Cockpit Eye Alignment Guides for Helmet Tracking Accuracy

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Solution Overview

Problem

Existing cockpit designs fail to effectively accommodate pilots of varying sizes, leading to difficulties in accessing controls, blind spots, and increased collision risks due to misalignment with the eye reference point, particularly when using position-sensitive equipment like helmets.

Innovation Solution

An alignment system comprising indicators, guides, and a bracket that allow pilots to adjust their position in the cockpit such that the indicators and guides align with their vision, enabling precise head movement detection and accurate operation of helmet systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If the cockpit is designed with a fixed eye reference point, then the design is simple and consistent, but pilots of varying sizes cannot effectively use position-sensitive equipment like hunter helmets

Engineering Contradiction:
Improveaccommodation of pilots of varying sizesVSAvoidcockpit design complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent introduces movable indicators that can be repositioned along the cockpit structure to accommodate different pilot eye positions. Instead of a fixed reference point, the system dynamically adjusts the indicator location to match each pilot's anatomy, enabling effective use of position-sensitive equipment like hunter helmets while maintaining a relatively simple overall design

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The alignment system is divided into separate components: movable indicators, guides, and reference marks that can be independently positioned. This segmentation allows each element to be adjusted to suit different pilots, providing versatility without requiring complete redesign of the cockpit structure

Inventive Principle:
Principle #1Segmentation

2Reliability

If the pilot does not adjust the seat position to the eye reference point, then the pilot has freedom of movement, but the pilot cannot see all displays and control panels, causing blind spots and false readings

Engineering Contradiction:
Improvevisibility of displays and control panelsVSAvoidpilot seat adjustment
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system provides self-aligning visual indicators that automatically guide the pilot to the correct eye position. The movable indicators and guides create an intuitive visual reference system that the pilot can use independently without external assistance, ensuring proper alignment for complete visibility of all displays and controls

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent employs visually distinct indicators and guides with contrasting colors or patterns that are easily visible to the pilot. These color-coded elements create clear visual cues that guide the pilot's eye to the correct position, ensuring all displays and control panels are within the field of view

Inventive Principle:
Principle #32Color changes

3Measurement precision

If traditional alignment methods using two or three balls are used, then the method is simple to implement, but the alignment precision is insufficient for accurate head movement detection

Engineering Contradiction:
Improvehead movement detection precisionVSAvoidalignment system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent introduces intermediate visual elements (guides and movable indicators) that mediate between the simple ball alignment method and the precise head movement detection requirement. These intermediaries provide refined visual references that enhance measurement precision without requiring complex electronic or mechanical systems

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The system adds a visual dimension to the traditional tactile ball alignment method. By incorporating movable indicators and guides that create visual alignment references, the system transitions from purely mechanical alignment to a multi-sensory approach, significantly improving precision for head movement detection

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

4Reliability

If the pilot uses a helmet with position-sensitive equipment, then the equipment can detect head movements, but the equipment does not work effectively when the pilot's eye position is not aligned with the reference point

Engineering Contradiction:
Improvehelmet system functionalityVSAvoidcompatibility with pilots of varying sizes
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The movable indicators can be dynamically repositioned to match each pilot's eye position, ensuring that the helmet's position-sensitive equipment remains effectively aligned with the pilot's head movements. This dynamic adjustment capability maintains helmet system functionality across pilots of varying sizes

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The alignment system creates a universal reference framework that works with different helmet types and pilot anatomies. The movable indicators and guides provide a standardized alignment method that ensures helmet equipment effectiveness regardless of pilot size, enhancing both reliability and adaptability

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

Data Source

PatentUS12466577B2Alignment system
Publication Date: 2025.11.11 TUSAS TURK HAVACILIK VE UZAY SANAYII ANONIM SIRKETI
  • US12466577B2 patent drawing
  • US12466577B2 patent drawing

AI summary

An alignment system includes a body provided at the air vehicle. An indicator is located on the body and in the pilot's field of vision where at least one guide is located on the body between the indicator and the pilot at a distance from the indicator and the pilot. A reference position enables the pilot to move in the cockpit to the position where the guide and the indicator coincide with respect to the pilot's point of vision enabling the pilot to reach a predetermined position.