Aircraft Pressure Relief Valve Seat for Adjustable Sealing

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Solution Overview

Problem

The manufacture of conventional aircraft pressure relief valves is costly and time-consuming due to an iterative process involving coining and shim selection to ensure proper functionality, leading to potential leakage and manufacturing inefficiencies.

Innovation Solution

The pressure relief valve design includes a conical valve seat and a threaded end stop element, allowing for improved sealing and adjustable biasing force without iterative processes, featuring a conical valve seat for precise sealing and a threaded end stop element for adjustable biasing force adjustment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a conventional ball and spring assembly with iterative coining and shim selection process is used, then proper seating and functionality can be achieved, but manufacturing time and cost increase significantly

Engineering Contradiction:
Improveproper seating and functionalityVSAvoidmanufacturing time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The conical valve seat is pre-formed during housing manufacturing rather than requiring post-manufacturing coining operations. The precise conical geometry is established in advance, eliminating the need for iterative seating adjustments and shim selection during assembly.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention changes the geometric parameters of the valve seat from a flat or slightly radiused surface to a precise conical surface with specific angle tolerances. This parameter change enables self-aligning seating that eliminates the need for iterative adjustment processes.

Inventive Principle:
Principle #35Parameter changes

2Ease of manufacture

If conventional flat valve seats are used, then manufacturing is simpler, but sealing reliability decreases due to improper ball seating

Engineering Contradiction:
Improvevalve seat manufacturingVSAvoidsealing reliability
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The invention employs a conical surface geometry for the valve seat instead of a flat surface. The conical shape provides a self-aligning seating surface that ensures proper ball engagement and sealing, while the precision is achieved through standard machining operations rather than complex iterative processes.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Device complexity

If fixed spring preload is used in conventional designs, then assembly is simpler, but adjustment of biasing force becomes impossible

Engineering Contradiction:
Improveassembly complexityVSAvoidbiasing force adjustment
Core Design Contradiction:
Device complexityVSAdaptability or versatility

Solution Approach 1:

The invention transforms the static spring preload system into an adjustable one by incorporating a threaded end stop element. This allows the biasing force to be dynamically adjusted by rotating the end stop, changing the spring compression length, and thereby modifying the force applied to the ball carrier assembly.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The adjustable end stop element enables field adjustment of the valve's operating parameters without requiring specialized tools or expertise. The threaded mechanism provides intuitive, self-explanatory adjustment capability that allows end users to optimize valve performance as needed.

Inventive Principle:
Principle #25Self-service

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

This design reduces manufacturing time and complexity by eliminating the need for iterative processes, enhances sealing reliability, and allows for precise adjustment of the biasing force, improving overall valve performance and efficiency.

Implementation Method 1

a conical valve seat for precise sealing

Methodology Applied
Scientific EffectGeometric sealing: Geometry

Implementation Method 2

a threaded end stop element for adjustable biasing force adjustment

Methodology Applied
Scientific EffectThreaded mechanical advantage: Screw

Implementation Method 3

a biasing element arranged within the inner cavity and configured to bias the ball carrier toward the inlet end wall

Methodology Applied
Scientific EffectElastic potential energy storage: Spring

Data Source

PatentUS20250377047A1Aircraft pressure relief valves
Publication Date: 2025.12.11 HAMILTON SUNDSTRAND CORP
  • US20250377047A1 patent drawing
  • US20250377047A1 patent drawing
  • US20250377047A1 patent drawing

AI summary

Pressure relief valves include a valve housing having an inlet end wall and an inner cavity defined within the valve housing. An inlet opening defining a valve seat is formed within the inlet end wall. A valve ball is configured to sealingly engage with the valve seat to seal the inlet opening. A ball carrier is arranged to retain the valve ball between the ball carrier and the inlet end wall. A biasing element is configured to bias the ball carrier toward the inlet end wall. An end stop element is configured to threadedly engage with an interior surface of the valve housing and the biasing element is biased against a stop surface of the end stop element. A locking nut is configured to threadedly engage with an end of the end stop element and secure the end stop element to the valve housing.