Modular UAV Propulsion Modules for Rapid Maintenance

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Solution Overview

Problem

Unmanned aerial vehicles (UAVs) face downtime due to the need for routine maintenance and repair of complex components, which can be time-consuming and inefficient, especially when one component fails, requiring the entire system to be taken out of service until issues are identified and resolved.

Innovation Solution

The implementation of detachable propulsion modules with integrated motors, propellers, sensors, and communication devices that can be quickly installed, removed, and replaced on UAV frames, allowing for modular operation and maintenance, enabling rapid identification and replacement of faulty components without halting the entire system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the entire UAV system is taken out of service for maintenance or repair of a single component, then the component can be properly diagnosed and repaired, but the overall system availability and productivity are reduced

Engineering Contradiction:
Improvecomponent reliabilityVSAvoidsystem availability
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The propulsion system is divided into separate modular units, each comprising a motor, propeller, and associated components. This segmentation allows individual modules to be maintained or replaced without affecting the entire UAV system, thereby maintaining system availability while ensuring component reliability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent implements a replacement strategy where faulty propulsion modules are quickly swapped out and sent for maintenance, while healthy modules continue operating. This approach recovers system productivity by maintaining operational capacity while ensuring reliable maintenance of individual components.

Inventive Principle:
Principle #34Discarding and recovering

2Adaptability or versatility

If multiple components are integrated into a single UAV system, then the system becomes more capable and versatile, but the complexity of maintenance and repair increases

Engineering Contradiction:
Improvesystem capabilityVSAvoidmaintenance complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

By segmenting the propulsion system into standardized modular units, the patent reduces maintenance complexity despite having multiple integrated components. Each module can be independently maintained, and the standardized interfaces simplify the maintenance process across the entire system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The propulsion modules are designed with universal characteristics that allow them to be interchanged and maintained using the same procedures and equipment. This universality reduces maintenance complexity while preserving the system's overall capability and versatility.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Strength

If proprietary connection methods are used for propulsion modules, then the modules can be securely attached, but the ease of replacement and maintenance is reduced

Engineering Contradiction:
Improveconnection strengthVSAvoidmodule replacement ease
Core Design Contradiction:
StrengthVSEase of repair

Solution Approach 1:

The connection system employs dynamic elements such as spring-loaded electrical contacts and mechanically coupled features that provide secure attachment during operation. These same dynamic features enable easy disconnection and replacement when maintenance is needed, balancing connection strength with replacement ease.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS9975644B1Aerial vehicle propulsion modules
Publication Date: 2018.05.22 AMAZON TECH INC
  • US9975644B1 patent drawing
  • US9975644B1 patent drawing
  • US9975644B1 patent drawing

AI summary

An aerial vehicle may be equipped with propulsion modules that include motors, sensors, transceivers, controllers, power sources or other components therein. The propulsion modules may be releasably mounted to the aerial vehicle in a manner that allows a propulsion module to be removed and replaced when one or more of the components within the propulsion module requires maintenance or repairs, thereby enabling the aerial vehicle to return to service promptly. The propulsion modules may communicate via wired or wireless means with one another, or with a central computer system onboard the aerial vehicle. The propulsion modules may be interchangeably installed on each of the aerial vehicles in a class, or on aerial vehicles in different classes. Furthermore, aerial vehicles may be equipped with varying numbers of propulsion modules, as needed, subject to one or more operational requirements or constraints.