Detachable Wing Construction for Ultra-Light Flying Devices

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Solution Overview

Problem

Existing ultra-light flying devices face challenges in achieving a balance between portability and security, as they are often too small and light to be easily transported and secured, and their design does not facilitate easy detachment and reattachment of wings for convenient transportation.

Innovation Solution

The flying device features a unique wing construction with a strongly swept-back lower wing design that allows for easy detachment and reattachment, utilizing recesses and quick-release locking pieces to securely attach and detach the wings from the fuselage, enabling efficient packing and transportation on a conventional trailer.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If the flying device is made small and light to improve portability, then it can be transported easily on conventional trailers, but it becomes vulnerable to theft and cannot be left unwatched

Engineering Contradiction:
ImproveportabilityVSAvoidsecurity
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The wing is divided into multiple sections that can be detached from the fuselage. The wing construction includes a first wing section and a second wing section that can be separated, allowing the device to be configured for easy transportation while maintaining security through controlled detachment mechanisms.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The wing attachment system transitions from a fixed state during flight to a detachable state during transportation. The quick-release locking pieces allow the wing to be rapidly attached and detached, providing dynamic adaptability between operational and transportational requirements.

Inventive Principle:
Principle #15Dynamics

2Ease of operation

If the wing is designed to be easily detachable for transportation, then portability is improved, but the structural integrity and security during flight may be compromised

Engineering Contradiction:
Improveease of detachmentVSAvoidstructural integrity
Core Design Contradiction:
Ease of operationVSStrength

Solution Approach 1:

The locking pieces are pre-positioned and designed to engage automatically when the wing is attached to the fuselage. The recesses and locking pieces are configured so that proper alignment and engagement ensure secure attachment before flight, while the quick-release mechanism allows easy detachment when needed.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The locking pieces act as intermediary elements between the wing and fuselage, providing a secure mechanical connection. These locking pieces engage with the recesses to create a strong bond during flight, while the same locking pieces can be quickly released for transportation, mediating between the conflicting requirements of strength and ease of detachment.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Strength

If conventional locking mechanisms are used to secure the wing, then structural integrity is maintained, but the time required for attachment and detachment increases

Engineering Contradiction:
Improvesecurity of attachmentVSAvoidtime for attachment and detachment
Core Design Contradiction:
StrengthVSLoss of time

Solution Approach 1:

The locking pieces are designed to self-engage with the recesses when the wing is positioned correctly during attachment. The quick-release mechanism allows the locking pieces to be easily released by a simple action, eliminating the need for complex manual locking procedures and reducing the time required for both attachment and detachment operations.

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS9308984B2Flying device and a wing construction for the same
Publication Date: 2016.04.12 INNVOLVE CAPITAL OY
  • US9308984B2 patent drawing
  • US9308984B2 patent drawing
  • US9308984B2 patent drawing

AI summary

Flying device, in which there is a fuselage (2, 2′), wings (8, 9), which are connected to each other to form an essentially looped structure, elements (4, 5) for creating a flying force, and the desired elements (e.g., 7, 7′) for controlling the flying device (1). The wings (8, 9) of the flying device (1) form a unified totality detachable from the fuselage (2, 2′). A wing construction is also included.