UAV Damper Isolates Payload from Propulsion Vibrations

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Solution Overview

Problem

Unmanned aerial vehicles (UAVs) experience vibrations from their propulsion systems, which can negatively impact the accuracy of sensors mounted on them, leading to erroneous measurements.

Innovation Solution

Incorporating a damper between the propulsion-receiving module and the payload-receiving module to inhibit the transmission of vibrations, ensuring the payload remains vibrationally decoupled from the propulsion system, thereby maintaining sensor accuracy and operational stability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If the propulsion system is mounted directly to the main body, then the structural simplicity is improved, but the vibration transmission to sensors worsens

Engineering Contradiction:
Improvestructural simplicityVSAvoidsensor accuracy
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

A damper is introduced as an intermediary component between the propulsion-receiving module and the payload-receiving module. This damper absorbs and dissipates vibrations generated by the propulsion system, preventing them from being transmitted to the payload and sensors mounted on the payload-receiving module, thereby maintaining sensor accuracy while preserving structural simplicity.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Stability of the object's composition

If the payload is rigidly connected to the propulsion system, then the structural stability is improved, but the vibration isolation deteriorates

Engineering Contradiction:
Improvestructural stabilityVSAvoidvibration transmission
Core Design Contradiction:
Stability of the object's compositionVSObject-affected harmful factors

Solution Approach 1:

The main body is divided into functionally independent modules: a propulsion-receiving module that accepts the propulsion system and a payload-receiving module that accepts the payload. These modules are connected through a damper that provides vibration isolation, allowing each module to maintain its structural stability independently while preventing harmful vibration transmission between them.

Inventive Principle:
Principle #1Segmentation

3Measurement precision

If vibration damping is added at the sensor level, then the sensor accuracy is improved, but the overall system complexity increases

Engineering Contradiction:
Improvesensor accuracyVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

Vibration damping functionality is merged into the structural connection between modules by incorporating a damper into the main body's modular architecture. This centralized damping approach protects all sensors and payload components simultaneously, achieving improved sensor accuracy without the need for individual sensor-level damping solutions, thereby avoiding increased system 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

This solution effectively reduces the impact of vibrations on sensor accuracy, allowing for precise measurements and improved UAV performance by isolating the payload from the propulsion-induced oscillations, thus enhancing sensor reliability and reducing the need for additional damping in individual sensors or subsystems.

Implementation Method 1

a damper interposed between the payload-receiving module and the propulsion-receiving module to inhibit transmission of vibrations from the propulsion-receiving module to the payload-receiving module

Methodology Applied
Scientific EffectVibration damping: Damping

Data Source

PatentUS11767135B2Unmanned vehicle
Publication Date: 2023.09.26 AERYON LABS
  • US11767135B2 patent drawing
  • US11767135B2 patent drawing
  • US11767135B2 patent drawing

AI summary

A main body of an unmanned vehicle is provided. The main body comprises a propulsion-receiving module having a mount point for removably mounting a propulsion source, a payload-receiving module having a mount point for removably mounting a payload, and a damper interposed between the payload-receiving module and the propulsion-receiving module to inhibit transmission of vibrations from the propulsion-receiving module to the payload-receiving module when the payload-receiving module and the propulsion-receiving module are in mechanical communication.