Elevated VTOL Docking Pole Reduces Ground Noise

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Solution Overview

Problem

Existing take-off and landing technologies for vertical take-off and landing aircrafts face challenges in reducing airflow and noise impact on the environment, and require significant site space for operations, which is limited in urban areas.

Innovation Solution

A take-off and landing apparatus comprising a take-off and landing pole, a mooring transfer base, and a sleeve docking device, which allows the aircraft to start or stop at a position away from the ground, reducing airflow and noise impact during operations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Area of stationary object

If vertical take-off and landing aircraft operate close to the ground, then site space usage is reduced, but airflow and noise impact on the environment increases

Engineering Contradiction:
Improvesite spaceVSAvoidairflow and noise impact
Core Design Contradiction:
Area of stationary objectVSObject-generated harmful factors

Solution Approach 1:

The patent introduces a vertical dimension by using a take-off and landing pole that extends upward from the ground. The aircraft docks at an elevated position on the pole rather than at ground level, effectively moving the operation point to a higher vertical dimension. This resolves the contradiction by maintaining compact ground footprint while reducing harmful ground-level airflow and noise impact.

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

Solution Approach 2:

The take-off and landing pole serves as an intermediary structure between the ground and the aircraft. It provides an elevated docking platform that mediates the interaction between the aircraft and the ground environment, allowing the aircraft to operate close to the ground site while minimizing direct harmful effects on the ground level through the pole's protective structure.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of operation

If helicopter landing platforms are installed on building roofs, then take-off and landing capability is achieved, but site space constraints in urban areas are not adequately addressed

Engineering Contradiction:
Improvetake-off and landing capabilityVSAvoidsite space
Core Design Contradiction:
Ease of operationVSArea of stationary object

Solution Approach 1:

Instead of requiring horizontal roof space for traditional helicopter platforms, this invention utilizes the vertical dimension by extending a docking pole upward from the ground or building facade. The aircraft docks at an elevated point on the pole, transforming the space requirement from horizontal (roof area) to vertical (pole height), thereby solving urban space constraints while maintaining full take-off and landing capability.

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

3Productivity

If multiple aircraft operate simultaneously in urban areas, then transportation capacity increases, but limited land use conditions create restrictions

Engineering Contradiction:
Improvetransportation capacityVSAvoidland use
Core Design Contradiction:
ProductivityVSArea of stationary object

Solution Approach 1:

The take-off and landing pole is designed with multiple docking levels or positions along its length, allowing multiple aircraft to dock at different vertical levels simultaneously. This segmentation of the docking space into multiple vertical zones enables increased transportation capacity without requiring proportionally more ground area, effectively resolving the contradiction between productivity and land use constraints.

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 apparatus effectively reduces the environmental impact of airflow and noise during take-off and landing, and optimizes site space usage by enabling vertical take-off and landing aircrafts to operate in constrained urban environments.

Implementation Method 1

a top of the take-off and landing pole is provided with a contact head, the contact head is elastic

Methodology Applied
Scientific EffectElasticity: Elasticity

Data Source

PatentUS12269626B2Take-off and landing apparatus for vertical take-off and landing aircraft
Publication Date: 2025.04.08 ZHU NING
  • US12269626B2 patent drawing
  • US12269626B2 patent drawing
  • US12269626B2 patent drawing

AI summary

A take-off and landing apparatus for a vertical take-off and landing aircraft is disclosed, including a take-off and landing pole, a mooring transfer base and a sleeve docking device. The top of the take-off and landing pole is provided with a contact head which is elastic. The mooring transfer base is disposed on the take-off and landing pole, the mooring transfer base is movable along the take-off and landing pole, the mooring transfer base is configured to receive the vertical take-off and landing aircraft. The sleeve docking device is disposed on the vertical take-off and landing aircraft, and the sleeve docking device is provided with a docking hole adapted to the take-off and landing pole.