Aircraft Fire-Fighting Distribution Line Drainage Mechanism

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Solution Overview

Problem

The existing fire-fighting system in aircraft propulsion assemblies suffers from extinguishing agent loss through drainage holes at low points in the distribution line, leading to increased reservoir volume and difficulty in integration due to moisture condensation and freezing at high altitudes.

Innovation Solution

A drainage device with a shut-off mechanism that opens and closes based on pressure in the distribution line, preventing the loss of pressurized extinguishing agent by evacuating water and ice-forming condensation while keeping the agent inside, thus maintaining the agent's volume and reducing reservoir size.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If drainage holes are arranged at low points to evacuate water, then water evacuation is effective, but extinguishing agent is lost through the holes

Engineering Contradiction:
Improvewater evacuation effectivenessVSAvoidextinguishing agent loss
Core Design Contradiction:
ReliabilityVSLoss of substance

Solution Approach 1:

The drainage device employs a dynamic shut-off mechanism that automatically opens and closes based on pressure conditions. At low pressure (ground level), the drain hole remains open for water evacuation. At high pressure (during extinguishing agent discharge), the mechanism automatically closes to prevent agent loss, thus resolving the contradiction between reliable water evacuation and preventing substance loss

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The invention utilizes pressure as a changing parameter to control the state of the drainage device. The shut-off mechanism responds to pressure threshold changes, transitioning between open and closed states. This parameter-based control allows the system to adapt its behavior to different operational phases, eliminating agent loss while maintaining water drainage capability

Inventive Principle:
Principle #35Parameter changes

2Loss of substance

If reservoir volume is increased to compensate for extinguishing agent loss, then agent loss is compensated, but reservoir integration becomes more difficult

Engineering Contradiction:
Improveextinguishing agent loss compensationVSAvoidreservoir volume
Core Design Contradiction:
Loss of substanceVSVolume of moving object

Solution Approach 1:

The invention extracts the harmful function of continuous drainage and converts it into a selective function. By removing the need for continuous open drainage holes and replacing them with pressure-controlled shut-off mechanisms, the system eliminates unnecessary agent loss, thereby eliminating the need for increased reservoir volume compensation

Inventive Principle:
Principle #2Taking out (Extraction)

3Object-affected harmful factors

If drainage holes are used to evacuate water, then water accumulation is prevented, but extinguishing agent volume must be increased

Engineering Contradiction:
Improvewater accumulation preventionVSAvoidextinguishing agent quantity
Core Design Contradiction:
Object-affected harmful factorsVSQuantity of substance

Solution Approach 1:

The dynamic pressure-responsive shut-off mechanism allows the drainage system to selectively evacuate water when needed while preventing extinguishing agent discharge through the same drainage path, thereby preventing water accumulation without increasing agent quantity

Inventive Principle:
Principle #15Dynamics

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 solution effectively prevents the loss of extinguishing agent, avoiding the need for larger reservoirs and ensuring the fire-fighting system's correct operation by maintaining the agent within the system, even at high altitudes.

Implementation Method 1

the mechanism being able to move under the effect of the pressure prevailing in the distribution line, between a first position in which it opens the fluid passage and a second position in which it closes the fluid passage

Methodology Applied
Scientific EffectPressure: Pressure Increase

Implementation Method 2

A drainage device in the form of a hole is consequently arranged at each low point so as to evacuate, under gravity, the water that could accumulate there

Methodology Applied
Scientific EffectGravity: Gravitation

Implementation Method 3

This air contains moisture that condenses and accumulates at the low points, and freezes when the aircraft flies at high altitude

Methodology Applied
Scientific EffectCondensation: Condensation

Data Source

PatentUS11524192B2Aircraft propulsion assembly comprising a fire-fighting system with a line for distributing extinguishing agent
Publication Date: 2022.12.13 AIRBUS OPERATIONS (SAS)
  • US11524192B2 patent drawing
  • US11524192B2 patent drawing
  • US11524192B2 patent drawing

AI summary

A propulsion assembly including a turbomachine attached to a pylon, and a fire-fighting system, the turbomachine including fire zones, the fire-fighting system including two reservoirs of pressurized extinguishing agent in the pylon and a distribution line connecting the reservoirs to nozzles. The distribution line includes connected pipes having a low point between the reservoirs and the nozzles, and, for each low point, a fluid drainage device for evacuating fluid. The drainage device includes a fluid passage for fluid evacuation from the distribution line and a mechanism for shutting off the fluid passage, the mechanism movable under effect of distribution line pressure, between a first position where it opens the fluid passage and a second position where it closes the fluid passage, the second position being reached when the pressure in the distribution line is greater than or equal to a predetermined pressure.