Hydrogen Balloon UAV for Silent Long-Endurance Flight

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Solution Overview

Problem

Unmanned aerial vehicles with fixed wings cannot stay in the air for long periods and require a track for take-off and landing, limiting their operational capabilities and stability.

Innovation Solution

An autonomous unmanned aerial vehicle equipped with a balloon inflated behind it, using a combination of internal combustion and electrical engines, allowing vertical take-off and landing, silent long-duration flight, and eliminating the need for a landing track, with a hydrogen fuel system for eco-friendliness.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If fixed-wing unmanned aerial vehicles are used, then flight speed and range are improved, but flight duration is limited and a landing track is required

Engineering Contradiction:
Improveflight speedVSAvoidflight duration
Core Design Contradiction:
SpeedVSDuration of action of moving object

Solution Approach 1:

The aerial vehicle is divided into two main functional segments: a fixed-wing aircraft portion for high-speed flight and a balloon portion for stationary hovering. This segmentation allows each component to perform its optimal function - the fixed wings provide speed and range while the balloon provides extended duration by enabling stationary airtime without requiring continuous forward motion or a landing track

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention merges a fixed-wing aircraft with a balloon system into a single integrated aerial vehicle. The balloon is attached to the fixed-wing aircraft, combining the high-speed capabilities of fixed-wing flight with the stationary hovering capability of balloons, thereby eliminating the need for a landing track while extending flight duration

Inventive Principle:
Principle #5Merging (Combining)

2Length of moving object

If fixed-wing unmanned aerial vehicles are used, then flight range is improved, but stability and operational flexibility deteriorate due to requiring a landing track

Engineering Contradiction:
Improveflight rangeVSAvoidoperational flexibility
Core Design Contradiction:
Length of moving objectVSAdaptability or versatility

Solution Approach 1:

By segmenting the vehicle into fixed-wing and balloon portions, the system can operate in two distinct modes: high-speed transit mode using the fixed wings for extended range, and stationary mission mode using the balloon for stable positioning without requiring a landing track, thereby improving operational flexibility

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The merged fixed-wing and balloon system provides adaptability by allowing the vehicle to transition between different operational states - using the fixed wings for long-range travel and the balloon for stable stationary operations, eliminating the constraint of requiring a landing track for takeoff and landing

Inventive Principle:
Principle #5Merging (Combining)

3Power

If conventional engines are used, then thrust and power are improved, but noise level increases reducing stealth capability

Engineering Contradiction:
Improveengine powerVSAvoidnoise level
Core Design Contradiction:
PowerVSObject-generated harmful factors

Solution Approach 1:

The balloon acts as an intermediary element that enables the vehicle to transition from powered flight to passive stationary hovering. Once the balloon is inflated, the engine can be reduced or shut off, and the vehicle maintains its position using buoyant forces, thereby eliminating engine noise while preserving the ability to generate thrust when needed

Inventive Principle:
Principle #24Intermediary (Mediator)

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 prolonged silent flight, precise image capture, and stable operation without the need for a landing track, with enhanced load-bearing capacity and control, while being eco-friendly and adaptable to various environments.

Implementation Method 1

a balloon (7) which is wrapped around the liquid hydrogen tank (6), which is inflated with the hydrogen in the liquid hydrogen tank (6), and enables suspension of the unmanned aerial vehicle in the air

Methodology Applied
Scientific EffectBuoyancy: Archimedes' Principle (Buoyancy)

Implementation Method 2

An autonomous unmanned aerial vehicle equipped with a balloon inflated behind it, using a combination of internal combustion and electrical engines

Methodology Applied
Scientific EffectCombustion: Combustion

Data Source

PatentUS11535375B2Autonomous unmanned aerial vehicle
Publication Date: 2022.12.27 MITOS MIKRODALGA GORUNTULEME SISTEMLERI MUHENDISLIK SANAYI VE TICARET LTD SIRKETI
  • US11535375B2 patent drawing
  • US11535375B2 patent drawing
  • US11535375B2 patent drawing

AI summary

An autonomous unmanned aerial vehicle for land, sea and air use. The autonomous unmanned aerial vehicle is more specifically related to an unmanned aerial vehicle, wherein the autonomous unmanned aerial vehicle is configured to vertically take off and vertically land, fly with fixed wings and stay in the air silently for a long time by means of a balloon inflated behind it.