Aircraft Cabin Rail Fastening for Tolerance Compensation

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Solution Overview

Problem

The challenge of aligning individual interior components in aircraft with varying manufacturing tolerances to achieve visual appeal and proper assembly is difficult due to tolerances in the primary structure, especially in serial production.

Innovation Solution

A fastening device with a base structure and profile legs, a rail device with a longitudinal recess, and a locking unit that allows for adjustable and universal fastening, compensating for tolerances along the longitudinal axis, enabling a continuous secondary structure interface with tolerance compensation and load distribution.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If traditional fastening methods are used to attach interior components to the aircraft frame, then the assembly process is simple, but manufacturing tolerances cause misalignment and poor visual appearance

Engineering Contradiction:
Improvealignment precisionVSAvoidfastening device complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The fastening device incorporates a rotational joint that allows the second elongated profile edge to rotate relative to the base structure, enabling dynamic adjustment to compensate for manufacturing tolerances and achieve proper alignment of interior components with the aircraft frame

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The fastening device is divided into multiple functional segments: a base structure with first profile edge, a second profile edge connected via rotational joint, and a fastening element. This segmentation allows each part to perform its specific function while collectively solving the alignment problem caused by tolerances

Inventive Principle:
Principle #1Segmentation

2Manufacturing precision

If adjustable fastening devices are used to compensate for tolerances, then alignment precision improves, but the device becomes more complex and costly

Engineering Contradiction:
Improvealignment precisionVSAvoidmanufacturing ease
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

The rotational joint provides the necessary adjustability for tolerance compensation while maintaining a relatively simple mechanical structure that can be manufactured using conventional processes, balancing alignment precision with manufacturing ease

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The fastening device design with its rotational joint and multiple profile edges serves multiple functions: it provides adjustable alignment, maintains structural strength, and ensures proper load distribution, making it a universal solution for various interior components while avoiding the need for multiple specialized parts

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

3Manufacturing precision

If tolerance compensation mechanisms are added to the fastening system, then alignment and visual appeal improve, but weight increases

Engineering Contradiction:
Improvealignment precisionVSAvoidfastening device weight
Core Design Contradiction:
Manufacturing precisionVSWeight of moving object

Solution Approach 1:

The rotational joint enables tolerance compensation through a simple rotational movement rather than requiring complex mechanical mechanisms, minimizing the additional weight needed to achieve proper alignment while maintaining visual appeal

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP4582340A1Fastening device and rail device for compensating tolerances when fastening a component to a support structure of a means of transport as well as fastening system, aircraft, assembly method for compensating tolerances when fastening a component to a support structure of a means of transport and manufacturing method for manufacturing a fastening device for compensating tolerances
Publication Date: 2025.07.09 AIRBUS OPERATIONS GMBH
  • EP4582340A1 patent drawingFigure 1~2
  • EP4582340A1 patent drawingFigure 3~4
  • EP4582340A1 patent drawingFigure 5

AI summary

The present invention provides a fastening device (10) for compensating tolerances when fastening a component (101) to a support structure (2) of a means of transport, in particular when fastening a cabin fitting element to a frame of an aircraft (100). Further, the present invention provides a rail device for compensating tolerances when fastening a component (101) to a support structure (2) of a means of transport, in particular when fastening a cabin fitting element to a frame of an aircraft (100). The present invention further provides a fastening system (1) and an aircraft (100) comprising such a fastening device (10) and such a rail device (20). Further, the present invention provides an assembly method for compensating tolerances when fastening a component to a support structure of a means of transport as well as a manufacturing method for manufacturing a fastening device for compensating tolerances.