Pneumatic Isolation Valve for Aircraft Engine Oil Circuit
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Solution Overview
Problem
Existing shut-off and isolation valves in airplane engines require separate components for fire protection and anti-siphon functions, necessitating electrical power and complex control logic, which is not feasible in all turboprop engines, especially during flight stops where residual rotation is lost.
Innovation Solution
A pneumatically controlled isolation valve that uses compressed air from the engine compressor or pneumatic starter to perform both fire prevention and anti-siphon functions, eliminating the need for electronic control logic and separate components, utilizing a shuttle valve to select the higher pressure source and a flap valve with a bellows cylinder for efficient operation.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Device complexity
If a single isolation valve is used to perform both fire prevention and anti-siphon functions, then device complexity is reduced, but reliability must be maintained through pneumatic control
Solution Approach 1:
The patent combines two separate valves (fire protection valve and anti-siphon valve) into a single isolation valve that performs both functions. This merging reduces device complexity and the number of components while maintaining the necessary reliability through integrated pneumatic control that responds to both fire detection signals and engine stop conditions.
Solution Approach 2:
The isolation valve is designed with multi-functionality to serve dual purposes: fire protection by isolating the oil circuit during fire conditions, and anti-siphon by preventing oil leakage during engine stop. The pneumatic control system enables this universal valve to respond appropriately to different operational scenarios without requiring separate dedicated valves for each function.
2Measurement precision
If electrical control valves are used for fire protection and anti-siphon functions, then control precision is improved, but use of energy increases and device complexity increases
Solution Approach 1:
The patent replaces electrical control systems with a pneumatic control system for the isolation valve. Instead of using electric motors or solenoids that consume electrical energy, the system uses pneumatic actuators powered by compressed air from the engine's air compressor or pneumatic starter. This substitution eliminates electrical power requirements while maintaining reliable and precise control through pneumatic pressure regulation.
3Reliability
If separate valves are used for fire protection and anti-siphon functions, then reliability for each function is maximized, but device complexity and weight increase
Solution Approach 1:
The patent merges two separate valve systems into one integrated isolation valve, thereby reducing the total weight of the valve system. By combining the fire protection valve and anti-siphon valve into a single unit with shared pneumatic control, the design eliminates redundant components while maintaining the reliability needed for both fire protection and oil leakage prevention functions.
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 provides a single, weight- and cost-efficient valve that ensures fire protection and prevents oil leaks without electrical power, suitable for turboprop engines, by using pneumatic control for both power and signal, ensuring reliable operation during engine stops and starts.
Implementation Method 1
the isolation valve is pneumatically controlled and provided with a device allowing to automatically select as an operation the more highly compressed source of compressed air from two different sources
Implementation Method 2
a shuttle valve whose two intakes are connected to said two sources of compressed air respectively and whose outlet is connected to the isolation valve
Implementation Method 3
The isolation valve is preferably a flap valve provided with a bellows cylinder
Data Source
AI summary
The present invention relates to a turbomachine comprising an air compressor (3) and a lubrication circuit with an oil tank (1), said oil tank (1) being possibly isolated from the rest of the lubrication circuit (4,4A; 6,6A) by means of an isolation valve (7), wherein the isolation valve (7) is configured so as to:operate, i.e. to close and open respectively as the engine (2) stops and starts;remain open when the engine (2) is running;remain closed when the engine (2) is stopped.

