Emergency Drone With Multidirectional Mini Turbine Propulsion

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Solution Overview

Problem

During emergency responses, public safety personnel often lack sufficient information about the location of threats and surrounding areas, leading to delayed and ineffective responses due to the limitations of existing communication and data collection methods.

Innovation Solution

An emergency response drone equipped with a novel propulsion system using mini turbines and multidirectional propulsion elements, enabling rapid deployment and situational awareness through imaging and sensor technologies, which can be remotely controlled and integrated with external emergency systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of time

If traditional ground-based emergency response methods are used, then personnel can respond to incidents, but they lack sufficient situational awareness and take longer to reach the scene

Engineering Contradiction:
Improveresponse timeVSAvoidsituational awareness
Core Design Contradiction:
Loss of timeVSLoss of information

Solution Approach 1:

The patent transitions from ground-based to aerial-based emergency response by deploying drones that can fly overhead to capture images and video of incident scenes. This dimensional shift provides superior situational awareness and dramatically reduces response time by bypassing ground traffic and physical barriers.

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

2Loss of information

If aerial vehicles are used for emergency response, then situational awareness is improved, but the vehicle must overcome weather obstacles and achieve rapid deployment

Engineering Contradiction:
Improvesituational awarenessVSAvoidweather resistance
Core Design Contradiction:
Loss of informationVSReliability

Solution Approach 1:

The patent employs multiple propulsion elements with adjustable thrust parameters that can adapt to varying weather conditions. The system changes operational parameters such as thrust magnitude and direction to maintain stability and achieve rapid deployment despite wind, rain, or other adverse weather factors.

Inventive Principle:
Principle #35Parameter changes

3Ease of operation

If a propulsion system with multiple outlets is used, then pinpoint direction control is achieved, but the system complexity increases

Engineering Contradiction:
Improvedirection controlVSAvoidpropulsion system complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The patent divides the propulsion system into multiple independent outlet units, each capable of being controlled individually. This segmentation allows pinpoint directional control by selectively activating specific outlets, while the modular architecture actually reduces overall system complexity compared to a single complex propulsion unit.

Inventive Principle:
Principle #1Segmentation

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

The drone provides timely and accurate situational awareness, enhancing response efficiency by quickly reaching incident areas, capturing and disseminating critical information, thereby reducing risks and improving response outcomes in emergency situations.

Implementation Method 1

each propulsion element has a four-way tube fluidly coupled to high pressure elements to propel the drone

Methodology Applied
Scientific EffectPressure gradient: Pressure Gradient

Data Source

PatentUS11794896B2Emergency response drone
Publication Date: 2023.10.24 HUNT GENE
  • US11794896B2 patent drawing
  • US11794896B2 patent drawing
  • US11794896B2 patent drawing

AI summary

An emergency response drone having a multidirectional propulsion system and data capturing equipment and operatively associated computer system for providing information and situational awareness for emergency areas and related targets.