Removable UAV Adapter Assemblies for Launcher Compatibility

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Solution Overview

Problem

Fixed wing UAVs typically require a large runway for deployment, which is not always available, and existing launchers are often manufacturer-specific, limiting flexibility and accessibility.

Innovation Solution

The development of adapter assemblies that can be removeably coupled to UAVs, allowing them to interface with various launchers, enabling deployment on different types of launchers and reducing the need for a runway by using a carriage that accelerates along a short track to propel the UAV into the air.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If fixed wing UAVs use traditional runway-based deployment, then they achieve reliable takeoff, but they require a large runway which is not always available

Engineering Contradiction:
Improvedeployment location flexibilityVSAvoidrunway length
Core Design Contradiction:
Adaptability or versatilityVSLength of stationary object

Solution Approach 1:

The patent introduces a launcher as an intermediary device between the ground and the UAV. The launcher includes a carriage that moves along a track and provides a grip mechanism to hold and propel the UAV. This intermediary system enables UAV deployment in locations without traditional runways by providing a compact alternative launch mechanism.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The launcher system is segmented into distinct functional components: a track structure, a movable carriage with grip portions, and a release mechanism. This segmentation allows the system to be compact while providing the necessary functions for UAV deployment, eliminating the need for a long continuous runway.

Inventive Principle:
Principle #1Segmentation

2Adaptability or versatility

If manufacturer-specific launchers are used, then the launcher is optimized for specific UAVs, but flexibility and accessibility are limited

Engineering Contradiction:
Improvelauncher compatibilityVSAvoidlauncher configuration complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The launcher is designed with universal features that allow it to accommodate different UAV types. The grip portions can be adjusted or configured to match different UAV configurations, and the track system can be adapted to various mounting surfaces. This multi-functionality enables a single launcher design to serve multiple UAV models without requiring completely different launcher systems for each manufacturer.

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

3Adaptability or versatility

If adapter assemblies are removeably coupled to UAVs, then flexibility in launcher selection is improved, but the coupling process becomes more complex

Engineering Contradiction:
Improvelauncher selection flexibilityVSAvoidadapter assembly coupling
Core Design Contradiction:
Adaptability or versatilityVSEase of manufacture

Solution Approach 1:

The adapter assembly is pre-configured with specific coupling features that match the launcher's grip portions. The mounting brackets and attachment mechanisms are prepared in advance during adapter manufacturing, so that during deployment, the adapter can be quickly attached to the UAV without complex field assembly procedures. This preliminary preparation simplifies the coupling process while maintaining flexibility.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentEP4079635B1Adapter assemblies for aircraft and launchers for deploying aircraft
Publication Date: 2025.01.01 INSITU INC
  • EP4079635B1 patent drawingFigure 1A~1C
  • EP4079635B1 patent drawingFigure 2
  • EP4079635B1 patent drawingFigure 3

AI summary

Adapter assemblies for aircraft and launchers for deploying aircraft are described herein. An example adapter assembly for an unmanned aerial vehicle (UAV) includes a first adapter to be removeably coupled to a first side of a fuselage of the UAV. The first adapter includes first and second posts to interface with a carriage of a launcher. The adapter assembly also includes second adapter to be removeably coupled to a second side of the fuselage of the UAV. The second adapter includes third and fourth posts to interface with the carriage of the launcher. (Fig. 3)