Suspended Load Cable Sock for Aircraft Rebound Containment

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Solution Overview

Problem

Existing aircraft hovering systems face risks of steel cables or ropes rebounding elastically and impacting the aircraft, particularly the rotors, during breakage, posing safety hazards while maintaining structural integrity and ease of inspection.

Innovation Solution

The implementation of elastically deformable cables and ropes surrounded by socks that contain the elastic return, ensuring the cables and ropes remain within protective casings, reducing the risk of impact and maintaining structural integrity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If steel cables or ropes are used for suspending loads from hovering aircraft, then the structural integrity and load-bearing capacity are improved, but the risk of elastic rebound impacting the aircraft and rotors during breakage increases

Engineering Contradiction:
Improveload-bearing capacityVSAvoidelastic rebound impact risk
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

A guide structure (such as a guide ring or guide fairing) is introduced as an intermediary component between the cable/rope and the aircraft body. This guide structure intercepts and redirects the elastic rebound of the cable away from critical components like the rotors and aircraft fuselage, thereby resolving the contradiction between maintaining strong load-bearing cables and preventing harmful rebound impacts.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The elastic rebound property of the cable, which is inherently harmful, is redirected to serve a protective function. By designing the guide structure to channel the rebound energy in a controlled manner, the harmful elastic reaction is converted into a predictable and contained motion that does not threaten aircraft safety, thus transforming the harmful factor into a manageable characteristic.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

2Reliability

If protective structures are added to contain cable rebound, then the safety against impact is improved, but the device complexity and weight increase

Engineering Contradiction:
Improvesafety against impactVSAvoidstructural complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The guide structure is designed using flexible materials such as fabric or thin-walled structures that can deform elastically to accommodate cable movement and rebound. These flexible shells provide protection against impact while maintaining low weight and minimal structural complexity, as they rely on material flexibility rather than rigid mechanical components to achieve the containment function.

Inventive Principle:
Principle #30Flexible shells and thin films

Solution Approach 2:

Rather than designing a complete enclosure or complex multi-component protective system, the solution employs a partial protective structure (such as a guide ring or fairing) that provides sufficient protection for the critical areas. This partial action approach achieves adequate safety without the excessive complexity and weight of a full protective enclosure.

Inventive Principle:
Principle #16Partial or excessive action

3Adaptability or versatility

If the cable length is increased for load transport, then the operational versatility is improved, but the elastic rebound energy and impact risk increase

Engineering Contradiction:
Improveload transport capabilityVSAvoidelastic rebound energy
Core Design Contradiction:
Adaptability or versatilityVSForce

Solution Approach 1:

The guide structure serves as a mediator that decouples the relationship between cable length and impact risk. By introducing this intermediate component, longer cables can be used to extend operational versatility without proportionally increasing the hazard, as the guide structure contains and redirects the rebound energy regardless of cable length.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 socks effectively manage the elastic rebound, preventing damage to the aircraft and rotors, while allowing for easy inspection and minimal weight increase, ensuring safety and functionality.

Implementation Method 1

In the event of breakage, the steel cable in the first solution of the known type or the rope in the second solution of the known type can be subject to an elastic rebound directed upwards

Methodology Applied
Scientific EffectElasticity: Elasticity

Data Source

PatentUS12600474B2Aircraft capable of hovering and method for transporting a load suspended from such aircraft
Publication Date: 2026.04.14 LEONARDO SPA
  • US12600474B2 patent drawing
  • US12600474B2 patent drawing
  • US12600474B2 patent drawing

AI summary

There is described an aircraft configured to be able to hover, comprising a fuselage; and a support element adapted to support a load, made of elastically deformable material and constrained to said fuselage; the support element being movable in an operating position in which it is arranged at least partially outside said fuselage and supports said load; the aircraft comprises a sock surrounding the support element arranged in said operating position; the sock is configured to contain the elastic return of the support element, in case the support element arranged in said operating position is sheared off.