[0001] In heating systems comprising a combustion air blower and a fuel valve for providing
fuel to a burner, it is generally desired to provide fuel to the burner only when
proper conditions exist for the flame and to maintain an optimum fuel-to-air ratio
when the burner is in operation. Prior art approaches to these problems are relatively
complex. The furnace control system disclosed in US-A 4 251 025 (DE-A 30 26 190) requires
a pressure regulator valve comprising a regulating chamber as well as an operator
valve actuated by a suitable electro-magnetic actuator. Furthermore, a separate pressure
switch is required to check for a blocked stack, and this pressure switch is incorporated
with a specialized control system which shuts off the fuel flow if pressure conditions
are not correct.
[0002] It is the main object of the present invention to simplify over prior art systems
and to achieve one or more of three separate and distinct features: (1) fuel should
be allowed to flow only upon sensing a predetermined minimum air flow; (2) the fuel
flow may be modulated so that a fixed fuel-to-air ratio is maintained; and (3) fuel
supply to the burner is shut off completely if air flow substantially ceases, such
as in the case of a blocked stack or malfunctioning combustion blower. These objects
are achieved by the invention as characterized in claim 1. Preferred improvements
and embodiments are described in the subclaims. Through the present invention, substantially
simplified controls may be used; for example, no separate regulator chamber and no
electro-magnetic actuator is required within the fuel control. Embodiments of the
invention will be described with reference to the attached drawings.
Figures 1 and 5 schematically illustrate heating systems incorporating the present
invention;
Figures 2, 3 and 6 show alternate embodiments of the fuel control valve and its operating
means;
Figures 4 and 7 illustrate typical performance of the embodiments shown in Figures
2 and 6, respectively.
[0003] US-A 4 251 025 describes how a furnace control system functions generally, so that
several details need not to be explained again in the present specification.
[0004] Figure 1 illustrates an induced draft furnace incorporating a fuel control in accordance
with two alternate embodiments 100 and 100A of the valves as shown in Fig. 2 and 3.
Although the present invention is not limited to induced draft furnaces, it will be
explained here in connection with such a heating system. Other applications of the
present invention include forced draft systems and power burners.
[0005] After operation of the Figure 1 furnace system is explained, fuel controls 100 and
100A will be explained. An alternate fuel control valve 100B shown in Fig. 6 is compatible
with the furnace system illustrated in Figure 5 will then be explained.
[0006] The heating system shown in Figure 1 comprises a combustion chamber 20 which has
a burner 40 located near its bottom and which is substantially enclosed by exterior
walls 36. Fuel, which in the preferred embodiment is a gas such as natural gas or
liquified petroleum, is fed to burner 40 by a gas outlet 24 near the mouth of burner
40. Air enters burner 40 and combustion chamber 20 at air inlets 22 located near the
tip of gas outlet 24 and the mouth of burner 40. Burner 40 is ignited by a pilot burner,
not shown.
[0007] Alternately, the system could include a direct ignition system (i.e., sparking the
main burner directly) or an intermittent pilot flame.
[0008] Surrounding combustion chamber 20 is a heat exchanger 30 with its interior boundary
being formed by exterior walls 36 of combustion chamber 20, the exterior boundary
of heat exchanger 30 being formed by walls 35.
[0009] Thus, two separate fluid paths are formed. The combustion chamber path leads from
gas outlet 24 and air inlets 22 through burner 40 and out of a flue 25. The heat exchanger
path follows the exterior walls 36 of combustion chamber 20; the fluid to be heated
enters below burner 40 and proceeds along a vertical portion of the enclosed area
between walls 35 and the exterior burner wall 36 to exit above combustion chamber
20. While in the embodiment shown air is the fluid to be heated, other fluids such
as water may be used with minor design changes.
[0010] Movement of air into and through heat exchanger 30 is provided by a fan 34 driven
by an electric motor. Cold air is pulled into heat exchanger 30 at a cold air return
duct 32 and passes through an air filter 33 before it enters fan 34. Fan 34 drives
the air into heat exchanger 30 through an opening in its bottom wall. Heated air passes
out of heat exchanger 30 through a warm air duct 37 which extends from an opening
in a top wall in heat exchanger 30.
[0011] With the exception of flue 25 and combustion air inlets 22, combustion chamber 20
is enclosed and substantially air tight. Accordingly, the only exit for combustion
material is provided by flue 25. In order to induce air to enter combustion chamber
at bottom air inlets 22 and to induce combusted gases to exit from combustion chamber
20 and flow out of flue 25 in exhaust stack or vent 80, an induced draft blower 60
is used. This induced draft blower is powered by an electric motor 61 and is located
in line with flue 25 and exhaust stack or vent 80. Blower 60 may be single or multiple
speed, depending upon the type of control system with which it is to be used.
[0012] A fluid, preferably natural gas or liquified petroleum, is provided to burner 40
at gas outlet 24 which is fed by an outlet pipe 104 of a modulating fuel valve such
as valve 100. Gas from a supply line at line pressure enters gas valve 100 at a gas
inlet pipe 101. Gas regulated to the desired output pressure flows out of gas valve
100 through outlet pipe 104. The detailed structure and operation of gas valve 100
is described later. Although gas valve 100 is the preferred valve embodiment, an alternate
embodiment to gas valve 100 will also be described.
[0013] By way of further describing operation of the heating system illustrated in Figure
1, fan 34 is electrically connected via wires 18 to a fan limit control switch 56
which is driven by a temperature sensitive element 57 such as a bimetal thermostat.
This temperature sensitive element 57 causes fan 34 to be switched on when the air
temperature in heat exchanger 30 rises above a predetermined temperature (fan start
set point) and to be switched off when the temperature of the air in heat exchanger
30 falls below a predetermined temperature (fan stop set point). To minimize condensation
in heat exchanger 30, the fan start set point is chosen substantially at or somewhat
above the dew point. One suitable temperature sensitive switch for this purpose is
the L4064 fan and limit switch manufactured by Honeywell Inc. of Minneapolis, Minnesota.
[0014] Because one purpose of fan limit control switch 56 is to delay fan start up until
heat exchanger 30 contains air at or above the dew point, a time delay mechanism may
be substituted for temperature sensitive element 57. This mechanism may be activated
at the same time as blower motor 61, but it would delay fan start up for a predetermined
period sufficient to let heat exchanger 30 reach the dew point temperature.
[0015] Gas inlet pipe 101 may comprise a manually-actuated on-off valve (not shown) between
inlet 101 and the supply of fuel. Such a manually-actuated valve may be used to manually
activate or deactivate the fuel controls In such a case, opening of the manually actuated
valve would be a prerequisite to any flow of gas from outlet pipe 104. Other "redundant"
closure points, e.g. a safety valve may also be employed in order to provide additional
conditions which must be met before valve 100 permits gas to flow to burner 40. However,
such manually-actuated valves or other redundant closure points are not necessary
to the present invention.
[0016] Fuel controls 100 and 100A discussed below operate in connection with venturi nozzle
106 on one side of combustion blower 60. An aperture in venturi nozzle 106 is connected
directly to pressure chambers 118 and 118A in valves 100 and 100A, respectively by
a pressure conduit 108. The preferred location for venturi nozzle 106 is in exhaust
stack 80 downstream of combustion air blower 60. However, venturi nozzle 106 may be
located on either side of combustion air blower 60 in any suitable portion of the
air flow. Note also that, while venturi 105 is shown occupying the entire cross-sectional
area of exhaust stack 80, a smaller venturi, not occupying the entire cross-sectional
area of exhaust stack 80 or other housing, would also be compatible with the present
invention.
[0017] Fuel controls 100 and 100A are actuated (turned on) and deactiviated (turned off)
by pressure signals received directly from venturi nozzle 106. In addition, as will
be further explained below, fuel control 100 is constructed so that its output is
modulated based on the pressure communicated to control chamber 118 through conduit
108 from nozzle 106. Similarly, as explained in connection with Fig. 5 and 6 fuel
control 100B provides a modulated output based on the pressure communicated to control
chamber 118B from the region upstream of orifice plate 107. Accordingly, with fuel
controls 100A and 100B, the firing rate of the furnace or other appliance will be
determined by the combustion air flow rate, which is determined primarily by the speed
of combustion blower 60. Thus, proof of combustion air as well as blocked stack detection
is inherent in systems incorporating these controls.
[0018] For example, in the case of fuel controls 100 and 100A operating in connection with
venturi nozzle 106 as illustrated in Figure 1, a totally blocked stack will result
in positive pressure from venturi nozzle 106 being communicated through conduit 108
to valve 100 or 100A which will then turn off gas flow to outlet 104. A partially
blocked stack will decrease the flow through venturi nozzle 106 resulting in a lower
feedback signal through pressure conduit 108 and, in the case of fuel control 100,
less gas flow through valve 100. Accordingly, appropriate clean combustion will be
maintained.
[0019] The system is inherently safe and requiresno flow o pressure sensor to prove combustion
air or to detect blocked stacks. Further, the valves are much simpler than valves
previously available.
[0020] Figure 2 illustrates fuel control 100, which is an alternate preferred embodiment
of the present invention. Fuel control 100 comprises an inlet chamber 110 having an
inlet 101 for receiving a supply of gas. The control also comprises an outlet chamber
112 having an outlet 104 for providing a supply of gas. The inlet and outlet chambers
are connected by valve opening 114. Fuel control 100 also comprises a valve 116 operatively
associated with opening 114, valve 116 having a closed position for preventing the
flow of gas through opening 114 and an open position for permitting the flow of gas
through the opening.
[0021] As illustrated in Figure 2, fuel control 100 also comprises a control chamber 118
bounded in part by diaphragm means 120 mechanically coupled to valve 116 for moving
the valve in response to movement of diaphragm means 120. In the embodiment shown,
diaphragm means 120 comprises a first diaphragm 122 and a second diaphragm 124, the
two diaphragms being shown mechanically coupled by a pin 126 located approximately
central to the diaphragms. Diaphragm 122, which also partially encloses outlet chamber
112, is mechanically coupled to valve 116 and to pin 126 by a pin 128. In the Figure
2 embodiment of fuel control 100, an optional bias means or spring 130 is illustrated
for keeping valve 116 in its closed position whenever the pressure in control chamber
118 is above a predetermined negative pressure level and for permitting valve 116
to move to its open position(s) whenever the pressure in control chamber 118 is below
the predetermined negative pressure level. As an alternate example to bias spring
130, diaphragm means 120 could employ a configuration which inherently provides the
bias provided by spring 130. Pressure conduit 108 provides means for directly connecting
control chamber 118 to venturi nozzle 106 so that valve 116 moves in response to the
pressure signal from venturi nozzle 106.
[0022] In the embodiment illustrated in Figure 2, control chamber 118 is bounded by an upper
diaphragm 122 which is smaller than a lower diaphragm 124. As previously indicated,
these two diaphragms form diaphragm means 120 mechanically coupled to valve 116 for
moving valve 116 in response to movement of diaphragms 122 and 124. For the Figure
2 embodiment, a negative pressure below a predetermined level introduced into control
chamber 118 through pressure conduit 108 from venturi nozzle 106 causes valve 116
to move in an upward direction, thus permitting the flow of gas through orifice 114
from inlet chamber 110 to outlet chamber 112. If the negative pressure in chamber
118 is or goes above the predetermined negative pressure, valve 116 will remain or
will go closed.
[0023] In the embodiment shown, lower diaphragm 124 is protected by housing 132 comprising
air leak orifice 134 for permitting valve means 116 to freely move in response to
the pressure changes within chamber means 118.
[0024] Although fuel control 100 may be configured as merely an on-off valve (so that the
fuel control does not modulate the output gas pressure) the preferred embodiment of
the present control modulates the pressure available at outlet 104 as a function of
the negative pressure in venturi nozzle 106. Figure 4 is a typical plot of the output
pressure at outlet 104 versus the negative pressure in venturi nozzle 106 for a valve
of the embodiment shown in Figure 2. Note that, as the negative pressure in venturi
nozzle 106 and, accordingly, in control chamber 118 goes below a predetermined negative
pressure, the fuel pressure at outlet 104 increases.
[0025] The Figure 2 embodiment provides this modulation by the combined effect of the outlet
gas pressure acting against one side of diaphragm 122 and the effect of the pressure
in control chamber 118 acting on the other side of diaphragm 122 as well as exerting
a force on diaphragm 124. As negative pressure in chamber 118 decrease (i.e., as the
absolute value of this pressure increases), the forces on diaphragms 122 and 124 tend
to open valve 116 (i.e., to push it upward), resulting in increased pressure in outlet
chamber 112 and at outlet 104; the resulting increased outlet pressure in chamber
112 results in a downward force on diaphragm 122, tending to close valve 116 (i.e.,
to push it downward). The equilibrium position of valve 116 and, accordingly, the
pressure at outlet 104 is determined by this system balance, which changes as the
pressure in chamber 118 changes. Thus, as can be seen from Figure 4, the gas pressures
provided at outlet 104 vary in relation to the pressure in venturi nozzle 106 and,
accordingly, in relation to the pressures within control chamber 118. As a secondary
effect, the input gas pressure at inlet 101 and in inlet chamber 110 affects this
equilibrium position as an offset; see, for example, the three plots in Figure 4 which
represent typical data for input pressures at inlet 101 of 4, 7 and 12 inches of water
respectively.
[0026] Although Figure 2 illustrates the preferred embodiment of fuel control 100, other
embodiments within the scope of the present invention are also possible. For example,
as illustrated in Figure 3, diaphragm 122 could be replaced with a non-flexible member
122A having a pin 126A moveably passing through the member; pin 126A is connected
to valve 116 and to diaphragm 124 and is sealed with a pressure seal 136 at the point
it passes through member 122A. Valve 116 moves in response to movement of diaphragm
124 which in turn moves pin 126A up and down through sealed hole 136 in member 124A.
As with the embodiment shown in Figure 2, diaphragm 124 in the Figure 3 embodiment
moves in response to the negative pressure in the control chamber above it; i.e.,
in response to the negative pressure in chamber 118A, the pressure in chamber 118A
being communicated to the chamber through pressure conduit 108 from venturi nozzle
106.
[0027] An alternate fuel control 100B illustrated in Figure 6 and compatible with the furnace
system illustrated in Figure 5 will now be explained.
[0028] The furnace system of Figure 5 is identical to that of Figure 1 except that stack
80 comprises an orifice plate 107 rather than a venturi 105 and venturi nozzle 106.
Orifice plate 107 comprises an orifice which causes a positive pressure build up upstream
of orifice plate 107 during proper operating conditions of the furnace. Pressure conduit
108 connects directly to fuel control 100B and into stack 80 upstream of orifice plate
107.
[0029] Fuel control 100B is very similar to fuel controls 100 and 100A except that, with
fuel control 100B, pressures above a predetermined positive level cause valve 116
to open. Other than that, the 100B fuel control illustrated in Figure 6 operates substantially
like the fuel control illustrated in Figure 2, and the Figure 6 embodiment modulates
the output pressure at outlet 104 in a manner similar to the modulation which occurs
in the Figure 2 embodiment. As can be seen from the typical data plotted in Figure
7, as the positive pressure in stack 80 orifice plate 107 and, accordingly, in control
chamber 118B goes above a predetermined positive pressure the fuel pressure at outlet
104 increases.
[0030] The Figure 6 embodiment provides this modulation by the combined effect of the outlet
gas pressure acting against one side of diaphragm 122 and the effect of the pressure
in control chamber 118B acting on the other side of diaphragm 122. As the positive
pressure in chamber 118B increases, the forces on diaphragm 122 tend to open valve
116 (i.e., to push it upward), resulting in increased pressure in outlet chamber 112
and at outlet 104; the resulting increased outlet pressure in chamber l12 results
in a downward force on diaphragm 122, tending to close valve 116 (i.e., to move it
downward). The equilibrium position of valve 116 and, accordingly, the pressure at
outlet 104 is determined by this system balance, which changes as the pressure in
chamber 118B changes. Thus, as can be seen from Figure 7 the gas pressures provided
at outlet 104 vary in relation to the pressure below orifice plate 107 and, accordingly,
in relation to the pressures within control chamber 118B. As a secondary effect, the
input gas pressure at inlet 101 and in inlet chamber 110 affects this equilibrium
position as an offset; see for example, the three plots in Figure 7 which represent
typical data for input pressures at inlet 101 of 5, 7 and 10 inches of water respectively.
[0031] Fuel controls in accordance with the present invention typically also comprise a
bias adjustable from the exterior of the fuel control which, for example, may be used
to adjust for manufacturing tolerances. For the embodiments illustrated in Figures
2 and 3, such a bias may comprise a spring (not shown) coupled between the center
of diaphragm 124 and an adjustment screw (not shown) passing through housing 132.
The spring and screw combination serves to adjust the bias or predetermined pressure
at which the fuel control will permit gas to flow through valve opening 114. In the
case of the embodiment illustrated in Figure 6, the adjustable bias is typically placed
between diaphragm 122 and a screw (not shown) passing through housing 132B, a pressure
seal around the screw typically being employed in such a configuration. Means for
biasing the diaphragm of a pressure regulating valve are shown e.g. in US-A 41 82
488 and US-A 44 06 400.
[0032] Fig. 4 and 7 illustrate the relation of the fuel outlet pressure with respect to
the pressure sensed in the stack which depends on the flow rate of the flue gases.
Since a pressure ratio is shown the diagrams could be labeled in mm water column or
in bar or in every other pressure value instead of inches water column without changing
the curves as such. The scale factor is of no importance.
1. A heating system comprising
a) a fuel valve (100;114,116) for supplying fuel to a burner (40);
b) pressure controlled operating means (120) for controlling said valve (100;114,116)
between an open and a closed position with said operating means forming a wall portion
of a control chamber (118,118A;118B);
c) a blower (60) for supplying combustion air to said burner (40);
d) pressure sensing means (105,106;107) at one side of said blower (60) for controlling
said operating means (120);
characterized in that
the controlled chamber (118;118A;118B) is directly connected (108) to a pressure sensing
port provided at said side of the combustion air blower (60).
2. A system according to claim 1, characterized in that
e) the pressure sensing port is located in a venturi nozzle (106) provided between
the blower (60) and an exhaust stack (80) connected to a combustion chamber (20) wherein
said burner (40) is provided;
f) an increasing negative pressure in said control chamber (118,118A) tends to move
via the operating means (124) the valve (116) towards its open position.
3. A system according to claim 1, characterized in that
g) the pressure sensing port is located upstream of an orifice plate (107) provided
between the blower (60) and an exhaust stack (80) connected to a combustion chamber
(20) wherein said burner (40) is provided;
h) an increasing positive pressure in said control chamber (118b) tends to move via
the operating means (122) the valve (116) towards its open position.
4. A system according to claim 2 or 3, characterized in that the pressure controlled
operating means (120) comprises at least one diaphragm (124,122) and the valve (116)
is spring biased (130) in closing direction.
5. A system according to claims 2 and 4, characterized in that the control chamber
(118) is provided between two diaphragms (122,124) with one diaphragm (122) carrying
a valve stem (114) which has an extension (126) projecting through the control chamber
into engagement with the other diaphragm (124).
6. A system according to one of claims 2, 4 or 5, characterized in that operating
means (120) move the valve (116) so that, when the pressure in the control chamber
(118) is lower than a predetermined negative pressure, gas will be provided to the
outlet (104) at a pressure related to the pressure in the control chamber (118,118A)
and so that, when the pressure in the control chamber is above the predetermined negative
pressure, no gas will flow through the opening (114) to the outlet.
7. A system according to claim 3, characterized in that the operating means (120)
move the valve (116) so that, when the pressure in the control chamber (118B) is higher
than a predetermined positive pressure, gas will be provided to the outlet (104),
at a pressure related to the pressure in the control chamber and so that, when the
pressure in the control chamber (118B) is lower than the predetermined positive pressure,
no gas will flow through the opening (114) to the outlet (104).
8. A system according to one of the preceding claims, characterized in that the combustion
air blower (60) comprises means for variably controlling the volume delivery rate
of the blower.