Aircraft Engine Fireproof Assembly with Internal Shield
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Fireproofing components in aircraft engines is challenging due to the high cost and weight of traditional fireproof materials, necessitating a more efficient and cost-effective solution.
Innovation Solution
A fireproof assembly comprising a housing with a fireproof internal shield and non-fireproof sealing component, supported by fireproof fasteners, which provides dual-layer fire resistance while allowing for weight and cost savings by using less expensive materials for the sealing component.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If traditional fireproof materials are used to enclose the entire housing, then fire resistance is improved, but cost and weight increase significantly
Solution Approach 1:
The patent applies local quality by providing fireproofing only in critical areas where fire resistance is most needed. The housing includes fireproof walls at specific locations (such as walls adjacent to fire zones) while other portions of the housing may use lighter, non-fireproof materials. This selective application of fireproof materials reduces overall weight and cost while maintaining adequate fire protection where required.
Solution Approach 2:
The housing is segmented into different zones with varying fireproofing requirements. The patent divides the housing structure into fireproof portions and non-fireproof portions, allowing each segment to be optimized for its specific function. This segmentation enables the use of heavy fireproof materials only where necessary rather than throughout the entire housing structure.
2Reliability
If traditional fireproof materials are used to enclose the entire housing, then fire resistance is improved, but manufacturing cost increases
Solution Approach 1:
The patent reduces manufacturing cost by applying fireproof materials only to specific locations within the housing where fire resistance is required, rather than enclosing the entire housing in expensive fireproof materials. This localized approach significantly reduces material costs and associated manufacturing expenses.
Solution Approach 2:
The housing structure is divided into segments that require fireproofing and segments that do not, allowing for more cost-effective manufacturing. The fireproof portions can be manufactured separately and assembled with non-fireproof portions, enabling flexible production strategies that reduce overall manufacturing cost.
3Reliability
If fireproof materials are used throughout the housing, then fire safety is improved, but weight increases
Solution Approach 1:
The patent implements local quality by providing fireproofing only in specific areas of the housing where fire safety is most critical, such as walls adjacent to fire zones or areas containing flammable components. This selective fireproofing maintains adequate fire safety while minimizing the addition of heavy materials.
Solution Approach 2:
Instead of making the entire housing fireproof and then removing unnecessary portions, the patent inverts the approach by designing the housing to be non-fireproof throughout and adding fireproofing only where absolutely necessary. This inverted strategy minimizes weight while achieving required fire safety levels.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
The assembly effectively shields engine components from fire, limiting breach and leakage, and meets fire safety requirements without the prohibitive costs and weight of fully fireproof materials, while allowing heat rejection to maintain internal components within design temperature limits.
Implementation Method 1
a fireproof internal shield located within the fireproof housing and dividing the volume into a first sub-volume and a second sub-volume
Implementation Method 2
a non-fireproof component sealing the opening of the fireproof housing
Implementation Method 3
fireproof fasteners supporting the fireproof internal shield in the fireproof housing
Data Source
AI summary
A fireproof assembly for an aircraft engine, comprises a fireproof housing having an internal volume and an opening. A fireproof internal shield is located within the fireproof housing. The internal shield divides the volume into a first sub-volume and a second sub-volume, the first sub-volume configured for receiving a component of the aircraft engine. A non-fireproof component seals the opening of the fireproof housing. Fireproof fasteners are used to support internal shield inside the housing.


