Helicopter-Mediated Aircraft Launch and Retrieval System

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Solution Overview

Problem

Aircraft capable of long-distance efficient cruising flight typically require long runways for take-off and landing, making them unsuitable for use in spaces with insufficient runway space.

Innovation Solution

A helicopter-mediated system and method that uses connectors and mating devices to link a helicopter with an aircraft, allowing for launch and retrieval without a long runway, enabling secure connection and disconnection in various flight phases, including hover and wing-borne flight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Use of energy by moving object

If an aircraft is designed for long-distance efficient cruising flight, then cruising efficiency is improved, but runway length requirement increases

Engineering Contradiction:
Improvecruising efficiencyVSAvoidrunway length
Core Design Contradiction:
Use of energy by moving objectVSLength of stationary object

Solution Approach 1:

A helicopter acts as an intermediary vehicle to launch and retrieve the fixed-wing aircraft. The helicopter mediates the takeoff and landing process by carrying the aircraft to and from the runway, allowing the aircraft to operate from locations with limited runway infrastructure while maintaining its efficient cruising capability.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The launch and retrieval operation is segmented into multiple phases: helicopter approaches the aircraft, connectors engage to link the two vehicles, helicopter lifts the aircraft to altitude, and finally the aircraft is released for autonomous flight. This segmentation allows each vehicle to perform its optimal function without requiring the aircraft to use a long runway for takeoff.

Inventive Principle:
Principle #1Segmentation

2Use of energy by moving object

If an aircraft is designed for long-distance efficient cruising flight, then cruising performance is improved, but adaptability to small spaces deteriorates

Engineering Contradiction:
Improvecruising performanceVSAvoidadaptability to small spaces
Core Design Contradiction:
Use of energy by moving objectVSAdaptability or versatility

Solution Approach 1:

The system combines two different aircraft types with complementary capabilities: the helicopter provides vertical takeoff and landing capability suitable for small spaces, while the fixed-wing aircraft provides efficient long-distance cruising. Together, they form a universal system that can operate from both constrained and unconstrained environments.

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

Solution Approach 2:

The helicopter serves as an intermediary that enables the fixed-wing aircraft to access small spaces. The helicopter transports the aircraft to the launch point, allowing the aircraft to operate from locations that would otherwise be inaccessible due to its long runway requirements.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If connectors and mating devices are designed for secure connection during flight, then connection reliability is improved, but device complexity increases

Engineering Contradiction:
Improveconnection reliabilityVSAvoidconnector complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The mating devices are designed to automatically engage and lock when the helicopter and aircraft come into proximity. The connectors include self-aligning features and automatic locking mechanisms that require minimal manual intervention, reducing operational complexity while maintaining high connection reliability during dynamic flight conditions.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS10144511B2Helicopter-mediated system and method for launching and retrieving an aircraft
Publication Date: 2018.12.04 HOOD TECHNOLOGY CORP
  • US10144511B2 patent drawing
  • US10144511B2 patent drawing

AI summary

Various embodiments of the present disclosure provide a helicopter-mediated system and method for launching and retrieving an aircraft capable of long-distance efficient cruising flight from a small space without the use of a long runway.