Jam-Tolerant Linear Control Motor for Hydraulic Actuator
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Solution Overview
Problem
Rotorcraft control motors are prone to magnetic seizing and bearing failures, which can lead to catastrophic failures of actuators and hydraulic systems, especially in systems with limited redundancy, posing a significant risk to flight safety.
Innovation Solution
The development of a jam-tolerant linear control motor design that incorporates non-magnetic materials to prevent magnetic seizing and includes features such as break wires to detect bearing failures, allowing for early detection and prevention of failures before they become catastrophic, and mechanisms to reduce failures in joints that convert rotary motion into linear motion.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Force
If magnetic components are used in the control motor, then the motor can generate sufficient force to actuate the hydraulic valve, but magnetic seizing occurs leading to catastrophic failure
Solution Approach 1:
The patent removes magnetic components from the control motor design, extracting the source of magnetic seizing while maintaining motor functionality through alternative non-magnetic actuation mechanisms. This eliminates the harmful magnetic interactions that caused seizing between rotor and stator components.
Solution Approach 2:
The patent introduces non-magnetic intermediary materials and designs between moving components, using materials such as non-magnetic metals or composites that mediate the interaction between rotor and stator, preventing direct magnetic contact while still allowing force transmission.
2Ease of operation
If traditional bearing designs are used in the control motor, then the motor can operate smoothly, but bearing failures occur without early detection leading to catastrophic failure
Solution Approach 1:
The patent incorporates feedback mechanisms including break wires and sensors that continuously monitor bearing condition and provide real-time information about motor operation, enabling detection of bearing degradation and failure modes before they lead to catastrophic system failure.
Solution Approach 2:
The patent implements preliminary detection features such as break wires positioned to detect bearing failure early in the failure process, allowing preventive action to be taken before the bearing failure propagates to other critical components.
3Adaptability or versatility
If joints converting rotary motion to linear motion are used in the actuator, then the hydraulic valve can be actuated, but joint failures occur leading to loss of actuator function
Solution Approach 1:
The patent replaces traditional mechanical joints that convert rotary to linear motion with alternative mechanisms such as bellcranks or direct-coupled linear actuators, eliminating the joint interfaces that are prone to failure while maintaining the necessary motion conversion functionality.
4Device complexity
If redundant systems are not implemented in the control system, then the system complexity is reduced, but the system is highly vulnerable to single-point failures
Solution Approach 1:
The patent implements beforehand cushioning through detection and warning systems that prepare the operator for potential failures, allowing preventive maintenance or graceful degradation before catastrophic failure occurs, effectively cushioning against the impact of single-point failures.
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 reduces the occurrence of magnetic seizing and bearing failures, enhancing the reliability of rotorcraft control systems by enabling early detection and maintenance, thereby improving flight safety and reducing the likelihood of system failures.
Implementation Method 1
a coil wrapped around the armature and operable to selectively add and subtract magnetic flux from the magnetic flux path
Implementation Method 2
a non-magnetic material disposed between the coil and the magnet and magnetic material
Data Source
AI summary
According to one embodiment, a linear control motor includes a first permanent magnet, a coil, a first magnetic material, a shaft, and a first non-magnetic material. The first non-magnetic material is disposed between at least one of the movable components and at least one of the static components and operable to prevent physical contact between at least one of the movable components and at least one of the static components.


