Pressure proving gas valve

• US 6,571,817 B1
• Filed: 02/28/2000
• Issued: 06/03/2003
• Est. Priority Date: 02/28/2000
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Bohan, John E. Jr.
• Primary Examiner(s): Walton, George L.
• Application Number:
  US09/514,117
• Time in Patent Office: 1,191 Days
• Field of Search: 137/65, 137/66, 137/6, 137/9, 137/87.01, 137/100, 137/101.19, 137/486, 137/487.5, 137/88, 137/4, 431/12, 431/18, 431/19, 431/75, 431/77, 431/78, 431/89, 431/90, 126/116.A
• US Class Current: 137/88
• CPC Class Codes: F23N 2005/181 using detectors sensitive to rate of flow of air
• CPC Class Codes: F23N 2005/182 Air flow switch
• CPC Class Codes: F23N 2225/04 pressure
• CPC Class Codes: F23N 2225/06 for determining flow
• CPC Class Codes: F23N 2233/08 with variable speed
• CPC Class Codes: F23N 2235/16 variable flow or proportional valves
• CPC Class Codes: F23N 5/184 using electronic means
• CPC Class Codes: F23N 5/265 using electronic means
• CPC Class Codes: Y10T 137/0335 Controlled by consistency of mixture
• CPC Class Codes: Y10T 137/0346 Controlled by heat of combustion of mixture
• CPC Class Codes: Y10T 137/0363 For producing proportionate flow
• CPC Class Codes: Y10T 137/2496 Self-proportioning or correlating systems
• CPC Class Codes: Y10T 137/2499 Mixture condition maintaining or sensing
• CPC Class Codes: Y10T 137/2529 With electrical controller
• CPC Class Codes: Y10T 137/7761 Electrically actuated valve

Abstract

A pressure proving gas valve insures safe and efficient operation of a fuel-burning appliance by monitoring combustion air pressure and appropriately controlling the valve based upon this air pressure. An air pressure sensor is incorporated into a pressure proving valve housing itself thus providing integrated solution for the control of the combustion process. Consequently, when heat is called for, no fuel is provided to the combustion chamber unless appropriate combustion air pressure is sensed. Further, by monitoring the actual air pressure, additional control capability is provided. That is, a variable speed blower associated with the combustion apparatus can be controlled to provide very precise fuel to air mixtures.

Claims

1. A pressure proving valve for use in a fuel burning furnace, comprising:

a single housing integratable with a fuel burning heating system, the single housing comprising;

a controller section for enclosing a controller and connections thereto;

a valve mechanism section for enclosing a valve and associated valve controls;

a connection channel to permit connection and associated controls between the controller and the valve;

a fuel inlet for receiving combustion fuel;

a fuel outlet for connecting combustion fuel to a combustion chamber; and

a combustion air inlet;

a valve located within the valve mechanism section for controlling the flow of fuel from the fuel inlet to the fuel outlet in a predetermined manner;

a transducer mounted within the single housing and in communication with the combustion air inlet, the transducer further having an output for providing a signal indicative of the presence of combustion air within the combustion chamber, wherein the transducer is a pressure transducer for sensing the pressure of combustion air within the combustion chamber;

a controller mounted within the controller section, the controller comprising;

a pressure input attached to the transducer output;

an output attached to the valve for providing signals to the controller to control the operation of the valve to maintain an air to fuel ratio within the combustion chamber that is within a predetermined parameter; and

wherein when the air to fuel ratio can no longer be maintained within the predetermined parameters, the signal communicates with the valve to stop fuel flow, thereby fuel is not provided to the combustion chamber until a predetermined amount of combustion air is present inside the combustion chamber wherein the valve is re-opened.

2. The valve of claim 1 wherein the controller further has an input terminal for receiving signals from a thermostat, wherein the controller further provides signals to control the valve in a predetermined manner in response to both the thermostat signals and the pressure signals.

3. The valve of claim 1 wherein the transducer further comprises an airflow sensor for sensing the flow of combustion air at the combustion air inlet.

4. The valve of claim 3 wherein the airflow sensor is a microbridge airflow sensor.

5. The valve of claim 3 wherein the airflow sensor is a mass flow sensor.

6. The valve of claim 1 wherein the controller further controls the valve to provide variable amounts of fuel to the combustion chamber depending upon the amount of combustion air sensed by the transducer.

7. The valve of claim 1 wherein the controller includes a blower output for controlling the operation of a related variable speed blower at least when the air to fuel ratio approaches the predetermined parameters.

8. The valve of claim 7 wherein the amount of air provided by the variable speed blower is proportional to the amount of fuel in order to achieve a predetermined fuel to air ratio.

9. An integral pressure proving gas valve for use in a heating system, the pressure proving gas valve comprising a single housing having:

a valve system permitting and controlling the flow of gas between a valve input and a valve output;

a gas inlet channel in communication with the valve input;

a gas outlet channel in communication with the valve output;

a sensor for determining the presence of combustion airflow within a combustion chamber, wherein the sensor is a pressure transducer for sensing the pressure of combustion air within the combustion chamber; and

a controller having an input in communication with the sensor and having an output in communication with the valve system such that the controller is capable of adjusting the valve system to continuously maintain an air to fuel ratio within the combustion chamber that is within a predetermined parameter regardless of amount of air flow, wherein when the air to fuel ratio cannot be maintained within the predetermined parameters by the controller, the controller will signal the valve to stop gas flow and not allow gas to flow from the valve input until sufficient combustion air pressure is present in the combustion chamber, wherein the valve is re-opened.

10. The integral valve of claim 9 wherein the sensor is in communication with the combustion air at a combustion air inlet, thus allowing the sensor to determine if the combustion airflow is present.

11. The integral valve of claim 10 wherein the sensor is an airflow sensor for sensing the flow of combustion air at the combustion air inlet.

12. The integral valve of claim 11 wherein the airflow sensor is a microbridge airflow sensor.

13. The integral valve of claim 11 wherein the airflow sensor is a mass flow sensor.

14. The integral valve of claim 9 wherein the controller further has a thermostat input for receiving signals from a thermostat, wherein the controller further provides signals to control the valve system in a predetermined manner in response to both the thermostat signals and the pressure signals.

15. The integral valve of claim 9 wherein the controller further controls the valve system to provide variable amounts of gas to the combustion chamber depending upon the amount of airflow sensed by the sensor.

16. A method of controlling the flow of fuel into a combustion chamber in order to maintain an air to fuel ratio that is within predetermined parameters, comprising:

providing a single housing integratable with a fuel burning heating system, the single housing comprising;

a controller section for enclosing a controller and connections thereto;

a valve system section for enclosing a valve system and associated controls;

a connection channel to permit connection between the controller and the valve system;

a fuel inlet for receiving combustion fuel;

a fuel outlet for connecting combustion fuel to a combustion chamber; and

a combustion air inlet;

a valve system located within the valve system section for controlling the flow of fuel from the fuel inlet to the fuel outlet in a predetermined manner;

a transducer mounted within the single housing and in communication with the combustion air inlet; and

a controller mounted within the controller section, the controller comprising a pressure input attached to the transducer output, an output attached to the valve for providing signals to the controller to control the operation of the valve;

receiving a signal from an integral combustion air sensor indicative of the amount of combustion air flowing through the combustion chamber;

determining if the air pressure is outside of a predetermined parameters; and

controlling the valve system to maintain the predetermined fuel to air ratio such that fuel and air are provided to the combustion chamber as necessary, wherein when the air to fuel ratio can no longer be maintained within the predetermined parameters, the controller signals the valve to stop gas flow such that fuel is not provided to the combustion chamber until a predetermined amount of combustion air is present inside the combustion chamber, wherein the valve is re-opened.