Rotorcraft Retrieval System for Fixed-Wing Aircraft

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Solution Overview

Problem

Fixed-wing aircraft require long runways for takeoff and landing, limiting their use in areas without sufficient space, and existing aircraft-launch and retrieval systems are inefficient for these aircraft.

Innovation Solution

A rotorcraft-assisted aircraft retrieval system with a winch-equipped retrieval assembly that includes a base, drum, motor, and flexible capture member, allowing a rotorcraft to retrieve a fixed-wing aircraft from wing-borne flight by winding the capture member around the drum and drawing the aircraft closer for landing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If fixed-wing aircraft use long runways for takeoff and landing, then efficient cruising flight is achieved, but the aircraft cannot be used in areas without sufficient space

Engineering Contradiction:
Improveaircraft usability in constrained spacesVSAvoidrunway length
Core Design Contradiction:
Adaptability or versatilityVSLength of stationary object

Solution Approach 1:

A rotorcraft serves as an intermediary platform to launch and retrieve the fixed-wing aircraft. The rotorcraft hovers in place or moves slowly while the fixed-wing aircraft takes off from or lands on its wings, eliminating the need for long runways. This mediator approach allows the fixed-wing aircraft to operate in constrained spaces without requiring traditional runway infrastructure.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The launch and retrieval operation transitions from a ground-based horizontal runway system to an aerial three-dimensional system. The rotorcraft hovers in the air space above the constrained area, and the fixed-wing aircraft takes off by running along the rotorcraft's wings or is launched directly into the air, utilizing vertical and lateral dimensions instead of horizontal ground space.

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

2Productivity

If existing aircraft-launch and retrieval systems are used, then aircraft can be launched without runways, but the systems are inefficient for fixed-wing aircraft

Engineering Contradiction:
Improvelaunch and retrieval efficiencyVSAvoidsystem suitability for fixed-wing aircraft
Core Design Contradiction:
ProductivityVSAdaptability or versatility

Solution Approach 1:

The rotorcraft is designed with multi-functionality to serve both as a transportation platform and as a launch/retrieval system for fixed-wing aircraft. The rotorcraft's wings serve dual purposes: providing lift for the rotorcraft itself and serving as a runway or launch surface for the fixed-wing aircraft. This universal design eliminates the need for separate specialized equipment.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The launch and retrieval functions are merged with the rotorcraft's primary flight capabilities. Instead of using separate ground-based launchers or cranes, the rotorcraft integrates the launch surface (wings) and propulsion system into a single aerial platform that can hover and move to position the fixed-wing aircraft for optimal launch and retrieval operations.

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

Enables the retrieval of fixed-wing aircraft from wing-borne flight without the need for a runway, facilitating efficient launch and retrieval operations in constrained spaces.

Implementation Method 1

The flexible capture member is wound around the drum

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 2

The operator remotely controls the rotorcraft to fly into the wind

Methodology Applied
Scientific EffectAerodynamic force: Aerofoil

Implementation Method 3

The tensioning object is attached to the attachment device

Methodology Applied
Scientific EffectTension: Tension

Data Source

PatentUS11524797B2Aircraft-retrieval system
Publication Date: 2022.12.13 HOOD TECHNOLOGY CORP
  • US11524797B2 patent drawing
  • US11524797B2 patent drawing
  • US11524797B2 patent drawing

AI summary

The present disclosure provides various embodiments of an aircraft retrieval system including winch-equipped retrieval assembly that is removably attachable to a rotorcraft to facilitate retrieval of a fixed-wing aircraft from wing-borne flight.