Rotorcraft Joystick Embedded Rod Force Sensing

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Solution Overview

Problem

Existing electric flight control mechanisms for rotorcraft are structurally complex, prone to mechanical issues like seizure of moving parts and operational clearances, and are costly to maintain, while also lacking the tactile feedback provided by mechanical systems.

Innovation Solution

A simplified electric flight control mechanism featuring a joystick articulated on a support with a rod embedded in the support, utilizing intrinsic bending resistance for force sensing and limited mobility mounting, which generates resisting forces to provide tactile feedback and is designed to reduce the number of components and structural complexity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a simplified electric flight control mechanism with embedded rod is used, then device complexity is reduced, but reliability may worsen due to potential seizure of moving parts

Engineering Contradiction:
Improvestructural complexityVSAvoidoperational reliability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The patent replaces complex mechanical linkages with an electric flight control system where a simplified rod structure is actuated by electric motors. The rod can tilt multidirectionally with fewer mechanical constraints, and control signals are transmitted electrically rather than through complex mechanical kinematic chains, reducing the number of moving parts that can seize.

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

Solution Approach 2:

The simplified rod structure serves multiple functions: it acts as both the mechanical support structure and the sensor element for detecting pilot input. The same rod that provides structural support also detects tilt movements through integrated sensors, eliminating the need for separate mechanical linkages and sensors, thereby reducing complexity while maintaining reliability through functional integration.

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

2Ease of operation

If traditional mechanical flight control transmission is used, then tactile feedback is provided, but device complexity and maintenance costs increase

Engineering Contradiction:
Improvetactile feedbackVSAvoidmechanical structure
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The patent replaces traditional mechanical flight control transmission systems with an electric actuation system. Electric motors provide the necessary forces to move the rod, and force sensors detect pilot input, converting mechanical pressure into electrical signals. This substitution eliminates complex mechanical linkages while maintaining tactile feedback through the force sensors that detect pilot pressure on the control stick.

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

Solution Approach 2:

The patent introduces force sensors as intermediary elements between the pilot's manual input and the electronic flight control system. These sensors detect the mechanical pressure applied by the pilot on the control stick and convert it into electrical signals, serving as a mediator that preserves the tactile feedback loop while eliminating the need for complex mechanical transmission components.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Adaptability or versatility

If multiple moving parts are used in flight control mechanism, then adaptability is improved, but ease of repair worsens due to increased maintenance requirements

Engineering Contradiction:
Improvecontrol rangeVSAvoidmaintenance costs
Core Design Contradiction:
Adaptability or versatilityVSEase of repair

Solution Approach 1:

The patent employs a dynamic control system where the rod can tilt multidirectionally with continuous range of motion in multiple axes. Electric motors provide dynamic actuation capability, allowing the system to adapt to various flight control requirements without requiring multiple discrete mechanical linkages. The electric system can be reprogrammed to provide different control characteristics, maintaining adaptability while reducing mechanical complexity.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent replaces numerous mechanical moving parts with an electric actuation system centered around a single tiltable rod. Electric motors and electronic control systems provide the necessary adaptability and range of motion that would otherwise require complex mechanical linkages. This substitution dramatically reduces the number of components requiring maintenance while preserving full control capability through electronic programming and control algorithms.

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

The solution enhances operational reliability and precision while reducing maintenance costs by simplifying the structural organization and allowing for easier installation and maintenance of ancillary control devices, while maintaining the ability to provide tactile feedback to the pilot.

Implementation Method 1

utilizing intrinsic bending resistance for force sensing and limited mobility mounting, which generates resisting forces to provide tactile feedback

Methodology Applied
Scientific EffectBending resistance: Elasticity

Data Source

PatentEP2810871B1Flight control handle for a rotorcraft tiltably mounted on a mounting by recessing a flexible rod
Publication Date: 2020.11.11 EUROCOPTER FRANCE SA
  • EP2810871B1 patent drawingFigure 1~3

AI summary

The present invention relates to an electric flight control mechanism for a rotorcraft, comprising a joystick (1) articulated in multidirectional tilt on a support (2), means for detecting the tilted position of the joystick (1) generating electrical signals (7), and means for sensing forces providing the pilot with a feeling of resistance forces (12) to the tilting of the joystick (1). The joystick (1) has a rod (13) embedded at its distal end in the support (2), thus providing the joystick (1) with a movable mounting on the support (2). Tilting the joystick (1) causes the rod (13) to flex from its anchoring zone (16) in the support (2), the resistance to bending deformation of the rod (13) developing the resistance forces (12) and being measured to generate the electrical signals (7).