Magnetic Propeller Safety Device for UAVs

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Solution Overview

Problem

Existing propeller safety devices for unmanned aerial vehicles (UAVs) either fail to prevent damage during propeller strikes or terminate UAV flight, as they either have undesirable aerodynamic characteristics, increase manufacturing costs, or require additional power and reduce flight time.

Innovation Solution

A magnetic propeller safety device that uses magnetic elements to passively disengage the propeller from the motor shaft during a strike, allowing it to rotate independently and reengage once the strike ends, thereby reducing damage and enabling continuous UAV flight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a propeller safety device uses traditional mechanical engagement methods, then the propeller remains firmly attached to the motor shaft, but the device cannot reduce damage during strikes and may terminate flight

Engineering Contradiction:
Improvepropeller attachment reliabilityVSAvoidstrike damage
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent replaces traditional mechanical engagement mechanisms with magnetic fields. Magnetic elements in the propeller interact with magnetic elements in the motor shaft assembly to provide engagement and disengagement functions, eliminating complex mechanical components and enabling passive response to strike conditions.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The magnetic coupling strength varies dynamically based on the relative position and alignment between propeller and motor shaft. During normal operation, strong magnetic attraction maintains firm engagement. During strikes, misalignment reduces magnetic coupling, allowing passive disengagement to reduce damage while maintaining attachment.

Inventive Principle:
Principle #15Dynamics

2Strength

If a propeller safety device uses rigid mechanical coupling, then the propeller remains firmly attached, but damage during object strikes increases and flight must be terminated

Engineering Contradiction:
Improvepropeller attachment strengthVSAvoidobject strike damage
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

The magnetic coupling parameters (strength, engagement depth) change based on the operational state. During normal flight, strong magnetic attraction provides firm attachment. During strikes, the coupling parameters effectively reduce as misalignment increases, allowing the propeller to partially disengage and reduce damage while remaining attached.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The magnetic coupling system provides inherent compliance that cushions strike forces before they reach the motor shaft. The magnetic field acts as a buffer that can absorb and redistribute impact forces, reducing peak loads on the motor and propeller during strikes.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

3Force

If a propeller safety device uses magnetic elements with strong holding force, then the propeller remains firmly attached during flight, but the propeller cannot passively disengage during strikes

Engineering Contradiction:
Improvemagnetic holding forceVSAvoidstrike damage
Core Design Contradiction:
ForceVSObject-affected harmful factors

Solution Approach 1:

The magnetic element arrangement creates asymmetric engagement characteristics. The magnetic coupling is strong when aligned (during normal flight) but weakens rapidly when misaligned (during strikes). This asymmetric response allows firm attachment during operation while enabling passive disengagement during abnormal conditions.

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

The magnetic coupling strength is dynamic rather than static. It automatically adjusts based on the relative position between propeller and motor shaft, providing strong holding force during aligned operation but reducing coupling strength during misaligned strike conditions, enabling both firm attachment and strike mitigation.

Inventive Principle:
Principle #15Dynamics

4Ease of manufacture

If a propeller safety device uses conventional mechanical components, then manufacturing is straightforward, but device complexity and manufacturing cost increase

Engineering Contradiction:
Improvemanufacturing simplicityVSAvoidsafety device complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The patent eliminates complex mechanical engagement components (gears, springs, latches) by using magnetic fields for propeller attachment and disengagement. This reduces the number of moving parts, simplifies the device structure, and lowers manufacturing complexity while maintaining safety functions.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The magnetic elements are integrated into the existing propeller and motor shaft assembly structures, combining the attachment function with the structural components. This merging reduces the need for separate safety device components, simplifying manufacturing and reducing overall device complexity.

Inventive Principle:
Principle #5Merging (Combining)

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 magnetic propeller safety device reduces damage to the propeller, object, and UAV during strikes while allowing UAV flight to continue, with improved installation and retention forces compared to traditional propeller safety devices.

Implementation Method 1

The propeller and shaft mount each have a magnetic element. When both magnetic elements are aligned, the propeller engages the shaft mount by way of a magnetic holding force between the magnetic elements.

Methodology Applied
Scientific EffectMagnetic force: Magnetism

Implementation Method 2

During a propeller object strike, when the propeller displaces 5 to 10°, the magnetic elements passively disengage the propeller from the shaft mount due to misalignment of the magnetic elements.

Methodology Applied
Scientific EffectMagnetic force: Magnetism

Data Source

PatentUS9677564B1Magnetic propeller safety device
Publication Date: 2017.06.13 WING AVIATION LLC
  • US9677564B1 patent drawing
  • US9677564B1 patent drawing
  • US9677564B1 patent drawing

AI summary

A magnetic propeller device for an unmanned aerial vehicle (UAV) includes a propeller and a shaft mount that engage with a motor shaft of a UAV. The propeller and shaft mount each have a magnetic element. When both magnetic elements are aligned, the propeller engages the shaft mount by way of a magnetic holding force between the magnetic elements. When a propeller contacts an object and the propeller is displaced, the magnetic elements passively disengage the propeller from the shaft mount due to misalignment of the magnetic elements. Passive disengagement allows the propeller to rotate independently of the motor shaft. Once the UAV moves clear of the object, the magnetic elements can realign, such that the propeller re-engages the shaft mount and resumes rotation with the motor shaft.