Patent US4330237A successfully refreshed from Google Patents.
US4330237A
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Compressor and engine efficiency system and method
Assignee: Michigan Consolidated Gas Co
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Filing: 1979-10-29
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Granted: 1982-05-18
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Expires: 1999-10-29
Abstract
Abstract A method and system for controlling natural gas compressor and engine units. Particularly, the control method provides for the adjustment of the engine speed and compressor loading, so as to minimize the compressing energy required while maintaining a desired gas flow through the pipeline. The control of the engine speed and compressor loading is based in part on an energy quotient value for the unit. The control method further provides for efficient operation during multiple-stage compression, by controlling the interstage pressure. The control method is also adapted to predict impending compressor and engine unit failures. The control system is based upon a digital-type controller which generates control signals in response to changes in the energy quotient value for the unit.
Inventors
- 👤 Husam Battah
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-27 12:12
CPC Classifications
F; F02; F02B; F02B63/00; F02B63/06; F04; F04B; F04B35/00; F04B35/002; F02B43/00; F02B43/10; F02B2043/103
Claims Analysis
Total Claims: 31
Claim 1
Independent Claim
73 words
A method of controlling a gas compressor and engine unit, the steps comprising: (a) sensing the values of a set of operating and control parameters at determinable intervals; (b) determining an energy quotient for said unit from said operating and control parameters; (c) adjusting at least one control parameter in response to a change in said energy quotient, so that said energy quotient for said gas compressor and engine unit is substantially maximized.
Claim 2
Independent Claim
73 words
A method of controlling a gas compressor and engine unit, the steps comprising: (a) sensing the values of a set of operating and control parameters at determinable intervals; (b) determining an energy quotient for said unit from said operating and control parameters; (c) adjusting at least one control parameter in response to a change in said energy quotient, so that said energy quotient for said gas compressor and engine unit is substantially maximized.
Claim 3
Dependent Claim
16 words
The method according to claim 1 wherein one of said control parameters is a compressor loading.
Claim 4
Dependent Claim
16 words
The method according to claim 1 wherein one of said control parameters is an engine speed.
Claim 5
Dependent Claim
47 words
The method according to claim 1 wherein said operating parameters include a suction and discharge gas pressure, a lower heating value of a fuel gas, a rate of fuel gas consumption by said engine, a suction gas temperature, and a capacity of gas flow from said compressor.
Claim 6
Dependent Claim
17 words
The method according to claim 1 wherein said adjustment further provides a desired capacity of gas flow.
Claim 7
Independent Claim
70 words
A method of increasing the efficiency of a gas compressor and engine unit, the steps comprising: (a) adjusting a compressor loading and engine speed so that a desired capacity of gas flow is achieved; (b) readjusting said compressor loading and said engine speed after a determinable interval so that an energy quotient for said gas compressor and engine unit is substantially maximized, while maintaining said desired capacity of gas flow.
Claim 8
Independent Claim
70 words
A method of increasing the efficiency of a gas compressor and engine unit, the steps comprising: (a) adjusting a compressor loading and engine speed so that a desired capacity of gas flow is achieved; (b) readjusting said compressor loading and said engine speed after a determinable interval so that an energy quotient for said gas compressor and engine unit is substantially maximized, while maintaining said desired capacity of gas flow.
Claim 9
Dependent Claim
23 words
The method according to claim 6 wherein said adjustment minimizes the required engine speed necessary to achieve said desired capacity of gas flow.
Claim 10
Dependent Claim
23 words
The method according to claim 6 wherein said adjustment maximizes the required compressor loading necessary to achieve said desired capacity of gas flow.
Claim 11
Independent Claim
71 words
A method of controlling an engine speed and a compressor loading for a gas compressor and engine unit, the steps comprising: (a) sensing a suction and a discharge gas pressure from said compressor; (b) determining a compression ratio from said suction and discharge pressure; (c) adjusting said engine speed and compressor loading in response to a change in said compression ratio, so that an energy quotient for said unit is maximized.
Claim 12
Independent Claim
71 words
A method of controlling an engine speed and a compressor loading for a gas compressor and engine unit, the steps comprising: (a) sensing a suction and a discharge gas pressure from said compressor; (b) determining a compression ratio from said suction and discharge pressure; (c) adjusting said engine speed and compressor loading in response to a change in said compression ratio, so that an energy quotient for said unit is maximized.
Claim 13
Dependent Claim
105 words
A computer-implemented method of controlling a gas compressor and engine unit, the steps comprising: (a) calculating an initial energy quotient from a selected set of operating and control parameter values; (b) storing said energy quotient value in a memory of a computer; (c) initiating the operation of said gas compressor and engine unit; (d) sensing at determinable intervals said operating and control parameter values; (e) calculating a new energy quotient from said sampled parameter values; (f) comparing said new energy quotient with said initial energy quotient; (g) modifying at least one of said control parameters in response to a difference between said energy quotient values.
Claim 14
Dependent Claim
105 words
A computer-implemented method of controlling a gas compressor and engine unit, the steps comprising: (a) calculating an initial energy quotient from a selected set of operating and control parameter values; (b) storing said energy quotient value in a memory of a computer; (c) initiating the operation of said gas compressor and engine unit; (d) sensing at determinable intervals said operating and control parameter values; (e) calculating a new energy quotient from said sampled parameter values; (f) comparing said new energy quotient with said initial energy quotient; (g) modifying at least one of said control parameters in response to a difference between said energy quotient values.
Claim 15
Dependent Claim
18 words
The computer-implemented method according to claim 10 wherein said modification minimizes said difference between said energy quotient values.
Claim 16
Dependent Claim
17 words
The computer-implemented method according to claim 10 wherein said modification maintains a desired capacity of gas flow.
Claim 17
Dependent Claim
17 words
The computer-implemented method according to claim 10 wherein one of said control parameters is a compressor loading.
Claim 18
Dependent Claim
17 words
The computer-implemented method according to claim 10 wherein one of said control parameters is an engine speed.
Claim 19
Dependent Claim
92 words
A controller device for use with a gas compressor and engine unit, comprising: transducer means for sensing a set of operating and control parameter values; input interface means for receiving signals from said transducer means; processing means for determining an energy quotient, for said gas compressor and engine unit, from said operating and control parameter values; means for comparing said energy quotient with a predeterminable energy quotient in order to control at least one of said control parameters; and output interface means for applying control signals in response to said comparing means.
Claim 20
Dependent Claim
92 words
A controller device for use with a gas compressor and engine unit, comprising: transducer means for sensing a set of operating and control parameter values; input interface means for receiving signals from said transducer means; processing means for determining an energy quotient, for said gas compressor and engine unit, from said operating and control parameter values; means for comparing said energy quotient with a predeterminable energy quotient in order to control at least one of said control parameters; and output interface means for applying control signals in response to said comparing means.
Claim 21
Dependent Claim
40 words
The controller device according to claim 15 wherein said operating parameters include a suction and discharge gas pressure, a suction gas temperature, a rate of fuel gas consumption by said engine, and a lower heating value of said fuel gas.
Claim 22
Dependent Claim
19 words
The controller device according to claim 15 wherein said control parameters include a compressor loading and an engine speed.
Claim 23
Dependent Claim
23 words
The controller device according to claim 15 wherein said control signals maximize said energy quotient value for said gas compressor and engine unit.
Claim 24
Dependent Claim
20 words
A controller device according to claim 15 wherein said control signals minimize a difference between said compared energy quotient values.
Claim 25
Dependent Claim
21 words
The controller device according to claim 16 wherein said operating parameters further include a capacity of gas flow from said compressor.
Claim 26
Dependent Claim
36 words
The controller device according to claim 20 which includes means for comparing said sensed capacity with a predeterminable capacity of gas flow from said compressor in order to control at least one of said control parameters.
Claim 27
Dependent Claim
27 words
The controller device according to claim 21 wherein said control signals maintain said predeterminable capacity at a maximum energy quotient for said gas compressor and engine unit.
Claim 28
Independent Claim
90 words
A method of predicting impending gas compressor and engine unit failures, the steps comprising: (a) sensing the values of a set of operating and control parameters at determinable intervals; (b) determining a first energy quotient for said unit, from said operating and control parameters, wherein said determination is based upon a calculated capacity of gas flow from said compressor; (c) comparing said first energy quotient with a second pre-determined standard energy quotient; and (d) shutting said unit down with a difference between said energy quotient values exceeds a predetermined value.
Claim 29
Independent Claim
90 words
A method of predicting impending gas compressor and engine unit failures, the steps comprising: (a) sensing the values of a set of operating and control parameters at determinable intervals; (b) determining a first energy quotient for said unit, from said operating and control parameters, wherein said determination is based upon a calculated capacity of gas flow from said compressor; (c) comparing said first energy quotient with a second pre-determined standard energy quotient; and (d) shutting said unit down with a difference between said energy quotient values exceeds a predetermined value.
Claim 30
Independent Claim
66 words
A method of controlling at least two gas compressor and engine units combined in series for multiple-stage operation, the steps comprising: (a) adjusting an engine speed and a compressor loading for each of said units so that an equivalent capacity of gas flow from each compressor is achieved; and (b) readjusting said engine speeds and said compressor loadings so that a predeterminable inter-stage pressure is maintained.
Claim 31
Independent Claim
66 words
A method of controlling at least two gas compressor and engine units combined in series for multiple-stage operation, the steps comprising: (a) adjusting an engine speed and a compressor loading for each of said units so that an equivalent capacity of gas flow from each compressor is achieved; and (b) readjusting said engine speeds and said compressor loadings so that a predeterminable inter-stage pressure is maintained.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-05-17 | 1985-11-16 | 1986-05-18 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-05-17 | 1989-11-16 | 1990-05-18 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-05-17 | 1993-11-16 | 1994-05-18 | $7700.00 | Window Closed / Lapsed |