UAV Vertical Passage Pressure Control for Stable Flight

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Solution Overview

Problem

Unmanned aerial vehicles with rotary wings experience instability when ascending and descending in passage spaces due to air pressure differences caused by air conditioning or other environmental factors, leading to increased energy consumption and reduced flight efficiency.

Innovation Solution

An operation facility with a passage space extending in the up-down direction equipped with an air pressure control system that maintains a lower air pressure above the unmanned aerial vehicle than below it, using an air discharge unit and an air supply unit to manage air pressure and stabilize flight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the unmanned aerial vehicle ascends and descends in a passage space with conventional air pressure control, then the passage space can be used for vertical transport, but the flight becomes unstable due to air pressure differences caused by air conditioning or environmental factors

Engineering Contradiction:
Improveflight stabilityVSAvoidair pressure control system
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent applies parameter changes by actively controlling air pressure in the passage space to create a pressure gradient where pressure above the unmanned aerial vehicle is lower than pressure below it. This parameter change in air pressure distribution provides a stabilizing force that counteracts flight instability, allowing the vehicle to maintain stable flight during vertical movement through the passage space.

Inventive Principle:
Principle #35Parameter changes

2Use of energy by moving object

If the unmanned aerial vehicle operates in a passage space without air pressure control, then the system is simpler, but energy consumption increases due to the need for additional lift force to overcome unstable air pressure conditions

Engineering Contradiction:
Improveenergy consumptionVSAvoidair pressure control system
Core Design Contradiction:
Use of energy by moving objectVSDevice complexity

Solution Approach 1:

By changing the air pressure parameter in the passage space to create a pressure gradient, the system reduces the energy consumption of the unmanned aerial vehicle. The pressure difference generates a stabilizing force that assists the vehicle's lift, reducing the power needed from the vehicle's propulsion system to maintain stable flight during vertical transport.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If air pressure in the passage space is not controlled, then the air conditioning system is simpler, but flight stability deteriorates due to air pressure differences from environmental factors

Engineering Contradiction:
Improveflight stabilityVSAvoidair conditioning energy
Core Design Contradiction:
ReliabilityVSUse of energy by stationary object

Solution Approach 1:

The patent implements parameter changes by using the air conditioning system to actively control and maintain a specific air pressure gradient in the passage space. This controlled pressure distribution, where pressure above the vehicle is lower than pressure below it, stabilizes flight while the energy cost is managed through efficient pressure control rather than temperature control alone.

Inventive Principle:
Principle #35Parameter changes

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

This configuration stabilizes the flight of the unmanned aerial vehicle, reducing energy consumption and improving flight efficiency by ensuring a consistent lift force.

Implementation Method 1

an air pressure control system configured to control air pressure in the passage space, wherein the air pressure control system performs control in such a manner that an air pressure above the unmanned aerial vehicle is lower than an air pressure below the unmanned aerial vehicle

Methodology Applied
Scientific EffectAir pressure difference: Pressure Gradient

Data Source

PatentUS20240077893A1Operation Facility for Unmanned Aerial Vehicle
Publication Date: 2024.03.07 DAIFUKU CO LTD
  • US20240077893A1 patent drawing
  • US20240077893A1 patent drawing
  • US20240077893A1 patent drawing

AI summary

An operation facility for an unmanned aerial vehicle with rotary wing of the present invention includes: a passage space that extends in the up-down direction and is for the ascent and descent of the unmanned aerial vehicle; and an air pressure control system that controls the air pressure in the passage space. The air pressure control system performs control such that the air pressure above the unmanned aerial vehicle is lower than the air pressure below the unmanned aerial vehicle.