US2197904A - Combustion control - Google Patents

Combustion control Download PDF

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US2197904A
US2197904A US155953A US15595337A US2197904A US 2197904 A US2197904 A US 2197904A US 155953 A US155953 A US 155953A US 15595337 A US15595337 A US 15595337A US 2197904 A US2197904 A US 2197904A
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air
fuel
combustion
rate
pressure
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US155953A
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Charles M Terry
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AW Cash Co
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AW Cash Co
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/60Devices for simultaneous control of gas and combustion air
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/0318Processes
    • Y10T137/0324With control of flow by a condition or characteristic of a fluid
    • Y10T137/0363For producing proportionate flow
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/2496Self-proportioning or correlating systems
    • Y10T137/2514Self-proportioning flow systems

Definitions

  • Fig. 1 is a diagrammatic view, partly in section, showing a furnace to which air is supplied for combustion by natural draft;
  • This regulator 44 comprises a pilot valve db supplied with a suitable fluid under pressure by a pipe 66 and connected by tubes 48 to a fluid motor 49, this motorbeing connected by a link 50 to the arm IQ of the damper It.
  • the pilot valve is controlled by a lever 52 which is" connected to a pressure plate 53 located beneath and in contact with a flexible diaphragm 54.
  • the diaphragm is connected to the lower end of a coiled tension spring 56 having its upper end secured to anut 51 mounted on a vertical adjusting screw 58.
  • the edge portions of the diaphragm are supported by a casing 60 shaped to provide a chamber 6! above the diaphragm and a chamber 62 beneath the diaphragm.
  • a pipe 66 connects the chamber M with the combustion chamber ii, and a pipe 65 connects the chamber 62 with the gas outlet duct l6 anterior to thedamper i8.
  • the regulator A l is provided with a second and preferably somewhat smaller diaphragm 66 having a chamber 67 therebeneath.
  • the two diaphragms are connected centrally to move as a unit, and they jointly control the lever 52 and the pilot valve 45.
  • the chamber 6'? beneath the lower diaphragm 66 is connected by a pipe 68 to the pipe 36 anterior to the valve 37.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Regulation And Control Of Combustion (AREA)

Description

April 23, 1940. c. TERRY 2,197,904
' COMBUSTION CONTROL Filed July 27, 1937 2 Sheets-Sheet 2 amen too CHARLES M. TERRY Patented Apr. 23,
PATENT OFFICE COIMBUSTION CONTROL CharlesMs'lerry, Decatur, llL, assig'nor to A. W. Cash Company, Decatur, 111., a corporation of Delaware Application July 27, 1937, Serial No. 155,953
9 Claims.
This invention relates to combustion. control,
and more particularly-to .tliecontrol of the combution of fluent fuels, such as oil and gas.
It is customary to vary the supplies'of fuel and 5. air in accordance with the demand for heat, but
'difilculties have been encountered in maintaining the correct proportions between the rate of fuel supply and the rate of air supply. Unless this fuel-air ratio is maintained at the proper in value, it will be impossible to obtain eflicient combustion conditions. It is also important to provide means whereby the fuel-air ratio can be adiusted to compensate for changes in the quality or heating value of the fuel. While attempts have been made to solve this problem, no thoroughly satisfactory solution has heretofore been disclosed.
It is accordingly one object of the invention to provide a comparatively simple and dependable method and apparatus for controlling the com- -bustion of fluent fuel and maintaining the fuel an: air supplies in the correct proportions at all a It is a further object of the invention to provide a, comparatively simple and dependable 26. method and apparatus for burning fluent fuel and for adjusting the fuel-air ratio.
With these and other objects in view, as will be apparent to those skilled in the art, the in vention resides in the combination of parts and the steps of the process set forth-in the speciflcation and covered by the claims appended hereto. Y
In accordance with my invention in its preferred form, I cause a fluid, such as air, to flowin a stream at a rate dependent upon the rate of supply of fuel for combustion, and I control the supply of air for combustionin accordance with pressure characteristics of the fluid stream. The fluid is preferably compelled to flow in a conduit from which it is allowed to escape at a rate which can be adjusted to vary the fuel-air ratio. The fluid is preferably forced into the conduit by a pressure-generator driven by a motor, the
w latter being actuated by the stream of fuel flowing to the furnace.
Referring to the'drawings illustrating one em- 1 bodiment of the invention, and in which like reference numerals indicate like-parts, go Fig. 1 is a diagrammatic view, partly in section, showing a furnace to which air is supplied for combustion by natural draft;
Fig. 2 is a section on the line 2-2 of Fig. 1; Fig. 3 is a section on the line 3-3 of Fig. 1; and Fig. 4 is a view similar to Fig. 1, showing an arrangement in which the furnace is supplied with air for combustion by forced draft. The embodiment illustrated in Fig. 1 comprises a furnace ill arranged to form a combustion chamber H, and a steam boiler l2 associated therewith. The boiler is provided with banks of water tubes II and a baflle I! of usual construction, this 'bailieserving to direct the hot gases from the combustion chamber into proper contact with the water tubes and thence to a gas 1 outlet duct it, which may lead to a suitable stacl;
or induced draft fan (not shown). The outlet duct I 6 is provided with; a damper I8 having an operating arm IS. The boiler l2 is provided with j the usual steam delivery pipe 20. 16 On the front of the furnace Hi there are mounted two 011 burners 22 of the natural draft type. These burners are arranged to discharge oil in theform of a spray rearwardly into the combustion chamber through openings 23 in the furnace 20 wall. Air for combustion enters the combustion chamber through these openings at ara .te controlled by the damper I8. Fuel oil is supplied under pressure from any suitable source through a pipe 25 having branches 26 which-lead to the 25 burners 22. Each branch 26 is shown provided with a valve 21 which is normally open but which can be closed when it is desired to shut down the corresponding burner. The pipe 25 is provided with a valve 29 having an operating lever 30 which so is controlled by an automatic regulator 3| of the type disclosed in the patent to Temple, No. 2,049,549, granted August 4, 1936. This regulator is connected to the boiler steam pipe 20 by means of a pipe- 32. These parts are so constructed and 85 arranged that the regulator 3| will control the valve 29 (and hence the supply of fuel oil to the. burners) in accordance with variations in the demand forheat as indicated by changes in the boiler steam pressure transmitted through the P p 32. v
In order to maintain the correct ratio between the supply of fuel and the supply of combustion air, I have shown a pressure-generator in the form of. a positive-displacement blower 8t arranged to receive air at atmospheric pressure through a pipe 35, and deliver this air-to a conduit in the form of a pipe 36 having a valve ii'i therein through which the air may escape to the atmosphere. As shown in Fig. 3, the blower 3% may be of a well known type having a pair oi I oppositely rotating impellers 2t.
Means is provided to vary the air pressure in the pipe 36 in accordance with variations in the rate of supply of the fuel'oil to the furnace. For
this purpose the blower 34 is driven by means of a motor 40 which is connected to theblower by a coupling 4!, this motor being mounted in the pipe line and arranged to be actuated by the fuel oil flowing therethrough. As shown in Fig. 2, the motor may be of a well known construction having a pair of intermeshing spur gears 42 which are rotated by the fuel oil at a speed varying substantially in direct proportion with variations in the rate of fuel flow. Any
change in the rate of supply oi the fuel oil will thus vary the speed of the motor 40 and of the blower as, thereby varying the rate at which air is delivered to the pipe 36 and causing a change in the air pressure in this pipe.
'I'hesevariations in the pressure of the air in the pipe 36 are utilized to control the rate at which air is supplied for combustion of the fuel. For this purpose there is shown an automatic regulator 44 of a construction similar to that disclosed in the patent to Temple,,No. 1,992,048.
granted February 19, 1935. This regulator 44 comprises a pilot valve db supplied with a suitable fluid under pressure by a pipe 66 and connected by tubes 48 to a fluid motor 49, this motorbeing connected by a link 50 to the arm IQ of the damper It. The pilot valve is controlled by a lever 52 which is" connected to a pressure plate 53 located beneath and in contact with a flexible diaphragm 54. The diaphragm is connected to the lower end of a coiled tension spring 56 having its upper end secured to anut 51 mounted on a vertical adjusting screw 58. The edge portions of the diaphragm are supported by a casing 60 shaped to provide a chamber 6! above the diaphragm and a chamber 62 beneath the diaphragm. A pipe 66 connects the chamber M with the combustion chamber ii, and a pipe 65 connects the chamber 62 with the gas outlet duct l6 anterior to thedamper i8. In addition to the main diaphragm 55 the regulator A l is provided with a second and preferably somewhat smaller diaphragm 66 having a chamber 67 therebeneath. The two diaphragms are connected centrally to move as a unit, and they jointly control the lever 52 and the pilot valve 45. The chamber 6'? beneath the lower diaphragm 66 is connected by a pipe 68 to the pipe 36 anterior to the valve 37.
The operation of this embodiment will now be apparent from the above disclosure. Under steady load conditions, the regulator 3| will hold the valve 29 in the proper position to supply fuel oil to the burners 22 at the rate necessary to maintain the boiler steam pressure constant,
and the regulator 48 will hold the damper I8 in the proper position to ensure the correct supply of air for combustion. The fuel oil will actuate the motor 60 at a constant speed, and the motor will drive the blower 3d at the same speed, thus maintaining a uniform air pressure in the pipe 36 and chamber 61. With asteady fiow of gases pastthe boiler water tubes, a constant differential pressure will be transmitted to the diaphragm 54 by the pipes 6t and 65, and the regulator #14 will be in balance, with its pilot valve 45 in neutral position. If now' the demand for steam increases, the steam pressure transmitted through the pipe 32 will decrease, and the regulator 3! will open the valve 29 and increase the flow of the fuel oil to the burners. This will cause the motor Ml and blower 38 to operate at a higher speed, increasing the air pressure in the pipe 36 and chamber 61. This increased air pressure on the diaphragm 66. will throw the regulator M out of balance, causing its pilot valve 45 'to admit operating fluid to the moton 49 and thus open the damper l8 to increase the flow of combustion airthrough the burners. As soon as the rate of air flow has increased sufliciently, the resulting increased pressure diiferential transmitted to the diaphragm 54 through the pipes 64 and 65 will restore the regulator to balance, and the damper l8 will be brought to rest. Similarly, a decrease in the demand for steam will cause the steam pressure to increase, and the' regulator 31 will close the valve 729 to decrease the flow of fuel oil. This will reduce the speed of motor 40 and blower 34, decreasing the pressure in the chamber 61. The. regulator 44 will thereupon close the damper it until a balanced condition is again obtained. If the heating value of the fuel oil is changed, or if for any other reason it is desirable to change the fuel-air ratio in order to maintain proper combustion conditions, it is merely' necessary to adjust the valve 3'1 which controls the rate at which air escapes from the pipe 36. Opening this valve will produce a richer mixture, since it will decrease thepressure in the chamber 6.! for a given rate of fuel flow, and a decreased flow of combustion air will be required to maintain the regulator 45 in balance. Similarly, closing the valve 31 will produce a leaner mixture by increasing the flow of combustion air for a given. rate of fuel supply.
In Fig. 4 there is illustrated a slightly modified form of the invention in which the combustion air is supplied to the furnace under forced draft. In this modification the burners 22 of Fig. l are replaced by burners 22' of the forced draft type, these burners being supplied with air at a pressure above atmospheric by means of a fan 16 connected to the burners by a duct II. This duct is provided with a damper 12 havingzin operating arm 73 which is connected by a link 14 to the motor 15 of a regulator 16. This regulator is of the type disclosed in the patent to Temple, No. 1,992.048, granted February 19, 1935, and comprises a pilot valve 18 supplied with fluid under pressure from a suitable source through a pipe 79 and connected with the motor -75 by means of tubes 80. This pilot valve is actuated by means of a lever 8i which is controlled by a flexible diaphragm 82 connected to the lower end .of a coiled tension spring 83. The upper end of the spring 83 is secured to a nut 86 mounted on a vertical adjusting screw 85. The edge portions of the diaphragm 82 are supported by I there is mounted in the pipe 25 a motor 92 similar to the motor 46 of Fig. l and connected by means of a coupling 93 to a pressure-generator in the form of a rotary fan 96. This fan receives air from the atmosphere and delivers it under pressure to a conduit in the form of a duct 95 having a valve 96 connected thereto through which the air may escape to the atmosphere. The duct is preferably provided with an orifice plate 91. A pipe 98 serves to connectthe chamber 89 with the duct 95 posterior to the orifice plate 91.
The gas outlet damper I6 in Fig. 4 is preferably controlled to maintain a substantially constant pressure, slightly below atmospheric, in the combustion chamber II, and for this purpose there is shown a regulator I00 of the same type as the regulator I6. This regulator I00 is connected to the combustion chamber by a pipe IOI. Pressure fluid is supplied to the regulator by a pipe I02,-and tubes I03 leadfrom the regulator to a fluid motor I04 which is connected by a link I05 to the operating arm IQ of the damper I8.
The operation of the embodiment illustrated in Fig. 4 will now be apparent from the above disclosure. Under steady load conditions, the regulator 3| will hold the valve 29 in the proper position to supply fuel oil to the burners 22' at the rate necessary to maintain the steam pressure constant, and the regulator I6 will hold the damper 12 in the proper position to ensure the correct supply of air for combustion. The fuel oil will actuate the motor 92, and the motor will drive the fan 94 at aconstant speed, thus maintaining a uniform air pressure in the duct 95 and chamber 89. A constant pressure will be transmitted through the pipe to the chamber 89, and the regulator I6 will be in-balance with its pilot valve 18 in neutral position. If now the demand for steam increases, the steam pressure transmitted through the pipe 32 will decrease, and the regulator 3! will open the valve 29 and increase the flow of the fuel oil to the burners. This will cause the motor 92 and fan M to operate at a higher speed, increasing the air pressure in the duct and chamber 80. This increased air pressure will throw the regulator'lli out of balance, causing its pilot val-ve I8 to admit operating fluid to the motor I5 and thus open the damper 12 to increase the flow of combustion air through the burners until the pressure transmitted through the pipe 90 to the diaphragm 82 has increased sufficiently to restore the regulator to balance, whereupon the damper I2 will be brought to rest. Similarly, a decrease in the demand for steam will cause the steam pressure to increase, and the regulator 3| will close the valve 29 to decrease the flow of fuel oil. This will reduce the speed of the motor 92 and fan at, decreasing the pressure in the chamber 89. The regulator I6 will thereupon close the damper 52 until. a balanced condition is again obtained. By adjusting the valve 96 the fuel-air ratio can be varied as desired in a very simple manner. The orifice plate 91 improves the pressure characteristics of the fan 96 in relation to its speed, and makes it possible to obtain a wider range of adjustment by means of the valve 58 without requiring an excessively large valve. Regardless of changes in the rate of combustion, the regulator I09 will control the gas outlet damper IS in such a way as to maintain a predetermined pressure in the combustion chamber It will be understood that the positive displacement blower St of Fig. 1 can be utilized in place of the fan 90 and orifice plate 91 of Fig. 4. and vice versa.
Having thus described my invention, what I claim as new and desire to secure by Letters Patent is:
1. The method of controlling the combustion of fluent fluid in a furnace comprising the steps of delivering a stream of fuel to the furance, supplying air to the furnace for combustion of the fuel, deriving power from the fuel stream,uti-' the fuel, deriving power from the fuel stream,
utilizing said power to force a separate control fluidinto a confined space at a rate unaflected by the rate of air supply, allowing-the control fluid to escape from said space at a controlled rate, and varying the rate of air supply in ac- .cordance with variations in the fluid pressure in the confined space.
3. Thewmethod of controlling the combustion of fluent fuel in a furnace comprising the steps of delivering a stream of fuel to the furnace, supplying air to the furnace for combustion of the fuel, deriving power from the fuel stream, utilizing said power to force a separate stream of air into a conflned space at a rate unaffected by the rate at which combustion air is supplied, allowing air to escape from the confined space at a controlled rate, and varying the rate of supply of the combustion air in accordance with variations in the air pressure in the confined space. I
4. Combustion control apparatus comprising a furnace, means to deliver a stream of fluent fuel to the furnace, means to supply air to the furnace for combustion of the fuel, means actuated by the fuel stream to produce a continuous stream of a separate control fluid which flows at a rate unaffected by the rate of air supply, and means to vary the rate of air supply in accordance with variations in pressure characteristics of the stream of fluid.
5.- Combustion control apparatus comprising a furnace, means to deliver a stream of fluent fuel to the furnace, means to supply air to the furnace for combustion of the fuel, a motor actuated by the fuel stream, means driven by the motor to produce a continuous stream .of a separate control fluid which flows at a rate unaffected by the rate of air supply, and means to vary the rate of air supply in accordance with variations in pressure characteristics of the stream of fluid.
ated by-the fuel stream, a conduit, 9. pressuregenerator driven by the motor and arranged to force a continuous stream of a separate control fluid into the conduit at a rate unaffected by the rate of air supply, a valve through which the control fluid may escape from the conduit, and means to vary the rate of air supply in accordance with variations in the conduit.
7. Combustion control apparatus comprising a furnace, means to deliver a stream of fluent fuel to the furnace, means to supply air to the furnace for combustion of the fuel, a motor actuated by the fuel stream, a conduit, a pressuregenerator driven by the motor and arranged to force a separate stream of air into the conduit at a rate unaffected by the rate at which combustion air is supplied, a valve through which air may escape from the conduit, and means to vary the rate of supply of the combustion air in accordance with variations in the air pressure in the conduit.
the fluid pressure in 8. Combustion control apparatus comprising a furnace, means to deliver a stream of fluent fuel to the furnace, means to supply air to the furnace for combustion of the fuel, a motor actuated by the fuel stream, a conduit, a pressuregenerator driven by the motor and arranged to force a separate stream of air into the conduit at a rate unafiected by the rate at which combustion air is supplied, a valve through which air may escape from the conduit, and a regulator arranged to control the rate of flow of the combustion air, the regulator being responsive both to changes in the rate of flow of the combustion air and to changes in the air pressure in the 15 conduit.
9. Combustion control apparatus comprising a furnace, means to deliver a stream of fluent fuel to the furnace, means to supply air to the furnace for combustion of the fuel, a rotatable motor actuated by the fuel stream at a speed substantially in direct proportion to the rate of fuel flow, a conduit, a pressure-generator driven by the motor and arranged to force a separate stream of air into the conduit at a rate unaffected by the rate at which combustion air is supplied, a valve through which air may escape from the conduit, and means to vary the rate of supply of the combustion air in accordance with variations in the air pressure in the conduit.
C M. TERRY.
US155953A 1937-07-27 1937-07-27 Combustion control Expired - Lifetime US2197904A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2436282A (en) * 1943-03-26 1948-02-17 Continental Oil Co Surface combustion cracking furnace
US2445466A (en) * 1944-06-02 1948-07-20 Solar Aircraft Co Fluid fuel combustion device
US2776872A (en) * 1946-05-24 1957-01-08 Babcock & Wilcox Co Apparatus suitable for the fixation of nitrogen
US2777457A (en) * 1951-06-21 1957-01-15 Bailey Meter Co Fluid pressure characterizing relay
US2785960A (en) * 1951-09-04 1957-03-19 Phillips Petroleum Co Safety system for combustion process
US2800394A (en) * 1955-04-11 1957-07-23 Phillips Petroleum Co Method of and apparatus for controlling carbon black furnaces
US2863500A (en) * 1952-02-04 1958-12-09 Hauck Mfg Co Fluid fuel burners
US4116614A (en) * 1977-02-02 1978-09-26 Kutrieb Wolfgang A Oil heater having controlled oil flow
WO1981003056A1 (en) * 1980-04-24 1981-10-29 S Nilsson Device for controlling a damper regulator at heating boilers
US6568933B1 (en) * 2002-06-03 2003-05-27 R. E. Guerra Enterprises Ltd. Apparatus to burn gases
US7140873B1 (en) * 1999-03-01 2006-11-28 Michael J. House Multi all fuel processor system and method of pretreatment for all combustion devices

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2436282A (en) * 1943-03-26 1948-02-17 Continental Oil Co Surface combustion cracking furnace
US2445466A (en) * 1944-06-02 1948-07-20 Solar Aircraft Co Fluid fuel combustion device
US2776872A (en) * 1946-05-24 1957-01-08 Babcock & Wilcox Co Apparatus suitable for the fixation of nitrogen
US2777457A (en) * 1951-06-21 1957-01-15 Bailey Meter Co Fluid pressure characterizing relay
US2785960A (en) * 1951-09-04 1957-03-19 Phillips Petroleum Co Safety system for combustion process
US2863500A (en) * 1952-02-04 1958-12-09 Hauck Mfg Co Fluid fuel burners
US2800394A (en) * 1955-04-11 1957-07-23 Phillips Petroleum Co Method of and apparatus for controlling carbon black furnaces
US4116614A (en) * 1977-02-02 1978-09-26 Kutrieb Wolfgang A Oil heater having controlled oil flow
WO1981003056A1 (en) * 1980-04-24 1981-10-29 S Nilsson Device for controlling a damper regulator at heating boilers
US7140873B1 (en) * 1999-03-01 2006-11-28 Michael J. House Multi all fuel processor system and method of pretreatment for all combustion devices
US6568933B1 (en) * 2002-06-03 2003-05-27 R. E. Guerra Enterprises Ltd. Apparatus to burn gases

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