Roadable VTOL Rotor Parking and Folding for Compact Flight Efficiency
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Solution Overview
Problem
Existing flying car prototypes face efficiency issues due to high weight-to-rotor surface area ratios, leading to limited flight duration, high operational costs, and safety concerns, while foldable mechanisms are complex and expensive, hindering the development of practical roadable VTOL vehicles.
Innovation Solution
A roadable VTOL flying vehicle design featuring a single main rotor or twin rotors with a simple folding mechanism, utilizing a balanced rotor configuration and electronic position control to park and unlock rotors, enhancing efficiency by increasing rotor surface area without enlarging the vehicle dimensions, and incorporating a hybrid propulsion system for versatility.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Productivity
If the rotor surface area is increased to improve flight efficiency, then the vehicle dimensions become oversized
Solution Approach 1:
The rotor blades are folded along their span during road configuration, with inner portions nested within outer portions. This nesting allows the rotor surface area to be substantially contained within the vehicle dimensions when not in use, while providing full rotor surface area when deployed for flight operations.
Solution Approach 2:
The rotor blades are designed with foldable sections that can dynamically change configuration between road mode (folded) and flight mode (unfolded). This dynamic transformation allows the same rotor structure to provide large surface area for efficient flight while maintaining compact dimensions for road operation.
2Adaptability or versatility
If a mechanical folding mechanism is added to enable rotor folding, then the device complexity increases
Solution Approach 1:
The complex mechanical folding mechanism is replaced with an electronic position control system. Sensors detect rotor position and provide feedback to control circuits that adjust motor operation to achieve precise rotor parking and folding without complex mechanical linkages.
Solution Approach 2:
The rotor folding system uses self-contained electric motors with integrated position sensors and control circuits. Each rotor assembly is self-sufficient, with the motor serving both propulsion and folding functions, eliminating the need for separate mechanical folding mechanisms.
3Ease of operation
If separate folding mechanisms are added to each rotor blade, then the manufacturing cost increases
Solution Approach 1:
Multiple rotor blade folding functions are merged into a single integrated control system. The control circuit receives position feedback from sensors on individual blades and coordinates motor operation to fold all blades simultaneously, reducing manufacturing cost by eliminating separate folding mechanisms for each blade.
Solution Approach 2:
The electric motor serves multiple functions: propulsion during flight and folding during road configuration. This multi-functionality eliminates the need for separate folding mechanisms, reducing manufacturing complexity and cost while maintaining ease of operation.
4Stability of the object's composition
If the rotor is positioned at the middle of the vehicle, then the folding mechanism complexity increases
Solution Approach 1:
The rotor folding mechanism utilizes the vertical dimension by folding blades along their span rather than requiring horizontal reconfiguration. This dimensional approach allows the rotor to be positioned at the vehicle center for stable road configuration while maintaining simple folding mechanics that don't require complex lateral movement mechanisms.
Data Source
AI summary
A roadable VTOL flying vehicle having a road-configuration and a flight-configuration. The roadable VTOL flying vehicle includes a roadable vehicle; at least one rotor having at least one blade, the rotor is rotatably attached to an upper section of the roadable vehicle of the flying vehicle; at least one motor configured to operatively rotate the least at least one rotor; at least one angular position sensor configured to detect the angular position of each of the at least one rotor; and a vehicle control sub-system configured to affect automatic transformation of the flying vehicle from the road-configuration to the flight-configuration and from the flight-configuration to the road-configuration, wherein the vehicle control sub-system is configured bring the at least one rotor into a parking state, when in road-configuration.


