Collapsible Engine Inlet Cover for Full Ground Protection

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Solution Overview

Problem

Current engine inlet covers are bulky, difficult to install, require multiple people, and do not cover the entire inlet, necessitating additional cleaning and posing risks during installation on rotating engines.

Innovation Solution

A lightweight, collapsible cover with a frame of interconnected arms and a web that can be easily installed by a single person, covering the entire engine inlet without touching the fan or nose cone, and securely anchored to the engine housing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If traditional engine inlet covers are used, then the engine inlet can be covered, but the cover is bulky and difficult to carry on smaller aircraft

Engineering Contradiction:
Improvecover sizeVSAvoidportability
Core Design Contradiction:
Volume of moving objectVSEase of operation

Solution Approach 1:

The cover is divided into multiple collapsible arms that can be folded together, transforming a large rigid structure into a compact portable form factor suitable for smaller aircraft

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The cover transitions from a static rigid structure to a dynamic collapsible structure that can change its volume and shape, allowing it to be both large when deployed and compact when stored

Inventive Principle:
Principle #15Dynamics

2Reliability

If traditional engine inlet covers are used, then the engine inlet can be covered, but multiple ladders or lifts/stands are necessary to complete the installation

Engineering Contradiction:
Improvecoverage effectivenessVSAvoidinstallation equipment
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The cover is segmented into multiple arms that can be independently positioned and collapsed, allowing installation from ground level without requiring ladders or lifts

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The collapsible arms can be dynamically adjusted during installation, enabling the cover to be assembled and positioned without additional equipment

Inventive Principle:
Principle #15Dynamics

3Ease of operation

If the cover is designed to be positioned inside the inlet in front of the engine fan, then installation is simplified, but the entire engine inlet is not covered requiring additional cleaning

Engineering Contradiction:
Improveinstallation simplicityVSAvoidcontaminant prevention
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The cover structure integrates both the inlet coverage function and the fan protection function into a single unified structure, eliminating the need for separate components or additional cleaning operations

Inventive Principle:
Principle #5Merging (Combining)

4Ease of operation

If some engine covers are designed to rest on part of the rotating engine turbomachinery, then the cover can be supported, but this is problematic in windy scenarios where the engine fan may be rotating

Engineering Contradiction:
Improvecover supportVSAvoidwind-induced fan rotation
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The support function is extracted from the cover itself and transferred to the engine housing, allowing the cover to rest on stationary structures rather than rotating components

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The engine housing serves as an intermediary support structure, providing a stable stationary base for the cover without requiring direct contact with rotating fan blades

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS12589886B2Collapsible cover for engine inlet and method for covering engine inlet
Publication Date: 2026.03.31 GULFSTREAM AEROSPACE CORP
  • US12589886B2 patent drawing
  • US12589886B2 patent drawing
  • US12589886B2 patent drawing

AI summary

An engine inlet cover and a method for covering an engine inlet are provided. A method for covering an engine inlet includes providing a collapsible cover comprising a connection pin defining an axis; a frame including interconnected arms; and a web. Further, the method includes storing the collapsible cover in a stowed configuration in which the arms are aligned. Also, the method includes rotating the arms from the stowed configuration to an operating configuration in which the arms are radially spaced about the axis, enclosing the frame in the operating configuration with the web to define an interior volume, and placing the cover over the engine inlet.