Aircraft Door Latch Actuation Mechanisms

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Solution Overview

Problem

Aircraft door latch systems pose a safety hazard when locking mechanisms are engaged during emergency egress, as they can prevent unauthorized access while also restricting emergency exit, necessitating a system that secures doors during flight without impeding emergency access.

Innovation Solution

A door latch system featuring independent interior and exterior actuation mechanisms, where a control cable connects a conversion block to a latch module, allowing rotation to retract the latch for emergency egress even when the lock is engaged, ensuring the door remains secured to the airframe during flight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a locking mechanism is engaged to prevent unauthorized access, then security is improved, but emergency egress is prevented

Engineering Contradiction:
ImprovesecurityVSAvoidemergency egress
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The actuation system is divided into two independent mechanisms: an exterior actuation mechanism with an exterior handle connected to an inner rod, and an interior actuation mechanism with an interior handle connected to an outer rod. The lock engages with a lock tab on the inner rod to prevent exterior actuation, while the interior mechanism operates independently through the outer rod to enable emergency egress from inside the aircraft.

Inventive Principle:
Principle #1Segmentation

2Device complexity

If a single actuation mechanism is used, then device complexity is reduced, but the ability to provide both security and emergency egress is compromised

Engineering Contradiction:
Improveactuation mechanism structureVSAvoiddual function capability
Core Design Contradiction:
Device complexityVSAdaptability or versatility

Solution Approach 1:

The actuation mechanism is segmented into two independent systems: the exterior actuation mechanism (inner rod, exterior handle, lock tab) that is controlled by the lock, and the interior actuation mechanism (outer rod, interior handle) that operates independently. This segmentation allows each mechanism to be optimized for its specific function while maintaining overall system simplicity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The door latch system provides multiple functions through its dual actuation mechanisms: normal secure operation when the lock is engaged, unauthorized access prevention through the lock mechanism, and emergency egress capability from the interior. The system universally handles different operational requirements (security vs. emergency access) through its segmented design.

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

Data Source

PatentUS10982471B2Independent internal and external door latch actuation mechanisms
Publication Date: 2021.04.20 TEXTRON INNOVATIONS INC
  • US10982471B2 patent drawing
  • US10982471B2 patent drawing
  • US10982471B2 patent drawing

AI summary

A latch system includes an actuation module having first and second actuation mechanisms. The first actuation mechanism includes a first handle, a lock tab and an inner rod coupled together. The second actuation mechanism includes at least one second handle, a conversion block and an outer rod coupled together with the outer rod and the conversion block each having a slot. At least one latch module has a retractable latch. A control cable connects the conversion block and the latch module such that rotation of the conversion block in a first direction retracts the latch. A lock is operably engagable with the lock tab to selectively allow and prevent rotation of the inner rod. Rotation of the inner rod in the first direction rotates the conversion block. Rotation of the outer rod in the first direction rotates the conversion block without rotating the inner rod.