configuration tool, an installation report and a configuration report that comprises identifying configurable software on the aircraft configured in accordance with the configuration selection; and delivering to the user interface, from a notification generator in the configuration tool, in response to an action occurring in the configuration tool, a notification. 16 . The method of claim 15 , further comprising the notification indicating an authorization to install the selected aircraft software on the aircraft. 17 . The method of claim 15 , further comprising the network comprising an Internet. 18 . The method of claim 15 , a further comprising the configuration tool transmitting the notification, installation instructions, and selected aircraft software via the network to a software installer comprising a portable installation device. 19 . The method of claim 18 further comprising: loading the selected aircraft software in the portable installation device; and installing the selected aircraft software on the aircraft from the portable installation device. 20 . The method of claim 19 further comprising: receiving via the network, the installation confirmation in the configuration tool, wherein the installation confirmation indicates that the selecte

Assignees

Inventors

Classifications

  • G06F8/61Primary

    Installation · CPC title

  • Version control (security arrangements therefor G06F21/57); Configuration management · CPC title

  • specially adapted for proprietary or special-purpose networking environments, e.g. medical networks, sensor networks, networks in vehicles or remote metering networks · CPC title

  • G06F8/65Primary

    Updates (security arrangements therefor G06F21/57) · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US2016154642A1 cover?
A system and method for selecting and installing a software configuration for an aircraft. A configuration tool is configured to display configuration options for aircraft software to a user and to receive configuration selections for the aircraft software from the user. The configuration selections identify selected ones of the configuration options. The configuration tool is further configure…
Who is the assignee on this patent?
Boeing Co, Boeing Co
What technology area does this patent fall under?
Primary CPC classification G06F8/61. Mapped technology areas include Physics.
When was this patent published?
Publication date Thu Jun 02 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).