US4533315A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Integrated control system for induced draft combustion
Assignee: Honeywell Inc
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Filing: 1984-02-15
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Granted: 1985-08-06
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Expires: 2004-02-15
Abstract
Abstract An integrated, closed loop system for controlling the fuel to air ratio in an induced draft combustion chamber which has a control pilot through which a draft is induced so that the fuel to air ratio in the control pilot chamber has a predetermined ratio to the fuel to air ratio in the primary combustion chamber.
Inventors
- 👤 Lorne W. Nelson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 20:17
CPC Classifications
F; F23; F23N; F23N5/00; F23N5/02; F23N5/12; F23N5/126; F23N1/00; F23N1/06; F23N1/065
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
159 words
A system for controlling the fuel to air ratio in an induced draft combustion chamber comprising in combination: a combustion chamber; a gas fuel burner in said combustion chamber; means for supplying fuel to said combustion chamber fuel burner; means for inducing a flow of air in said combustion chamber to support combustion of said fuel; a control pilot chamber; a gas fuel burner in said control pilot chamber means for supplying fuel to said control pilot burner; means for establishing a proportional ratio between the quantity of fuel fed to the combustion chamber burner and the quantity of fuel fed to said control pilot burner; means coupling said control pilot chamber to said means for inducing a flow of air so that a quantity of air drawn through said control pilot chamber is proportional to the quantity of air drawn through said combustion chamber; and means for controlling the fuel to air ratio in said control pilot chamber.
Claim 2
Independent Claim
159 words
A system for controlling the fuel to air ratio in an induced draft combustion chamber comprising in combination: a combustion chamber; a gas fuel burner in said combustion chamber; means for supplying fuel to said combustion chamber fuel burner; means for inducing a flow of air in said combustion chamber to support combustion of said fuel; a control pilot chamber; a gas fuel burner in said control pilot chamber means for supplying fuel to said control pilot burner; means for establishing a proportional ratio between the quantity of fuel fed to the combustion chamber burner and the quantity of fuel fed to said control pilot burner; means coupling said control pilot chamber to said means for inducing a flow of air so that a quantity of air drawn through said control pilot chamber is proportional to the quantity of air drawn through said combustion chamber; and means for controlling the fuel to air ratio in said control pilot chamber.
Claim 3
Dependent Claim
14 words
A system as in claim 1 wherein said control means includes a flame rod.
Claim 4
Dependent Claim
41 words
A system as in claim 1 wherein said means for inducing a flow of air for said combustion chamber includes a flue and a venturi in said flue and said means for coupling connects said control pilot chamber to said venturi.
Claim 5
Dependent Claim
101 words
A system as in claim 1 wherein said means for supplying fuel to said combustion chamber burner and said means for supplying fuel to said control pilot burner includes; a control valve; said control valve having a main gas inlet and an outlet to said combustion chamber burner; means to regulate the flow between said inlet and said outlet; and means to initially supply fuel from said inlet to said control pilot fuel supply means when said regulating means is closed, and to supply fuel from said outlet to said control pilot fuel supply means when said regulating means are open.
Claim 6
Dependent Claim
76 words
A system as in claim 1 wherein said means for controlling the fuel to air ratio in said pilot chamber includes: means for establishing a maximum flame current or maximum flame temperature in said control pilot chamber independently of the fuel heat content of said gas, whereby the fuel to air ratio in said combustion chamber can be established at an optimum desired ratio based upon the proportionality between the control pilot chamber and combustion chamber.
Claim 7
Dependent Claim
32 words
A system as in claim 4 wherein the fuel to air ratio in said pilot chamber rapidly passes through the stoichiometric ratio as said fuel supply switches from inlet to said outlet.
References Cited (Backward Citations)
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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) | 1988-08-05 | 1989-02-04 | 1989-08-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-08-05 | 1993-02-04 | 1993-08-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-08-05 | 1997-02-04 | 1997-08-06 | $7700.00 | Window Closed / Lapsed |