Composite Wiper Blade Clip Assembly for High-Speed Sweep Accuracy

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Solution Overview

Problem

Traditional aircraft windshield wiper blades experience weakness and bending due to rivets extending through both the frame and rubber blade, leading to difficulties in meeting specified sweep angle requirements during high-speed operation.

Innovation Solution

A wiper blade design featuring a support member coupled to a blade element via a clip and fastener, with the clip surrounding both components and the fastener securing the clip to the blade element, eliminating apertures through the support member to enhance rigidity and attachment, and a coupler securing the blade to the wiper arm.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If rivets extend through both the frame and rubber blade, then the blade elements are secured to the frame, but the blade develops locations of weakness that cause bending and flexing during high-speed operation

Engineering Contradiction:
Improveblade structural integrityVSAvoidblade rigidity
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The blade assembly is divided into separate components: the frame (support member) and the rubber blade are not directly connected through penetrating fasteners. Instead, discrete blade elements are positioned within the frame structure, with rivets extending only through the frame to secure retaining clips, not penetrating the blade elements themselves. This segmentation eliminates direct mechanical penetration points in the blade, preventing weakness locations while maintaining secure attachment through the clip-retainer system.

Inventive Principle:
Principle #1Segmentation

2Device complexity

If traditional rivet construction is used, then the wiper blade structure is simple, but the blade bends and flexes during high-speed operation causing overshoot of sweep angle requirements

Engineering Contradiction:
Improveblade construction simplicityVSAvoidsweep angle precision
Core Design Contradiction:
Device complexityVSManufacturing precision

Solution Approach 1:

A retaining clip acts as an intermediary component between the frame and blade elements. The rivet secures the clip to the frame, and the clip in turn retains the blade elements in position. This intermediary structure allows the blade elements to be securely held without direct rivet penetration into the blade material, maintaining structural integrity and precise sweep angle control while keeping the overall construction relatively simple.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Ease of manufacture

If rivets extend through both components, then the blade elements are attached to the frame, but weakness locations are created allowing bending during operation

Engineering Contradiction:
Improveblade assembly easeVSAvoidblade resistance to bending
Core Design Contradiction:
Ease of manufactureVSStrength

Solution Approach 1:

Instead of extending rivets through the blade elements to secure them (traditional approach), the invention inverts the attachment logic: rivets extend only through the frame to secure retaining clips, which then hold the blade elements in place. This inverted approach eliminates penetration points in the blade material itself, preventing bending weaknesses while maintaining secure attachment and ease of assembly through the clip-retainer mechanism.

Inventive Principle:
Principle #13The other way round (Inversion)

Data Source

PatentEP4059786B1Composite wiper blade assembly
Publication Date: 2023.12.27 ROSEMOUNT AEROSPACE INC
  • EP4059786B1 patent drawingFigure 1A~1B
  • EP4059786B1 patent drawingFigure 2A~2C
  • EP4059786B1 patent drawingFigure 3A~3B

AI summary

An aircraft windshield wiper system includes a wiper arm (24), a wiper blade (26) coupled to a first end of the wiper arm, and an output shaft (16) coupled to a second end of the wiper arm. The wiper blade (26) includes a support member (34) coupled to a blade element (36) through a clip (38) and a fastener (40) extending through the blade element (36). The support member (34) can be made from a composite material and the clip (38) and fastener (40) allow for attachment of the blade element (36) to the support member (34) without piercing the support member (34).