Drone Base Station for Remote Broadband Coverage
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Solution Overview
Problem
Current communication technologies, such as cellular systems and geosynchronous satellites, face challenges in providing broadband access to remote areas and are costly and impractical for high-speed applications, especially when mobility is required.
Innovation Solution
A vertical take-off and landing drone equipped with a lightweight carbon fiber frame, multiple power generator systems, and adjustable antenna arrays, capable of hovering for extended periods and providing wireless communication services as a base station, utilizing satellite communication and mmWave links to connect users to the internet.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Area of stationary object
If geosynchronous satellites are used for communication, then coverage area is improved, but implementation cost and complexity increase significantly
Solution Approach 1:
The patent replaces expensive, complex geosynchronous satellites with shorter-lived, lower-cost drone platforms that can be deployed more economically. The drone provides temporary but effective communication coverage without the巨额 investment required for satellite deployment and maintenance.
Solution Approach 2:
The drone acts as an intermediary communication platform between ground-based cellular systems and remote users. It carries base station equipment and antennas to provide wireless communication services in areas where traditional infrastructure is unavailable, bridging the gap without requiring full satellite implementation.
2Area of stationary object
If LEO satellites are used for communication, then coverage area is improved, but hardware cost and power requirements increase
Solution Approach 1:
The patent uses cost-effective drone platforms instead of expensive LEO satellite constellations. The drone can be deployed locally to provide coverage without requiring thousands of satellites, dramatically reducing hardware costs while maintaining adequate service area through strategic positioning.
Solution Approach 2:
The patent transitions from horizontal satellite orbital coverage to vertical aerial positioning coverage. By deploying the communication platform vertically in the airspace above remote areas, the system achieves coverage without requiring the extensive horizontal satellite network needed for LEO constellations.
3Ease of operation
If cellular base stations are deployed in remote areas, then communication service is improved, but infrastructure cost and deployment complexity increase
Solution Approach 1:
The drone serves multiple functions: it carries base station equipment for wireless communication, provides aerial positioning for coverage, and can be deployed without ground infrastructure. This multi-functionality eliminates the need for separate communication towers, power infrastructure, and site preparation required by traditional cellular deployments.
Solution Approach 2:
The patent extracts the base station functionality from ground-based infrastructure and relocates it to an aerial drone platform. This removes the dependency on complex ground infrastructure including towers, power grids, and physical sites, simplifying deployment in remote areas where such infrastructure is unavailable or prohibitively expensive.
4Reliability
If traditional base stations are used for high-speed communication, then communication quality is improved, but mobility and adaptability are reduced
Solution Approach 1:
The patent transforms the static nature of traditional base stations by implementing them on mobile drone platforms. The drone can dynamically reposition to maintain optimal communication quality, adapt to moving users, and provide service in varying environmental conditions, combining high-quality communication with full mobility.
Data Source
AI summary
A drone includes a frame and a fuselage. The fuselage is coupled to the frame extending away from the frame. The fuselage has a front panel and a bottom panel, and the front panel is positioned at an angle between the bottom surface of the frame and the bottom panel of the fuselage. A first wing is opposite a second wing and are coupled to the frame. The first and second wings extend outwardly from opposite sides of the frame. A first and second mounting member are coupled to the frame and extend outwardly from opposite sides of the frame. A plurality of power generator systems are included and each system is coupled to the first or second mounting member. Each power generator system comprises a power source coupled to a propeller.