US2642128A - Pressure responsive combustion control apparatus - Google Patents
Pressure responsive combustion control apparatus Download PDFInfo
- Publication number
- US2642128A US2642128A US696735A US69673546A US2642128A US 2642128 A US2642128 A US 2642128A US 696735 A US696735 A US 696735A US 69673546 A US69673546 A US 69673546A US 2642128 A US2642128 A US 2642128A
- Authority
- US
- United States
- Prior art keywords
- valve
- burner
- pressure
- fuel
- switch
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N1/00—Regulating fuel supply
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23Q—IGNITION; EXTINGUISHING-DEVICES
- F23Q9/00—Pilot flame igniters
- F23Q9/08—Pilot flame igniters with interlock with main fuel supply
- F23Q9/12—Pilot flame igniters with interlock with main fuel supply to permit the supply to the main burner in dependence upon existence of pilot flame
Definitions
- This invention relates to combustion control and is particularly applicable to the burning of fluid fuel under automatic control
- An object ofthe invention is to provide an improved combustion control which will be extremely safe in operation.
- Another object of the invention is to provide an improved combustion control which will accurately supply fuel in accordance with the heat requirements of the apparatus.
- Another object of the invention is to provide an improved combustion control which will insure automatic ignition of fuel.
- Another object of the invention is to provide an improved combustion control whichwill prevent the supply ofundesirable quantit es of fuel under any of a number'of adverse fuel burning conditions.
- Another object of the invention is to provide. an improved combustion control-which will be extremely reliable. a 7
- Another object of the invention is to provide an improved combustion control which will be composed'of few and simple parts.
- Another object of the invention is to provide an improved combustion control which will require a minimum amount of servicing.
- Another object of the invention is to provide an improved combustion control which will be compact.
- Another object of the invention is to provide an improved combustion control which may be easily andeconomically manufactured.
- Another object of the invention is to provide an improved combustion control which will be extremely positive in its operation.
- Figures-2, 3, 4 and 5 are fragmentary sectional viewsto an enlarged scale taken on the line 7 Claims. (01.158-7) clarity of illustration, and showing the parts in;
- Figure 6 is a view similar to Figure 1 showing' a second embodiment of the invention
- E Figure 7 is a view similar to a portion of Figure 1 showing a third embodiment intended for the burning of fuel at atmospheric pressures.
- I have shown a combustion system in which fuel is burned within a sealed combustion chamber I, fuel and air being supplied to this chamber by the control apparatus to be described.
- the products of combustion are exhausted from the combustion chamber by a pump or blower 2. driven by a motor 3, so that the pressure within the combustion chamber is maintained at all timesbelow that of the atmosphere.
- Fuel is supplied from any source of fuel fluid under a pressure greater than atmospheric, such as the pipe or conduit 4, which, for the purpose of my present description, may be considered as connected to an ordinary city gas line.
- the fuel passes'through a gas pressure regulator at 5, which may be of any well known.
- the topof the valve bodyis provided with.
- valve stem l9 having its upper end, head or armature 20 in alignment with the poles of the core [8, while the lowerend of the stem is provided with valve 2
- a spring 23 is interposed between the valve. at 22 and-the casing .16. I It will be understood that the casing I8 is fixed to and seals the top of the valve body.
- the bottom of the valve body has a depend-' 'ing boss 24 which is bored for the reception of a plunger 25 which has an upper end of reduced diameter shown as carrying a valve head 21 provided with packing 28.
- the valve stem 26 is slidable through the valve head 21 and is provided with a flange or collar 29 adjacent its upper end which limits the upward motion of the valve relative the stem. 7
- betweenthe upper end of the larger diametric part of plunger 25 and the lower side of the valve head.
- the lower end of the plunger is provided with a roller 32 which travels on a cam 33, which will be described more fully hereinafter.
- valve 9 From the valve 9 the fuel passes through a pipe or conduit 34 to an orifice plate 35 secured at the end of pipe 34 as by an elbow or other fitting 36 and constituting the main burner orifice of the apparatus.
- a pipe or conduit 31 extends to the main burner 38 within the combustion chamber.
- a branch 39 connected to conduit 3] is provided with a manually adjustable regulating valve 40 which controls the ad-, mission of air to support combustion, this air being drawn in through the valve by the subatmospheric pressure within the pipe 31.
- a casing Connected to pipe 34, as by a nipple 4
- the diaphragm is provided with a plate 46 having a depending stem or pin 47 arranged to actuate a normally open switch 48.
- Tube l4 ends at an electrically operated valve 49, from which a tube 50 passes to a pilot burner 5
- an igniting spark gap Arranged adjacent the pilot burner is an igniting spark gap, consisting 'of an electrode 52 insulated from but passing through the combustion chamber wall, as by means of insulating bushings 52a, and a grounded electrode 53.
- thermocouple 54 Also positioned adjacent the pilot burner and the main burner, where it will be subjected to flame from either or both, is a thermocouple 54.
- a pipe 55 communicates with the interior of the. combustion chamber and is connected by fittings, such as a T 56 and nipple 57, to a casing consisting of a cover 58 and a bottom 59 between the edges of which is clamped the edge of a diaphragm 6
- the diaphragm 60 has a pressure plate 6
- a compression sprin 64 Passing upwardly from the pressure plate within the T 55 is a compression sprin 64, the tension of which may be adjusted by a screw plug E5 threaded in the upper branch of the T.
- a motor 65 Connected to rotate the cam 33 is a motor 65, and positioned adjacent the cam is aswitch 81, having an arm 68, which may be moved to operate the switch by a projecting cam 69 formed on the side of cam 33.
- a relay comprising a coil 10, an armature H and contacts 12 is positioned adjacent the casing l6 and valve 9 and motor 55, so that these parts, together with switch 67, may all conveniently be enclosed in a box or cover 13.
- Covers or boxes 14 and [5 also conveniently may be provided for enclosing and protecting switches 48 and 63, respectively.
- a transformer is shown at 6 to furnish current at suitable potential for the spark gap.
- a thermostat which is positioned in the room or other space which it is desired to maintain at a uniform temperature.
- power is supplied by any suitable source such as a central power house generator 18 through line 19 and 80.
- Line 19 includes motor 3 and thermostat 1! and terminates at switch 63.
- Line 88 has four branches, one of which 89a terminates at transformer 16, another 801) at switch 48, a third 890 at relay coil 70 and a fourth 8003 at electro-magnetic switch 49.
- extends to switch 61, and from switch 6? a conductor 82 extends to transformer 16.
- is a conductor 85a which connects with the other end of coil Til of the relay, and which has a branch Blb connected to the other side of valve 49.
- c connects with motor 66, While the opposite side of the motor is connected by a conductor 83 to switch 48.
- Switch 48 is normally open, and is closed only when the vacuum within pipe 34 is sufii: cient to raise diaphragm 44.
- I Switch 63' is normally closed, and is opened only in the event of an extremely high vacuum which causes the diaphragm SEi-to overcome the pressure of spring 64.
- conductors 84 and 85 pass, respectively, to electrode 52 and to the ground.
- the cam 33 is in the position shown in Figures 1 and 2, where the roller 32 is at its lowermost position with valve 21 open and valve 2
- switch 48 closes and current cannow pass through this switch between co'nductors 83 and 891), thus supplyin current to motor 66 which starts to rotate and to move cam 33.
- This cam rotates in a clockwise direction, as seen in Figures 2 to .5, so that the roller for a short period is free of the cam while the latter passes through the sector marked 33a, and thereafter climbs upon the sector 33b to the position shown in Figure 3 where both valves 2
- the succeeding sector of the cam is a dwell, indicated at 330, which may be for a substantial period, such as about a quarter of a minute, permitting the blower to completely purge the combustion chamber of any unburned fuel.
- sector 33d of the cam again raises plunger 25, as shown in Figure 4, so that valve 2
- This. permits gas to flow from the intake side .of valve body ID to port 12, and thence through tubes l4 and I 5 to the pilot burn-
- cam lug 69 engages switch arm 88 and as this'lug extends axially a sufiicient distance to actuate switch 6! this engagement closes the switch 61, permitting current to bow through 82 to the primary of transformer 76, and thus inducing a high tension current in conductors 84 and 85 producing a spark between electrodes 52 and 53.
- Pressure in pipe 34 opens switch 48 preventing the motor 66 from causing the parts to go through their cycle until a proper vacuum has been produced.
- valve 2! Immediately upon exhaustion of the gas burning at the main burner, de-energization of coil I! permits valve 2! to snap shut, cutting off all fuel to the main burner as well as to the pilot burner.
- the apparatus will re-cycle until ignition takes place.
- valve I49 As shown in this figure, deenergization thereof shuts off the entire gas supply, not merely that to the pilot burner.
- the apparatus is shown as adapted to burning fuel at atmospheric pressure.
- the pipe 234 terminates at the frustro-conical end 240 of the pipe 231 leading to the main burner, the two pipes forming an inspirator or injector-like structure for drawing in air to support combustion at the burner.
- the branch MI is provided with an apertured plate 235, through which the extension communicates with the interior of the casing con-. sisting of halves 242 and 243.
- a diaphragm 244 having a rod or pin 24'! arranged, when the diaphragm is raised, to contact the arm of switch 248, this switch being normally open and closed only when engaged by the shank 241.
- Combustion control apparatus comprising a combustion chamber, a burner in the chamber,
- valve control means operabl associated with the valve and controlled by the pressure in the line between the valve and restricting member.
- Combustion control apparatus comprising a combustion chamber, a burner in the chamber, a fuel supply line leading to the burner and including a valve, a restricting member in said supply line between the valve and burner, actuating means connected to said valve, control means for said valve connected to and responsive to the pressure in the chamber, and retaining means for said valve controlled by the existence or absence of a flame at the burner.
- Combustion control apparatus comprising a combustion chamber, a burner therein, a fuel supply line leading to the burner and including a valve, a restricting memberin said supply line between the valve and burner, actuating means for said valve connected to and responsive to the pressure in the chamber, and retaining means for said actuating means controlled by the existence or absence of a flame at the burner, and operating means for said valve controlled by the pressure in the conduit between the valve and the restricting member.
- a combustion apparatus comprising a combustion chamber, gas exhausting means connected with said chamber, a main burner and a nected to said valve, and a pressure operated control connected to said actuating means controlled by the pressure in said conduit between the-valve and the combustion chamber.
- Combustion control apparatus comprising a combustion chamber, a burner therein, a source of fuel under pressure, a conduit leading from said source of fuel to said burner, a valve in the conduit, a restricting member in the conduit between the valve and the burner, an electric motor, power transmission means connected thereto and arranged to open said valve, resilient valve closing means, electro-magnetic valve retaining means arranged to hold the valve open, a pressure responsive control connected to and actuated by the pressure in the conduit between the valve and the restricting member and controlling said valve retaining means, a pressure responsive controlling means connected to and responsive to the pressure in the combustion chamber controlling the motor, and a thermocouple adjacent the burner controlling the valve retaining means.
- Combustion control apparatus comprising a combustion chamber, a burner therein, a source of fuel under pressure, a conduit leading from said source of fuel to said burner, a valve in the conduit, 3, restricting member in the conduit between the valve and the burner, an electric motor, power transmission thereto and arranged to open said valve, resilient valve closing means, electro-inagnetic valve retaining means arranged to hold the valve open, a pressure responsive control connected to and actuated by the pressure in the conduit between the valve and the restricting member and controlling said valve retaining means, a pressure responsive controlling means connected to and responsive to the pressure in the combustion chamber controlling the motor, and a thermocouple adjacent the burner controlling the valve retaining means, a second conduit from the fuel supply conduit terminating in a pilot burner admeans connected 8 jacent the first mentioned burner, and a valve in saidsecond mentioned conduit actuated by said motor.
- a combustion apparatus comprising a combustion chamber, gas exhausting means connected with said chamber, a main burner and a pilot burner within the chamber adjacent each other, a source of fluid fuel under pressure, conduit means leading from said source of fuel to said main burner and having successively interposed therein a valve and a conduit restricting member and an air inlet, the valve being closest the source of fuel and the air inlet closest the main burner, electrical actuating means connected to said valve, and a pressure operated con trol connected to said actuating means controlled by thepressure in said conduit between the valve and the conduit restricting member.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Feeding And Controlling Fuel (AREA)
Description
W. L. RIEHL.
June 16, 1953 4 Sheet sSheet 1 Filed Sept. 13, 1946 W. L. RIEHL.
June 16, 1953 PRESSURE RESPONSIVE COMBUSTION CONTROL APPARATUS Filed Sept. 13; 1946 4 Sheets-Sheet 2 June 16, 1953 w, L. RIEHL 2,642,128
PRESSURE RESPONSIVE COMBUSTION CONTROL APPARATUS Filed Sept. 13, 1946 v 4 Sheets-Sheet 3 18 17 L E 16 Z0 June 16, 1953 W. L. RIEHL PRESSURE RESPONSIVE COMBUSTION CONTROL APPARATUS Filed Sept. 15, 1946 4 Sheets-Sheet 4 Patented June 16, 1953' v PRESSURE RESPONSIVE COMBUSTION CONTROL APPARATUS William L. Rich], Rome, N. Y., assignor to Union Fork & Hoe Company poration of Ohio Columbus, Ohio, a cor- 7 Application September 13, 1946, Serial No. 696,735
v This invention relates to combustion control and is particularly applicable to the burning of fluid fuel under automatic control,
An object ofthe invention is to provide an improved combustion control which will be extremely safe in operation.
Another object of the invention is to provide an improved combustion control which will accurately supply fuel in accordance with the heat requirements of the apparatus.
Another object of the invention is to provide an improved combustion control which will insure automatic ignition of fuel.
Another object of the invention is to provide an improved combustion control whichwill prevent the supply ofundesirable quantit es of fuel under any of a number'of adverse fuel burning conditions.
Another object of the invention is to provide. an improved combustion control-which will be extremely reliable. a 7
- Another object of the invention is to provide an improved combustion control which will be composed'of few and simple parts.
Another object of the invention is to provide an improved combustion control which will require a minimum amount of servicing.
Another object of the invention is to provide an improved combustion control which will be compact.
Another object of the invention is to provide an improved combustion control which may be easily andeconomically manufactured.
Another object of the invention is to provide an improved combustion control which will be extremely positive in its operation.
Other objec'ts'will hereinafter appear.
The invention will be better understood from the description of several practical embodiments thereof, illustrated in the accompanying drawings, in which: j V
Figural is a somewhat diagrammatic view, partly in elevation andpartly in section, of one form of control intended for the burning of fluid, and preferably gaseous, fuels at subatmospheric pressures;
Figures-2, 3, 4 and 5 are fragmentary sectional viewsto an enlarged scale taken on the line 7 Claims. (01.158-7) clarity of illustration, and showing the parts in;
positions they occupy during various phases of the cycle of operation of the apparatus;
Figure 6 is a view similar to Figure 1 showing' a second embodiment of the invention; and E Figure 7 is a view similar to a portion of Figure 1 showing a third embodiment intended for the burning of fuel at atmospheric pressures.
Referring ,flrst to the embodiment, namely, that of Figures 1 to 5, I have shown a combustion system in which fuel is burned within a sealed combustion chamber I, fuel and air being supplied to this chamber by the control apparatus to be described. The products of combustion are exhausted from the combustion chamber by a pump or blower 2. driven by a motor 3, so that the pressure within the combustion chamber is maintained at all timesbelow that of the atmosphere.
Fuel is supplied from any source of fuel fluid under a pressure greater than atmospheric, such as the pipe or conduit 4, which, for the purpose of my present description, may be considered as connected to an ordinary city gas line.
The fuel passes'through a gas pressure regulator at 5, which may be of any well known.
upper and lower sides and having a perforation.
l2 extending to the exterior of the valve, beyond which it is provided with a fitting [3 connecting.
it to a pipe'or tube I 4.
The topof the valve bodyis provided with.
an enlarged boss 1 5 into which is-received the lower end of a casing I6 carrying an-eleotro-,
'magnet I! provided with a U-shaped core I 8. Through the bottom of the casing [6 extends a valve stem l9 having its upper end, head or armature 20 in alignment with the poles of the core [8, while the lowerend of the stem is provided with valve 2| carrying packing 22.
A spring 23 is interposed between the valve. at 22 and-the casing .16. I It will be understood that the casing I8 is fixed to and seals the top of the valve body.
against the passage of fuel therethrough.
, The bottom of the valve body has a depend-' 'ing boss 24 which is bored for the reception of a plunger 25 which has an upper end of reduced diameter shown as carrying a valve head 21 provided with packing 28. The valve stem 26 is slidable through the valve head 21 and is provided with a flange or collar 29 adjacent its upper end which limits the upward motion of the valve relative the stem. 7
Normally holding the valve head against the flange 29 is a spring 3| betweenthe upper end of the larger diametric part of plunger 25 and the lower side of the valve head.
The lower end of the plunger is provided with a roller 32 which travels on a cam 33, which will be described more fully hereinafter.
From the valve 9 the fuel passes through a pipe or conduit 34 to an orifice plate 35 secured at the end of pipe 34 as by an elbow or other fitting 36 and constituting the main burner orifice of the apparatus.
From the fitting 35 a pipe or conduit 31 extends to the main burner 38 within the combustion chamber. A branch 39 connected to conduit 3] is provided with a manually adjustable regulating valve 40 which controls the ad-, mission of air to support combustion, this air being drawn in through the valve by the subatmospheric pressure within the pipe 31.
Connected to pipe 34, as by a nipple 4|, is a casing consisting of a top 42 and bottom 43 between which is clamped a diaphragm 44., the two parts of the casing being secured together in any desired manner, as by bolts 45.
The diaphragm is provided with a plate 46 having a depending stem or pin 47 arranged to actuate a normally open switch 48.
Tube l4 ends at an electrically operated valve 49, from which a tube 50 passes to a pilot burner 5| within the combustion chamber l adjacent the outlet of main burner 38.
Arranged adjacent the pilot burner is an igniting spark gap, consisting 'of an electrode 52 insulated from but passing through the combustion chamber wall, as by means of insulating bushings 52a, and a grounded electrode 53.
7 Also positioned adjacent the pilot burner and the main burner, where it will be subjected to flame from either or both, is a thermocouple 54.
A pipe 55 communicates with the interior of the. combustion chamber and is connected by fittings, such as a T 56 and nipple 57, to a casing consisting of a cover 58 and a bottom 59 between the edges of which is clamped the edge of a diaphragm 6| the casing sections being held together by bolts 6|. The diaphragm 60 has a pressure plate 6| on its upper surface having a depending pin 62 by which it may actuate a switch 63.
Passing upwardly from the pressure plate within the T 55 is a compression sprin 64, the tension of which may be adjusted by a screw plug E5 threaded in the upper branch of the T.
Connected to rotate the cam 33 is a motor 65, and positioned adjacent the cam is aswitch 81, having an arm 68, which may be moved to operate the switch by a projecting cam 69 formed on the side of cam 33.
A relay comprising a coil 10, an armature H and contacts 12 is positioned adjacent the casing l6 and valve 9 and motor 55, so that these parts, together with switch 67, may all conveniently be enclosed in a box or cover 13.
Covers or boxes 14 and [5 also conveniently may be provided for enclosing and protecting switches 48 and 63, respectively.
A transformer is shown at 6 to furnish current at suitable potential for the spark gap.
At i1 is shown a thermostat, which is positioned in the room or other space which it is desired to maintain at a uniform temperature.
Passing now to the description of the electrical circuits which are associated with the mechanical parts above described, power is supplied by any suitable source such as a central power house generator 18 through line 19 and 80.
Line 88 has four branches, one of which 89a terminates at transformer 16, another 801) at switch 48, a third 890 at relay coil 70 and a fourth 8003 at electro-magnetic switch 49.
From the opposite side of switch 63, a conductor 8| extends to switch 61, and from switch 6? a conductor 82 extends to transformer 16.
Branching from conductor 8| is a conductor 85a which connects with the other end of coil Til of the relay, and which has a branch Blb connected to the other side of valve 49.
Another branch 8|c connects with motor 66, While the opposite side of the motor is connected by a conductor 83 to switch 48.
I Switch 63' is normally closed, and is opened only in the event of an extremely high vacuum which causes the diaphragm SEi-to overcome the pressure of spring 64.
From the secondary of transformer 16, conductors 84 and 85 pass, respectively, to electrode 52 and to the ground.
With the parts as above described; and the apparatus at rest, let it be assumed that the temperature at thermostat TI falls below the setting of this thermostat.
This, of course, closes the contacts of the thermostat and permits current to be supplied through line 19 to motor 3, driving blower 2, the current flowing through switch 63, conductors 8|, 8|a, 800, Mb, d, and 80 back to the generator, thus energizing the coil 10 of the relay to close contacts 12 and opening valve 49, current to the valve. being supplied to it through conductors 8|d and BI!) which connect it in parallel with the coil 10.
The closing of the contacts I2 establishes communication through conductors and 86 between the thermo-couple 54' and coil while the opening of the valve 49 permits pilot gas to pass through pipes I4 and Site the pilot burner 5|.
At the time this is taking place, the cam 33 is in the position shown in Figures 1 and 2, where the roller 32 is at its lowermost position with valve 21 open and valve 2| closed.
As soon as pump 2 has exhausted the contents of combustion chamber sufficiently to raise diaphragm 44, switch 48 closes and current cannow pass through this switch between co'nductors 83 and 891), thus supplyin current to motor 66 which starts to rotate and to move cam 33.
This cam rotates in a clockwise direction, as seen in Figures 2 to .5, so that the roller for a short period is free of the cam while the latter passes through the sector marked 33a, and thereafter climbs upon the sector 33b to the position shown in Figure 3 where both valves 2| and 21 are closed. The succeeding sector of the cam is a dwell, indicated at 330, which may be for a substantial period, such as about a quarter of a minute, permitting the blower to completely purge the combustion chamber of any unburned fuel.
Passing beyond the dwell of sector 33c, sector 33d of the cam again raises plunger 25, as shown in Figure 4, so that valve 2| is opened while valve 21 is held closed. .This. permits gas to flow from the intake side .of valve body ID to port 12, and thence through tubes l4 and I 5 to the pilot burn- While'cam 33 is moving its sector 3311 under the roller 32, its cam lug 69 engages switch arm 88 and as this'lug extends axially a sufiicient distance to actuate switch 6! this engagement closes the switch 61, permitting current to bow through 82 to the primary of transformer 76, and thus inducing a high tension current in conductors 84 and 85 producing a spark between electrodes 52 and 53.
.This spark is of suflicient intensity to ignite the pilot gas, which is now entering through the pilot burner 5|.
Continued rotation of motor 66 carries cam 33 beyond the dwell 33c, allowing the plunger to slide down the last sector 33 to the position shown in Figure 5.
Of course, when the parts are brought into the position shown in Figure 4, armature 20 is brought into contact with the poles of core [8, and if ignition of the gas has taken place within'the combustion chamber, coil I! is energized by the thermocouple and holds this armature in a raised position as shown in Figure 5, keeping valve 2| above its seat.
The dropping of plunger 25, of course, moves valve 21 below its seat so that valve 9 is fully It will beobserved that the control above de-' scribed operates automatically to render the apparatus safe against the undesired supply of fuel in the event of various types of failure.
Pressure in pipe 34 opens switch 48 preventing the motor 66 from causing the parts to go through their cycle until a proper vacuum has been produced.
Interruption of electric current, whether by operation of thermostat 71 or from other causes, causes magnetic valve 49 to snap shut instantly stopping any supply of pilot gas.
Immediately upon exhaustion of the gas burning at the main burner, de-energization of coil I! permits valve 2! to snap shut, cutting off all fuel to the main burner as well as to the pilot burner.
Absence of flame in the combustion chamber for any reason de-energizes coil I! and closes valve 2|.
Failure of vacuum-like pressure in pipe 34 breaks the motor circuit at switch 48.
If the pilot burner is not lit on the first cycle of the apparatus, but proper conditions of vacuum continue, the apparatus will re-cycle until ignition takes place.
Thus the control illustrated will guard against many types of failure and dangerous conditions which might arise as pointed out above.
In Figure 6, the electrically operated valve M9 has been inserted in conduit I 88 instead of between tube parts H4 and I53. The operation of the deviceis otherwise just as above described.
Of course with valve I49 as shown in this figure, deenergization thereof shuts off the entire gas supply, not merely that to the pilot burner.
In Figure 7 the apparatus is shown as adapted to burning fuel at atmospheric pressure. In this form, the pipe 234 terminates at the frustro-conical end 240 of the pipe 231 leading to the main burner, the two pipes forming an inspirator or injector-like structure for drawing in air to support combustion at the burner.
The branch MI is provided with an apertured plate 235, through which the extension communicates with the interior of the casing con-. sisting of halves 242 and 243.
Within the casing is a diaphragm 244 having a rod or pin 24'! arranged, when the diaphragm is raised, to contact the arm of switch 248, this switch being normally open and closed only when engaged by the shank 241.
It will be seen that the actuation of this switch is precisely'the same as that of switch 48 of Figure 1, excepting that in the first figure the switch is controlled by vacuum created by the blower:
modifications and variations coming within the scope of the appended claims.
I claim:
1. Combustion control apparatus comprising a combustion chamber, a burner in the chamber,
a fuel supply line leading to the burner, a valvein said line, a restricting member in the line between the valve and burner, and valve control means operabl associated with the valve and controlled by the pressure in the line between the valve and restricting member.
2. Combustion control apparatus comprising a combustion chamber, a burner in the chamber, a fuel supply line leading to the burner and including a valve, a restricting member in said supply line between the valve and burner, actuating means connected to said valve, control means for said valve connected to and responsive to the pressure in the chamber, and retaining means for said valve controlled by the existence or absence of a flame at the burner.
3. Combustion control apparatus comprising a combustion chamber, a burner therein, a fuel supply line leading to the burner and including a valve, a restricting memberin said supply line between the valve and burner, actuating means for said valve connected to and responsive to the pressure in the chamber, and retaining means for said actuating means controlled by the existence or absence of a flame at the burner, and operating means for said valve controlled by the pressure in the conduit between the valve and the restricting member.
4. In a combustion apparatus comprising a combustion chamber, gas exhausting means connected with said chamber, a main burner and a nected to said valve, and a pressure operated control connected to said actuating means controlled by the pressure in said conduit between the-valve and the combustion chamber.
5. Combustion control apparatus comprising a combustion chamber, a burner therein, a source of fuel under pressure, a conduit leading from said source of fuel to said burner, a valve in the conduit, a restricting member in the conduit between the valve and the burner, an electric motor, power transmission means connected thereto and arranged to open said valve, resilient valve closing means, electro-magnetic valve retaining means arranged to hold the valve open, a pressure responsive control connected to and actuated by the pressure in the conduit between the valve and the restricting member and controlling said valve retaining means, a pressure responsive controlling means connected to and responsive to the pressure in the combustion chamber controlling the motor, and a thermocouple adjacent the burner controlling the valve retaining means.
6. Combustion control apparatus comprising a combustion chamber, a burner therein, a source of fuel under pressure, a conduit leading from said source of fuel to said burner, a valve in the conduit, 3, restricting member in the conduit between the valve and the burner, an electric motor, power transmission thereto and arranged to open said valve, resilient valve closing means, electro-inagnetic valve retaining means arranged to hold the valve open, a pressure responsive control connected to and actuated by the pressure in the conduit between the valve and the restricting member and controlling said valve retaining means, a pressure responsive controlling means connected to and responsive to the pressure in the combustion chamber controlling the motor, and a thermocouple adjacent the burner controlling the valve retaining means, a second conduit from the fuel supply conduit terminating in a pilot burner admeans connected 8 jacent the first mentioned burner, and a valve in saidsecond mentioned conduit actuated by said motor.
7. In a combustion apparatus comprising a combustion chamber, gas exhausting means connected with said chamber, a main burner and a pilot burner within the chamber adjacent each other, a source of fluid fuel under pressure, conduit means leading from said source of fuel to said main burner and having successively interposed therein a valve and a conduit restricting member and an air inlet, the valve being closest the source of fuel and the air inlet closest the main burner, electrical actuating means connected to said valve, and a pressure operated con trol connected to said actuating means controlled by thepressure in said conduit between the valve and the conduit restricting member.
WILLIAM L. RIEHL.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 1,814,947 McGuinness July 14, 1931 1,954,405 Dotterweich Apr. 10, 1934 2,062,605 Peters Dec. 1, 1936 2,125,473 Vaughan Aug. 2, 1938 2,240,163 Pick Apr. 29, 1941 2,259,299 Dewey Oct. 14, 1941 2,290,048 Hildebrecht July 14, 1942 2,297,854 Alfery Oct. 6, 1942 2,335,471 Ashcraft Nov. 30, 1943 2,363,073 Mantz Nov. 21, 1944 2,369,746 Miller Feb. 20, 1945 2,373,326 Miller Apr. 10, 1945 2,403,611 Ray July 9, 1946 2,412,990 Kruse Dec. 24, 1946 2,424,154 Dunham et al. July 15, 1947 FOREIGN PATENTS Number Country Date 474,271 Great Britain Oct. 28, 1937
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US696735A US2642128A (en) | 1946-09-13 | 1946-09-13 | Pressure responsive combustion control apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US696735A US2642128A (en) | 1946-09-13 | 1946-09-13 | Pressure responsive combustion control apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
US2642128A true US2642128A (en) | 1953-06-16 |
Family
ID=24798313
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US696735A Expired - Lifetime US2642128A (en) | 1946-09-13 | 1946-09-13 | Pressure responsive combustion control apparatus |
Country Status (1)
Country | Link |
---|---|
US (1) | US2642128A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2953196A (en) * | 1954-02-24 | 1960-09-20 | Fred B Aubert | Safety control apparatus for fuel burners |
US2953197A (en) * | 1956-03-26 | 1960-09-20 | Baso Inc | Burner control apparatus |
US2958377A (en) * | 1956-07-16 | 1960-11-01 | Baso Inc | Fuel control and ignition system |
US2964049A (en) * | 1957-03-25 | 1960-12-13 | Baso Inc | Fuel control and ignition system |
US2974869A (en) * | 1955-11-17 | 1961-03-14 | Baso Inc | Control apparatus |
US3039522A (en) * | 1958-11-18 | 1962-06-19 | Zimmermann & Jansen Gmbh | Gas safety means for use in hot blast stoves |
US3106239A (en) * | 1960-03-29 | 1963-10-08 | Zimmermann & Jansen Gmbh | Gas safety device |
US3115302A (en) * | 1959-08-03 | 1963-12-24 | Ronald D Corey | Heating method, means and control |
US3834856A (en) * | 1973-08-30 | 1974-09-10 | Coleman Co | Pilot reclamation system for gas-fires forced draft heater |
Citations (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1814947A (en) * | 1930-07-30 | 1931-07-14 | Western Union Telegraph Co | Automatic selective pneumatic tube carrier relay |
US1954405A (en) * | 1924-01-19 | 1934-04-10 | Gen Water Treat Corp | Water-softening apparatus |
US2062605A (en) * | 1933-04-01 | 1936-12-01 | Alexander D Bruce | Air conditioning apparatus |
GB474271A (en) * | 1935-12-07 | 1937-10-28 | Askania Werke Ag | Improvements in safety cut off valve assemblies for gas apparatus |
US2125473A (en) * | 1936-06-18 | 1938-08-02 | Metals & Controis Corp | Gas burner control system |
US2240163A (en) * | 1938-09-30 | 1941-04-29 | Permutit Co | Valve apparatus for controlling hydraulic or pneumatic machines |
US2259299A (en) * | 1938-04-18 | 1941-10-14 | Maurice J Dewey | Heating apparatus |
US2290048A (en) * | 1938-12-12 | 1942-07-14 | Milwaukee Gas Specialty Co | Safety device for heating and other apparatus |
US2297854A (en) * | 1929-11-09 | 1942-10-06 | Milwaukee Gas Specialty Co | Combined thermoelectric safety shut-off and electroresponsive valve |
US2335471A (en) * | 1940-06-05 | 1943-11-30 | Honeywell Regulator Co | Fluid fuel burner control system |
US2363073A (en) * | 1942-01-19 | 1944-11-21 | Milwaukee Gas Specialty Co | Valve structure |
US2369746A (en) * | 1945-02-20 | miller | ||
US2373326A (en) * | 1941-03-01 | 1945-04-10 | Union Fork & Hoe Co | Gas burner heating system and apparatus therefor |
US2403611A (en) * | 1941-02-04 | 1946-07-09 | Gen Controls Co | Reset valve and control therefor |
US2412990A (en) * | 1942-07-06 | 1946-12-24 | American Can Co | Drying oven control |
US2424154A (en) * | 1940-09-12 | 1947-07-15 | Ex Lab Inc | Subatmospheric gas burner |
-
1946
- 1946-09-13 US US696735A patent/US2642128A/en not_active Expired - Lifetime
Patent Citations (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2369746A (en) * | 1945-02-20 | miller | ||
US1954405A (en) * | 1924-01-19 | 1934-04-10 | Gen Water Treat Corp | Water-softening apparatus |
US2297854A (en) * | 1929-11-09 | 1942-10-06 | Milwaukee Gas Specialty Co | Combined thermoelectric safety shut-off and electroresponsive valve |
US1814947A (en) * | 1930-07-30 | 1931-07-14 | Western Union Telegraph Co | Automatic selective pneumatic tube carrier relay |
US2062605A (en) * | 1933-04-01 | 1936-12-01 | Alexander D Bruce | Air conditioning apparatus |
GB474271A (en) * | 1935-12-07 | 1937-10-28 | Askania Werke Ag | Improvements in safety cut off valve assemblies for gas apparatus |
US2125473A (en) * | 1936-06-18 | 1938-08-02 | Metals & Controis Corp | Gas burner control system |
US2259299A (en) * | 1938-04-18 | 1941-10-14 | Maurice J Dewey | Heating apparatus |
US2240163A (en) * | 1938-09-30 | 1941-04-29 | Permutit Co | Valve apparatus for controlling hydraulic or pneumatic machines |
US2290048A (en) * | 1938-12-12 | 1942-07-14 | Milwaukee Gas Specialty Co | Safety device for heating and other apparatus |
US2335471A (en) * | 1940-06-05 | 1943-11-30 | Honeywell Regulator Co | Fluid fuel burner control system |
US2424154A (en) * | 1940-09-12 | 1947-07-15 | Ex Lab Inc | Subatmospheric gas burner |
US2403611A (en) * | 1941-02-04 | 1946-07-09 | Gen Controls Co | Reset valve and control therefor |
US2373326A (en) * | 1941-03-01 | 1945-04-10 | Union Fork & Hoe Co | Gas burner heating system and apparatus therefor |
US2363073A (en) * | 1942-01-19 | 1944-11-21 | Milwaukee Gas Specialty Co | Valve structure |
US2412990A (en) * | 1942-07-06 | 1946-12-24 | American Can Co | Drying oven control |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2953196A (en) * | 1954-02-24 | 1960-09-20 | Fred B Aubert | Safety control apparatus for fuel burners |
US2974869A (en) * | 1955-11-17 | 1961-03-14 | Baso Inc | Control apparatus |
US2953197A (en) * | 1956-03-26 | 1960-09-20 | Baso Inc | Burner control apparatus |
US2958377A (en) * | 1956-07-16 | 1960-11-01 | Baso Inc | Fuel control and ignition system |
US2964049A (en) * | 1957-03-25 | 1960-12-13 | Baso Inc | Fuel control and ignition system |
US3039522A (en) * | 1958-11-18 | 1962-06-19 | Zimmermann & Jansen Gmbh | Gas safety means for use in hot blast stoves |
US3115302A (en) * | 1959-08-03 | 1963-12-24 | Ronald D Corey | Heating method, means and control |
US3106239A (en) * | 1960-03-29 | 1963-10-08 | Zimmermann & Jansen Gmbh | Gas safety device |
US3834856A (en) * | 1973-08-30 | 1974-09-10 | Coleman Co | Pilot reclamation system for gas-fires forced draft heater |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2319676A (en) | Safety shutoff system | |
US2318823A (en) | Safety shut-off and control device | |
US2642128A (en) | Pressure responsive combustion control apparatus | |
US2253670A (en) | Valve | |
US2297854A (en) | Combined thermoelectric safety shut-off and electroresponsive valve | |
US2527286A (en) | Safety shutoff control for plural pilot gaseous fuel burner systems | |
US2456147A (en) | Burner control system | |
US2321095A (en) | Thermoelectric safety shutoff device | |
US2578194A (en) | Thermoelectric burner control system | |
US2588179A (en) | Safety control device | |
US2291805A (en) | Burner control system | |
US2077297A (en) | Automatic control and electric ignition for gas burners | |
US2333261A (en) | Safety switch and pilot valve | |
US2125473A (en) | Gas burner control system | |
US2146660A (en) | Igniter for gas burners | |
US2340234A (en) | Trip means for safety control devices and the like | |
US2268959A (en) | Burner control system | |
US2329682A (en) | Burner control apparatus | |
US2132057A (en) | Thermo-electric safety switch | |
US2249442A (en) | Burner control apparatus | |
US2610682A (en) | Control system for fluid fuel burners | |
US2518804A (en) | Safety control system for gaseous fuel burners | |
US2676757A (en) | Burner control valve | |
US2501850A (en) | Control and ignition system for | |
US3005487A (en) | Gas valve control with plural thermocouples |