Blended Wing Body Ceiling Panels for Cabin Light Without Side Windows

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Solution Overview

Problem

Blended wing body aircraft have limited windows, leading to a claustrophobic and unenjoyable experience for passengers due to the lack of natural light and panoramic views.

Innovation Solution

Incorporating a plurality of transparent panels on the cabin ceiling, which are configured to illuminate in different colors and display images, providing passengers with real-time video and enhancing the interior design by eliminating the need for traditional window seats.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If traditional window seats are used in blended wing body aircraft, then structural integrity is maintained, but passenger comfort deteriorates due to claustrophobic feelings and lack of natural light

Engineering Contradiction:
Improvepassenger comfortVSAvoidstructural integrity
Core Design Contradiction:
Ease of operationVSStrength

Solution Approach 1:

The patent transitions from traditional side windows to ceiling-mounted transparent panels, changing the spatial dimension of light entry from lateral to vertical. This allows panoramic views and natural light to be provided from the ceiling rather than the sides, resolving the contradiction between structural integrity and passenger comfort.

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

Solution Approach 2:

The ceiling is divided into multiple transparent panels that can be individually installed and removed. These panels are integrated into the existing rib structure, segmenting the ceiling into functional units that maintain structural integrity while providing multiple viewing zones throughout the cabin.

Inventive Principle:
Principle #1Segmentation

2Ease of operation

If transparent panels are installed in the cabin ceiling, then passenger comfort is improved through natural light and views, but device complexity increases due to integration with rib structure

Engineering Contradiction:
Improvepassenger comfortVSAvoidintegration complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The transparent panels are merged with the existing rib structure of the blended wing body aircraft. The ribs serve dual purposes as both structural support elements and mounting frameworks for the transparent panels, reducing overall device complexity by combining structural and functional components.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The rib structure serves multiple functions: providing structural support for the aircraft body, acting as mounting frames for transparent panels, and defining channels for panel installation. This multi-functionality reduces the need for separate components, simplifying the overall system despite the added transparency feature.

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

3Weight of moving object

If transparent panels are used instead of traditional windows, then weight is reduced, but manufacturing precision requirements increase for integration with aircraft structure

Engineering Contradiction:
Improveaircraft weightVSAvoidpanel integration precision
Core Design Contradiction:
Weight of moving objectVSManufacturing precision

Solution Approach 1:

The transparent panels are installed in specific locations within the rib-defined channels on the ceiling, rather than throughout the entire structure. This localized approach allows for precise installation in key areas while maintaining structural integrity, reducing overall manufacturing precision requirements compared to full-coverage transparent structures.

Inventive Principle:
Principle #3Local quality

Data Source

PatentUS11939059B2Blended wing body aircraft with transparent panels
Publication Date: 2024.03.26 JETZERO INC
  • US11939059B2 patent drawing
  • US11939059B2 patent drawing
  • US11939059B2 patent drawing

AI summary

The present disclosure is directed to a blended wing body aircraft including a blended wing body, wherein the blended wing body is characterized by having no clear dividing line between wings and a main body along a leading edge of the aircraft, at least a rib, wherein the at least a rib runs longitudinally from fore to aft of the main body, and a plurality of transparent panels located in the top surface of the main body, wherein the plurality of transparent panels are located in channels, wherein the channels are separated by the at least a rib.