Blended Wing Body Transparent Panels for Cabin Light and Views

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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 visibility.

Innovation Solution

Incorporation of transparent panels on the cabin ceiling, which are configured to transmit visible light, display images, and adjust transparency, providing passengers with a more open and spacious feel while allowing real-time video at every seat to replace traditional window views.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If traditional windows are used in blended wing body aircraft, then structural integrity is maintained, but passenger comfort deteriorates due to limited visibility and claustrophobic experience

Engineering Contradiction:
Improvepassenger comfortVSAvoidwindow structure
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The patent moves the window function from the lateral walls to the top surface of the blended wing body, utilizing the third dimension (vertical space) to provide transparent panels. This dimensional shift allows passengers to experience views and natural light without compromising the streamlined fuselage structure, thereby improving comfort while maintaining structural integrity.

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

Solution Approach 2:

The transparent panels are segmented and distributed across the top surface of the aircraft body, rather than using large continuous windows. This segmentation allows the structure to maintain strength while providing multiple viewing points, resolving the contradiction between structural integrity and passenger comfort.

Inventive Principle:
Principle #1Segmentation

2Illumination intensity

If transparent panels are installed on the aircraft body, then natural light transmission is improved, but structural strength may be compromised

Engineering Contradiction:
Improvenatural light transmissionVSAvoidaircraft body strength
Core Design Contradiction:
Illumination intensityVSStrength

Solution Approach 1:

The transparent panels are strategically positioned in specific locations on the top surface where they can transmit natural light effectively while avoiding critical structural zones. This local placement optimizes light transmission without compromising overall structural strength.

Inventive Principle:
Principle #3Local quality

3Ease of operation

If multiple transparent panels are added to the aircraft, then passenger entertainment and comfort are enhanced, but aircraft weight increases

Engineering Contradiction:
Improvepassenger entertainmentVSAvoidaircraft weight
Core Design Contradiction:
Ease of operationVSWeight of moving object

Solution Approach 1:

The patent utilizes electrochromic or similar variable transparency materials that can change their optical properties on demand. This allows the panels to provide entertainment and comfort features when needed while maintaining a lighter overall structure compared to traditional fixed window systems with multiple mechanical components.

Inventive Principle:
Principle #35Parameter changes

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The transparent panels enhance passenger comfort by providing natural light, reducing the aircraft's weight, and offering a more enjoyable travel experience through adjustable lighting and visual entertainment.

Implementation Method 1

the plurality of transparent panels allow the transmission of visible light

Methodology Applied
Scientific EffectLight transmission: Light

Data Source

PatentUS20240246675A1Blended wing body aircraft with transparent panels
Publication Date: 2024.07.25 JETZERO INC
  • US20240246675A1 patent drawing
  • US20240246675A1 patent drawing
  • US20240246675A1 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. The blended wing body aircraft also includes 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 plurality of transparent panels allow the transmission of visible light.