Ejection Seat Cushion Length Adjuster Mechanism

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Solution Overview

Problem

Ejection seat cushions in aircraft lack ergonomic features and are non-adjustable, leading to pilot fatigue during long missions due to inadequate leg support, which can impair concentration and performance.

Innovation Solution

A cushion length adjusting system for aircraft ejection seats, comprising hingedly or slidingly coupled adjustable pads that can be customized to varying occupant heights, allowing manual or automatic adjustment of leg support length, with features like tracks, rails, and handles for easy operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If the seat cushion is made fixed and non-adjustable, then the device complexity is reduced, but the pilot comfort and leg support are insufficient during long missions

Engineering Contradiction:
Improvepilot comfortVSAvoidcushion adjustment mechanism
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The seat cushion is divided into multiple adjustable segments or sections that can be independently positioned. This allows the cushion to be segmented into different length configurations, providing ergonomic support for various pilot leg lengths while maintaining a relatively simple overall structure through modular design.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The cushion transitions from a static, fixed design to a dynamic, adjustable system that can change its length and configuration. This dynamic capability allows the cushion to adapt to different pilot sizes and mission requirements, improving comfort without requiring a completely complex mechanism through clever use of movable joints and locking positions.

Inventive Principle:
Principle #15Dynamics

2Reliability

If the seat cushion is made adjustable for different leg support lengths, then pilot fatigue is reduced, but the device complexity increases

Engineering Contradiction:
Improvepilot performanceVSAvoidadjustable cushion system
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The adjustable cushion components are designed with nested structures where smaller elements fit within larger ones. This nesting approach allows multiple adjustment functions and components to be compactly integrated, reducing the overall space required and simplifying the apparent complexity while maintaining full adjustability for different leg support needs.

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The cushion adjustment mechanism is designed to serve multiple functions: adjusting length, providing support at different angles, and accommodating various pilot sizes. This multi-functionality consolidates what could be multiple separate systems into a single integrated mechanism, reducing overall device complexity while improving pilot performance and reducing fatigue.

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

3Adaptability or versatility

If a single fixed cushion design is used, then manufacturing is simplified, but adaptability to different pilot heights is lost

Engineering Contradiction:
Improvecushion fit for different pilotsVSAvoidcushion production
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The cushion is manufactured as segmented modules that can be produced using standardized processes and then assembled in different configurations. This segmentation allows each module to be manufactured efficiently with standard tooling, while the modular assembly provides adaptability for different pilot heights without requiring completely different cushion designs.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The cushion design incorporates adjustable parameters such as length, angle, and positioning that can be modified after manufacturing. This allows a single base design to be produced efficiently, then adapted to different pilots through parameter adjustments rather than requiring custom-manufactured cushions for each pilot size.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS11623755B2Seat cushion length adjuster for ejection seat
Publication Date: 2023.04.11 AMI IND INC
  • US11623755B2 patent drawing
  • US11623755B2 patent drawing
  • US11623755B2 patent drawing

AI summary

A cushion length adjusting system for use in an ejection seat of an aircraft may include a seat pan and first cushion length adjuster coupled to the seat pan. The cushion length adjuster may be hingedly or slidingly coupled to the seat pan. The cushion length adjuster may be configured to adjust a leg support length for greater ergonomics for a pilot of an aircraft.