Wireless Nacelle Unit Image Boot Validation

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing systems face challenges in efficiently transferring and managing engine data from aerial vehicle electronic engine controllers to ground systems, particularly due to difficulties in data validity checks and boot processes.

Innovation Solution

A wireless communication unit is integrated with an aerial vehicle's engine, performing data validity checks on primary and secondary image index locations, and rebooting if both fail, while loading and validating images in RAM and performing cryptographic signature checks to ensure secure boot processes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of information

If automated engine data transfer is implemented, then data availability at ground system is improved, but data validity check complexity increases

Engineering Contradiction:
Improvedata availabilityVSAvoiddata validity check complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The patent performs data validity checks on primary and secondary image indexes before transferring engine data to the ground system. By conducting these checks in advance during the boot process, the system ensures data integrity is verified before transmission, resolving the contradiction between improving data availability and managing check complexity.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system implements a dual-image index architecture with primary and secondary indexes, where the secondary index serves as a backup validation mechanism. This beforehand cushioning approach ensures that if the primary index fails validation, the system can fall back to the secondary index, maintaining data availability while distributing validation complexity across multiple prepared structures.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

2Reliability

If dual image index validation is performed, then system reliability is improved, but boot process time increases

Engineering Contradiction:
Improvesystem reliabilityVSAvoidboot process time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent performs validation checks on both primary and secondary image indexes during the boot process before system operation begins. By completing these reliability checks preliminarily during startup rather than during operation, the system ensures high reliability while minimizing time loss to the critical operational phase.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system performs validation on the primary image index first, and only performs secondary index validation if the primary validation fails or is insufficient. This partial action approach maintains system reliability through dual-validation capability while reducing the average boot process time by avoiding unnecessary secondary validations when the primary index is valid.

Inventive Principle:
Principle #16Partial or excessive action

3Measurement precision

If cryptographic signature checks are implemented, then data integrity is improved, but processing complexity increases

Engineering Contradiction:
Improvedata integrity verificationVSAvoidprocessing complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent introduces cryptographic signature checks as an intermediary validation layer between the image index and the actual engine data. This intermediary mechanism provides precise data integrity verification by using cryptographic signatures to authenticate data origin and integrity, while the modular implementation keeps processing complexity manageable through standardized cryptographic operations.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS10467016B2Managing an image boot
Publication Date: 2019.11.05 GE AVIATION SYSTEMS LLC
  • US10467016B2 patent drawing
  • US10467016B2 patent drawing
  • US10467016B2 patent drawing

AI summary

One example aspect of the present disclosure is directed to a wireless communication unit configured to be located in a nacelle associated with an engine of an aerial vehicle. The wireless communication unit includes a random access memory. The wireless communication unit includes one or more processors. The one or more processors are configured to perform a first data validity check on a first location for a primary index. The one or more processors are configured to perform a second data validity check on a second location for a secondary index. When the first data validity check fails and the second data validity check fails, the one or more processors are configured to reboot.