UAV Arm Integrating ESC for Weight Reduction

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Unmanned vehicles face challenges in achieving compactness and lightness due to the need for electronic speed controllers (ESCs) that add weight and hinder design, as these controllers are often separate components within the vehicle.

Innovation Solution

Integrating electronic speed control components directly into the structural arms of the unmanned aerial vehicle (UAV), such as circuit boards with printed components, which serve as both the arm and ESC, eliminating the need for separate ESCs and reducing weight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If separate electronic speed controllers are installed in the unmanned vehicle, then the motor speed control function is achieved, but the vehicle weight increases and compactness is reduced

Engineering Contradiction:
Improvemotor speed control functionVSAvoidvehicle weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent integrates the electronic speed controller (ESC) with the structural arm of the UAV, combining two previously separate components (ESC and arm) into a single integrated unit. This merging eliminates the need for separate ESC housing and mounting structures, directly reducing vehicle weight while maintaining the motor speed control function.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The arm structure is designed to serve multiple functions: it provides structural support for the motor and simultaneously houses the electronic speed controller components. This multi-functionality approach allows the same physical structure to fulfill both mechanical support and electronic control housing roles, reducing overall vehicle weight and improving compactness.

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

2Reliability

If separate electronic speed controllers are installed in the unmanned vehicle, then the motor speed control function is achieved, but the vehicle compactness is reduced

Engineering Contradiction:
Improvemotor speed control functionVSAvoidvehicle volume
Core Design Contradiction:
ReliabilityVSVolume of moving object

Solution Approach 1:

The electronic speed controller components are integrated within the arm structure itself, merging the control function with the structural component. This eliminates the need for separate ESC housing space, reducing the overall vehicle volume and improving compactness while maintaining full motor speed control capability.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The ESC components are nested within the arm structure, with the electronic components housed inside the arm's internal cavity or space. This nesting approach allows the ESC to occupy space that would otherwise be empty or structurally necessary, maximizing space utilization and improving vehicle compactness.

Inventive Principle:
Principle #7Nested doll (Nesting)

3Temperature

If heat-producing electrical components are placed near the propeller, then cooling of the components is improved, but the component placement constraints increase

Engineering Contradiction:
Improveelectronic component temperatureVSAvoidcomponent placement constraints
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The propeller-generated airflow automatically cools the heat-producing electronic components without requiring additional active cooling systems. The rotating propeller creates a natural airflow that passes over the ESC components, providing passive cooling through convection, eliminating the need for fans or heat sinks while managing thermal dissipation.

Inventive Principle:
Principle #25Self-service

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 configuration allows for reduced size, weight, and improved performance, enabling more agile flight and longer flight times by integrating ESC functions into the UAV's structural components, thereby enhancing the vehicle's compactness and performance capabilities.

Implementation Method 1

the heat-producing electrical component is exposed to and located proximate to the propeller to receive airflow generated by the propeller

Methodology Applied
Scientific EffectConvection: Convection

Data Source

PatentUS9981743B2Electronic speed controller arm for vehicle
Publication Date: 2018.05.29 QUALCOMM INC
  • US9981743B2 patent drawing
  • US9981743B2 patent drawing
  • US9981743B2 patent drawing

AI summary

According to various embodiments, an unmanned aerial vehicle (UAV) is provided. The UAV may include a motor controller. The UAV may further include a motor connected to the motor controller. The UAV may further include an arm connected between the motor controller and the motor. The UAV may further include a plurality of electronic speed control components integrated within the arm, the electronic speed control components configured to control the speed of the motor.