Helicopter Door Emergency Release Mechanism

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Solution Overview

Problem

Existing emergency release devices for aircraft doors are bulky, heavy, and difficult to operate, especially when fitted to the door, making them inefficient for quick exit in emergency situations.

Innovation Solution

A door assembly for helicopters with an emergency release device that automatically detaches the door from its hinges using a handle-operated mechanism, eliminating the need for rods and levers, and allowing for adjustable hinge positioning for easy assembly and operation, enabling quick and lightweight emergency exit.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If traditional emergency release devices with rods and levers are used to act simultaneously on two hinges, then the door can be detached from the post, but the device becomes bulky and heavy

Engineering Contradiction:
Improvedoor detachment reliabilityVSAvoidemergency release device weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The emergency release device is divided into two independent release mechanisms, one for each hinge. Each hinge has its own release lever that can be operated independently, eliminating the need for a single complex device with rods and levers that spans both hinges. This segmentation reduces the weight and bulk of the emergency release system while maintaining reliable door detachment capability.

Inventive Principle:
Principle #1Segmentation

2Reliability

If the emergency release device is fitted to the door, then the door can be detached from hinges, but the door becomes more difficult to expel due to increased weight

Engineering Contradiction:
Improvedoor detachment capabilityVSAvoiddoor expulsion ease
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The emergency release device is extracted from the door and relocated to the post structure. By removing the release mechanism from the door, the door's weight remains minimal, making it easier to expel. The release device is instead integrated into the post, where it can detach the hinge pins without adding weight to the door itself.

Inventive Principle:
Principle #2Taking out (Extraction)

3Reliability

If rods and levers are used to act simultaneously on two vertically spaced hinges, then the door can be detached, but the device complexity increases

Engineering Contradiction:
Improvesimultaneous hinge releaseVSAvoidemergency release mechanism complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The simultaneous hinge release function is achieved through segmentation into two independent release mechanisms. Each hinge has its own release lever that can be operated independently, eliminating the need for complex rods and levers that would be required to synchronize two distant hinges. The segmentation approach simplifies the overall device complexity while maintaining reliable simultaneous detachment capability.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS8752794B2Door assembly, in particular for a helicopter, provided with an emergency release device
Publication Date: 2014.06.17 LEONARDO FINMECCANICA SPA
  • US8752794B2 patent drawing
  • US8752794B2 patent drawing
  • US8752794B2 patent drawing

AI summary

A door assembly, in particular for a helicopter, has a post; a door fitted to the post by a first and second hinge arranged on an outer wall of the post, so as to rotate about a hinge axis to open and close a door opening; and an emergency release device having a release handle, and a stem which extends through the post along a release axis substantially perpendicular to the hinge axis, rotates axially, in response to operation of the release handle, from a first to a second angular position to detach the door from the post, and is fixed at one axial end to the first hinge; the release handle being connected to the stem to rotate together with the stem about its release axis.