Information
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Patent Grant
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6561791
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Patent Number
6,561,791
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Date Filed
Friday, March 9, 200123 years ago
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Date Issued
Tuesday, May 13, 200321 years ago
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Inventors
-
Original Assignees
-
Examiners
Agents
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CPC
-
US Classifications
Field of Search
US
- 431 90
- 431 12
- 431 89
- 431 76
- 431 80
- 431 20
- 236 15 BD
- 236 15 BB
- 236 15 E
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International Classifications
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Abstract
The invention relates to a regulating system for a gas burner. Regulating systems for gas burners are used for guiding a gas flow and a combustion air flow to the burner. The gas flow can be regulated depending on combustion air pressure. Pressure is measured in known regulating devices with the aid of a membrane, that is pneumatically. The pneumatic pressure measurement limits the scope of application of known regulating devices. In the invention regulating device, a sensor (16) is arranged between a first line (10) guiding a gas flow and a second line (12) guiding the combustion air flow, an electric or electronic signal (19) being generated by the sensor that is used to regulate the gas valve (11).
Description
BACKGROUND OF THE INVENTION
This invention relates to a regulating device for gas burners. Regulating devices for gas burners serve to provide a gas-air mixture, which supplies a gas stream and a combustion air stream to a burner. According to various embodiments described herein, the gas stream is capable of being set as a function of the combustion air pressure by means of a gas valve.
Regulating devices for gas burners of the above type are well known from the prior art. In one regulating device, the pressure is determined with the aid of a diaphragm, or pneumatically. See EP 0 390 964 A1. The gas stream is regulated by means of the gas valve as a function of this pressure measurement. However, the one disadvantage with this pneumatic method is that it restricts the scope of use of known regulating devices. In such devices the hysteresis properties of the diaphragm and the forces acting between the diaphragm and the gas valve restrict the working range and therefore the scope of use. Furthermore, the interaction between the low actuating forces and the operating tolerances of the diaphragm as a result of disturbing influences, such as temperature fluctuations or the like, cause a restriction in the scope of use of known regulating devices.
There are other regulating devices for gas burners found in the prior are with similar disadvantages. See DE 24 27 819 A1 and DE 43 17 981 A1.
SUMMARY OF INVENTION
The present invention attempts to provide a regulating device for gas burners, which avoids the disadvantages of known devices, thus providing a greater scope of use. Various embodiments described herein solve the scope of use problem by means of a regulating device for gas burners.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1
is a first embodiment of a regulating device for a gas burner system, and
FIG. 2
is a second embodiment of a regulating device for a gas burner system.
DETAILED DESCRIPTION OF THE INVENTION
The present invention relates to regulating devices for gas burners. A gas/air mixture is to be supplied to a burner(not illustrated). In
FIG. 1
, a first line
10
supplies a gas stream to a gas burner. The gas stream in the first line
10
flows from a valve
11
to a gas nozzle
15
.
A second line
12
supplies a combustion air stream to the gas burner. The combustion air in the second line
12
flows from a blower
13
. The rotational speed of the blower
13
determines the combustion air pressure, and therefore the combustion air stream. The second line
12
contains a throttle point
14
upstream of the gas nozzle
15
. The gas stream in the first line
10
exits from the nozzle
15
into the second line
12
. Therefore, a gas/air mixture exists downstream of the gas nozzle
15
in the direction of the combustion air stream.
The embodiment illustrated by
FIG. 1
provides a combined 1:1 gas/air mixture regulation. Thus, if the combustion air pressure increases 1 millibar (mbar), the gas pressure will likewise increase by 1 mbar. A sensor
16
located between the first line
10
and the second line
12
provides the combined 1:1 gas/air mixture regulation. The sensor
16
functions as a differential pressure sensor, of the flowmeter or anemometer type.
The sensor
16
is connected to the first line
10
by means of a first measuring point
17
. The sensor
16
is connected to the second line
12
by means of a second measuring point
18
. The first measuring point
17
is positioned upstream of the gas nozzle
15
. The second measuring point
18
is positioned upstream of the throttle point
14
.
To accomplish the combined 1:1-gas/air regulation presented in the
FIG. 1
embodiment, the gas pressure must equal the combustion air pressure. Thus, when the sensor
16
is a flowmeter or anemometer, the flow through the sensor
16
will be zero. If, for example, the combustion air pressure decreases in relation to the gas pressure, the sensor
16
experiences a throughflow from the first line
10
in the direction of the second line
12
. By contrast, if the combustion air pressure increases in relation to the gas pressure, the sensor
16
experiences a throughflow from the second line
12
in the direction of the first line
10
. Accordingly, based on the throughflow quantity and direction, the sensor
16
can determine the pressure ratios between the combustion air pressure and the gas pressure. The sensor
16
generates, as a function of these pressure ratios, an electric or electronic signal
19
that adjusts the gas valve
11
. According to
FIG. 1
, the signal
19
is supplied to a control or regulating unit
20
which generates a regulating signal
21
for an actuating drive
22
of the gas valve
11
.
Consequently, the regulating device of
FIG. 1
, regulates the gas stream using the gas valve
11
to achieve combined 1:1-gas/air regulation. When the sensor
16
detects a pressure differential of zero between the combustion air pressure and gas pressure, the signal
19
corresponds to a pressure difference of zero and the gas valve
11
operates unchanged. When the sensor
16
detects a combustion air pressure higher than the gas pressure, the signal
19
will activate the gas valve
11
so that the gas stream is increased. This is accomplished by the regulating unit
20
generating a regulating signal
21
for the actuating drive
22
of the gas valve
11
, so that the signal
19
corresponds to a pressure difference of zero. By contrast, when the sensor
16
detects a combustion air pressure lower than the gas pressure, the signal
19
activates the gas valve
11
so that the gas stream is decreased.
The gas valve
11
may be designed in a variety of ways. For example, the actuating drive
22
of the gas valve
11
is controlled or regulated so the gas valve
11
switches between the on/off or open/shut states. If the combustion air pressure is higher than the gas pressure, a regulating signal
21
is generated, causing either the actuating drive
22
to open or the gas valve
11
to activate. Likewise, if the combustion air pressure is lower than the gas pressure, the actuating drive
22
will close or deactivate the gas valve
11
based on the regulating signal
21
. A resulting oscillating signal provides information on the proper operation of the regulating system, thus it and can function as a safety signal. With the oscillating sensor signal present, a safety valve (not illustrated) preceding the gas valve
11
can be activated or opened.
Alternatively, it is also possible to activate the gas valve
11
to assume any desired opening positions between the on/off or open/shut states. The regulating device of
FIG. 1
can be used for air quantity measurement when the gas valve
11
is closed. This is because the sensor
16
has the second measuring point
18
on the second line
12
, upstream of the throttle point
14
in the flow direction of the combustion air. Furthermore, the sensor
16
has the first measuring point
16
on the first line
10
downstream of the throttle point
14
and the gas valve
11
is closed. If the gas valve
11
is closed, the pressure difference across the throttle point
14
can be determined by the sensor
16
, and an air quantity can be measured.
The air quantity measurement can be used to set the parameter range of the blower
13
as a function of a configuration of the combustion air supply and smoke gas discharge. The air quantity measurement also can be used to monitor and set a minimum combustion air supply, which is required to reliably start the gas burner.
FIG. 2
illustrates another embodiment of a regulating device for a gas burner system that provides combined 1:N gas/air regulation. This is accomplished by using a different transmission ratio in the
FIG. 2
embodiment than in the
FIG. 1
embodiment. In
FIG. 2
, a coupling line
23
is positioned between a first line
10
supplying the gas stream and a second line
12
supplying the combustion air stream. In the coupling line
23
there is a first contraction
24
and a second contraction
25
. The first contraction
24
and the second contraction
25
are throttle points.
No specific position of the first contraction
24
and the second contraction
25
within the coupling line
23
in relation to the first line
10
and the second line
12
is required. However, the flow resistance of the first line
10
and the second line
12
must be noticeably lower than the flow resistance of the first contraction
24
and the second contraction
25
.
In
FIG. 2
, the coupling line
23
is connected to the second line
12
downstream of the throttle point
14
in the direction of flow of the combustion air. The coupling line
23
is connected to the first line
10
upstream of the gas nozzle
15
in the direction of flow of the gas.
In the
FIG. 2
embodiment, like in the
FIG. 1
embodiment, a sensor
16
is positioned between the first line
10
and the second line
12
. However, in
FIG. 2
, a first measuring point
17
is positioned in the coupling line
23
between the first contraction
24
and the second contraction
25
. A second measuring point
18
is positioned in the second line
12
upstream of the throttle point
14
.
In
FIG. 2
, a regulating unit
20
generates a regulating signal
21
for an actuating drive
22
of the gas valve
11
, so that a signal
19
from the sensor
16
corresponds to a pressure difference of zero. However, because of the arrangement of the coupling line
23
with the first contraction
24
and the second contraction
25
, combined 1:N-gas/air regulation can be implemented. Thus, an increase in the combustion air pressure of 1 mbar will increase the gas pressure by N mbar.
Consequently, in
FIG. 2
, the gas pressure is intensified in relation to the combustion air pressure. The degree of intensification is determined by the first contraction
24
and the second contraction
25
.
Furthermore, either the first contraction
24
or the second contraction
25
may be designed to be variable or modifiable. In that case, it is possible, by modifying or adjusting either the first contraction
24
or the second contraction
25
, to vary the transmission ratio between the combustion air stream and the gas stream, or the intensification.
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List of reference symbols
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|
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10
First Line
|
11
Gas valve
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12
Second Line
|
13
Blower
|
14
Throttle point
|
15
Gas nozzle
|
16
Sensor
|
17
First Measuring point
|
18
Second Measuring point
|
19
Signal
|
20
Regulating unit
|
21
Regulating signal
|
22
Actuating drive
|
23
Coupling line
|
24
First Contraction
|
25
Second Contraction
|
|
Claims
- 1. A regulating device for a gas burner system, the gas burner system including a first line through which a gas stream flows from a gas valve to a gas nozzle, and a second line through which a combustion air stream flows from a blower, the gas nozzle located downstream from the blower and a throttle point in the second line, the regulating device comprising, in combination:a first measuring point on the first line, the first measuring point positioned upstream from the gas nozzle; a second measuring point on the second line, the second measuring point positioned upstream of the throttle point; a sensor coupled to the first measuring point and the second measuring point, the sensor providing a signal indicating a pressure differential; and a control unit operative to provide a regulating signal to an actuating drive for controlling the gas valve.
- 2. The regulating device of claim 1, wherein the actuating drive associated with the gas valve receives the regulating signal generated as a function of the signal indicating the pressure differential.
- 3. The regulating device of claim 1, wherein an oscillating signal results from the regulating signal and can be monitored to ensure proper operation of the regulating device.
- 4. A regulating device for a gas burner system, the gas burner system including a first line through which a gas stream flows from a gas valve to a gas nozzle, and a second line through which a combustion air stream flows from a blower, the gas nozzle located downstream from the blower and a throttle point in the second line, the regulating device comprising, in combination:a coupling line connected to the second line downstream of the throttle point and the first line upstream of the gas nozzle, the coupling line containing a first contraction and a second contraction, the first contraction controlling the amount of gas being supplied to the coupling line, the second contraction controlling the amount of air being supplied to the coupling line; a first measuring point on the coupling line, the first measuring point positioned between the first contraction and the second contraction; a second measuring point on the second line, the second measuring point positioned upstream of the throttle point; a sensor coupled to the first measuring point and the second measuring point, the sensor providing a signal indicating a pressure differential; and a control unit operative to provide a regulating signal to an actuating drive for controlling the gas valve.
- 5. The regulating device of claim 4, wherein at least one of the first contraction and the second contraction is adjustable.
- 6. The regulating device of claim 4, wherein a transmission ratio between the gas stream and the combustion air stream is modified by an adjustable first contraction or an adjustable second contraction.
- 7. The regulating device of claim 4, wherein the regulating signal produces an oscillating signal that can be monitored to ensure proper operation of the regulating system.
- 8. A method for regulating a gas-air mixture to a gas burner system, the gas burner system including a first line through which a gas stream flows from a gas valve to a gas nozzle, and a second line through which a combustion air stream flows from a blower, the gas nozzle located downstream from the blower and a throttle point in the second line, comprising in combination:providing a signal indicating a differential pressure between the first line and the second line; and regulating an actuating drive based on the signal, thereby controlling the gas valve.
- 9. The method of claim 8, wherein the differential pressure is measured between a first measuring point positioned upstream from the gas nozzle and a second measuring point positioned upstream from the throttle point.
- 10. The method of claim 8, wherein regulating the actuating drive includes receiving the signal indicating the pressure differential and providing a regulating signal to the actuating drive.
- 11. The method of claim 8, wherein monitoring the regulating signal includes monitoring a resulting oscillating signal to ensure proper operation of the regulating system.
- 12. A method for regulating a gas-air mixture to a gas burner system, the gas burner system including a first line through which a gas stream flows from a gas valve to a gas nozzle and a second line through which a combustion air stream flows from a blower, the gas nozzle located downstream from the blower and a throttle point in the second line, the system further including a coupling line connected to the second line downstream of the throttle point and the first line upstream of the gas nozzle, the coupling line containing a first contraction and a second contraction, the method comprising in combination:providing a signal indicating a differential pressure between the second line and the coupling line; and regulating an actuating drive based on the signal, thereby controlling the gas valve.
- 13. The method of claim 12, wherein the differential pressure is measured between a first measuring point positioned between the first contraction and the second contraction and a second measuring point positioned upstream of the throttle point.
- 14. The method of claim 12, wherein modifying a transmission ratio between the gas stream and the combustion air stream includes adjusting either the first or second contraction.
- 15. The method of claim 12, wherein monitoring the regulating signal includes monitoring a resulting oscillating signal to ensure proper operation of the regulating system.
Priority Claims (1)
Number |
Date |
Country |
Kind |
198 24 521 |
Jun 1998 |
DE |
|
PCT Information
Filing Document |
Filing Date |
Country |
Kind |
PCT/EP99/03670 |
|
WO |
00 |
Publishing Document |
Publishing Date |
Country |
Kind |
WO99/63272 |
12/9/1999 |
WO |
A |
US Referenced Citations (3)
Foreign Referenced Citations (2)
Number |
Date |
Country |
58-224226 |
Dec 1983 |
JP |
60-122818 |
Jul 1985 |
JP |