Removable Aircraft Storage Shell With Sealing Gasket

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Solution Overview

Problem

Conventional aircraft designs with non-removable baggage holds limit adaptability to user needs, as they cannot easily be modified or replaced to accommodate different requirements such as maximizing range or carrying alternative loads without significant effort and weight changes.

Innovation Solution

An aircraft with a modular storage structure featuring a sealing device and interchangeable storage shells, allowing users to select and attach removable storage shells to non-removable fittings using elongate fasteners, which can be easily swapped to convert the aircraft for different purposes, such as carrying baggage or additional fuel tanks.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a non-removable baggage hold is installed in the aircraft, then the structural integrity and sealing are maintained, but the adaptability to different user needs (such as carrying baggage or fuel tanks) is limited

Engineering Contradiction:
Improveadaptability to user needsVSAvoidstructural complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The baggage hold is divided into two parts: a non-removable structural frame that remains integrated with the aircraft airframe, and a removable container that can be detached and replaced. This segmentation allows the structural integrity to be maintained while enabling adaptability through container replacement.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The non-removable structural frame is designed with universal attachment features (such as longerons and frames) that can accommodate different types of containers (baggage holds, fuel tanks, etc.). This allows a single structural design to serve multiple functions and adapt to different user needs.

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

2Adaptability or versatility

If a removable storage shell is introduced to enhance adaptability, then the ease of modification improves, but the sealing reliability may deteriorate

Engineering Contradiction:
Improveease of modificationVSAvoidsealing reliability
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

Sealing means (such as gaskets or seals) are pre-installed on the non-removable structural frame before the removable container is attached. This preliminary action ensures that sealing is built into the attachment mechanism itself, maintaining reliability while enabling easy removal and reattachment of containers.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

A sealing element acts as an intermediary between the removable container and the non-removable frame. This intermediary component ensures a reliable seal during attachment while allowing the container to be easily detached and replaced, thus maintaining both sealing reliability and ease of modification.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Strength

If conventional non-removable baggage holds are used, then the structural strength is maintained, but the weight increases when converting between different configurations

Engineering Contradiction:
Improvestructural strengthVSAvoidweight changes during conversion
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

By separating the structural frame from the container, only the container weight changes during conversion while the structural frame remains constant. This allows the aircraft to maintain structural strength while minimizing weight changes when switching between different configurations (e.g., baggage hold to fuel tank).

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS10640192B2Aircraft having a removable hold
Publication Date: 2020.05.05 EUROCOPTER FRANCE SA
  • US10640192B2 patent drawing
  • US10640192B2 patent drawing
  • US10640192B2 patent drawing

AI summary

An aircraft having an airframe including a hollow structure referred to as a “storage” structure, the storage structure having an opening that is open to the outside of the aircraft. A sealing device extends around the opening, the sealing device including at least one compressible gasket. A plurality of non-removable fittings are fastened to the storage structure. At least one removable storage shell comprises at least a covering configured to close the opening while compressing each gasket. Removable fittings of the storage shell are attached in reversible manner to the non-removable fittings by respective elongate fasteners passing through each removable fitting and the non-removable fitting.