Host-Parasite Drone Deployment Mechanism for Relay Communication

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Solution Overview

Problem

Unmanned aerial vehicles (UAVs) face challenges with line of sight communication issues and limited flight time due to terrain obstructions and battery power limitations, respectively.

Innovation Solution

Attaching UAVs, referred to as parasite aerial vehicles, to a host aircraft that maintains line of sight with a ground control system, allowing the UAVs to detach and fly closer to the region of interest undetected, with the host aircraft using a series-hybrid power source for extended flight times and a retention mechanism for precise deployment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Duration of action of moving object

If UAVs use point-to-point radios for communication, then communication is possible, but terrain obstructions reduce communication range

Engineering Contradiction:
Improvecommunication rangeVSAvoidterrain obstruction
Core Design Contradiction:
Duration of action of moving objectVSObject-affected harmful factors

Solution Approach 1:

The host aircraft serves as an intermediary communication relay between the parasite UAV and the ground control station. The parasite UAV communicates with the host aircraft via radio, which then relays the communication to the ground control station, bypassing terrain obstructions that would block direct line-of-sight communication.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The host aircraft operates at a higher altitude dimension, allowing it to maintain line-of-sight communication with the ground control station while the parasite UAV operates closer to the terrain. This vertical dimensionality change enables the intermediary to overcome terrain obstructions.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Duration of action of moving object

If UAVs use battery power, then operation is possible, but flight time is limited

Engineering Contradiction:
Improveflight timeVSAvoidbattery energy density
Core Design Contradiction:
Duration of action of moving objectVSUse of energy by moving object

Solution Approach 1:

The parasite UAV merges with the host aircraft's power system by harvesting electrical power during attachment. The host aircraft's electrical system charges the parasite UAV's battery, combining the power resources of both platforms to extend the parasite's operational duration.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The parasite UAV's battery is charged in advance during the attachment phase before deployment. This preliminary energy accumulation allows the parasite to achieve extended flight time without carrying a larger battery, as the charging occurs while the host aircraft is already operational.

Inventive Principle:
Principle #10Preliminary action

3Manufacturing precision

If parasite UAVs are deployed from host aircraft, then deployment precision is improved, but retention mechanism complexity increases

Engineering Contradiction:
Improvedeployment precisionVSAvoidretention mechanism
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The retention mechanism uses magnetic coupling instead of complex mechanical fasteners. The magnetic attachment provides sufficient holding force during flight while allowing for simple, precise deployment through electronic control, reducing mechanical complexity while maintaining deployment precision.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Data Source

PatentUS11815888B1Deployment mechanism, communication and operation for a host-parasite drone system
Publication Date: 2023.11.14 SKYFRONT CORP
  • US11815888B1 patent drawing
  • US11815888B1 patent drawing
  • US11815888B1 patent drawing

AI summary

A carrier aerial vehicle system includes a propulsion component configured to enable the carrier aerial vehicle system to be in flight. The carrier aerial vehicle system further includes a retention mechanism configured to allow a plurality of deployable parasite aerial vehicles to be coupled to the retention mechanism and released from the retention mechanism while the carrier aerial vehicle system is in flight. The carrier aerial vehicle system further includes a communication component configured to enable the carrier aerial vehicle system to wireless communicate with the plurality of parasite deployable aerial vehicles. The carrier aerial vehicle system further includes a processor configured to determine a position on the retention mechanism for each deployable parasite aerial vehicle of the plurality of deployable parasite aerial vehicles.