Aircraft Windowless Suite Video System for Attitude Reference

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Solution Overview

Problem

Passengers in windowless aircraft suites experience discomfort due to lack of visual attitude reference during flight maneuvers, as existing video systems fail to provide a reliable and intuitive indication of the aircraft's attitude, leading to potential motion sickness.

Innovation Solution

A video system with cameras mounted near the windows and monitors positioned to simulate the view from actual windows, capturing and displaying images from different angles to match the passenger's perspective, providing a real-time, intuitive attitude reference through peripheral vision.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a single image is replicated on all screens on the same side of the mockup, then the device complexity is reduced, but the reliability of attitude reference is compromised during takeoff maneuvers when the nose is pointed skyward

Engineering Contradiction:
Improvevideo system complexityVSAvoidattitude reference reliability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The patent divides the video system into multiple independent camera units, each capturing a different view (forward, downward, rearward). Each monitor receives a dedicated camera feed rather than replicating a single image, allowing each screen to provide appropriate attitude reference for its specific viewing angle and position.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different cameras are positioned and angled to capture specific local views appropriate for their location on the aircraft. The forward camera captures the horizon during level flight, the downward camera captures the ground during takeoff, and the rearward camera captures the sky during descent, with each feed displayed on corresponding monitors.

Inventive Principle:
Principle #3Local quality

2Ease of operation

If forward looking cameras are used to provide attitude reference, then the ease of operation is improved, but the reliability deteriorates during takeoff when the horizon disappears

Engineering Contradiction:
Improveintuitiveness of attitude referenceVSAvoidattitude reference availability
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The system dynamically switches between different camera feeds based on aircraft attitude and flight phase. During takeoff when the forward camera loses the horizon, the downward-looking camera automatically provides the appropriate visual reference. The system adapts to changing flight conditions by selecting the most reliable camera feed for each situation.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The downward-looking camera serves as an intermediary attitude reference source when the primary forward-looking camera cannot provide reliable horizon information. This secondary camera captures the ground track and aircraft orientation from a different perspective, maintaining attitude reference reliability during critical phases like takeoff and landing.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Area of stationary object

If monitors are positioned farther from the passenger to cover more area, then the area of coverage is improved, but the measurement precision of attitude reference deteriorates due to smaller vertical field of view

Engineering Contradiction:
Improvemonitor coverage areaVSAvoidattitude reference precision
Core Design Contradiction:
Area of stationary objectVSMeasurement precision

Solution Approach 1:

Instead of increasing monitor size in the horizontal dimension, the system adds vertical dimension coverage by using multiple cameras at different angles (forward, downward, rearward). Each camera provides a focused view with adequate vertical field of view, and the combination of multiple feeds covers the entire vertical space without sacrificing precision in any single display.

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

Data Source

PatentUS10650258B1Apparatus and method for providing attitude reference for vehicle passengers
Publication Date: 2020.05.12 BE AEROSPACE INC
  • US10650258B1 patent drawing
  • US10650258B1 patent drawing
  • US10650258B1 patent drawing

AI summary

A system. The system may include a glare shield positioned between an exterior pane of an aircraft window and an interior portion of an aircraft. The glare shield may include at least one anti-reflective mask and at least one viewing aperture. Each of the at least one anti-reflective mask may be positioned adjacent one of the at least one viewing aperture.