Variable Aircraft Engine Inlet Guard Screen

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Solution Overview

Problem

Existing aircraft engine inlet guard screens are ineffective in dynamically adjusting to changing operational conditions, such as foreign object debris ingestion and ice accretion, which can lead to engine damage.

Innovation Solution

A variable inlet guard system comprising a first screen, a second screen, and an actuation system that moves the first screen along the second screen, changing the geometry of perforations to adapt to different operational conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a fixed inlet guard screen is used, then the structure is simple and reliable, but it cannot adapt to changing operational conditions such as foreign object debris ingestion and ice accretion

Engineering Contradiction:
Improveadaptability to operational conditionsVSAvoidinlet guard structure complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The inlet guard screen transitions from a fixed structure to a dynamic adjustable structure. The screen can change its configuration by moving between different positions (retracted, extended, partially extended) to adapt to varying operational conditions such as foreign object debris ingestion risks and ice accretion, while maintaining structural reliability through controlled actuation mechanisms.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The inlet guard screen is divided into multiple independent segments or sections that can be actuated separately. This segmentation allows different portions of the screen to be adjusted independently based on local conditions, providing fine-grained adaptability while keeping the overall structure manageable and controllable.

Inventive Principle:
Principle #1Segmentation

2Reliability

If the inlet guard screen is made adjustable to reduce foreign object debris ingestion, then protection effectiveness improves, but the device complexity increases

Engineering Contradiction:
Improveengine protection effectivenessVSAvoidactuation system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The inlet guard screen system incorporates sensors and control mechanisms that enable it to automatically detect operational conditions (such as foreign object debris presence or ice accretion) and adjust its configuration without requiring constant manual intervention. This self-service capability improves engine protection effectiveness while minimizing the complexity of external control systems.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The inlet guard screen can be positioned in advance to prevent harmful conditions before they occur. For example, the screen can be extended preemptively when foreign object debris is detected in the intake airflow, or adjusted before ice accretion becomes problematic, thereby improving protection effectiveness while allowing the actuation system to operate in controlled, planned manner rather than reacting to emergencies.

Inventive Principle:
Principle #10Preliminary action

3Reliability

If the perforation geometry is dynamically changed, then foreign object debris filtering improves, but the manufacturing complexity increases

Engineering Contradiction:
Improveforeign object debris filteringVSAvoidinlet guard manufacturing difficulty
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The perforation geometry is designed to be dynamically adjustable through the movement of screen segments relative to each other. By changing the relative positions of screen sections, the effective perforation size and pattern can be modified to optimize foreign object debris filtering for different operational conditions. The screen structure uses standardized components and movement mechanisms that can be manufactured using conventional processes, balancing manufacturing ease with dynamic adaptability.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS20250116229A1Variable inlet guard for an inlet of an aircraft engine
Publication Date: 2025.04.10 PRATT & WHITNEY CANADA CORP
  • US20250116229A1 patent drawing
  • US20250116229A1 patent drawing
  • US20250116229A1 patent drawing

AI summary

A system is provided for an aircraft. This aircraft system includes an aircraft engine, an inlet guard and an actuation system. The aircraft engine has a flowpath projecting into the aircraft engine from an airflow inlet. The inlet guard is arranged at the airflow inlet and extends across the flowpath. The inlet guard includes a first screen, a second screen and a plurality of perforations. The first screen is adjacent and overlaps the second screen. The perforations project through the inlet guard and are formed by the first screen and the second screen. The actuation system is configured to move the first screen along the second screen. The movement of the first screen along the second screen changes a geometry of each of the perforations.