Radial Windbreak Layout for Stable VTOL Take-Off and Landing

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Solution Overview

Problem

Existing airports for vertical take-off and landing aircrafts (VTOL) suffer from destabilizing wind flows, such as secondary flows and vortices, which compromise the stability and safety of aircraft during take-off and landing due to the configuration of windbreak walls surrounding the landing area.

Innovation Solution

The airport design incorporates three or more radially extending windbreak walls with partitioned take-off and landing areas, featuring open radially outer portions and slits between adjacent areas to minimize destabilizing wind effects, and includes a control device for directing aircraft to optimal landing zones based on wind conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If four walls surround four sides of a landing point to reduce cross wind influence, then the vertical take-off and landing aircraft can take off and land more safely, but a complicated vortex is formed in the landing place which destabilizes the posture of the aircraft

Engineering Contradiction:
Improvesafety of take-off and landingVSAvoidcomplicated vortex and secondary flow
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent divides the landing area into multiple sectors using three or more windbreak walls that extend radially from a central axis. Each wall creates a separate sector, allowing wind to be blocked effectively while preventing the formation of complicated vortices that would occur with a fully enclosed four-wall structure. The radial arrangement ensures that wind flows are managed in a controlled manner without creating destabilizing secondary flows.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent employs an asymmetric radial configuration where three or more walls extend from a central axis at different angles, creating unequal sector divisions. This asymmetric arrangement prevents the symmetric vortex formation that occurs with traditional four-sided enclosures, as the wind flow paths are intentionally made unequal to disrupt vortex development while maintaining effective wind protection.

Inventive Principle:
Principle #4Asymmetry

2Object-affected harmful factors

If three or more windbreak walls extend radially to partition take-off and landing areas, then destabilizing wind flows are suppressed, but the device complexity increases

Engineering Contradiction:
Improvedestabilizing wind flowVSAvoidnumber of windbreak walls
Core Design Contradiction:
Object-affected harmful factorsVSDevice complexity

Solution Approach 1:

Instead of enclosing the landing area with walls on all four sides (traditional approach), the patent inverts the approach by using three or more radial walls that extend from a central axis outward, creating open sectors rather than a closed enclosure. This inverted radial configuration effectively blocks destabilizing wind flows from multiple directions while maintaining structural simplicity through the shared central support structure.

Inventive Principle:
Principle #13The other way round (Inversion)

Solution Approach 2:

The patent merges multiple wall structures into a unified radial system where three or more windbreak walls share a common central axis and support structure. This consolidation reduces overall structural complexity compared to four separate enclosed walls, as the radial walls can be supported by a central column or hub, efficiently using shared structural elements to achieve wind protection across multiple sectors.

Inventive Principle:
Principle #5Merging (Combining)

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 design stabilizes the posture of VTOL aircraft during take-off and landing by reducing secondary flows and vortices, enhances safety, improves land use efficiency, and allows multiple aircraft to operate simultaneously, thereby increasing operational efficiency.

Implementation Method 1

three or more windbreak walls that extend radially about a reference axis... capable of suppressing a wind flow that destabilizes a posture of the vertical take-off and landing aircraft

Methodology Applied
Scientific EffectWind flow blocking and redirection:

Data Source

PatentUS12539987B2Airport for vertical take-off and landing aircraft
Publication Date: 2026.02.03 HITACHI LTD
  • US12539987B2 patent drawing
  • US12539987B2 patent drawing
  • US12539987B2 patent drawing

AI summary

An airport for a vertical take-off and landing aircraft includes three or more windbreak walls that extend radially about a reference axis, and three or more take-off and landing areas for the vertical take-off and landing aircrafts, which are partitioned by two adjacent windbreak walls among the three or more windbreak walls.