High-Speed Drone With Separate VTOL Propellers And Fixed Wings
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Solution Overview
Problem
Existing aircraft, such as normal airplanes, helicopters, and drones, lack the ability for vertical landing and take-off, have inefficient aerodynamics, slow horizontal speeds, and are limited in long-distance flight capabilities, making them unsuitable for all-weather operations and efficient delivery services.
Innovation Solution
Aircraft equipped with propellers for vertical ascent and descent, stability wings for horizontal flight, and a simplified control structure that allows for high-speed, long-distance travel and all-weather operation without the need for tilt rotors, reducing production costs and accident risks.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of operation
If a helicopter uses a propeller for vertical take-off and landing, then vertical landing and take-off functions are achieved, but horizontal flight speed becomes slow and cruising distance is limited
Solution Approach 1:
The aircraft is divided into two functional systems: a vertical take-off and landing system using a propeller, and a horizontal flight system using a fixed wing. This segmentation allows each system to optimize for its specific function, resolving the contradiction between vertical operation capability and horizontal speed.
Solution Approach 2:
The aircraft integrates multiple functions into a single vehicle design, combining vertical take-off/landing capability with high-speed horizontal flight capability. The fixed wing provides both horizontal flight support and structural stability, while the propeller handles vertical operations, creating a multi-functional aircraft that overcomes the limitations of single-function designs.
2Ease of operation
If an Osprey-type aircraft uses a tilt rotor for vertical take-off and landing, then vertical landing and take-off functions are achieved, but aerodynamic efficiency deteriorates due to propeller airflow beating against wings
Solution Approach 1:
The aircraft separates the vertical take-off function (propeller) from the horizontal flight function (fixed wing), eliminating the aerodynamic interference that occurs in tilt rotor designs where the same rotating blade must serve both functions. The propeller is positioned and oriented to avoid beating against the fixed wing during vertical operations.
Solution Approach 2:
Instead of using a rotating tilt rotor that changes orientation, the design inverts the approach by using a fixed wing that remains stationary during horizontal flight and a separate propeller for vertical operations. This inversion of the traditional rotor-wing integration resolves the aerodynamic efficiency problem.
3Ease of operation
If a drone is used for vertical take-off and landing, then vertical landing and take-off functions are achieved, but horizontal flight speed becomes slow and long-distance flight capability is limited
Solution Approach 1:
The aircraft divides functions between a propeller for vertical operations and a fixed wing for horizontal flight. The fixed wing provides aerodynamic efficiency for long-distance horizontal travel, while the propeller handles vertical take-off and landing, overcoming the drone's limitation of slow horizontal speed and short range.
Solution Approach 2:
The design changes the operational parameters by using a fixed wing configuration that maintains aerodynamic efficiency at high speeds during horizontal flight, while the propeller operates at optimized parameters for vertical take-off and landing. This parameter optimization enables both vertical capability and long-distance horizontal flight.
4Ease of operation
If a tilt rotor is used for vertical take-off and landing, then vertical landing and take-off functions are achieved, but device complexity increases and accident risk increases
Solution Approach 1:
The aircraft segments the control functions into separate systems: the propeller handles vertical take-off and landing with its own independent control, while the fixed wing handles horizontal flight. This segmentation simplifies the overall control structure compared to the complex tilt rotor mechanism that requires precise angle control and coordination.
Solution Approach 2:
The design extracts the tilt rotor mechanism entirely and replaces it with a simpler configuration of a fixed wing and separate propeller. This extraction of the complex rotating mechanism resolves the contradiction by maintaining vertical take-off and landing capability through a simpler, more reliable structure.
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
Enables vertical take-off and landing, high-speed horizontal flight, efficient energy use, and safe operation in adverse weather conditions, facilitating efficient package delivery and rescue operations with reduced production costs and improved safety.
Implementation Method 1
a propeller for vertical ascent, descent, forward-moving
Implementation Method 2
a stability wing for horizontal flight
Implementation Method 3
the airflow given off by the propeller beats against its wings
Data Source
AI summary
By providing propellers for vertical ascent and descent and for horizontal flight, and a blade for horizontal flight, it is possible to obtain an aerial vehicle capable of high-speed horizontal flight and capable of flying a long distance.