Aircraft Cabin Quick-Release Latch for Seat and Divan Access

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Solution Overview

Problem

Accessing equipment and accessories positioned behind or beneath interior aircraft cabin apparatuses, such as divans or aircraft seats, is difficult due to the need for complete removal of these apparatuses from their tracks, which is time-consuming and inefficient.

Innovation Solution

A quick release system for interior aircraft cabin apparatuses, comprising a release assembly with handles and cables, a latch assembly, and a lock assembly, allowing the apparatuses to rotate and translate, enabling easy access to hidden areas without requiring full removal, while meeting aviation standards.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If the interior aircraft cabin apparatus is completely removed from the track to access equipment and accessories, then full access to all components is achieved, but the process becomes time-consuming and inefficient

Engineering Contradiction:
ImproveAccess to equipment and accessoriesVSAvoidTime required for removal and reinstallation
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The apparatus is divided into separable components with independent locking mechanisms. The locking assembly includes multiple latches that can be individually engaged or disengaged, allowing selective access to different portions of the apparatus without requiring complete removal from the track

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The locking mechanism transitions from a static fixed position to a dynamic quick-release system. The release handles and cables enable rapid transformation between locked and unlocked states, allowing the apparatus to be quickly positioned in access mode without full removal

Inventive Principle:
Principle #15Dynamics

2Reliability

If the locking mechanism is made secure and robust to ensure safety, then reliability is improved, but the complexity of the release system increases

Engineering Contradiction:
ImproveSecurity of locking mechanismVSAvoidComplexity of release system
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The locking assembly is designed to be self-latching and self-locking through the interaction of latch hooks, lock plates, and tracking mechanisms. Once engaged, the system maintains its locked state automatically without requiring continuous external force or complex control systems

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Multiple locking functions are combined into an integrated assembly where latches, lock plates, and release mechanisms work together as a unified system. This consolidation reduces the number of separate components while maintaining robust security

Inventive Principle:
Principle #5Merging (Combining)

3Ease of operation

If the release handles and cables are made accessible for operation, then ease of release is improved, but safety risks arise from passenger access

Engineering Contradiction:
ImproveAccessibility of release mechanismVSAvoidSafety risks from unauthorized access
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The release handles are positioned in locations that are accessible to maintenance personnel during normal operation but are not accessible to passengers during flight. The cable routing and handle placement create localized access zones that differ between operational modes

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The cable system acts as an intermediary between the release handles and the locking mechanisms. This allows the release function to be transmitted through a protected pathway that can be shielded from passenger access while maintaining operational accessibility

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentEP4431392A1Quick release system and method for an interior aircraft cabin apparatus
Publication Date: 2024.09.18 BE AEROSPACE INC
  • EP4431392A1 patent drawingFigure 1
  • EP4431392A1 patent drawingFigure 2
  • EP4431392A1 patent drawingFigure 3A

AI summary

A quick release system for an interior apparatus is disclosed. The system may include a release assembly (106) including a release handle (216) and release cables (218). The release handle may pull the release cables (218) when a force is applied. The system may include a latch assembly (108) including latches (400) coupled to the release cables (218). The latches (400) may include a latch hook positioned in an open position or a closed position. Upon applying the force to the release handle, the latch hook may release the apparatus to cause the apparatus to rotate about an axis. The system may include a locking assembly (110) including a lever (500) and a lock plate (502). Upon applying the force to the release handle, the lock plate (502) may translate between the locked position and the unlocked position to disengage the lock plate (502) from the tracks (214) to cause the apparatus to translate along the tracks (214).