IP Library Granted Patent US 7,365,521
Granted Patent B2
US 7,365,521 · App. 11/807,089 · Granted Apr 29, 2008

Fault tolerant architecture for permanent magnet starter generator subsystem

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Quick Facts
Patent No.
US 7,365,521
App. No.
11/807,089
Granted
Apr 29, 2008
Kind
B2
Abstract

A permanent magnet starter/generator subsystem configured in a fault tolerant architecture is described herein for small engine applications. The system allows for lighter system weight, improved system reliability, higher performance capability and reduced maintenance.

Claims (47)

1. A method of operating an engine with permanent magnet generator (PMG) and power conversion unit (PCU) including the steps of:

(1) initiating a start sequence;

(2) monitoring PMG rotational speed to assist in proper execution of an engine start;

(3) generating an AC excitation by use of a PCU, wherein the AC excitation is used to operate the PMG as a motor and cause an engine to rotate;

(4) controlling speed of the PMG by controlling the AC excitation generated in the PCU during an engine start including at least one of:

(a) using sensorless control method;

(b) using at least one of an open or a closed loop control method; and

(c) using a control method that enables motoring start;

(5) controlling torque produced by the PMG during an engine start by controlling the AC excitation applied by the PCU including at least one of:

(a) using a torque versus speed characteristic; and

(b) using a soft start characteristic;

(6) cutting of starter assist automatically at a predetermined PMG speed, monitoring for fault conditions prior to, during, and after the engine start to ensure that a proper action is taken including at least one of:

(a) verifying that the engine is rotating in the correct direction;

(b) verifying correct phasing of the PMG voltage;

(c) verifying proper PCU operation prior to, during and after the engine start sequence; and

(d) detecting a ground fault within at least one of the PMG, PCU and a feeder cable;

(7) controlling the start sequence by executing a control logic algorithm including at least one of:

(a) executing an engine brake function prior to executing engine start to ensure that the engine does not rotate in an incorrect direction;

(b) executing an engine brake function prior to executing engine start to halt an engine that is rotating in an incorrect direction prior to engine start;

(c) executing an engine brake function prior to executing engine start to ensure proper alignment of PMG rotor magnets and that the AC excitation from the PCU is achieved; and

(d) incorporating control logic to alter the control logic algorithm in a predetermined manner dependent upon the state of a signal.

2. A method of operating a permanent magnet starter/generator system for an engine, the method comprising:

generating an alternating current (AC) using a plurality of converter modules within a power conversion unit (PCU);

applying the AC to a permanent magnet generator (PMG) to rotate the PMG and enable an engine start operation;

after the engine start operation, converting AC generated by the PMG to a desired voltage form using the plurality of converter modules; and

applying the desired voltage form to an electrical load wherein converting the AC generated by the PMG includes converting AC generated by each phase of the PMG to the desired voltage form using a DC-DC bi-directional converter module, wherein the DC-DC bi-directional Converter module is connected to a bi-directional power factor corrected full wave bridge module and a feedback control module; correcting power with the bi-directional power factor corrected full wave bridge module; and controlling feedback with the feedback control module.

3. A method according to claim 2 , wherein the plurality of converter modules includes one converter module per phase of the PMG.

4. A method according to claim 2 , further comprising:

controlling the plurality of converter modules between a starter mode where the AC is generated by the plurality of power converter modules to rotate the PMG, and a generator mode where the AC generated by the PMG is converted by the plurality of converter modules to the desired voltage form.

5. A method according to claim 4 , further comprising:

filtering the desired voltage form before applying the desired voltage form to the electrical load.

6. A method according to claim 5 , wherein the desired voltage form is selected from at least one of AC and DC voltage.

7. A method according to claim 2 , further comprising:

operating the plurality of converter modules in a standby mode where no power is provided from the plurality of converter modules.

8. A method according to claim 2 , further comprising:

controlling the AC generated by the power converter modules to adjust a torque characteristic of the PMG.

9. A method according to claim 2 , further comprising:

controlling the AC generated by the power converter modules to adjust a speed of the PMG to approximately 40% maximum PMG drive speed for providing a soft start characteristic.

10. A method according to claim 2 , wherein converting the AC generated by the PMG includes:

converting AC generated by each phase of the PMG to the desired voltage form using a separate power converter module for each phase of the PMG, and

filtering the desired voltage form before applying the desired voltage form to the electrical load.

11. A method according to claim 2 , further comprising;

detecting speed and phase information of the AC generated by the PMG.

12. A method according to claim 11 , further comprising:

detecting ground faults with a ground fault detector module within the PCU.

13. A method according to claim 12 , further comprising:

equalizing the desired voltage form with an equalizer and phase balance control module within the PCU.

Assignments (6)
RELEASE OF SECURITY INTEREST Recorded Oct 23, 2025
From: HSBC BANK USA, NATIONAL ASSOCIATION, AS AGENT
To: ASTRONICS CONNECTIVITY SYSTEMS & CERTIFICATION CORP.; ASTRONICS AEROSAT CORPORATION; ASTRONICS CORPORATION; PECO, INC.; ASTRONICS ADVANCED ELECTRONIC SYSTEMS CORP.; ASTRONICS TEST SYSTEMS INC.; DIAGNOSYS INC.; LUMINESCENT SYSTEMS, INC.
Reel/Frame 073227/0325 →
RELEASE OF SECURITY INTEREST Recorded Dec 4, 2024
From: HSBC BANK USA, N.A., AS AGENT
To: ASTRONICS CORPORATION; ASTRONICS ADVANCED ELECTRONIC SYSTEMS CORP.; ASTRONICS AEROSAT CORPORATION; ASTRONICS TEST SYSTEMS INC.; LUMINESCENT SYSTEMS, INC.; ASTRONICS CONNECTIVITY SYSTEMS & CERTIFICATION CORP.; PECO, INC.; DIAGNOSYS INC.
Reel/Frame 069491/0184 →
RELEASE OF SECURITY INTEREST Recorded Jul 12, 2024
From: GREAT ROCK CAPITAL PARTNERS MANAGEMENT, LLC
To: ASTRONICS AEROSAT CORPORATION; ASTRONICS CONNECTIVITY SYSTEMS & CERTIFICATION CORP.; PECO, INC.; ASTRONICS ADVANCED ELECTRONIC SYSTEMS CORP.; ASTRONICS CORPORATION; ASTRONICS TEST SYSTEMS INC.; DIAGNOSYS INC.; LUMINESCENT SYSTEMS, INC.
Reel/Frame 068311/0938 →
SECURITY INTEREST Recorded Jul 11, 2024
From: ASTRONICS CORPORATION; ASTRONICS ADVANCED ELECTRONIC SYSTEMS CORP.; ASTRONICS AEROSAT CORPORATION; ASTRONIC TEST SYSTEMS INC.; LUMINESCENT SYTEMS, INC.; ASTRONICS CONNECTIVITY SYSTEMS & CERTIFICATION CORP.; PECO, INC.; DIAGNOSYS INC.
To: HSBC BANK USA, N.A.
Reel/Frame 068283/0900 →
SECURITY INTEREST Recorded Jan 20, 2023
From: ASTRONICS CUSTOM CONTROL CONCEPTS INC.; ASTRONICS DME LLC; ASTRONICS CORPORATION; LUMINESCENT SYSTEMS, INC.; ASTRONICS TEST SYSTEMS INC.; ASTRONICS ADVANCED ELECTRONIC SYSTEMS CORP.; ASTRONICS CONNECTIVITY SYSTEMS & CERTIFICATION CORP.; ASTRONICS AEROSAT CORPORATION; PECO, INC.; DIAGNOSYS INC.
To: GREAT ROCK CAPITAL MANAGEMENT, LLC
Reel/Frame 062444/0836 →
SECURITY INTEREST Recorded Jan 20, 2023
From: ASTRONICS AEROSTAT CORPORATION; ASTRONICS CONNECTIVITY SYSTEMS & CERTIFICATION CORP.; ASTRONICS CORPORATION; PECO, INC.; ASTRONICS ADVANCED ELECTRONICS SYSTEMS CORP.; ASTRONICS TEST SYSTEMS INC.; DIAGNOSYS INC.; LUMINESCENT SYSTEMS, INC.
To: HSBC BANK USA, NATIONAL ASSOCIATION, AS AGENT
Reel/Frame 062445/0342 →