Aircraft Wing Segmentation for Direct Travel Efficiency
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Solution Overview
Problem
The current hub-and-spoke air transportation model is inefficient, costly, and creates security vulnerabilities due to large passenger concentrations, requiring a system that offers faster, more direct travel with lower operational costs and enhanced security.
Innovation Solution
Aircraft design featuring a wing with a spar and box-shaped sleeve, spoiler, and vent system for improved aerodynamics and operational efficiency, capable of all-weather operation with a single pilot, and designed for non-stop transcontinental travel from any local airport, using a composite beam structure and truss elements for structural integrity and ease of maintenance.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Quantity of substance
If the hub-and-spoke model uses larger aircraft to accommodate more passengers, then passenger capacity is improved, but travel time and operational efficiency deteriorate
Solution Approach 1:
The patent applies segmentation by dividing the traditional single large aircraft into multiple smaller aircraft operating in a distributed network. Instead of consolidating all passengers into one large plane at a hub, the system segments passengers into smaller groups that travel directly from origin to destination on smaller planes, eliminating hub transfer time and reducing overall travel time while maintaining total passenger capacity.
2Ease of operation
If the hub-and-spoke model concentrates passengers at hub facilities, then operational coordination is improved, but security vulnerability and operational cost worsen
Solution Approach 1:
The patent segments the concentrated hub facility into multiple distributed smaller airports and terminals across the network. This segmentation reduces security vulnerability by eliminating large concentrated passenger populations at single hubs, while operational coordination is maintained through centralized computerized scheduling and routing that manages the distributed fleet and terminals efficiently.
3Strength
If the wing structure uses traditional rigid construction, then structural strength is improved, but ease of maintenance and adaptability worsen
Solution Approach 1:
The wing structure is segmented into modular sections with standardized interfaces. Each wing can be divided into interchangeable modules that can be independently maintained, repaired, or replaced. This modular segmentation maintains overall structural strength through standardized connection points while dramatically improving ease of maintenance, as damaged sections can be quickly swapped without affecting the entire wing assembly.
Solution Approach 2:
The wing structure incorporates dynamic characteristics with flexible joints and adaptive geometry that allow the rigid modular sections to work together as a unified strong structure during flight, while enabling easy disassembly and reconfiguration during maintenance. The structure transitions between rigid load-bearing mode during operation and flexible disassemblable mode during maintenance.
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 aircraft achieves higher speeds, lower operational costs, and enhanced security by minimizing passenger concentrations, while maintaining passenger comfort and ease of maintenance, thus providing a competitive and secure air transportation system.
Implementation Method 1
a vent affixed to the lower surface of the trailing edge of the spar below the spoiler... the vent is in communication with the spoiler such that the vent is open when the spoiler opens
Data Source
AI summary
A wing including a spar, a box shaped sleeve in the spar running substantially the entire length of the wing, a skin affixed to spar and to the corners of the sleeve and shaped to from a leading edge and trailing edge of the wing, a spoiler affixed to an upper surface of the trailing edge of the spar, a vent affixed to the lower surface of the trailing edge of the spar below the spoiler.