Movable Panel Vertical-Lift Augmentation System

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Solution Overview

Problem

Current ducted-rotor aircraft systems lack an efficient mechanism to augment vertical lift, particularly in transitioning between helicopter and airplane modes, which affects their operational versatility and efficiency.

Innovation Solution

A vertical-lift augmentation system comprising fan banks mounted on the aircraft's wings and fuselage, with adjustable panels that can enclose or expose the fans, allowing for engagement or disengagement to provide augmented vertical thrust in helicopter mode and reduce drag in airplane mode.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Force

If fan banks are mounted on the aircraft to provide augmented vertical thrust, then vertical lift capability is improved, but drag increases in airplane mode

Engineering Contradiction:
Improvevertical thrustVSAvoiddrag
Core Design Contradiction:
ForceVSObject-generated harmful factors

Solution Approach 1:

The panel is made movable between different positions (enclosed and exposed) to dynamically adjust the configuration based on flight mode. In helicopter mode, the panel encloses the fan bank to maximize vertical thrust; in airplane mode, the panel moves to expose the fan bank, reducing drag while maintaining flight capabilities.

Inventive Principle:
Principle #15Dynamics

2Force

If the aircraft operates in helicopter mode with enclosed fan banks, then vertical lift is maximized, but operational versatility decreases when transitioning to airplane mode

Engineering Contradiction:
Improvevertical liftVSAvoidoperational flexibility
Core Design Contradiction:
ForceVSAdaptability or versatility

Solution Approach 1:

The movable panel enables the aircraft to adapt its configuration between helicopter and airplane modes. The panel can be positioned to enclose fan banks for vertical lift in helicopter mode, and repositioned to expose fan banks for reduced drag in airplane mode, thus providing operational versatility across different flight regimes.

Inventive Principle:
Principle #15Dynamics

3Productivity

If panels are made movable to enclose or expose fan banks, then operational efficiency is improved, but device complexity increases

Engineering Contradiction:
Improveoperational efficiencyVSAvoidsystem complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The aircraft configuration is segmented into movable panel components and fixed fan bank components. This segmentation allows the panel to be independently moved between enclosed and exposed positions, enabling efficient operation in different flight modes without requiring complex reconfiguration of the entire aircraft system.

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

Enhances vertical thrust in helicopter mode while minimizing drag in airplane mode, improving the aircraft's operational flexibility and efficiency across different flight regimes.

Implementation Method 1

ducted-rotor aircraft systems lack an efficient mechanism to augment vertical lift

Methodology Applied
Scientific EffectAerodynamic lift: Aerofoil

Implementation Method 2

provide augmented vertical thrust in helicopter mode

Methodology Applied
Scientific EffectThrust: Jet

Implementation Method 3

minimizing drag in airplane mode

Methodology Applied
Scientific EffectAerodynamic drag: Drag

Data Source

PatentUS11591081B2Vertical-lift augmentation system
Publication Date: 2023.02.28 TEXTRON INNOVATIONS INC
  • US11591081B2 patent drawing
  • US11591081B2 patent drawing
  • US11591081B2 patent drawing

AI summary

In an embodiment, a vertical-lift augmentation system for an aircraft includes a fan bank mounted to the aircraft in proximity to a wing of the aircraft, where the fan bank may include at least one fan. The vertical-lift augmentation system also includes a panel movably attached to the aircraft in relation to the fan bank, where the panel is adjustable between at least a first position in which the panel encloses the fan bank in the aircraft and a second position in which the panel at least partially exposes the fan bank.