Modular UAV Mission Pod with Self-Aligning Attachment

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Solution Overview

Problem

Existing UAV systems with external mission pods are often purpose-built for specific missions, making them inflexible and requiring extensive ground crew intervention for installation and reconfiguration, limiting their versatility and efficiency in conducting diverse missions.

Innovation Solution

A standardized, modular mission pod system that can be easily attached and detached from UAVs without ground crew intervention, featuring mechanisms for secure attachment, power, fuel, and data transfer, and supporting various sensing modalities, enabling the UAV to perform a range of missions including ISR, cargo transport, and global strike.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If purpose-built external mission pods are used for specific missions, then mission-specific performance is improved, but adaptability and versatility deteriorate

Engineering Contradiction:
Improvemission-specific performanceVSAvoidmission flexibility
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The pod interface is designed with universal mounting structures, standardized electrical connectors, and common communication protocols that enable a single pod design to perform multiple mission types. The mounting interface accommodates different payload configurations while maintaining structural integrity, and the electrical interface supports various power and data transfer requirements across different mission scenarios.

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

Solution Approach 2:

The mission pod system is segmented into modular components: a standardized interface structure, interchangeable payload modules, and configurable electrical connections. This segmentation allows the same base pod to be rapidly reconfigured for different missions by swapping payload modules without replacing the entire pod assembly.

Inventive Principle:
Principle #1Segmentation

2Reliability

If ground crew intervention is required for pod installation and reconfiguration, then attachment security is improved, but operational efficiency and productivity deteriorate

Engineering Contradiction:
Improveattachment securityVSAvoidoperational efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The pod mounting system incorporates self-aligning features with guide rails and positioning pins that automatically align the pod with the aircraft fuselage during attachment. The electrical connectors include self-latching mechanisms that secure connections without manual intervention, and the system provides visual or electronic confirmation when proper attachment is achieved, enabling unattended installation and reconfiguration.

Inventive Principle:
Principle #25Self-service

3Adaptability or versatility

If standardized modular pod system is implemented, then adaptability and versatility are improved, but device complexity increases

Engineering Contradiction:
Improvemission diversityVSAvoidsystem complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

A standardized interface architecture provides universal mounting brackets, electrical connectors, and communication protocols that work across all pod types and mission configurations. This universal interface reduces the variety of unique components needed, thereby reducing overall system complexity while maintaining high adaptability.

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

Solution Approach 2:

The pod system employs homogeneous mounting structures, connector types, and interface standards across all pods. This homogeneity simplifies the interface design, reduces the number of unique parts, and facilitates easier integration and maintenance, thereby reducing device complexity while enabling mission diversity through payload interchangeability.

Inventive Principle:
Principle #33Homogeneity

4Productivity

If rapid unattended pod switching is enabled, then productivity and operational efficiency are improved, but attachment reliability may deteriorate

Engineering Contradiction:
Improvepod switching speedVSAvoidattachment reliability
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The pod mounting system includes pre-positioned alignment features, pre-engaged safety latches, and pre-configured electrical connectors that are ready for rapid engagement. The self-aligning guide rails and positioning mechanisms are pre-installed on the aircraft fuselage, eliminating the need for complex real-time alignment during pod switching and enabling rapid attachment while maintaining reliability.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The attachment system incorporates self-verifying mechanisms that automatically confirm proper pod engagement through mechanical interlocks, electrical connection verification, and sensor feedback. These self-checking features provide immediate confirmation of reliable attachment without requiring manual verification, enabling rapid pod switching while ensuring attachment reliability is maintained.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS11884391B2Mission pod for unattended UAV operations
Publication Date: 2024.01.30 ELROY AIR INC
  • US11884391B2 patent drawing
  • US11884391B2 patent drawing
  • US11884391B2 patent drawing

AI summary

A mission pod configured to be carried by a UAV or other aerial vehicle and accompanying systems and methods to allow the unattended accomplishment of diverse mission types is described. The mission pod having means for communication between the pod and UAV, mechanisms for removably attaching the pod to, and detaching the pod from, the UAV without the intervention of ground crew, mechanisms for facilitating power, fuel, and/or data transfer between the pod and UAV, means for securing various mission components within the pod, and pod configurations supporting various sensing modalities and other mission requirements.