Eccentric Wheel UAV Power Assembly Quick Detach Mechanism

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Solution Overview

Problem

Existing unmanned aerial vehicles (UAVs) have power assemblies that are difficult to detach from the airframe due to fixed or bolted connections, making them inconvenient to change in different working environments.

Innovation Solution

The UAV design incorporates eccentric wheels on the power assembly and connecting rods on the airframe, allowing the connecting rod to be inserted and locked into the eccentric wheel by rotating it, enabling easy detachment of the power assembly from the airframe.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If fixed connection or bolted connection is used between airframe and power assembly, then connection strength is improved, but ease of detachment deteriorates

Engineering Contradiction:
Improveconnection strengthVSAvoidease of detachment
Core Design Contradiction:
StrengthVSEase of operation

Solution Approach 1:

The connection mechanism transitions from static (fixed/bolted) to dynamic (rotatable eccentric wheel). The eccentric wheel can rotate between a first position (locked state) and a second position (unlocked state), enabling the connection to adapt between strong fixed connection and easy detachment states.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The eccentric wheel introduces a curved rotational motion path instead of linear insertion/removal. The rotating wheel with its eccentric geometry creates a mechanical locking action that provides strong connection when engaged, while allowing quick release through simple rotation.

Inventive Principle:
Principle #14Spheroidality (Curvature)

2Reliability

If fixed connection or bolted connection is used between airframe and power assembly, then connection reliability is improved, but device complexity deteriorates

Engineering Contradiction:
Improveconnection reliabilityVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The complex multi-step bolted connection process is extracted and replaced by a single rotational action of the eccentric wheel. The essential locking function is isolated into the eccentric wheel mechanism, simplifying the overall connection system while maintaining reliability.

Inventive Principle:
Principle #2Taking out (Extraction)

3Adaptability or versatility

If power assembly is designed for easy detachment, then adaptability is improved, but connection strength deteriorates

Engineering Contradiction:
ImproveadaptabilityVSAvoidconnection strength
Core Design Contradiction:
Adaptability or versatilityVSStrength

Solution Approach 1:

The eccentric wheel mechanism dynamically adjusts the connection state. When rotated to the first position, it creates a locked state with strong connection force. When rotated to the second position, it releases the lock for easy detachment. This dynamic behavior enables both strong connection and easy detachment.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The connection parameters (strength, detachment ease) are changed by rotating the eccentric wheel between different positions. The same mechanism can provide high connection strength when locked, and easy detachment when unlocked, by changing its rotational position parameter.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS12065241B2Unmanned aerial vehicle
Publication Date: 2024.08.20 AUTEL ROBOTICS CO LTD
  • US12065241B2 patent drawing
  • US12065241B2 patent drawing
  • US12065241B2 patent drawing

AI summary

The embodiment is an unmanned aerial vehicle. The unmanned aerial vehicle includes: an airframe, including first mounting portions, where the first mounting portion includes a first mounting body and connecting rods formed on the first mounting body, the connecting rods extending in a pitch axis direction; and a power assembly, including a first assembling body and eccentric wheels mounted on the first assembling body, where the eccentric wheel is rotatable between a first rotation position and a second rotation position of the first assembling body around a rotation axis of the first assembling body, the rotation axis being perpendicular to the pitch axis direction.