Universal Aircraft Wiper Assembly With Programmable Mount Adaptation

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Solution Overview

Problem

Aircraft operators face AOG situations due to the need to stock multiple windshield wiper motor/converter assemblies for various aircraft types, leading to delays and high costs, and existing wipers are noisy and inefficient.

Innovation Solution

A universal windshield wiper assembly with customized mounts and preset programmed electronics for permanent installation on aircraft, utilizing internally or externally commutated and asynchronous motors to match individual aircraft specifications, eliminating the need for multiple assemblies and reducing noise.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If multiple motor/converter assemblies are stocked for different aircraft types, then reliability of windshield wiper operation is improved, but device complexity and inventory requirements increase

Engineering Contradiction:
Improvewindshield wiper operation reliabilityVSAvoidinventory complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent creates a universal motor/converter assembly that can be adapted to multiple aircraft types through interchangeable mounting brackets and programmable control circuits. The control circuit receives aircraft type input and adjusts operational parameters accordingly, allowing one motor assembly to replace multiple type-specific assemblies, thereby reducing inventory complexity while maintaining reliability across different aircraft models

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

Solution Approach 2:

The control circuit is designed to accept aircraft type identification and dynamically change operational parameters such as speed, torque, and cycle timing to match the specific requirements of different aircraft windshield wiper systems. This parameter adaptability allows a single motor assembly to reliably operate various aircraft types without requiring multiple specialized assemblies

Inventive Principle:
Principle #35Parameter changes

2Manufacturing precision

If type-specific motor/converter assemblies are used for each aircraft model, then manufacturing precision for each aircraft type is improved, but adaptability across aircraft models deteriorates

Engineering Contradiction:
Improvemotor/converter assembly precisionVSAvoidaircraft model compatibility
Core Design Contradiction:
Manufacturing precisionVSAdaptability or versatility

Solution Approach 1:

The mounting system is divided into standardized base components and aircraft-specific adapter brackets. The base motor/converter assembly maintains precise manufacturing tolerances, while interchangeable adapter brackets provide the adaptation to different aircraft mounting points. This segmentation allows high precision manufacturing of the core assembly while achieving broad adaptability through modular adapters

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Interchangeable mounting brackets serve as intermediary components between the universal motor/converter assembly and various aircraft-specific mounting points. These adapter brackets translate between the standardized motor mounting interface and the diverse aircraft windshield geometries, enabling precise operation across different aircraft models without compromising the precision of the core assembly

Inventive Principle:
Principle #24Intermediary (Mediator)

3Ease of manufacture

If traditional motor/converter assemblies are used, then ease of manufacture is maintained, but noise generation increases

Engineering Contradiction:
Improveassembly manufacturing simplicityVSAvoidnoise
Core Design Contradiction:
Ease of manufactureVSObject-generated harmful factors

Solution Approach 1:

The patent replaces traditional mechanical timing and control mechanisms with electronically controlled systems. The control circuit electronically regulates motor operation, replacing mechanical linkages and timing devices that generated noise. This substitution maintains manufacturing simplicity while significantly reducing operational noise through electronic control of motor speed and activation cycles

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

Data Source

PatentUS20250256830A1Universal windshield wiper assembly
Publication Date: 2025.08.14 KALKA BENIO SIMOR
  • US20250256830A1 patent drawing
  • US20250256830A1 patent drawing
  • US20250256830A1 patent drawing

AI summary

A universal windshield wiper blade assembly for use with all aircraft, both commercial and military that removes the necessity of having assemblies for each individual type of aircraft in existence at locations where aircraft fly in and out. The system utilizes individual mounts for individual types of aircraft that are permanently installed and that contain preset programmed electronics for each individual type of aircraft after which the universal windshield wiper assembly is installed thereon. The universal windshield wiper assembly includes a gear box with a shaft that attaches to a windshield wiper arm that moves and windshield wiper blade, an electric motor, including internally and externally commutated as well as asynchronous motors relative to each other that actuates the gear box and a motor cover.