Patent Application
20210054998
The field of the disclosure relates generally to draft inducers in burner systems, and more particularly, to a system and method for burner ignition using sensorless constant mass flow draft inducers.
At least some known draft inducers move air across a gas burner and heat exchanger to provide adequate air mass flow for combustion. Draft inducers generally include a fan that rotates to draw combustion gasses from a collection manifold through the burner system. Generally, as the combustion gasses move through the burner and heat exchanger, a pressure drop is produced. To ensure adequate mass flow is present prior to starting the gas burner, heating appliances generally include a vacuum switch in or near the collection manifold, or other low pressure zone, and configured to actuate, due to the pressure drop, when mass flow through the burner system reaches a certain level for safe ignition of the burner. At least some known variable speed draft inducers also include another sensor in or near the collection manifold to verify the fan is producing a sufficient mass flow rate to actuate the vacuum switch and enable the burner to operate.
At least some known fan motors operate without airflow sensors using constant mass flow techniques, where the speed of the fan is determined based on a demanded mass flow rate and a known relationship between the fan speed and motor torque. Accordingly, fan motors using constant airflow techniques do not require a sensor to measure the airflow rate. Although mass flow rate is generally computed as a function of speed and torque, a mass flow rate produced by a given speed or a given torque depends on air temperature and barometric pressure, and ultimately the density of air in the burner system. According to Bernoulli's equation, before ignition, when air is cool and more-dense in the burner system, a fan turning to produce a given mass through the burner system will produce less pressure drop across the burner and heat exchanger than during normal operation, when the air is warmer and less dense. Consequently, a constant mass flow fan my not produce sufficient mass flow rate to actuate the vacuum switch where temperature and/or barometric pressure in the burner system fluctuate over a wide range. Further, under such circumstances, the burner system will not operate. For at least this reason, available sensorless constant mass flow fan motors generally are not used in draft inducers for burner systems. A sensorless motor capable of operating a fan to generate sufficient mass flow for ignition of a burner is therefore desirable.
In one aspect, a motor controller for a burner system is disclosed. The burner system includes a draft inducer fan configured to draw air through an airflow path through the burner system, and a vacuum switch. The motor controller includes an inverter and a processor. The inverter is configured to supply current to a motor configured to rotate the draft inducer fan. The processor is communicatively coupled to the inverter and is configured to receive a draft inducer control signal from a system controller. The processor is configured to instruct, in response to the draft inducer control signal, the inverter to supply a first current during a first period to the motor to rotate the draft inducer to produce a first mass flow through the burner system, the first mass flow having a first mass flow rate greater than a threshold mass flow rate to actuate the vacuum switch. The processor is configured to instruct the inverter to supply a second current, during a second period starting at an expiration of the first period, to the motor to rotate the draft inducer to produce a second mass flow through the burner system, the second mass flow having a target mass flow rate for normal operation of the burner.
In another aspect, a method of operating a motor for a draft inducer in a burner system is disclosed. The motor is coupled to a draft inducer fan configured to move air though an airflow path. The method includes receiving, by a motor controller configured to supply current to the motor, a draft inducer control signal from a system controller. The method includes supplying, in response to the draft inducer control signal, a first current, during a first period, to the motor to rotate the draft inducer fan to produce a first mass flow through the burner system, the first mass flow having a first mass flow rate greater than a threshold mass flow rate to actuate a vacuum switch for the burner system. The method includes supplying a second current, during a second period starting at an expiration of the first period, to the motor to rotate the draft inducer fan to produce a second mass flow through the burner system, the second mass flow having a target mass flow rate for normal operation of the burner.
In yet another aspect, a burner system is disclosed. The burner system includes a burner, a heat exchanger, a collection manifold, a motor coupled to and configured to turn a draft inducer fan, a vacuum switch, and a motor controller. The draft inducer fan is configured to draw an airflow through an airflow path from the collection manifold, across the burner, and through the heat exchanger. The vacuum switch is configured to actuate when a mass flow rate through the airflow path is sufficient to produce a vacuum above a vacuum threshold, thereby enabling operation of the burner. The motor controller is coupled to a system controller and the motor, and is configured to receive a draft inducer control signal from a system controller. The motor controller is configured to operate the motor, during a first period, to rotate the draft inducer to produce a first mass flow through the airflow path, the first mass flow having a first mass flow rate greater than the threshold mass flow rate. The motor controller is configured to operate the motor, during a second period starting at an expiration of the first period, to rotate the draft inducer fan to produce a second mass flow through the airflow path, the second mass flow having a target mass flow rate for normal operation of the burner.
Implementations of the system described herein produce a draft to start a burner using a constant mass flow fan motor. More specifically, when the ignition process is initiated, the fan motor operates at an elevated speed and mass flow to ensure sufficient airflow within the system for ignition of the burner and for actuation of the vacuum switch. After a predetermined period of time, the fan motor operates at a reduced speed and mass flow to produce a target airflow for normal operation of the burner. Additional features of the system are described in more detail herein.
As used herein, an element or step recited in the singular and preceded with the word “a” or “an” should be understood as not excluding plural elements or steps, unless such exclusion is explicitly recited. Furthermore, references to “example implementation” or “one implementation” of the present disclosure are not intended to be interpreted as excluding the existence of additional implementations that also incorporate the recited features.
Motor controller 112 includes a processor 118 and a memory device 120. In some alternative embodiments, processor 118 and/or memory device 120 are physically separate from and communicatively coupled to motor controller 112.
System controller 102 is communicatively coupled to burner 104, draft inducer assembly 106, and vacuum switch 108. System controller 102 generates a burner control signal 122 to control burner 104. Burner 104 ignites, maintains, or extinguishes a gas flame based on burner control signal 122. System controller 102 also generates a draft inducer control signal 124 to control draft inducer assembly 106. The efficiency with which burner 104 operates depends on the mass flow through airflow path 110. Burner 104 is configured to operate at a target mass flow rate where burner 104 can operate safely and at a desired efficiency. While burner 104 is operating, draft inducer assembly 106 moves air through airflow path 110 at the target mass flow rate.
Burner 104 requires a mass flow rate greater than a threshold mass flow rate in order to safely ignite. Vacuum switch 108 is generally disposed in the airflow path 110 or in some other low pressure zone. Vacuum switch 108 is configured to actuate only when a vacuum pressure, produced by the mass flow induced by fan 116, at vacuum switch 108 is greater than a threshold vacuum pressure. In response to actuating, vacuum switch 108 transmits a vacuum switch control signal 126 to system controller 102 indicating the mass flow in airflow path 110 is above a threshold mass flow rate for burner 104 to safely ignite and enabling system controller 102 to instruct burner 104 to ignite.
Motor controller 112 is communicatively coupled to motor 114 and is configured to provide a current 128 to motor 114. Motor controller 112 may include, for example, a rectifier, a direct current (DC) link or bus, and an inverter 130 for generating current 128. Motor controller 112 controls one or more of frequency, amplitude, phase, or duty cycle of current 128 based on instructions from processor 118. The speed at which motor 114 turns is a function of, for example, the frequency of current 128. Accordingly, motor controller 112 can vary the speed of motor 114 by varying the frequency, amplitude, phase, and/or duty cycle of current 128.
Motor 114 is mechanically coupled to fan 116 and configured to rotate fan 116 to produce an airflow through airflow path 110 and through burner system 100 by moving air from collection manifold 105, into draft inducer assembly 106 through an inlet 132, and out through an outlet 134. The airflow has, or is characterized by, a mass flow rate. The mass flow rate through airflow path 110 depends at least on the speed and torque output of motor 114 and fan 116, and the density of the combustion gasses.
Processor 118 is configured to instruct inverter 130 to supply current 128 to turn motor 114 at a target speed (or torque) based on a specific demanded, or target, mass flow rate for burner 104. The relationship between the mass flow rate through airflow path 110 and the speed (or torque output) of motor 114 can be expressed as a formula, or “curve,” defined as a function of speed, torque, and a target mass flow rate, which is sometimes referred to as a mass flow curve. The mass flow curve may be stored in memory device 120, for example, as a lookup table or an algorithm. Processor 118 determines a speed (or torque) at which to operate motor 114 for a given target mass flow based on the mass flow curve. Generally, as mass flow increases, torque output of motor 114 will increase. Accordingly, as combustion gasses are heated, the mass flow curve, or mass flow algorithm, will result in a higher speed (or torque) command for motor 114.
During the ignition process, motor controller 112 is configured to operate motor 114 at above the target mass flow rate in order to account for the reduced temperature and increased density of combustion gasses accumulating in collection manifold 105 prior to the ignition of burner 104. Because the combustion gasses in collection manifold 105 are cooler and more dense prior to ignition of burner 104, a given target mass flow of fan 116 produces a vacuum pressure at vacuum switch 108 that is less than the required vacuum pressure. Accordingly, processor 118 determines a first, or starting, mass flow rate a factor greater than the target mass flow rate, for example, a mass flow rate equal to the target mass flow rate multiplied by a factor of 1.2. Processor 118 then computes a starting speed (or torque) based on the determined starting mass flow rate using the mass flow curve and instructs inverter 130 to supply current 128 at a corresponding frequency, amplitude, phase, and duty cycle to motor 114 to operate at the starting speed (or torque). The actual mass flow rate across burner 104 and through heat exchanger 117 produced by operating motor 114 at the starting speed is a higher mass flow rate than an expected mass flow rate according to the mass flow curve, and is sufficient to actuate vacuum switch 108 and enable burner 104 to ignite when a flue temperature is low. After a period of time, 30 seconds for example, sufficient for the mass flow to actuate vacuum switch 108, ignite burner 104, and allow for heated combustion gases to reach fan 116, processor 118 then instructs motor controller 112 to supply a current 128 at a corresponding frequency, amplitude, phase, and duty cycle to operate motor 114 at the target mass rate through airflow path 110 and through burner system 100 for normal operation.
During a first period 508 between the initiation of the startup process at time zero and a time 510, motor controller 112 operates motor 114 at a first, or starting, speed sufficient to cause fan 116 to produce a first mass flow having a first mass flow rate. The first mass flow rate creates a vacuum pressure at vacuum switch 108 that is greater than a threshold vacuum pressure 512 to actuate vacuum switch 108.
During a second period 514 after time 510, motor controller 112 operates motor 114 at a second, or target, speed sufficient to cause fan 116 to induce a second mass flow having a second, or target, mass flow rate. The second mass flow rate is a target mass flow rate for operation of burner 104 and creates a vacuum pressure at vacuum switch 108 that is a corresponding target vacuum pressure 516.
The methods and systems described herein may be implemented using computer programming or engineering techniques including computer software, firmware, hardware or any combination or subset thereof, wherein the technical effect may include at least one of: (a) enabling a constant mass flow fan motor without an airflow sensor to be used in draft inducer for a burner system by initially operating a fan motor at an elevated speed to ensure sufficient airflow is within the system for ignition of the burner before operating the fan motor at a reduced speed to produce a target airflow for normal operation of the burner; (b) reducing the cost of a draft inducer for a burner system by eliminating the need for a fan motor of the draft inducer to have an airflow sensor; and (c) increasing the ease of manufacture and installation of a fan motor for a draft inducer for a burner system by eliminating the need for the fan motor to include an airflow sensor.
Some embodiments involve the use of one or more electronic processing or computing devices. As used herein, the terms “processor” and “computer” and related terms, e.g., “processing device,” “computing device,” and “controller” are not limited to just those integrated circuits referred to in the art as a computer, but broadly refers to a processor, a processing device, a controller, a general purpose central processing unit (CPU), a graphics processing unit (GPU), a microcontroller, a microcomputer, a programmable logic controller (PLC), a reduced instruction set computer (RISC) processor, a field programmable gate array (FPGA), a digital signal processing (DSP) device, an application specific integrated circuit (ASIC), and other programmable circuits or processing devices capable of executing the functions described herein, and these terms are used interchangeably herein. The above embodiments are examples only, and thus are not intended to limit in any way the definition or meaning of the terms processor, processing device, and related terms.
In the embodiments described herein, a memory device may include, but is not limited to, a non-transitory computer-readable medium, such as flash memory, a random access memory (RAM), read-only memory (ROM), erasable programmable read-only memory (EPROM), electrically erasable programmable read-only memory (EEPROM), and non-volatile RAM (NVRAM). As used herein, the term “non-transitory computer-readable media” is intended to be representative of any tangible, computer-readable media, including, without limitation, non-transitory computer storage devices, including, without limitation, volatile and non-volatile media, and removable and non-removable media such as a firmware, physical and virtual storage, CD-ROMs, DVDs, and any other digital source such as a network or the Internet, as well as yet to be developed digital means, with the sole exception being a transitory, propagating signal. Alternatively, a floppy disk, a compact disc-read only memory (CD-ROM), a magneto-optical disk (MOD), a digital versatile disc (DVD), or any other computer-based device implemented in any method or technology for short-term and long-term storage of information, such as, computer-readable instructions, data structures, program modules and sub-modules, or other data may also be used. Therefore, the methods described herein may be encoded as executable instructions, e.g., “software” and “firmware,” embodied in a non-transitory computer-readable medium. Further, as used herein, the terms “software” and “firmware” are interchangeable, and include any computer program stored in memory for execution by personal computers, workstations, clients and servers. Such instructions, when executed by a processor, cause the processor to perform at least a portion of the methods described herein.
Also, in the embodiments described herein, additional input channels may be, but are not limited to, computer peripherals associated with an operator interface such as a mouse and a keyboard. Alternatively, other computer peripherals may also be used that may include, for example, but not be limited to, a scanner. Furthermore, in the exemplary embodiment, additional output channels may include, but not be limited to, an operator interface monitor.
This written description uses examples to provide details on the disclosure, including the best mode, and also to enable any person skilled in the art to practice the disclosure, including making and using any devices or systems and performing any incorporated methods. The patentable scope of the disclosure is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal language of the claims.
