IP Library Granted Patent US 6,871,495
Granted Patent B2
US 6,871,495 · App. 10/431,690 · Granted Mar 29, 2005

Thermal cycle engine boost bridge power interface

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Quick Facts
Patent No.
US 6,871,495
App. No.
10/431,690
Granted
Mar 29, 2005
Kind
B2
Abstract

A system and method for controlling a thermal dynamic cycle engine, such as a Stirling engine. The system includes a controller able to execute a program to alter certain aspects of the system to provide for a maximum power transfer and substantially stall free start up of the thermal dynamic cycle engine. Generally the controller is able to alter the current load to achieve a selected stroke length, pattern or temperature of a heater head of the engine. The system allows for generally stall free start-up and continuous control for maximum power (with maximum power factor) transfer from the thermal cycle engine or the associated alternator.

Claims (57)

1. A system for controlling a thermal cycle engine powering an alternator to produce a power transfer, comprising:

a processor able to carry out a set of instructions;

a current sensing subsystem for sensing a current flowing through a current sensor to determine a V emf ; and

an error amplifying subsystem;

a temperature sensor to sense the temperature of a portion of the thermal cycle engine; and

a position sensor to sense the position of at least one of the thermal cycle engine and the alternator;

wherein said processor controls said error amplifying module depending upon the temperature in the position of the thermal cycle engine or the alternator to achieve a selected power transfer from the alternator to a load;

wherein said processor is able to control said error amplifying module to provide a load current that is substantially of the same wave shape and phase of the V emf of the thermal cycle engine to achieve a selected power transfer from the alternator.

2. A system for controlling a thermal cycle engine powering an alternator to produce a power transfer, comprising:

a processor able to carry out a set of instructions;

a current sensing subsystem for sensing a current flowing through a current sensor to determine a V emf ; and

an error amplifying subsystem;

a zero crossing link signal to said processor such that said processor can operate the thermal cycle engine synchronously with a second thermal cycle engine;

wherein said processor is able to control said error amplifying module to provide a load current that is substantially of the same wave shave and phase of the V emf of the thermal cycle engine to achieve a selected power transfer from the alternator.

3. A system for efficiently producing electrical power, comprising:

a thermal cycle engine;

an alternator driven by said thermal cycle engine;

a load to consume electrical power produced by said alternator; and

a digital controller for controlling at least a portion of at least one of said thermal cycle engine and said alternator to provide power transfer from said alternator to said load;

wherein said controller is able to control a stroke length of said alternator to obtain a selected power transfer from said alternator;

said controller is able to alter the consumption of electrical power from said alternator with said load during difference phases of a life cycle of said thermal cycle; and

said load is generally lower at a beginning of said life cycle and higher at a intermediate portion of said life cycle.

4. A method of operating a thermal cycle engine and an alternator to produce a power transfer from the alternator to a load during a life cycle of the thermal cycle engine, comprising:

transferring a generally maximum attainable power from the alternator;

determining a current of the alternator with a processor;

adjusting said current remotely to the thermal cycle engine;

determining a stroke length of the thermal cycle engine; and

selecting an optimal stroke length for the thermal cycle engine or the alternator;

starting the thermal cycle engine substantially stall free;

wherein the step of transferring a generally maximum obtainable power from the alternator includes transferring an amount of power less than an amount required to stall the thermal cycle engine; and

wherein selecting a stroke includes selecting a stroke generally less than the knocking stroke to remove the maximum amount of power.

5. The method of claim 4 , wherein starting the thermal cycle engine includes:

determining said stroke a plurality of times; and

adjusting said current prior to said determined stroke reaching said knocking stroke.

6. A computer program executed by a processor to control either a thermal cycle engine or an alternator to obtain a power transfer from the alternator, the program comprising:

starting the thermal cycle engine generally stall free;

optimizing a stroke length of at least one of the alternator and the thermal cycle engine;

optimizing a current from the alternator; and

optimizing a heater head temperature of the thermal cycle engine; wherein optimizing a current from the alternator includes;

reading a wave table stored in a computer accessible memory;

determining a error correction value to achieve a optimum current from the alternator;

providing the error correction value to a analog system to provide a feed forward signal such that the next cycle of detected current substantially matches the wave table.

7. The computer program of claim 6 , wherein starting the thermal cycle engine includes:

selecting a load to achieve a maximum stroke length at the start-up of the thermal cycle engine.

8. The computer program of claim 7 , wherein:

said load is selectable as said stroke length generally reaches a knocking stroke length;

said computer program controls an analog source to increase a load on the alternator to reduce the current stroke length.

9. A computer program executed by a processor to control either a thermal cycle engine or an alternator to obtain a power transfer from the alternator, the program comprising:

starting the thermal cycle engine generally stall free;

optimizing a stroke length of at least one of the alternator and the thermal cycle engine;

optimizing a current from the alternator; and

optimizing a heater head temperature of the thermal cycle engine;

wherein optimizing a heater head temperature includes;

calculating a current temperature of the heater head;

checking the calculated current temperature with a stored optimal temperature of the heater head; and

optimizing a stroke length to substantially equalize said sensed temperature and said stored selected temperature.

10. The computer program of claim 9 , wherein a longer stroke length cools said heater head.

Assignments (12)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 064424/0050 →
RELEASE OF SECURITY INTEREST Recorded Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 039597/0890 →
NOTICE OF SUCCESSION OF AGENCY (INTELLECTUAL PROPERTY) Recorded Jun 20, 2016
From: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS THE RESIGNING AGENT
To: BANK OF AMERICA, N.A., AS THE SUCCESSOR AGENT
Reel/Frame 039079/0857 →
CHANGE OF NAME Recorded Aug 5, 2014
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 033474/0766 →
SECURITY AGREEMENT Recorded Jun 21, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: U.S. BANK NATIONAL ASSOCIATION
Reel/Frame 030656/0615 →
SECURITY AGREEMENT Recorded Jun 17, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: WELLS FARGO BANK, NATIONAL ASSOCIATION
Reel/Frame 030628/0408 →
CHANGE OF NAME Recorded Jun 12, 2013
From: RUBY ACQUISITION ENTERPRISES CO.
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 030593/0055 →
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE'S NAME ON ORIGINAL COVER SHEET PREVIOUSLY RECORDED ON REEL 017882 FRAME 0126. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNEE WAS INCORRECTLY RECORDED AS "UNITED TECHNOLOGIES CORPORATION". ASSIGNEE SHOULD BE "RUBY ACQUISITION ENTERPRISES CO.". Recorded Jun 12, 2013
From: THE BOEING COMPANY AND BOEING MANAGEMENT COMPANY
To: RUBY ACQUISITION ENTERPRISES CO.
Reel/Frame 030592/0954 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 19, 2007
From: UNITED TECHNOLOGIES CORPORATION
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 019458/0247 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 16, 2006
From: BOEING C OMPANY AND BOEING MANAGEMENT COMPANY, THE
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 017882/0126 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 27, 2006
From: BOEING COMPANY AND BOEING MANAGEMENT COMPANY, THE
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 017681/0537 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 8, 2003
From: LYNCH, THOMAS H.; KOCH, BRIAN
To: BOEING COMPANY, THE
Reel/Frame 014056/0200 →