Aircraft Takeoff Velocity Control Using Real-Time Runway Data

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current aircraft flight management systems face challenges in accurately analyzing and optimizing the takeoff sequence due to the complexity of variables such as weather, aircraft weight, and runway conditions, which can lead to potential safety issues if not properly accounted for.

Innovation Solution

The system employs real-time data from sensors to calculate and compare actual and reference velocities, adjusting operational variables like thrust and flap settings to ensure the takeoff sequence aligns with predetermined safety parameters, and includes features for automatic abort or recalculations to maintain safety.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If real-time sensor data and complex calculations are implemented to improve takeoff sequence analysis accuracy, then measurement precision and reliability are improved, but device complexity increases

Engineering Contradiction:
Improvetakeoff velocity analysis accuracyVSAvoidflight management system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system pre-calculates and stores takeoff velocity data in a lookup table before flight operations. During actual takeoff, the system simply retrieves pre-computed velocity values based on current flight conditions rather than performing complex real-time calculations, thereby maintaining high measurement precision while reducing computational complexity and processing time

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system creates a simplified model by storing pre-computed takeoff velocity data in a lookup table that replicates the results of complex aerodynamic calculations. This copy of the velocity data can be quickly accessed and compared with actual sensor measurements without requiring the full computational machinery of the original complex models

Inventive Principle:
Principle #26Copying

2Reliability

If multiple real-time variables are monitored and compared to ensure safety, then reliability is improved, but the difficulty of detecting and measuring increases

Engineering Contradiction:
Improvetakeoff sequence safetyVSAvoidreal-time variable monitoring complexity
Core Design Contradiction:
ReliabilityVSDifficulty of detecting and measuring

Solution Approach 1:

The system pre-establishes the relationship between multiple flight variables and takeoff velocity in the lookup table. During operation, it only needs to monitor current flight conditions and retrieve the corresponding pre-analyzed velocity data, avoiding the need to perform complex real-time analysis of multiple variable interactions while maintaining comprehensive safety monitoring

Inventive Principle:
Principle #10Preliminary action

3Productivity

If automatic adjustment of operational variables is implemented to maintain optimal velocity, then productivity is improved, but device complexity increases

Engineering Contradiction:
Improvetakeoff sequence efficiencyVSAvoidautomatic control system complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The system automatically compares actual sensor measurements with pre-stored lookup table values and adjusts operational variables without requiring complex real-time optimization algorithms. The pre-computed lookup table provides the reference data needed for automatic adjustment, enabling the system to self-regulate takeoff performance efficiently

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The optimal operational parameters and their relationships are pre-calculated and stored in the lookup table. During takeoff, the system simply retrieves these pre-determined optimal settings based on current conditions and applies them, avoiding complex real-time optimization while maintaining high productivity

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS11837099B2Aircraft flight management system
Publication Date: 2023.12.05 GE AVIATION SYST LTD
  • US11837099B2 patent drawing
  • US11837099B2 patent drawing
  • US11837099B2 patent drawing

AI summary

An apparatus and method for an aircraft flight management system configured to analyze a takeoff sequence for an aircraft, the aircraft slight management system comprising a memory storing runway information associated with the runway from which the aircraft will depart, one or more inputs configured to receive variables comprising real-time aircraft variables and real-time condition variables that influence an actual velocity of the aircraft, sensors for sensing the actual velocity of the aircraft; and a processor configured to compare a real-time takeoff value to a takeoff requirement value.