Multi-Stage Pod Capsule UAV Deployment System

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Solution Overview

Problem

Small unmanned aerial vehicles (UAVs) are limited by their short range and endurance, making them unsuitable for long-range missions, and their fragile aero-structural components are prone to damage when launched from high-speed aircraft, restricting their deployment in target regions remote from the launch site.

Innovation Solution

A multi-stage delivery system comprising a pod and capsules that deploy from a high-altitude aircraft, using a parachute for controlled descent and a heat-activated adhesive mechanism to eject the UAV from the capsule, allowing for remote control and extended flight position transition.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Length of stationary object

If small UAVs are launched from high-speed aircraft, then deployment range is extended, but the fragile aero-structural components of the UAV are damaged due to high-speed airflow

Engineering Contradiction:
Improvedeployment rangeVSAvoidaero-structural component integrity
Core Design Contradiction:
Length of stationary objectVSStrength

Solution Approach 1:

The delivery system is divided into multiple stages: a pod that separates from the aircraft, a capsule that separates from the pod, and the UAV that separates from the capsule. This multi-level segmentation allows the UAV to be protected from high-speed airflow during transit while enabling progressive deployment. The pod acts as a protective container during initial separation, the capsule provides additional protection during descent, and only upon reaching the target region does the UAV finally separate to begin operation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system performs preliminary actions by pre-positioning the UAV in a protected capsule that is itself contained within a pod. The pod is deployed from the aircraft first, allowing it to slow down and stabilize before the capsule is ejected. This preliminary deceleration and stabilization action protects the UAV's fragile components from the harmful high-speed airflow that would occur if direct launch attempted.

Inventive Principle:
Principle #10Preliminary action

2Ease of operation

If small UAVs are hand-delivered to within range of target, then operational control is maintained, but military personnel are exposed to great risk

Engineering Contradiction:
Improveoperational controlVSAvoidrisk to personnel
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The pod-capsule-UAV delivery system acts as an intermediary mechanism that transfers the UAV from the aircraft to the target region without requiring personnel to physically transport it. The automated delivery system maintains operational control through remote monitoring and control systems while eliminating the need for personnel to approach hazardous target zones, thus resolving the contradiction between maintaining control and reducing personnel risk.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Ease of operation

If small UAVs are brought close to location of use, then deployment is simple, but operators are required to be in proximity to target location

Engineering Contradiction:
Improvedeployment simplicityVSAvoidoperator proximity to target
Core Design Contradiction:
Ease of operationVSLength of stationary object

Solution Approach 1:

The manual mechanical process of transporting and deploying UAVs is replaced with an automated aerial delivery system. The pod-capsule mechanism uses automated ejection systems, parachutes for controlled descent, and remote activation mechanisms to deploy the UAV without operator intervention during the critical transport and deployment phases. This mechanical substitution maintains simplicity while allowing operators to remain at safe distances.

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

4Productivity

If ground- or air-based launching systems are used, then UAV deployment is achieved, but high-speed airflow damages fragile UAV components

Engineering Contradiction:
Improvedeployment capabilityVSAvoidUAV component integrity
Core Design Contradiction:
ProductivityVSStrength

Solution Approach 1:

The system dynamically adjusts the deployment process through multiple stages with varying velocity profiles. The pod separates from the aircraft at high speed but then uses aerodynamic stabilization and parachute deployment to progressively reduce velocity. The capsule is ejected at controlled speeds and uses its own parachute system to further decelerate before UAV release. This dynamic velocity management allows deployment capability while protecting components by ensuring the UAV experiences minimal airflow stress upon final separation.

Inventive Principle:
Principle #15Dynamics

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 the safe and efficient deployment of small UAVs over long ranges with reduced risk of damage, minimizing human involvement and enhancing operational flexibility for military and commercial applications.

Implementation Method 1

a parachute operable to be deployed after the capsule is ejected from the capsule housing portion for providing a controlled drop of the capsule from the second region to the target region

Methodology Applied
Scientific EffectParachute: Parachute

Implementation Method 2

a heat-activated adhesive mechanism to eject the UAV from the capsule

Methodology Applied
Scientific EffectHeat-activated adhesive: Adhesive

Data Source

PatentUS11390382B1Delivery system for unmanned aerial vehicles
Publication Date: 2022.07.19 THE GOVERNMENT OF THE UNITED STATES AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE
  • US11390382B1 patent drawing
  • US11390382B1 patent drawing
  • US11390382B1 patent drawing

AI summary

A system for deploying an unmanned aerial vehicle in a target region. The system includes a pod configured to be deployed from an air craft in a first region remote from the target region. The pod includes a capsule housing portion and a capsule ejection system in operative communication with the capsule housing portion. A capsule is dimensioned and configured to be disposed in the capsule housing portion as the pod is deployed from the aircraft and is ejected from the capsule housing portion by the capsule ejection system in a second region remote from the first region and the target region. The capsule includes a UAV housing portion dimensioned and configured to encase the unmanned aerial vehicle and a UAV ejection system in operative communication with the UAV housing portion for deploying the unmanned aerial vehicle in the target region.