Modular Aircraft Pod With Center of Gravity Adjustment
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Solution Overview
Problem
Current aircraft designs lack versatility and efficiency in transitioning between flight modes and transportation methods, with limited adaptability for cargo and passenger transport across various environments, and inadequate solutions for adjusting the center of gravity during flight.
Innovation Solution
A modular aircraft configuration comprising a pod module assembly, wing assembly, and chassis module, allowing for selective attachment and detachment, with an adjustment mechanism to vary the center of gravity, enabling operation as a ground vehicle, watercraft, and aerial vehicle, and featuring a connector system for rapid configuration changes and storage.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If a modular aircraft configuration with selective attachment and detachment is implemented, then adaptability and versatility are improved, but device complexity increases
Solution Approach 1:
The aircraft is divided into modular components (pod module assembly, wing assembly, chassis module) that can be selectively attached and detached. This segmentation enables different configurations for various operations while maintaining manageable complexity through standardized interfaces and connector systems.
Solution Approach 2:
The pod module assembly serves multiple functions including cargo transport, passenger transport, medivac operations, and can be transported on ground or water by other vehicles. This multi-functionality improves adaptability without requiring separate specialized vehicles for each operation.
2Stability of the object's composition
If an adjustment mechanism is added to vary center of gravity, then flight stability is improved, but device complexity increases
Solution Approach 1:
The adjustment mechanism dynamically repositions weights or battery packs along tracks within the chassis module to vary the center of gravity during flight operations. This dynamic adjustment capability ensures flight stability under different loading conditions without requiring a completely redesigned airframe.
3Productivity
If rapid configuration changes are enabled through connector system, then productivity is improved, but manufacturing precision requirements increase
Solution Approach 1:
Connector systems and mating hardware are pre-designed and pre-positioned on modular components during manufacturing. This preliminary action ensures that when components are assembled in the field, the connectors align properly without requiring high-precision manual adjustment, enabling rapid configuration changes while maintaining manufacturing feasibility.
4Adaptability or versatility
If pod module assembly is made self-transportable or transportable by other vehicles, then adaptability is improved, but weight increases
Solution Approach 1:
The pod module assembly is designed with transport interfaces that allow it to be moved by other vehicles (ground vehicles, watercraft) or be self-transportable when detached from the aircraft. This multi-functionality enables the same component to serve both as a cargo/passenger module and as a transportable unit, improving adaptability without requiring separate transport equipment.
Data Source
AI summary
A modular aircraft includes a plurality of structural elements. The structural elements include a pod module assembly, a wing assembly, and a chassis module. The pod module assembly is configured to be selectively attached to and detached from at least one of the chassis module and the wing module when the aircraft is not in flight. The pod module assembly is configured to transport at least one of a passenger and cargo.