US5550456A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Voltage/current controlled voltage regulator to eliminate exciter field saturation
Assignee: Honeywell International Inc
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Filing: 1994-07-27
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Granted: 1996-08-27
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Expires: 2014-07-27
Abstract
Abstract A control scheme for a wound rotor synchronous generator whereby feedback signals corresponding to the exciter field current and the generator output voltage potential combine together to control the generator output voltage in such a way that at lower generator speeds and lower load requirements, exciter field current saturation is eliminated by reducing generator output voltage. The generator control scheme includes a circuit for sensing exciter field current in logic cooperation with a circuit for sensing generator voltage. Both sensing circuits regulate the current applied to the exciter field which corresponds to the rectified current applied to the field windings of the power generator. During steady state operations the generator output voltage is regulated using the generator output voltage as a feedback signal. At lower speeds and reduced loads and as the exciter field current approaches the saturation point, the generator output voltage is regulated using the exciter field current as a feedback signal.
Inventors
- 👤 Sampat Shekhawat
- 👤 Eli Liebermann
- 👤 William M. Scherzinger
- 👤 Gayton L. Silvestro
- 👤 Nick Suttora
- 👤 David Hodge
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 15:58
CPC Classifications
H; H02; H02P; H02P9/00; H02P9/14; H02P9/26; H02P9/30; H02P9/305; H02P2101/00; H02P2101/30
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
129 words
An aircraft electrical generating system producing an output potential comprising: (a) an excitation generator which is rotatably driven having a rotor from which a variable current is output; (b) a wound rotor synchronous generator which is rotatably driven having a rotor that accepts said variable current output and a stator from which current at the output potential is generated in response to said current output; and (c) a voltage regulator for controlling said current output comprising an excitation generator field current regulating circuit comprising an output potential sensing circuit in logic cooperation with a field current sensing circuit wherein said output potential sensing circuit regulates said output current at aircraft steady state engine speeds and said field current sensing circuit regulates said output current at low aircraft engine speeds.
Claim 2
Dependent Claim
129 words
An aircraft electrical generating system producing an output potential comprising: (a) an excitation generator which is rotatably driven having a rotor from which a variable current is output; (b) a wound rotor synchronous generator which is rotatably driven having a rotor that accepts said variable current output and a stator from which current at the output potential is generated in response to said current output; and (c) a voltage regulator for controlling said current output comprising an excitation generator field current regulating circuit comprising an output potential sensing circuit in logic cooperation with a field current sensing circuit wherein said output potential sensing circuit regulates said output current at aircraft steady state engine speeds and said field current sensing circuit regulates said output current at low aircraft engine speeds.
Claim 3
Dependent Claim
29 words
The aircraft electrical generating system of claim 1 wherein said field current sensing circuit and said output potential sensing circuit regulate said output current at low aircraft engine speeds.
Claim 4
Dependent Claim
27 words
A power generating system in accordance with claim 1 wherein said field current sensing circuit prevents the field coil of said excitation generator from reaching current saturation.
Claim 5
Dependent Claim
118 words
An aircraft electrical generating system producing an output potential comprising: (a) an excitation generator which is rotatably driven having a rotor from which a variable current is output; (b) a wound rotor synchronous generator which is rotatably driven having a rotor that accepts said variable current output and a stator from which current at the output potential is generated in response to said current output; and (c) a voltage regulator for controlling said current output comprising an excitation generator field current regulating circuit comprising an output potential sensing circuit in logic cooperation with a generator speed sensing circuit wherein said output potential sensing circuit and said speed sensing circuit regulate said output current at low aircraft engine speeds.
Claim 6
Dependent Claim
118 words
An aircraft electrical generating system producing an output potential comprising: (a) an excitation generator which is rotatably driven having a rotor from which a variable current is output; (b) a wound rotor synchronous generator which is rotatably driven having a rotor that accepts said variable current output and a stator from which current at the output potential is generated in response to said current output; and (c) a voltage regulator for controlling said current output comprising an excitation generator field current regulating circuit comprising an output potential sensing circuit in logic cooperation with a generator speed sensing circuit wherein said output potential sensing circuit and said speed sensing circuit regulate said output current at low aircraft engine speeds.
Claim 7
Dependent Claim
27 words
A power generating system in accordance with claim 4 wherein said generator speed sensing circuit prevents the field coil of said excitation generator from reaching current saturation.
Claim 8
Dependent Claim
168 words
A power generating system for producing a regulated output potential comprising: (a) a main generator having a stator and a rotor, said rotor is mounted on a shaft which is rotatably driven to cause current at said output potential to be generated by said stator of said main generator; (b) an excitation generator having a rotor mounted on said shaft and a stator from which a regulated current signal is output to the field windings of said rotor of said main generator; and (c) a voltage regulator coupled to said output potential, to the field coil of said excitation generator and to the excitation current applied to said field coil of said excitation generator for regulating said excitation current to control said current signal output; wherein said voltage regulator comprises a first regulation circuit means for controlling the output potential as a function of said excitation current in logic cooperation with a second regulation circuit means for controlling the output potential as a function of said output potential.
Claim 9
Dependent Claim
168 words
A power generating system for producing a regulated output potential comprising: (a) a main generator having a stator and a rotor, said rotor is mounted on a shaft which is rotatably driven to cause current at said output potential to be generated by said stator of said main generator; (b) an excitation generator having a rotor mounted on said shaft and a stator from which a regulated current signal is output to the field windings of said rotor of said main generator; and (c) a voltage regulator coupled to said output potential, to the field coil of said excitation generator and to the excitation current applied to said field coil of said excitation generator for regulating said excitation current to control said current signal output; wherein said voltage regulator comprises a first regulation circuit means for controlling the output potential as a function of said excitation current in logic cooperation with a second regulation circuit means for controlling the output potential as a function of said output potential.
Claim 10
Dependent Claim
23 words
A power generating system in accordance with claim 6 wherein said first regulation circuit means prevents said field coil from reaching current saturation.
Claim 11
Dependent Claim
21 words
A power generating system in accordance with claim 6 wherein said output potential is a three-phase alternating current at 400 Hz.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1999-08-27 | 2000-02-26 | 2000-08-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2003-08-27 | 2004-02-26 | 2004-08-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2007-08-27 | 2008-02-26 | 2008-08-27 | $7700.00 | Window Closed / Lapsed |