APU Overspeed Detection Circuit Using Discrete Components

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Solution Overview

Problem

Existing aircraft auxiliary power unit (APU) controllers rely on complex and costly microcontroller/CPLD/FPGA-based circuits for overspeed detection, which increases design complexity and certification costs, and are less accurate due to temperature variations in frequency-to-voltage conversion ICs.

Innovation Solution

The use of discrete circuit components, including a counter, digital-to-analog converter, and comparator, to accurately monitor APU engine speed and initiate shutdowns without field programmable gate arrays (FPGAs), reducing design complexity and certification costs while maintaining high accuracy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If microcontroller/CPLD/FPGA-based circuits are used for overspeed detection, then the detection functionality is achieved, but the design complexity and certification costs increase

Engineering Contradiction:
Improveoverspeed detection functionalityVSAvoiddesign complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent divides the overspeed detection system into separate functional modules: a frequency-to-voltage conversion module, a comparator module, and a shutdown control module. This segmentation allows each module to be independently designed and certified, reducing overall design complexity while maintaining reliable overspeed detection functionality.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent replaces complex digital logic systems (microcontrollers, CPLDs, FPGAs) with an analog-based detection mechanism using frequency-to-voltage conversion and voltage comparison. This substitution simplifies the system architecture and reduces certification requirements while achieving the same safety function.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Reliability

If frequency-to-voltage conversion ICs are used for speed monitoring, then the overspeed detection is implemented, but temperature variations reduce measurement accuracy

Engineering Contradiction:
Improveoverspeed detection accuracyVSAvoidspeed measurement accuracy
Core Design Contradiction:
ReliabilityVSMeasurement precision

Solution Approach 1:

The patent introduces a feedback mechanism where the output voltage from frequency-to-voltage conversion is continuously compared against a reference voltage corresponding to the maximum safe speed. This feedback loop ensures that temperature-induced drifts in the conversion IC are compensated by adjusting the comparison threshold, maintaining accurate overspeed detection across varying temperatures.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent compensates for temperature variations by dynamically adjusting the reference voltage parameter in the comparator. As temperature changes affect the frequency-to-voltage conversion characteristics, the reference voltage is adjusted accordingly to maintain the accuracy of the overspeed threshold comparison.

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If discrete circuit components are used instead of FPGAs, then certification costs and design complexity are reduced, but implementation complexity increases

Engineering Contradiction:
Improvecertification easeVSAvoidcircuit implementation complexity
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The patent extracts the critical overspeed detection function from complex programmable logic devices and implements it using discrete, well-understood electronic components. By taking out only the essential functionality and implementing it with standard analog components, the system achieves easier certification while managing implementation complexity through proven design patterns.

Inventive Principle:
Principle #2Taking out (Extraction)

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 approach achieves accurate overspeed detection with less than 1% error over the operating range, reduces certification complexities, and allows for scalable solutions, enhancing reliability and reducing development timelines and costs.

Implementation Method 1

a counter to count a number of pulses from the signal occurring within a time interval

Methodology Applied
Scientific EffectPulse counting:

Implementation Method 2

a digital-to-analog converter (DAC) to convert the number of pulses into an analog voltage signal

Methodology Applied
Scientific EffectDigital-to-analog conversion:

Implementation Method 3

a comparator to: compare the analog voltage signal to an overspeed threshold signal and generate a shutdown command in response to the analog voltage signal exceeding the overspeed threshold signal

Methodology Applied
Scientific EffectVoltage comparison:

Data Source

PatentUS12196091B2Aircraft auxiliary power unit (APU) controllers and related methods
Publication Date: 2025.01.14 THE BOEING CO
  • US12196091B2 patent drawing
  • US12196091B2 patent drawing
  • US12196091B2 patent drawing

AI summary

Aircraft Auxiliary Power Unit (APU) controllers and related methods are described herein. An example APU controller includes a sensor interface to receive a signal from a speed sensor. The signal includes pulses representing a rotational speed of an engine of an APU. The APU controller also includes an overspeed detection circuit including a counter to count a number of pulses from the signal occurring within a time interval, a digital-to-analog converter (DAC) to convert the number of pulses into an analog voltage signal and a comparator to: compare the analog voltage signal to an overspeed threshold signal and generate a shutdown command in response to the analog voltage signal exceeding the overspeed threshold signal. The APU controller also includes a valve driver to, in response to receiving the shutdown command, cause a fuel shutoff valve to cease fuel flow to the engine of the APU.