Aircraft Takeoff Performance Alert for Rotation Speed Prediction

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Solution Overview

Problem

During aircraft takeoff, pilots face time-sensitive decisions regarding whether to continue or abort takeoff due to less than optimal conditions, with existing systems failing to effectively detect deviations in performance that warrant rejection.

Innovation Solution

A system that determines takeoff rotation speed and rotation time based on initial data, predicts aircraft speed during the takeoff roll, and generates a takeoff performance alert if the disparity between actual and predicted speeds exceeds a threshold, using All-Engine performance parameters and real-time measurements to assess conditions such as go distance and tire limit speed.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If real-time speed monitoring and prediction systems are implemented during takeoff roll, then detection precision of performance deviations is improved, but device complexity increases

Engineering Contradiction:
Improvedetection precisionVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system pre-calculates expected takeoff performance parameters (rotation speed, go distance, tire limit speed) before takeoff based on aircraft weight, environmental conditions, and runway characteristics. During takeoff roll, real-time speed measurements are compared against these pre-established benchmarks, enabling rapid deviation detection without complex real-time modeling

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system continuously monitors actual takeoff roll speed and compares it against predicted performance curves. When deviations exceed predetermined thresholds, the system generates alerts to pilots. This closed-loop feedback mechanism uses simple threshold-based logic rather than complex algorithms, balancing detection precision with system simplicity

Inventive Principle:
Principle #23Feedback

2Reliability

If continuous data collection and analysis during takeoff roll is performed, then reliability of takeoff decision is improved, but loss of time for pilot decision-making increases

Engineering Contradiction:
ImprovereliabilityVSAvoiddecision time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The system focuses monitoring efforts on critical phases of takeoff roll where performance deviations are most indicative of problems. By concentrating analysis on key speed thresholds and time intervals rather than continuously processing all data points, the system maintains high reliability while minimizing processing time and enabling faster pilot response

Inventive Principle:
Principle #21Skipping (Rushing through)

Solution Approach 2:

The system implements monitoring at specific critical checkpoints during takeoff roll (e.g., rotation phase, V1 speed achievement, go distance milestones) rather than attempting to analyze every moment continuously. This partial monitoring approach captures sufficient information for reliable decision-making while reducing overall processing time and preserving pilot decision-making speed

Inventive Principle:
Principle #16Partial or excessive action

Data Source

PatentUS11846944B2Takeoff performance alert
Publication Date: 2023.12.19 THE BOEING CO
  • US11846944B2 patent drawing
  • US11846944B2 patent drawing
  • US11846944B2 patent drawing

AI summary

An aircraft includes at least one line replaceable unit (LRU) configured to determine, based on initial data collected prior to a takeoff roll of the aircraft, a takeoff rotation speed of the aircraft and a rotation time associated with the takeoff rotation speed. The LRU is configured to determine, during the takeoff roll and prior to the rotation time, a predicted speed of the aircraft at the rotation time. The predicted speed is at least partially based on data collected during the takeoff roll. The LRU is also configured to determine whether an alert condition is satisfied at least partially based on whether a disparity between the takeoff rotation speed and the predicted speed exceeds a rotation speed disparity threshold and to generate a takeoff performance alert in response to the alert condition being satisfied.