Method and system for operating a configuration platform

Patent metadata

Field	Value
Publication number	US-12561493-B2
Application number	US-202218087122-A
Country	US
Kind code	B2
Filing date	Dec 22, 2022
Priority date	Dec 29, 2017
Publication date	Feb 24, 2026
Grant date	Feb 24, 2026

Abstract

A method of and a system for propagating a configuration setting of a 3D model to other 3D models, the 3D model and the other 3Ds being part of a same 3D model category. The 5 method comprises dividing the 3D model into a first plurality of surfaces; associating to each one of the first plurality of surfaces, a unique surface identifier. For each one of the other 3D models, the method comprises dividing the one of the other 3D models into a second plurality of surfaces; establishing a correspondence; associating, for each one of the second plurality of surfaces corresponding to one of the first plurality of surfaces. The method also comprises 0 selecting the configuration setting of the 3D model; determining the unique identifier of the 3D model to which the configuration setting is to be applied; and propagating, the configuration setting to the other 3D models.

First claim

What is claimed is:

1 . A method of operating a configuration platform for real-time configuration and real-time visualization of 3D models of a monument of an aircraft cabin interior, the method comprising:
accessing, from a content management system, monument data representative of at least a portion of the monument, the monument data comprising polygon meshes suitable for rendering of the portion of the monument by a 3D real-time engine and configuration data, the configuration data comprising a kinematic sequence associated with the monument; capturing information relating to a country of certification of the aircraft; accessing, from a content management system, configuration rules data modeling internal monument configuration rules and external monument configuration rules, the internal monument configuration rules relating to an internal configuration of the monument affecting the monument itself, the external monument configuration rules relating to an external configuration of the monument affecting an environment in which the monument is to be represented, at least one subset of the configuration rules data modeling certification constraints corresponding to a country of certification of the aircraft; applying at least one subset of the configuration rules data to the monument data, resulting in generated configuration data that complies with regulations of the country of certification; determining, based on the generated configuration data, the kinematic sequence associated with the monument; and rendering a real-time visualization of the portion of the monument by the 3D real-time engine within the configuration platform.

2 . The method of claim 1 , wherein the configuration data is associated with one of a basic collector and a standard part collector, the basic collector being associated with a representation of a structure of the portion of the monument and the standard part collector being associated with a representation of accessories associated with the portion of the monument.

3 . The method of claim 2 , wherein the one of the basic collector and the standard part collector defines a configurability of the monument and a relationship of the one of the basic collector and the standard part collector with other collectors defining the monument.

4 . The method of claim 3 , wherein the one of the basic collector and the standard part collector defines at least one of an envelope collector, a zone configuration collector and a design feature collector.

5 . The method of claim 4 , wherein the envelope collector, the zone configuration collector and the design feature collector define available configuration permutations of the monument.

6 . The method of claim 5 , wherein the basic collector comprises a body defining a 3D object representative of at least a portion of the monument and wherein the body is further associated with parameters defining a property of a material surface associated with the monument, the parameters being reflective of at least one of a finish type associated with the material surface, a scale associated with the material surface, and a position associated with the material surface.

7 . The method of claim 6 , wherein the monument is associated with a position identifier allowing positioning of the monument within the aircraft cabin interior.

8 . The method of claim 7 , wherein the rendering is based on at least one of the one of the basic collector and the standard part collector, the parameters defining the property of the material and the position identifier.

9 . A computer-implemented system defining a configuration platform for real-time configuration and real-time visualization of 3D models of a monument of an aircraft cabin interior, the system comprising:
a processor; a non-transitory computer-readable medium coupled to the processor and storing instructions executable by the processor and configured to cause the processor to perform:
accessing, from a content management system, monument data representative of at least a portion of the monument, the monument data comprising polygon meshes suitable for rendering of the portion of the monument by a 3D real-time engine and configuration data, the configuration data comprising a kinematic sequence associated with the monument;
capturing information relating to a country of certification of the aircraft;
accessing, from a content management system, configuration rules data modeling internal monument configuration rules and external monument configuration rules, the internal monument configuration rules relating to an internal configuration of the monument affecting the monument itself,
the external monument configuration rules relating to an external configuration of the monument affecting an environment in which the monument is to be represented,
at least one subset of the configuration rules data modeling certification constraints corresponding to a country of certification of the aircraft;
applying at least one subset of the configuration rules data to the monument data, resulting in generated configuration data that complies with regulations of the country of certification;
determining, based on the generated configuration data, the kinematic sequence associated with the monument; and
rendering a real-time visualization of the portion of the monument by the 3D real-time engine within the configuration platform.

10 . A computer-implemented system configured to perform the method according to claim 1 .

11 . A non-transitory computer-readable medium comprising computer-executable instructions that cause a system to execute the method according to claim 1 .

Assignees

• Bombardier Inc

Inventors

• Arancibia Claudio

Classifications

• G06F2113/28

  Fuselage, exterior or interior · CPC title

• G06T19/00

  Manipulating three-dimensional [3D] models or images for computer graphics · CPC title

• G06F30/12

  characterised by design entry means specially adapted for CAD, e.g. graphical user interfaces [GUI] specially adapted for CAD · CPC title

• G06F2111/16

  Customisation or personalisation · CPC title

• G06F2111/20

  Configuration CAD, e.g. designing by assembling or positioning modules selected from libraries of predesigned modules · CPC title