IFE Component Simulator for In-Flight Entertainment Testing

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Solution Overview

Problem

Current In-Flight Entertainment (IFE) system testing methodologies are costly and inefficient, requiring the assembly of all airplane units in a lab for testing, leading to high mobilization costs, unit damage, and late availability of IFE units, which delays the discovery of major issues.

Innovation Solution

A system and method that replicates IFE components with simulator units, allowing for functional testing without the need for all seat end units, using a simulator server with a processor to connect to an IFE network and execute scenario instructions, reducing the number of required units by up to 75% and enabling portable, cost-effective testing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If all airplane units are assembled in a lab for testing purposes, then system-level testing can be performed, but costs related to unit mobilization and facility resources increase substantially

Engineering Contradiction:
Improvesystem-level testing capabilityVSAvoidnumber of units required for testing
Core Design Contradiction:
ReliabilityVSQuantity of substance

Solution Approach 1:

The patent creates virtual copies of physical IFE units through software simulations. These digital twins replicate the functional behavior of actual seat end units, distribution units, and head end units, allowing comprehensive system-level testing without requiring all physical units to be present in the lab. The virtual models can be instantiated on standard computing hardware, dramatically reducing the quantity of physical units needed.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The patent replaces the mechanical/physical assembly of units with a software-based simulation system. Instead of physically assembling and connecting actual IFE units in a lab environment, the system uses software models that run on servers and communicate through simulated networks, substituting the physical testing infrastructure with a virtual one.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Reliability

If all airplane units are assembled in a lab for testing purposes, then system-level testing can be performed, but cash advance and labor intensive activity increase

Engineering Contradiction:
Improvesystem-level testing capabilityVSAvoidtesting setup complexity
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent creates virtual copies of physical IFE units through software simulations. These digital twins replicate the functional behavior of actual seat end units, distribution units, and head end units, allowing comprehensive system-level testing without requiring all physical units to be present in the lab. The virtual models can be instantiated on standard computing hardware, dramatically reducing the quantity of physical units needed.

Inventive Principle:
Principle #26Copying

Solution Approach 2:

The patent changes the state of the testing system from physical to virtual. By transforming the testing environment into a software-based simulation, the system eliminates the need for physical assembly, reducing both cash advance requirements and labor-intensive activities. The simulation can be configured and modified through software parameters rather than physical reassembly.

Inventive Principle:
Principle #35Parameter changes

3Loss of time

If the lab is assembled early for testing, then IFE units are available earlier for testing, but costs related to unit mobilization increase for extended period

Engineering Contradiction:
Improvetesting availability timeVSAvoidnumber of units required for testing
Core Design Contradiction:
Loss of timeVSQuantity of substance

Solution Approach 1:

The patent enables preliminary testing actions to be performed using virtual models before physical units are available. The software simulations can be configured and tested in advance, allowing system-level validation to begin earlier in the development cycle. This preliminary action with virtual copies eliminates the waiting period that would otherwise be required for physical unit assembly.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent creates virtual copies of physical IFE units through software simulations. These digital twins replicate the functional behavior of actual seat end units, distribution units, and head end units, allowing comprehensive system-level testing without requiring all physical units to be present in the lab. The virtual models can be instantiated on standard computing hardware, dramatically reducing the quantity of physical units needed.

Inventive Principle:
Principle #26Copying

4Quantity of substance

If the lab is postponed for testing, then costs related to unit mobilization are reduced, but risk of late discovery of major issues increases

Engineering Contradiction:
Improvenumber of units required for testingVSAvoidrisk of late issue discovery
Core Design Contradiction:
Quantity of substanceVSReliability

Solution Approach 1:

The patent enables preliminary testing actions to be performed using virtual models before physical units are available. The software simulations can be configured and tested in advance, allowing system-level validation to begin earlier in the development cycle. This preliminary action with virtual copies eliminates the waiting period that would otherwise be required for physical unit assembly.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent creates virtual copies of physical IFE units through software simulations. These digital twins replicate the functional behavior of actual seat end units, distribution units, and head end units, allowing comprehensive system-level testing without requiring all physical units to be present in the lab. The virtual models can be instantiated on standard computing hardware, dramatically reducing the quantity of physical units needed.

Inventive Principle:
Principle #26Copying

Data Source

PatentUS9233764B2In-flight entertainment seat end simulator
Publication Date: 2016.01.12 THALES AVIONICS INC
  • US9233764B2 patent drawing
  • US9233764B2 patent drawing
  • US9233764B2 patent drawing

AI summary

A system and method are provided for testing a vehicle entertainment (IFE) system, comprising: functionally replicating each of a plurality of IFE components selected from the group consisting of an aircraft interface unit, a content server unit, a network distribution unit, and a seat unit with a corresponding simulator unit model that simulates functions of the respective IFE component; providing each simulator unit model on a simulator server having a processor, the simulator server connecting to an IFE network that also connects at least one of actual or simulated seat units to at least one of actual or simulated content servers; providing a test controller that controls each simulator unit model; transmitting scenario information containing operation instructions to the simulator unit model; and executing the scenario information by the simulator unit model to perform operations corresponding to the operation instructions that cause the simulator unit model to communicate over the IFE network.