Standardized Drone Carrier Pod Attachment Interface

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Solution Overview

Problem

Current passenger drone systems lack standardization, making them incompatible across different manufacturers, limiting flexibility and convenience in transportation, and are not designed to efficiently carry multiple passengers or parcels simultaneously.

Innovation Solution

A drone transport system featuring standardized carrier pods with attachment interfaces that can be easily connected and disconnected from flight-enabled drones, allowing for the carriage of passengers or parcels, with redundant attachment elements for safety and the ability to carry multiple pods, powered by rechargeable batteries with dual redundancy, and integrated control systems for navigation and communication.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If single-unit passenger drones are used, then each drone can operate independently, but the system lacks flexibility and compatibility across different manufacturers

Engineering Contradiction:
Improvesystem flexibilityVSAvoiddrone system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The drone system is divided into separate functional modules: a standardized carrier pod for passengers/cargo and a flight-enabled drone for transportation. This segmentation allows different manufacturers to produce compatible components that can be combined, improving system flexibility without requiring complete system redesign.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The carrier pod is designed with universal attachment interfaces that can be used across different drone models and manufacturers. The standardized interface enables a single pod to be compatible with multiple drone types, creating a multi-functional system that improves adaptability.

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

2Adaptability or versatility

If standardized attachment interfaces are implemented, then compatibility and flexibility improve, but attachment reliability may be compromised

Engineering Contradiction:
Improveinterface compatibilityVSAvoidattachment reliability
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The attachment interface incorporates redundant attachment elements (multiple attachment points) that provide backup connections. This beforehand cushioning ensures that if one attachment element fails, others can maintain the connection, preserving reliability while using standardized interfaces.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Solution Approach 2:

Different parts of the attachment interface have specialized functions: some elements are optimized for strength and others for quick release. This local quality optimization ensures that each component performs its specific function effectively, maintaining overall reliability while achieving standardization.

Inventive Principle:
Principle #3Local quality

3Productivity

If multiple pods are carried by a single drone, then transportation efficiency increases, but the drone's payload capacity and control complexity increase

Engineering Contradiction:
Improvetransportation efficiencyVSAvoidcontrol system complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

Multiple carrier pods are combined and attached to a single flight-enabled drone, allowing the drone to transport multiple passengers or cargo units simultaneously. This merging approach increases transportation efficiency by reducing the number of individual flights required.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The drone's control system dynamically adjusts to the changing payload configuration as pods are attached or detached. The system can adapt its flight characteristics, balance, and control responses in real-time, managing complexity through dynamic adjustment rather than static design.

Inventive Principle:
Principle #15Dynamics

4Reliability

If redundant attachment elements are used, then safety improves, but the device complexity and weight increase

Engineering Contradiction:
ImprovesafetyVSAvoiddrone weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

Redundant attachment elements are incorporated into the standardized interface design, providing backup connection points that enhance safety. These redundant elements are distributed throughout the interface structure, ensuring safety without requiring excessive additional weight.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Solution Approach 2:

The attachment elements use optimized material properties and structural parameters to achieve high strength-to-weight ratios. By changing material parameters and structural geometry, the redundant elements provide necessary safety while minimizing weight penalty.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS10207805B2Drone transport system
Publication Date: 2019.02.19 EVANS MICHAEL STEWARD
  • US10207805B2 patent drawing
  • US10207805B2 patent drawing
  • US10207805B2 patent drawing

AI summary

A drone transport system has a carrier pod adapted for carrying a passenger or parcels with the passenger or parcels enclosed, the carrier pod having a first attachment interface at an uppermost extremity, the attachment interface having one or first physical attachment elements, and a flight-enabled drone having a downward-facing second attachment interface having one or more second physical attachment elements compatible with the first physical attachment elements of the carrier pod. The flight-enabled drone is controllable to approach the carrier pod from above, to align and engage the second physical attachment elements with the first physical attachment elements, to lift and carry the pod from one place to another, and to land and disengage the first and second physical attachment elements, leaving the carrier pod at a new place.