Aircraft Armrest Pivot Layout for Fast, Secure Pilot Positioning

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Solution Overview

Problem

Conventional aircraft pilot seating with adjustable armrests are cumbersome due to the need for sequential adjustments and robust locking mechanisms, which are often slow and difficult to use, as they are constrained to tilt about a pivot near the elbow and require coarse adjustments to accommodate multiple operators safely and comfortably.

Innovation Solution

An adjustable armrest system where the armrest platform is hinged to an armrest support member near the wrist-end, allowing for vertical and angular adjustments independent of the elbow pivot, with telescoping struts that form triangular and quadrilateral trusses for precise locking, enabling smooth and effortless positioning relative to the side stick controller.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the armrest pivot is located near the elbow and requires sequential vertical and angular adjustments, then the locking mechanism can be robust against in-flight loads, but the adjustment process becomes cumbersome and time-consuming

Engineering Contradiction:
Improvelocking mechanism robustnessVSAvoidarmrest adjustment ease
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The patent inverts the conventional armrest adjustment approach by moving the pivot point from the elbow area to the wrist-end near the control stick. This allows the armrest to be adjusted in a single motion rather than requiring sequential vertical and angular adjustments, directly resolving the contradiction between robust locking and ease of operation

Inventive Principle:
Principle #13The other way round (Inversion)

Solution Approach 2:

The patent extracts the pivot function from the traditional elbow-mounted location and relocates it to the wrist-end attachment point. This separation allows the armrest support member to pivot independently near the seat back while the armrest platform itself pivots at the wrist-end, enabling direct positioning without sequential adjustments

Inventive Principle:
Principle #2Taking out (Extraction)

2Reliability

If robust locking mechanisms like ratchets or screw drives are used to resist in-flight acceleration and landing loads, then the armrest can be securely locked, but the adjustment mechanism becomes slow and cumbersome

Engineering Contradiction:
Improvearmrest locking securityVSAvoidadjustment speed
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent replaces complex mechanical locking systems (ratchets, screw drives) with a simplified telescoping strut mechanism that uses basic friction and geometric locking. The strut's telescoping action provides secure positioning through triangular truss formation rather than complex mechanical locks, dramatically increasing adjustment speed while maintaining reliability

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

Solution Approach 2:

The patent segments the armrest support structure into multiple components (armrest support member, armrest platform, telescoping struts) that can be independently adjusted. This segmentation allows the telescoping struts to provide both adjustment and locking functions separately, eliminating the need for integrated complex locking mechanisms

Inventive Principle:
Principle #1Segmentation

3Device complexity

If the armrest is constrained to tilt about a pivot fixed at the pilot's elbow, then the structure can be simple, but the hand positioning precision relative to the side stick controller is insufficient

Engineering Contradiction:
Improvearmrest structure simplicityVSAvoidhand position precision
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The patent inverts the pivot location from the elbow to the wrist-end, allowing the armrest platform to pivot directly at the point where positioning precision is most critical. This single pivot point provides both structural simplicity and precise hand positioning capability relative to the side stick controller

Inventive Principle:
Principle #13The other way round (Inversion)

Solution Approach 2:

The patent introduces dynamic adjustability through the telescoping struts that allow the armrest platform to be positioned at multiple discrete locations along the wrist-end pivot arc. This dynamic positioning capability provides precise hand placement without requiring a complex multi-pivot mechanical structure

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS20110049960A1Aircraft seat with adjustable armrest
Publication Date: 2011.03.03 AMI IND INC
  • US20110049960A1 patent drawing
  • US20110049960A1 patent drawing
  • US20110049960A1 patent drawing

AI summary

An aircraft seat has an adjustable armrest in which the armrest platform is supported by a hinged attachment to an armrest support member. The hinged attachment between the armrest platform and the arm support member is located at the wrist-end of the arm support member near the aircraft control stick. The armrest platform and the armrest support are locked into position by means of telescoping struts that are controlled at the wrist-end of the arm platform member. The telescoping struts can be selectively locked to create triangular and/or quadrilateral trusses that lock the armrest firmly into position and may include springs or other elements to bias the armrest platform up and forward so that the armrest “floats” when the telescoping struts re released.