Aircraft Hydraulic Distributor Seizing Detection
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Solution Overview
Problem
Existing hydraulic distributors for aircraft servo-controls face challenges with dynamic seals in seizing detection systems, leading to hydraulic leakage and increased maintenance costs due to the complexity and expense of dynamic gaskets.
Innovation Solution
A coaxial hydraulic distributor with a reed switch and amplification means using a magnetized lever and magnetic lenses to detect seizing, eliminating the need for dynamic seals by allowing the detector device to be immersed in hydraulic fluid, thus preventing leakage and reducing maintenance costs.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a dynamic seal is used in the detector device to separate it from the hydraulic system, then the detector can be positioned outside the hydraulic fluid, but hydraulic leakage occurs and maintenance costs increase
Solution Approach 1:
The detector device is extracted from the hydraulic system by using a magnetic coupling mechanism that allows the detector to sense hydraulic distributor position without being in direct contact with the hydraulic fluid, thereby eliminating the need for dynamic seals and preventing hydraulic leakage
Solution Approach 2:
The mechanical contact-based detection system is replaced with a magnetic field-based detection system. A magnet is attached to the movable part of the hydraulic distributor, and a reed switch or Hall effect sensor detects its position, eliminating the need for mechanical connections and dynamic seals
2Reliability
If a dynamic gasket is used to seal the detector device, then the detector can be isolated from the hydraulic system, but the complexity and expense of the sealing system increases
Solution Approach 1:
The detector device is extracted from the hydraulic system by using a magnetic coupling mechanism that allows the detector to sense hydraulic distributor position without being in direct contact with the hydraulic fluid, thereby eliminating the need for dynamic seals and preventing hydraulic leakage
Solution Approach 2:
The mechanical contact-based detection system is replaced with a magnetic field-based detection system. A magnet is attached to the movable part of the hydraulic distributor, and a reed switch or Hall effect sensor detects its position, eliminating the need for mechanical connections and dynamic seals
3Ease of operation
If a dynamic seal is used in the detector device, then the detector can function independently from the hydraulic system, but maintenance costs increase due to seal wear and leakage
Solution Approach 1:
The detector device is extracted from the hydraulic system by using a magnetic coupling mechanism that allows the detector to sense hydraulic distributor position without being in direct contact with the hydraulic fluid, thereby eliminating the need for dynamic seals and preventing hydraulic leakage
Solution Approach 2:
The mechanical contact-based detection system is replaced with a magnetic field-based detection system. A magnet is attached to the movable part of the hydraulic distributor, and a reed switch or Hall effect sensor detects its position, eliminating the need for mechanical connections and dynamic seals
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 leak-tight seizing detection system that effectively alerts pilots to servo-control issues without hydraulic leakage, enhancing safety and reducing maintenance expenses through the use of static seals and a reed switch activated by amplified movement.
Implementation Method 1
a magnetized free end that activates the reed switch in the event of the emergency distributor member moving
Implementation Method 2
amplification means for amplifying the movement of the emergency distributor member, the amplification means comprising a lever having a magnetized free end
Data Source
AI summary
The present invention relates to a hydraulic distributor (2) of a servo-control (1) of an aircraft, the hydraulic distributor comprising main distributor member (10) and emergency distributor member (20) that are coaxial, said emergency distributor member (20) being caused to move by said main distributor member (10) in the event of said main distributor member (10) seizing, said hydraulic distributor being provided with a detector device (60) for detecting said seizing. The detector device (60) is provided with a reed switch (66) and with amplification means (62, 69, 68) for amplifying said movement of the emergency distributor member, said amplification means comprising a lever (62) having a magnetized free end (62′) that activates said reed switch (66) in the event of said emergency distributor member (20) moving.


