Aircraft Washroom Door Lock Actuator Mechanism

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Solution Overview

Problem

Current door arrangements for aircraft washrooms require manual operation and lack efficient automatic locking mechanisms, which can compromise hygiene and accessibility.

Innovation Solution

A door arrangement with a locking mechanism featuring a blocking element and a closure element, actuated by mechanical pressure through a non-connected actuating system, allowing for contactless operation and integration with an electric drive device for enhanced functionality.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If manual operation of door is used, then device complexity is reduced, but ease of operation and hygiene are worsened

Engineering Contradiction:
Improveease of operationVSAvoiddevice complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The patent replaces manual mechanical operation with an electric drive device that automatically actuates the locking mechanism. The electric motor-driven actuating element moves the blocking element without requiring manual intervention, thereby improving ease of operation and hygiene while maintaining acceptable device complexity through integrated design.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Productivity

If automatic locking mechanism is added, then productivity and hygiene are improved, but device complexity increases

Engineering Contradiction:
ImproveproductivityVSAvoiddevice complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent merges the locking mechanism with the door actuation system by integrating the blocking element into the existing door structure. The electric drive device combines door opening/closing functionality with locking/unlocking functionality in a single integrated system, improving productivity and hygiene while minimizing the increase in device complexity through functional consolidation.

Inventive Principle:
Principle #5Merging (Combining)

3Reliability

If blocking element is connected to actuating element, then reliability of force transmission is improved, but ease of manufacture is worsened

Engineering Contradiction:
ImprovereliabilityVSAvoidease of manufacture
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent introduces a locking device as an intermediary component between the actuating element and the blocking element. This locking device includes a recess that receives the actuating element, providing reliable force transmission through a simple receptacle-based connection rather than complex mechanical coupling, thereby maintaining ease of manufacture while ensuring reliability.

Inventive Principle:
Principle #24Intermediary (Mediator)

4Ease of manufacture

If non-connected actuating system is used, then ease of manufacture is improved, but force transmission reliability is worsened

Engineering Contradiction:
Improveease of manufactureVSAvoidforce transmission reliability
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The locking device serves as a mediator that enables reliable force transmission from the non-connected actuating element to the blocking element. The recess in the locking device provides a precise mechanical interface that ensures consistent force transfer without requiring a permanent connection between components, thus maintaining both ease of manufacture and force transmission reliability.

Inventive Principle:
Principle #24Intermediary (Mediator)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables automatic and contactless operation of aircraft washroom doors, improving hygiene and accessibility while ensuring secure locking and unlocking mechanisms.

Implementation Method 1

The actuating element is not connected to the blocking element and is designed to transfer the blocking element from the movement position to the blocking position or from the blocking position to the movement position by mechanical contact pressure

Methodology Applied
Scientific EffectMechanical contact pressure: Mechanical Force

Implementation Method 2

The second actuating element is set up to transfer the closure element from the unlocking position to the locking position and/or from the locking position to the unlocking position by mechanical contact pressure

Methodology Applied
Scientific EffectMechanical contact pressure: Mechanical Force

Data Source

PatentEP4217270B1Door arrangement with lock actuator for integration in an aircraft
Publication Date: 2023.11.29 DIEHL AVIATION LAUPHEIM GMBH
  • EP4217270B1 patent drawingFigure 1
  • EP4217270B1 patent drawingFigure 2
  • EP4217270B1 patent drawingFigure 3

AI summary

A door arrangement contains a door (4) for a room (3) with a door leaf (30a, b), a wall portion (44) of a wall structure (45) laterally adjacent to the door (4), and a locking arrangement (9) for the door (4) containing: a locking device (43) in the door leaf (30a, 30b) with a blocking element (47), which can be moved in and contrary to a blocking direction (B) in order to block or release the door (4); and a lock actuator (6) in the wall portion (44) with a first mechanical actuating element (27), which is unconnected to the blocking element (47) in order to shift the blocking element (47), by means of mechanical contact pressure, from the movement position into the blocking position and vice versa. A control and information system (1) contains the door arrangement (9), a control device (7) for the lock actuator (6), a human/machine interface (10, 11) for capturing a triggering action (18a, 18b) of a user (15) of the door (4) and for transmitting same as a triggering signal (19a, 19b) for the lock actuator (6) to the control device (7), and a communication interface (21) for an authorised body (22) different from the user (15). A room (3) contains the door arrangement or the control and information system (1). An aircraft (2) contains the door arrangement or the control and information system (1) or the room (3).