Armrest-Integrated Collective Handle for Precise Helicopter Pitch Control

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Solution Overview

Problem

Existing collective control systems in helicopters, particularly in smaller aircraft, are ergonomically inefficient and limit the precision of pitch control due to mechanical linkages and lever-based mechanisms, which can be cumbersome and restrictive in tight space constraints.

Innovation Solution

A collective control arrangement featuring a slidable collective handle within an elongate channel integrated into the pilot's armrest, allowing for ergonomic control and precise adjustment of rotor blade pitch, with optional configurations for dual-pilot setups and single-pilot operations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a traditional lever-based collective handle is used, then the control mechanism is mechanically simple, but the ergonomic comfort and precision of pitch control are reduced

Engineering Contradiction:
Improveergonomic comfortVSAvoidcontrol mechanism complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The collective handle is repositioned from a traditional vertical lever configuration to a horizontal configuration within the armrest. This dimensional change allows the pilot to operate the collective with a more natural arm position, improving ergonomics while the channel guides the motion to maintain mechanical efficiency

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The elongate channel acts as an intermediary constraint that guides the collective handle's motion. It provides precise directional guidance while allowing smooth movement, bridging the gap between the pilot's ergonomic needs and the mechanical requirements of the control system

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If mechanical linkages are used to transmit collective handle movement, then the system is mechanically direct, but the precision of pitch control is limited

Engineering Contradiction:
Improvepitch control precisionVSAvoidmechanical linkage complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent replaces traditional mechanical linkages with an electronic signalling system. Sensors detect the position and movement of the collective handle within the channel, and electronic signals transmit this data to the flight control system, enabling more precise pitch control while reducing mechanical complexity

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

Solution Approach 2:

The system creates an electronic copy of the collective handle's physical position and movement characteristics. This electronic representation allows for precise measurement and control without the limitations of direct mechanical transmission

Inventive Principle:
Principle #26Copying

3Adaptability or versatility

If the collective handle is positioned traditionally to the left of the pilot's seat, then the control layout is conventional, but spatial constraints in small aircraft are exacerbated

Engineering Contradiction:
Improvecontrol positioning flexibilityVSAvoidcockpit space
Core Design Contradiction:
Adaptability or versatilityVSArea of stationary object

Solution Approach 1:

The collective handle is merged with the armrest structure, combining two previously separate control elements into one integrated component. This consolidation eliminates the need for additional space to the left of the pilot's seat, making the control system adaptable to tight cockpit spaces in small aircraft

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentEP4200207B1Helicopter collective control apparatus
Publication Date: 2025.11.12 HILL GRP TECH LTD
  • EP4200207B1 patent drawingFigure 1a
  • EP4200207B1 patent drawingFigure 1b
  • EP4200207B1 patent drawingFigure 2

AI summary

Disclosed is a collective control arrangement for a helicopter having a plurality of rotor blades, the collective control arrangement comprising: an armrest for a pilot's seat, the armrest comprising an elongate channel; and a collective handle comprising: a first end slidably disposed in the elongate channel for coupling to one or more helicopter actuators that control collective pitch of the plurality of rotor blades; and a second end for gripping by a pilot. Advantageously the armrest comprises an elbow support portion configured to be located backwards of the hollow when the armrest is installed in the helicopter.