Information
-
Patent Grant
-
6766820
-
Patent Number
6,766,820
-
Date Filed
Thursday, August 9, 200123 years ago
-
Date Issued
Tuesday, July 27, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 137 65
- 137 66
- 431 54
- 431 75
- 431 76
- 431 77
- 431 78
- 431 80
- 431 111
- 431 83
- 431 84
- 251 12915
- 251 12916
- 251 368
- 251 113
- 251 68
- 251 69
- 251 72
- 251 73
- 251 74
-
International Classifications
- F16K3166
- F23N510
- F23N524
- F23Q908
-
Abstract
An improved pilot guard for controlling the flow of gaseous fuel to both a pilot burner and a main burner, the pilot valve comprising a housing having an inlet port, a pilot port and a main burner port; a bore extending through the housing between the pilot port and main burner port; a stop shuttle normally biased to a seated position in which it blocks communication between the inlet port and the bore; a reset shuttle positioned in the bore for lifting the stop shuttle from its seated position, the reset shuttle supporting a sealing member for sealing the inlet port from the main burner port but permitting communication between the inlet port and the pilot port when the reset shuttle lifts the stop shuttle from its seated position; a thermocouple capable of generating a current from the heat of the pilot burner; an electromagnet connected to the thermocouple and capable, when fully energized, of holding the stop shuttle from moving to its seated position; wherein the reset shuttle is movable by the force of gas pressure from the inlet port to a position in which the sealing member permits both the main burner port and the pilot port to communicate with the inlet port, and a potentiometer that is used to adjust the current that is applied to the electromagnet by the thermocouple.
Description
BACKGROUND OF THE INVENTION
The present invention relates to pilot valves and, more particularly, to a guard for a pilot valve.
Automatic safety systems employing guards for pilot valves, which are also called pilot guards, are often used to control burners within fired equipment, such as to heat crude oil that has been collected in vessels in order to facilitate the separation of water droplets from the crude, which may be deployed in remote locations and be unattended (the word “control” as used herein simply means on-off accessibility to the fuel supply, i.e., access to the fuel supply is permitted in the “on” position and is precluded in the “off” position; whether fuel is actually directed to the main burner is determined by another valve, responsive to its own thermostat, interposed between this burner and the pilot guard). Such systems for both the pilot and main burner are required to avoid accumulation within the fired equipment of raw fuel discharged by unlit burners in volumes sufficient to be an explosive hazard. Because the collection vessels may be remotely located, a source of electrical power is often unavailable, or if available, is not reliable. To avoid reliance on electrical power in a control means, prior art pilot guards have utilized materials, such as mercury, which expand greatly when heated. Such arrangements are not desirable because the materials are often toxic, are susceptible to leakage, and since they have a relatively large mass from which heat must be dissipated after the removal of heat, do not react rapidly to failure of the flame being sensed. Many of these prior art devices that did use a thermocouple provided no means for emergency shutdown or means for testing the operation of the safety system.
U.S. Pat. No. 6,065,484 (“484”) discloses a burner and pilot guard safety and control system that provides a pilot guard having a stop shuttle normally biased to a seated position to completely block communication with a source of natural gas under pressure and a reset shuttle movable to a reset or start up position in which it unseats the stop shuttle while simultaneously permitting communication of the pilot burner with the gas source and blocking communications with the main burner. A reset latch is arranged to hold the reset shuttle in its reset position until released. A thermocouple capable of producing a voltage output proportional to its temperature is heated by the flame of the pilot burner and is connected to an electromagnet. The electromagnet, when fully energized, holds the stop shuttle in its unseated position. When the reset latch is released, the reset shuttle is then moved by the force of the gas pressure to an operational position in which both the pilot and main burners are in communication with the gas source. A momentary contact switch is arranged, when depressed to its closed position, to short circuit the thermocouple. When the thermocouple is short circuited, the holding force of the electromagnet immediately deteriorates and the stop shuttle is instantly biased to its seated position blocking all communication with the gas source.
The pilot guard that is disclosed in 484 works well in many applications. However, in some applications, the heat generated by the pilot flame is not adequate to energize the electromagnet sufficiently to allow it to hold the pilot guard assembly open after the pilot flame is lit. Consequently, in these applications, both the pilot guard assembly and the main burner valve assembly within the pilot guard will never “latch in” and will shut down upon release of the reset shuttle in the event of inadequate heat generated by the pilot flame. This condition of insufficient pilot flame heat could have several causes, including low BTU gas, excessive amounts of secondary air through the fire tube, low pilot pressure, and improper thermocouple alignment. Additionally, a pilot flame that is too hot could increase the time needed to de-energize the electromagnet and consequently shut off the pilot and burner gas upon occurrence of a flame-out to dangerous levels.
Therefore, there is a need for a pilot guard that overcomes the deficiencies of the prior art in handling the problems posed by the variable levels of heat produced by pilot flames.
SUMMARY OF THE INVENTION
The present invention provides a pilot guard that is safer and more adaptable than prior art guards, and that has improved gas supply shut-off times in the event of a loss of pilot flame. The present invention can be adjusted in the field to accommodate a variety of levels of heat produced by pilot flames. In the preferred embodiment of the present invention described below, the adjustment is provided by a potentiometer.
DESCRIPTION OF THE DRAWINGS
The following description of the preferred embodiment may be understood better if reference is made to the appended drawing, in which:
FIG. 1
is an elevational cross section of a pilot guard for use in an automatic safety control system according to the present invention;
FIG. 2
is a top plan view of the guard shown in
FIG. 1
with portions thereof broken away for clarity;
FIG. 3
is a bottom plan view of the pilot guard shown in
FIG. 1
;
FIG. 4
is a top plan view of the pilot guard shown in
FIG. 1
, with the acorn nut removed from the potentiometer;
FIG. 5
is an enlarged view of the electromagnet housing and part of the thermocouple of the pilot guard shown in
FIG. 1
; and
FIG. 6
is a schematic diagram of the electrical components of the pilot guard shown in FIG.
1
.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring to
FIGS. 1 through 5
, there is shown a pilot guard indicated generally at
10
, having a body
12
, which for ease of manufacture and assembly is composed of an electromagnet housing
14
, an inlet disc
16
, an output disc
18
, and a bottom cover disc
20
all of which are joined together as a unitary structure by screws
22
, shown in
FIG. 2
, that extend through aligned holes in the electromagnet housing
14
and the inlet disc
16
to engage tapped holes in the output disc
18
, and by screws
24
, shown in
FIG. 3
, that extend through holes in the bottom cover disc
20
to engage the same tapped holes. An O-ring seal
26
positioned in a peripheral groove in the inlet disc
16
contacts the inner diameter of the electromagnet housing
14
to prevent the escape of gas between the housing
14
and the inlet disc
16
. Another O-ring seal
28
is positioned between the output disc
18
and the inlet disc
16
to prevent the escape of gas between the adjacent surfaces of the inlet and output discs
16
and
18
respectively. The inlet disc
16
is provided with an inlet port
30
which is arranged in a conventional manner to connect with a natural gas supply line
32
through an in-line filter
33
, which may be any of the commercially available types, such as a sintered bronze filter, for example, for removal of water and solid contaminates that could otherwise interfere with the proper operation of the pilot guard
10
. The inlet port
30
communicates with a central cavity
34
formed in the inlet disc
16
. A central longitudinal bore
36
in the outlet disc
18
communicates with the cavity
34
and with a pilot port
38
and a main burner port
40
. A stop shuttle
42
extends through and reciprocates in a central bore
44
in the inlet disc
16
. The diameter of central bore
44
is slightly larger than the diameter of shuttle
42
to ensure that pressure in central bore
44
is always equal to that in bore
45
defined by housing
14
. The lower end
46
of the shuttle
42
is frusto-conically shaped for engagement with a counterbore
48
to assure alignment of the longitudinal axis of the shuttle
42
with the bore
36
. An O-ring
49
carried in a groove in the shuttle
42
is engageable with the intersection of the counterbore
48
with the upper surface of the output disc
18
to block communication between the cavity
34
and the bore
36
. A compression spring
50
trapped between the inlet disc
16
and a collar
52
on the shuttle
42
urges the O-ring
49
into sealing engagement with the outlet disc
18
. As the O-ring
49
is deformed by the force of the spring, i.e., takes a permanent set, the lower end
46
will simply travel downward further, so the sealing capability of the O-ring
49
is retained.
A reset shuttle
54
is reciprocal in the bore
36
but with sufficient clearance to permit an adequate flow of gas therebetween to provide the fuel requirement of both the pilot and main burners. An O-ring seal
56
is carried between lands
58
and
60
formed on the reset shuttle
54
, which lands
58
and
60
engage and reciprocate in a counterbore
62
. The engagement of the lower land
60
with the upper surface of the bottom cover disc
20
limits the downward travel of the reset shuttle
54
, in which position the seal
56
is below the main burner port
40
permitting communication of the bore
36
with the port
40
. An extension
64
is formed on the reset shuttle
54
and extends through a bore in the bottom cover disc
20
, the lower end of which protrudes to function as a reset button
66
. Pushing upward on the reset button
66
first causes the O-ring
56
to isolate the burner port
40
and then the upper face of the shuttle
54
to engage the end
46
to push the stop shuttle
42
upward, against the bias of the spring
50
, disengaging the O-ring
49
from its seat. Communication between the inlet port
30
and the pilot port
38
is thereby established.
A groove
68
is formed in the extension
64
and is engageable by the inner end
70
of a latch pin
72
which is reciprocably retained in a radial bore
79
in the bottom cover disc
20
by a bushing
74
that is screwed into a threaded counterbore
78
in the disc
20
, and that bears against a collar
80
formed on latch pin
72
. A compression spring
76
is trapped between the bottom of the bore
79
and collar
80
and urges the pin
72
toward the right, as viewed in
FIG. 1
, so that the inner end of the latch pin
72
clears the extension
64
and the opposite end thereof protrudes beyond the bushing
74
to function as a latch button
82
. The inner end
70
of the latch pin
72
has a frustroconical shape with the largest diameter at the extreme end thereof A complementary shape is provided to the upper surface of the groove
68
so that the force of the compression spring
50
will retain the inner end
70
of the latch pin
72
within the groove
68
, when upward manual force on the reset button
66
is released before the release of inward manual force on the latch button
82
, to hold the reset shuttle
54
in the raised position previously described, i.e., with the inlet port
30
in communication with the pilot port
38
but with the main burner port
40
isolated from the inlet port
30
. Gas is thereby permitted to flow to the pilot but not to the main burner. Subsequently manually pushing the reset button
66
upward, without any force being applied to latch button
82
, will permit compression spring
76
to release the end
70
from the groove
68
. Upon release of such upward manual force on the reset button
66
, the downward force of the gas pressure acting on the reset shuttle
54
will cause shuttle
54
to move downward until the land
60
engages the upper surface of bottom disc cover
20
. In this position of the reset shuttle
54
, the bore
36
is in communication with both ports
38
and
40
. Gas would thereafter be supplied to both ports
38
and
40
if, and only if, the stop shuttle
42
did not move downward under the force of the compression spring
50
so that the O-ring seal
49
precludes communication between the inlet port
30
and the bore
36
.
The stop shuttle
42
will move downward only if a horseshoe electromagnet
90
is not energized. A disc
92
, which is made of a magnetic material, is attached to the top of the stop shuttle
42
by a screw
94
extending through washer
96
. When electromagnet
90
is energized, the disc
92
will be held by magnetic attraction thereagainst, holding the stop shuttle
42
in its upward, open position against the bias of the spring
50
. The electromagnet
90
is energized by a thermocouple
100
, which is held by a suitable bracket
102
in a position to be heated by the flame of the pilot burner (not shown). Referring to
FIGS. 2 and 5
, lead wires
110
and
112
from the thermocouple
100
extend through a flexible sleeve
104
and terminate in a connector
106
which mates with a complementary socket
108
secured to the top of the electromagnet housing
14
. Wire
110
from thermocouple
100
connects with wire
116
leading from one terminal of socket
108
, and is connected to one terminal of the windings
119
of electromagnet
90
. Wire
112
is connected to wire
120
leading from the remaining terminal of socket
108
, and is connected to one terminal of a potentiometer
130
, which is mounted in any suitable fashion to the top of housing
14
. Potentiometer
130
can be a 100 ohm,
20
turn potentiometer manufactured by Spectrol, 4501 Greystone Drive, Ontario, Calif. 91761 as part no. 043P101 (and available from Mouser Electronics, Inc., 1000 North Main Street, Mansfield, Tex. 75063, 800-346-6873, as part no. 594-43P101). The resistance of potentiometer is decreased by turning it in the counterclockwise direction and increased by turning it in the clockwise direction. Wire
118
from the remaining terminal of windings
119
of electromagnet
90
is connected to the second terminal (or wiper) of potentiometer
130
, thus completing the series connection of the electromagnet
90
, potentiometer
130
and thermocouple
100
.
FIG. 6
shows this arrangement schematically. Electromagnet
90
, potentiometer
130
, and connectors
116
,
118
and
120
are potted within housing
14
as shown in FIG.
5
.
When thermocouple
100
is heated by the flame of the pilot burner, it will generate a voltage across wires
110
and
112
. Potentiometer
130
is adjusted to allow enough current to pass through windings
119
to cause electromagnet
90
to hold stop shuttle
42
in its upper position, in which natural gas is provided to both main burner port
40
and pilot burner port
38
. Referring to
FIG. 4
, potentiometer
130
is adjusted in well-known fashion by unthreading acorn nut
137
from post
133
of potentiometer
130
and inserting the blade of a screwdriver into slot
131
defined by post
133
of potentiometer
130
, and rotating the screwdriver to rotate post
133
about its longitudinal axis. If the resistance of potentiometer
130
is set too high, the current through windings
119
will be reduced to a level that is insufficient to allow electromagnet
90
to produce sufficient magnetic force to hold mating disk
92
against the opposing force of compression spring
50
in its upper position. Thus, O-ring
49
will prevent the flow of gas to both ports
38
and
40
, and neither the pilot burner nor the main burner will receive gas. Also, main burner port
40
also will not receive gas if the pilot flame is extinguished, the thermocouple
100
is not positioned properly in the pilot flame, or thermocouple
100
is defective. In all these cases, thermocouple
100
will not produce any significant voltage to the circuit shown in
FIG. 6
, and gas can never be supplied to main burner port
40
.
It has been discovered that using sintered metal oxide ferrite for the core of the horseshoe electromagnet
90
and sintered phosphorous iron (available, for example, as product number PSP-45 from Sintered Parts, LLC, of Tulsa Oklahoma) for the disc
92
will produce a magnetic force sufficient to hold the stop shuttle
42
against the bias of the spring
50
even at the low voltage and current output of a conventional thermocouple. A thermocouple producing an output voltage of 600 to 750 millivolts and a current of 100 milliamps has been found to reliably hold the stop shuttle
42
against a spring force of two pounds.
While the pull-in force, i.e., the magnetic force attracting the disc
92
toward the magnet
90
when an air gap exists between them, with the described arrangement is small, the holding force, i.e., the magnetic force generated when these two elements are in contact with each other, has been found to be quite large. The reason is that, when in contact, the disc
92
completes a magnetic circuit between the ends of the horseshoe magnet
90
, efficiently transferring the magnetic flux therebetween. Holding force, rather than pull-in force, is important since the disc
92
will be moved into contact with the ends of the electromagnet
90
by the manual upward movement of the reset button
66
to permit release of the latch pin
72
. The groove
68
is positioned so that when the end
70
of the latch pin
72
is in engagement therewith a small air gap exists between the disc
92
and the ends of the electromagnet
90
. Subsequent manual upward movement of the reset button
66
, which is necessary to release the latch pin
72
, will close this gap.
The pilot guard
10
with the thermocouple
100
properly positioned by attachment of the bracket
102
to be heated by the flame of a pilot burner, is placed in operation by initially introducing an ignition source adjacent the pilot burner. The reset button
66
is then depressed, i.e., manually moved upwardly, while simultaneously depressing the latch button
82
, i.e., manually urging the latch button
82
inward. When the operator feels the inner end
70
move into the groove
68
, the reset button
66
is released, while pressure on the latch pin is, at least momentarily, maintained. The engagement of the tapered end
70
with the upper surface of the groove
68
will retain the latch pin
72
in the groove
68
holding the reset shuttle
54
in an elevated position in which the stop shuttle
42
is unseated and only the pilot port
38
is provided with gas. The force of the gas pressure acting on the reset shuttle
54
and the force of the spring
50
will retain the end
70
within the groove. Once the thermocouple
100
is heated, the potentiometer
130
is adjusted such that the current supplied to electromagnet
90
is just above the latch-in current. Upon setting the potentiometer
130
, the reset button
66
is depressed again, with no force being applied to latch button
82
. The spring
76
will cause the latch pin to move outward extracting the end
70
from the groove
68
and allowing gas pressure to move the reset shuttle
54
downwardly connecting both the pilot port
38
and the main burner port
40
to be supplied with gas. Of course, this assumes the thermocouple
100
has produced sufficient voltage to energize the electromagnet
90
in order for magnetic force to hold the stop shuttle
42
in its unseated position. If the pilot flame has failed, or if the thermocouple is defective or improperly positioned, the spring
50
will immediately return the stop shuttle
42
to its seated position blocking all communication with the gas source. While the pull in, or latch in, and drop out currents for the guard will depend on the configuration of the guard and are readily ascertainable for those of ordinary skill in the art, latch in currents of 65 to 75 milliamps, and drop out currents of 40 to 45 milliamps are typical for common configurations.
A typical method of operating follows:
Clear the area of combustibles;
Close shut-off valves in the main burner line and pilot line, and wait for gas to vent from the system;
Decrease the effective resistance of potentiometer
130
by turning potentiometer
130
20 turns counterclockwise;
Stand to the side of the burner and light a torch; insert the torch into the fire tube next to the pilot burner;
Open the pilot shut off valve;
Depress reset button
66
until it and reset shuttle
54
latches to allow gas to flow to the pilot burner and ignite the pilot;
When thermocouple
100
comes up to temperature (usually 60 to 90 seconds after ignition), fully depress and then slowly release reset button
66
, at which point pilot guard
10
should latch in the open position, allowing gas to flow to both the pilot port
38
and main burner port
40
;
Increase the resistance of potentiometer
130
by (a) slowly turning potentiometer
130
clockwise until pilot guard
10
drops out (disc
92
becomes disengaged from magnet
90
), (b) turning potentiometer
130
counterclockwise 4 turns, (c) relight the pilot by following the preceding steps, except that the potentiometer is not turned 20 turns in the counterclockwise direction;
If unable to latch pilot guard
10
in the open position, turn potentiometer
130
1 more turn in the counterclockwise direction, and repeat this procedure until pilot guard
10
remains latched open, and then turn potentiometer
130
2 turns in the clockwise direction;
This procedure should result in a 12 to 20 second shut down time after loss of pilot flame. To obtain a shorter drop out time, slowly turn potentiometer
130
clockwise to find the maximum number of turns that can be made before pilot guard
10
drops out;
Slowly open the manual shut-off valve to the main burner line to light the main burner;
Test for proper operation by extinguishing the pilot flame and, with the manual shut-off valve to the pilot open, observing that gas pressure to the pilot and main burner control is shut off within 45 seconds; to shorten the drop out time, slowly turn potentiometer
130
further in the counterclockwise direction; use the foregoing procedure to relight the burner.
While a preferred embodiment of the present invention has been illustrated and described herein, it is to be understood that various changes may be made therein without departing from the spirit of the invention, as defined by the scope of the appended claims.
Claims
- 1. A pilot guard for controlling the flow of gaseous fuel to both a pilot burner and a main burner comprising:a housing having an inlet port, a pilot port, and a main burner port; a bore extending through said housing between said pilot port and said main burner port; a stop shuttle normally biased to a seated position in which it blocks communication between said inlet port and said bore and prevents the flow of gaseous fuel to both said pilot port and said main burner port; a reset shuttle positioned in said bore for lifting said stop shuttle from its seated position, said reset shuttle supporting a sealing member for sealing the inlet port from the main burner port but permitting communication between said inlet port and said pilot port when said reset shuttle lifts said stop shuttle from its seated position; a thermocouple capable of generating a voltage from the heat of the pilot burner; an electromagnet connected to said thermocouple and capable, when energized by a predetermined current produced by said thermocouple, of holding said stop shuttle from moving to its seated position; and a current adjustor connected between said thermocouple and said electromagnet by which the current applied to said electromagnet by said thermocouple can be adjusted; said reset shuttle being movable by the force of gas pressure from said inlet port to a position in which said sealing member permits both said main burner port and said pilot port to communicate with said inlet port: whereby, said stop shuttle moves to said seated position when said thermocouple does not produce at least said predetermined current to said electromagnet.
- 2. The invention according to claim 1, and further comprising a disc secured to said stop shuttle and made of a material capable of being magnetically held by said electromagnet when energized.
- 3. The invention according to claim 2, wherein said material is sintered phosphorous iron.
- 4. The invention according to claim 3 wherein said electromagnet has a horseshoe-shaped core made of a ferrite material.
- 5. The invention according to claim 4 wherein said ferrite material is a sintered metal oxide ferrite.
- 6. The invention according to claim 2 wherein said material is sintered phosphorous iron.
- 7. The invention according to claim 1 and further comprising a latch pin for engagement with said reset shuttle to hold said reset shuttle in its unseated position.
- 8. The invention according to claim 7 and further comprising a spring for normally biasing said latch pin to an outward position out of engagement with said reset shuttle.
- 9. The invention according to claim 1 wherein said latch pin has a tapered inner end and said reset shuttle has a groove with a surface complementary to said end for holding the latch pin against the bias of said spring.
- 10. The invention according to claim 9, wherein said disc is spaced from said electromagnet when said latch pin is in engagement with said reset shuttle and subsequent upward movement of said reset shuttle brings said disc into contact with said electromagnet while simultaneously permitting said latch pin to disengage from said reset shuttle.
- 11. The invention according to claim 1, wherein said current adjustor is a potentiometer.
- 12. A pilot guard for controlling the flow of gaseous fuel to both a pilot burner and a main burner comprising:an inlet port in communication with each of a pilot port and a main burner port; a stop adapted to move between a closed position in which it blocks communication between said inlet port and said pilot and main burner ports and prevents the flow of gaseous fuel to both said pilot port and said main burner port, and an open position in which it does not block communication between said inlet port and said pilot and main burner ports; an electromagnetic device configured to hold said stop in said open position when a current of at least a predetermined level is applied to said electromagnetic device; a thermal transducer mounted to produce a current in response to a flame produced by the pilot burner, said thermal transducer being electrically connected to said electromagnetic device to apply said current to said electromagnetic device; and a current adjustor operably connected between said electromagnetic device and said thermal transducer to permit adjustment of the current applied by said thermal transducer to said electromagnetic device; and whereby, said stop moves to said seated position when said thermocouple does not produce a current of at least said predetermined level to said electromagnet.
- 13. The pilot guard recited by claim 12 wherein said electromagnetic device is an electromagnet.
- 14. The pilot guard recited by claim 13 wherein said thermal transducer is a thermocouple.
- 15. The pilot guard recited by claim 14 wherein said current adjustor is a potentiometer.
US Referenced Citations (10)