Aircraft Cargo Roller Panel Load Cell Integration

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current aircraft cargo loading systems lack accurate verification of cargo weight and center of gravity, leading to potential safety issues and cost discrepancies due to under-reporting of cargo weights and changes in cargo configuration during flight.

Innovation Solution

An aircraft cargo roller panel equipped with load cells and motive devices, which generates signals indicative of cargo load and determines weight and center of gravity, ensuring compliance with reported parameters through a controller system that alerts crew members if parameters are not met, allowing for real-time verification and adjustment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If manual weight recording is used in the warehouse, then loading process is simple and fast, but cargo weight and center of gravity cannot be verified accurately during flight

Engineering Contradiction:
Improvecargo weight verificationVSAvoidloading system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The load cells are installed on the roller panel beforehand to automatically capture cargo weight and center of gravity data during the loading process itself, eliminating the need for separate verification steps and manual recording procedures

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The manual weight recording process is replaced with an automated electronic measurement system using load cells that convert mechanical force into electrical signals for digital processing and verification

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

2Reliability

If cargo weight is not verified, then loading process is fast, but safety risks and cost discrepancies occur due to under-reporting

Engineering Contradiction:
Improvecargo loading safetyVSAvoidloading speed
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system provides immediate feedback by comparing measured cargo parameters against the load and trim sheet data, automatically alerting crew members to any discrepancies so that safety verification does not slow down the loading process

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The roller panel system automatically performs verification functions without requiring additional manual intervention or separate verification equipment, making safety checking an inherent part of the loading process

Inventive Principle:
Principle #25Self-service

3Measurement precision

If multiple load cells are installed on the roller panel, then cargo parameters can be determined accurately, but device complexity and cost increase

Engineering Contradiction:
Improvecenter of gravity determinationVSAvoidroller panel structure
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The roller panel serves multiple functions simultaneously: it facilitates cargo loading through its roller mechanism while also serving as the mounting structure for load cells, making the panel itself a multi-functional measurement platform

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The load measurement function is merged with the cargo loading function by integrating load cells directly into the roller panel structure, so that the same physical structure performs both mechanical and measurement roles

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS11066168B2Aircraft cargo roller panel
Publication Date: 2021.07.20 THE BOEING CO
  • US11066168B2 patent drawing
  • US11066168B2 patent drawing
  • US11066168B2 patent drawing

AI summary

A method includes receiving, at a controller, a signal from each load cell of a plurality of load cells coupled to an aircraft cargo roller panel of an aircraft. Each signal is indicative of a load experienced by the load cell when cargo is on the aircraft cargo roller panel. The method also includes determining, based on the signals, a weight of the cargo, a center of gravity of the cargo, or both.