Rotolatch Female Latch for Actuator-Free Drone Package Release

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current drone delivery systems face limitations in fully automated package loading and unloading, requiring human intervention, which affects delivery efficiency and range, and existing fasteners are not suitable for all applications due to magnetism or vacuum grasp issues.

Innovation Solution

An advanced rotating tension latch system is developed for drones, allowing for automated package engagement and disengagement without actuators, which is lightweight and improves package stability, reducing precision requirements and increasing flight performance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Extent of automation

If actuator-based fastening systems are used for automated drone package delivery, then automation capability is improved, but device weight and complexity increase

Engineering Contradiction:
Improveautomated package loading and unloadingVSAvoiddrone weight
Core Design Contradiction:
Extent of automationVSWeight of moving object

Solution Approach 1:

The patent removes the actuator component from the fastening system, extracting the heavy mechanical actuation mechanism while retaining the essential latching function. The rotolatch uses passive spring-loaded engagement and manual rotation for operation, eliminating motors, sensors, and control electronics that would add weight and complexity to the drone system.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The rotolatch system employs self-actuating spring mechanisms that automatically engage and disengage the latch without requiring external power sources or control systems. The spring-loaded design provides automatic reset and engagement capabilities, making the system self-sufficient and eliminating the need for drone-borne actuators or power consumption for fastening operations.

Inventive Principle:
Principle #25Self-service

2Extent of automation

If actuator-based fastening systems are used for automated drone package delivery, then automation capability is improved, but device complexity increases

Engineering Contradiction:
Improveautomated package loading and unloadingVSAvoidfastening system complexity
Core Design Contradiction:
Extent of automationVSDevice complexity

Solution Approach 1:

The patent removes the actuator component from the fastening system, extracting the heavy mechanical actuation mechanism while retaining the essential latching function. The rotolatch uses passive spring-loaded engagement and manual rotation for operation, eliminating motors, sensors, and control electronics that would add weight and complexity to the drone system.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The rotolatch system employs self-actuating spring mechanisms that automatically engage and disengage the latch without requiring external power sources or control systems. The spring-loaded design provides automatic reset and engagement capabilities, making the system self-sufficient and eliminating the need for drone-borne actuators or power consumption for fastening operations.

Inventive Principle:
Principle #25Self-service

3Ease of manufacture

If traditional fasteners are used for package attachment, then ease of manufacture is improved, but adaptability to different applications deteriorates

Engineering Contradiction:
Improvefastener manufacturingVSAvoidapplication suitability
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The rotolatch design incorporates a universal engagement mechanism that can attach to various package types and drone configurations. The spring-loaded latch with rotating engagement features provides adaptable fastening capability across different application scenarios, while maintaining simple manufacturing processes suitable for mass production.

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

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

Enables fully automated package loading and unloading across various locations, enhancing delivery efficiency and range by improving flight stability and reducing the need for complex actuator-based systems.

Implementation Method 1

a spring operable to bias the cam in the engaged position and drive the hook to rotate

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

The latch does not require rotational accuracy and can be used with gravity as the axial force

Methodology Applied
Scientific EffectGravitation: Gravitation

Data Source

PatentUS20260022727A1Improved Rotolatch Configurations
Publication Date: 2026.01.22 ROTOLATCH LLC
  • US20260022727A1 patent drawing
  • US20260022727A1 patent drawing
  • US20260022727A1 patent drawing

AI summary

Provided is a female latch member and a pick-and-place system. The female latch member, in at least one aspect, includes a top enclosed aperture having a central axis and an inside surface. The female latch member, according to this aspect, further includes one or more prong receiving holes located along a top thereof of the top enclosed aperture, the one or more prong receiving holes configured to receive one or more prongs of a receiver therein to prevent two pins of a related hook member from unintentionally rotating through first and second channels and allowing the female latch member and the related hook member from decoupling from one another.