Aircraft Slat Track Guide Rail With Slot-Access Actuation

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Solution Overview

Problem

Existing wing designs face challenges in efficiently and flexibly actuating the slat track due to obstructions from guide rails, limiting the movement and installation of actuation devices.

Innovation Solution

Incorporating a guide rail with longitudinal slots in the upper and lower rail portions allows actuation devices to engage the slat track without obstruction, enabling efficient movement between retracted and extended positions, and facilitating simple installation and maintenance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a guide rail with continuous upper and lower rail portions is used, then the slat track is reliably guided, but the actuation device cannot engage the slat track from above or below

Engineering Contradiction:
Improveactuation of slat trackVSAvoidguiding of slat track
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The guide rail is segmented into an upper rail portion and a lower rail portion separated by a longitudinal slot. This segmentation allows the actuation device to access the slat track from above or below through the slot, while the separate rail portions maintain reliable guiding function.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The longitudinal slot acts as an intermediary element that enables the actuation device to reach the slat track without removing the guide rail structure. The slot provides a passage through which the actuation device can engage and move the slat track between retracted and extended positions.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Strength

If the guide rail blocks the actuation device, then structural integrity is maintained, but installation and maintenance become complex

Engineering Contradiction:
Improvestructural integrity of guide railVSAvoidinstallation and maintenance
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

By dividing the guide rail into upper and lower portions separated by a slot, the structure maintains its integrity and strength while allowing the actuation device to pass through. This segmentation simplifies installation and maintenance operations.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The longitudinal slot extracts or removes the blocking function from the guide rail, creating a passage that allows actuation device engagement. This extraction enables easier installation and maintenance without compromising the overall structural integrity of the guide rail.

Inventive Principle:
Principle #2Taking out (Extraction)

3Reliability

If a C-shaped guide rail is used, then guiding function is provided, but space and weight are increased

Engineering Contradiction:
Improveguiding functionVSAvoidweight of guide rail
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

Segmenting the guide rail into upper and lower portions with a longitudinal slot creates a more efficient structure that reduces material usage and weight while maintaining the guiding function. The separated portions can be optimized independently for minimal weight.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

By extracting the continuous material structure and introducing a longitudinal slot, the guide rail achieves the same guiding function with reduced material, thereby reducing weight and space requirements.

Inventive Principle:
Principle #2Taking out (Extraction)

Data Source

PatentUS12583575B2Wing for an aircraft
Publication Date: 2026.03.24 AIRBUS OPERATIONS GMBH
  • US12583575B2 patent drawing
  • US12583575B2 patent drawing
  • US12583575B2 patent drawing

AI summary

An aircraft wing (3) including a main wing (5), a slat (7), and a connection assembly (9) movably connecting the slat (7) to the main wing (5). The connection assembly (9) includes an elongate slat track (17) extending along a track longitudinal axis (19) having a front end (21) an intermediate portion (25) and a rear end (23). The front end (21) and/or the intermediate portion (25) is mounted to the slat (7). The rear end (23) and/or the intermediate portion (25) is mounted to the main wing (5) by a roller bearing (27). The roller bearing (27) includes a guide rail (29) mounted to the main wing (5) and a first roller unit (31) mounted to the rear end (23) of the slat track (17) and engaging the guide rail (29), and wherein the guide rail (29) includes an upper rail portion (32) and a lower rail portion (34).