Aircraft Flap Tracks With Segmented Carriages for Jam Resistance

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Solution Overview

Problem

Existing flap mechanical systems in aircrafts are prone to jams, which increase manufacturing complexity, cost, and maintenance, and require additional resources, impacting aircraft performance and reliability.

Innovation Solution

A flap assembly with a jam-resistant track design, featuring a C-channel configuration for the track and a three-piece flap carriage with redundant rollers, reduces manufacturing complexity and vulnerability to jams, using coupling components and passive support to supplement actuators.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional flap mechanical systems are used, then flaps can be extended and retracted to change wing profiles, but the systems are prone to jams increasing manufacturing complexity and maintenance requirements

Engineering Contradiction:
Improvejam resistanceVSAvoidmanufacturing complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The flap carriage is divided into three separate pieces that can be manufactured independently and then assembled. This segmentation allows each piece to be optimized for its specific function while simplifying the overall manufacturing process and reducing the complexity of producing the complete carriage assembly.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The track design incorporates features that prevent jams before they occur by providing adequate clearance and proper alignment guides. The C-channel configuration of the track provides built-in protection against foreign object debris causing jams, eliminating the need for complex additional protective mechanisms.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

2Reliability

If conventional flap mechanical systems are used, then flaps can be actuated to change wing profiles, but additional resources are required for maintenance and operational support

Engineering Contradiction:
Improveoperational reliabilityVSAvoidmaintenance efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The flap carriage design allows for self-alignment and self-adjustment during operation. The three-piece construction with specific geometric relationships between pieces enables the system to compensate for minor misalignments automatically, reducing the need for maintenance interventions and operational support resources.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The track's C-channel configuration provides pre-built protection against foreign object debris, preventing jams before they occur. This design feature eliminates the need for additional maintenance resources that would otherwise be required to address jam-related issues.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

3Manufacturing precision

If complex flap mechanical systems are used, then flaps can be precisely controlled, but manufacturing cost and complexity increase

Engineering Contradiction:
Improveflap positioning precisionVSAvoidmanufacturing ease
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

By dividing the carriage into three separate pieces, each can be manufactured using standard processes and then assembled with simple coupling components. This approach maintains the necessary positioning precision through careful design of the interface between pieces while significantly improving manufacturing ease compared to producing a single complex integrated carriage.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The track's C-channel configuration provides localized geometric precision where needed for roller guidance and alignment, while other portions of the track can be manufactured more simply. This localized approach to precision maintains overall positioning accuracy without requiring high precision throughout the entire component.

Inventive Principle:
Principle #3Local quality

Data Source

PatentEP4249372B1Flap assemblies with failsafe jam-resistant flap tracks
Publication Date: 2025.08.06 THE BOEING CO
  • EP4249372B1 patent drawingFigure 1
  • EP4249372B1 patent drawingFigure 2
  • EP4249372B1 patent drawingFigure 3

AI summary

The application relates to flap assemblies with failsafe jam-resistant flap tracks. The flap assembly includes a track (402A,402B) having an elongate structure and a flap carriage (404) configured to move along a length of the track. The track is configured to couple to an aircraft wing and the flap carriage includes a primary roller (602) and a pair of secondary rollers (604A,604B) configured to secure the flap carriage to the track. A top portion (414) of the flap carriage is configured to couple to a flap such that movement of the flap carriage along the length of the track enables movement of the flap relative to the aircraft wing.