Integrated control system for induced draft combustion

• US 4,533,315 A
• Filed: 02/15/1984
• Issued: 08/06/1985
• Est. Priority Date: 02/15/1984
• Status: Expired due to Fees

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Nelson, Lorne W.
• Primary Examiner(s): Focarino, Margaret A.
• Application Number:
  US06/580,325
• Time in Patent Office: 538 Days
• Field of Search: 431/12, 431/20, 431/42, 431/49, 431/59, 431/74, 431/75, 431/90, 236/15 BD, 236/15 E, 126/116 A, 110/185
• US Class Current: 431/20
• CPC Class Codes: F23N 1/065 using electrical or electromechanical means
• CPC Class Codes: F23N 5/126 using electrical or electromechanical means

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.

Claims

1. 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.

2. A system as in claim 1 wherein said control means includes a flame rod.

3. 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.

4. 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.

5. 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.

6. 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.