Active Linear Throttle Force Sensing for Accurate Haptic Control

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Solution Overview

Problem

Existing active throttles in aircraft lack accurate and reliable detection of the force applied by pilots, leading to potential errors in haptic feedback and overall control accuracy.

Innovation Solution

The implementation of a parameter sensing mechanism, such as force and torque detectors, positioned close to the point of force application, combined with a controller that predicts and corrects control data based on haptic feedback models, ensures precise detection and adaptation of the throttle to aircraft conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If parameter sensing mechanisms are positioned close to the point of force application, then measurement precision is improved, but device complexity increases

Engineering Contradiction:
Improveforce detection accuracyVSAvoidsensor placement complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent applies local quality by positioning parameter sensing mechanisms (force detectors, torque detectors) specifically at or near the point where force is applied to the throttle. This localized sensing arrangement ensures that measurements are taken at the most relevant location, maximizing measurement precision without requiring complex system-wide sensor networks. The sensing mechanism is strategically placed to directly detect the force applied by the pilot, providing accurate local measurements.

Inventive Principle:
Principle #3Local quality

2Ease of operation

If haptic feedback is provided to the pilot, then ease of operation is improved, but device complexity increases

Engineering Contradiction:
Improvepilot control easeVSAvoidthrottle assembly complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The patent implements feedback by incorporating actuators that provide haptic feedback to the pilot based on sensed throttle parameters and aircraft conditions. The control system processes force detection data and generates appropriate haptic responses through the actuator, creating a closed-loop feedback system. This allows the pilot to receive tactile information about engine response and aircraft state, improving control ease while managing complexity through integrated control logic.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The active throttle assembly provides self-service by automatically adjusting throttle position and providing haptic feedback without requiring constant manual intervention from the pilot. The system uses sensed parameters to autonomously modulate throttle response, reducing pilot workload while maintaining precise control. The actuator system serves itself by using feedback from the sensing mechanisms to automatically correct or augment pilot inputs.

Inventive Principle:
Principle #25Self-service

3Adaptability or versatility

If direct mechanical connection is replaced by electrical connection, then adaptability is improved, but measurement precision deteriorates

Engineering Contradiction:
Improvethrottle control adaptabilityVSAvoidforce sensing accuracy
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The patent applies mechanics substitution by replacing direct mechanical linkages between the throttle and engine with an electrical control system. The physical connection is substituted with electronic sensors, controllers, and actuators that communicate through electrical signals. This allows greater adaptability and programmability while maintaining measurement precision through careful selection and placement of force sensing mechanisms that directly detect pilot input forces.

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

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enhances the accuracy and reliability of force detection, reducing errors and improving the pilot's control of the throttle, thereby enhancing operational safety and efficiency.

Implementation Method 1

determining a linear movement caused by the linearly moveable grip from the received parameter data; transducing the linear movement into a current value

Methodology Applied
Scientific EffectLinear transduction:

Data Source

PatentEP4644254A1Active linear throttle
Publication Date: 2025.11.05 BAE SYSTEMS PLC
  • EP4644254A1 patent drawingFigure 1
  • EP4644254A1 patent drawingFigure 2
  • EP4644254A1 patent drawingFigure 3

AI summary

The present invention relates to a method for controlling an active linear throttle assembly. The method comprises receiving parameter data from a parameter sensing mechanism for a linearly moveable grip; determining a linear movement caused by the linearly moveable grip from the received parameter data; transducing the linear movement into a current value; and outputting control data based on the current value to control the actuator.