US2483907A - Liquid fuel controlling means - Google Patents

Liquid fuel controlling means Download PDF

Info

Publication number
US2483907A
US2483907A US737030A US73703047A US2483907A US 2483907 A US2483907 A US 2483907A US 737030 A US737030 A US 737030A US 73703047 A US73703047 A US 73703047A US 2483907 A US2483907 A US 2483907A
Authority
US
United States
Prior art keywords
valve
liquid fuel
passage
chamber
fuel
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
Application number
US737030A
Inventor
Ifield Richard Joseph
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ZF International UK Ltd
Original Assignee
Joseph Lucas Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Joseph Lucas Ltd filed Critical Joseph Lucas Ltd
Application granted granted Critical
Publication of US2483907A publication Critical patent/US2483907A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D1/00Controlling fuel-injection pumps, e.g. of high pressure injection type
    • F02D1/02Controlling fuel-injection pumps, e.g. of high pressure injection type not restricted to adjustment of injection timing, e.g. varying amount of fuel delivered
    • 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
    • Y10T137/2559Self-controlled branched flow systems
    • Y10T137/2574Bypass or relief controlled by main line fluid condition
    • Y10T137/2605Pressure responsive
    • Y10T137/2617Bypass or relief valve biased open

Definitions

  • LIQUID FUEL CONTROLLING MEANS Filed March 25, 1947 Patented Oct. 4, 1949 2,483,907 LIQUID FUEL CONTROLLING MEANS Richard Joseph Ifield, Birmingham, England, assignor to Joseph Lucas Limited, Birmingham,
  • This invention relates to means for controlling the supply of liquid fuel to the burner nozzles of .a combustion chamber formin part of a prime mover, the latter being of the kind in which the combustion chamber is provided with a main burner and also with a pilot burner for effecting ignition of the main combustible mixture in the chamber.
  • a pilot burner avoids the necessity for arranging the required igniting device in the vicinity of the main burner, and thereby subjecting the device to undesirable heating efiects.
  • the igniting device retractible so that it can be moved away from the main burner after ignition has been effected, but this entails complication of the igniting-device, and it is more usual to provide a pilot burner which enables the igniting device to be arranged away from the main burner, and which can project a flame for effecting ignition of the main combustible mixture.
  • a pilot burner which enables the igniting device to be arranged away from the main burner, and which can project a flame for effecting ignition of the main combustible mixture.
  • fuel shall be supplied thereto at a substantially constant pressure.
  • the object of the invention is to provide improved means for controlling the supply of fuel to the main and pilot burners, such that the supply to the pilot burner is effected at a substantially constant pressure.
  • Figure 1 is a diagrammatic sectional side view of means constructed in accordance with the invention for controlling the supply of liquid fuel to a prime mover of the kind specified.
  • Figure 2 is a part sectional side view illustrating a modified form of the invention.
  • I employ a hollow body part a. having an inlet b for connection to a fuel supply pump and an outlet for connection to the main burner. Between the inlet b and outlet 0 there is arranged in the body part a a manually controllable valve d of any convenient form.
  • the valve d is of the slidable-plunger type, and is operable by a lever e through the medium of a rack j and pinion ,q, the plunger having a conical end which co-operates with an annular seating i in the body part a to control the flow of liquid fuel from the inlet b to the outlet 0.
  • a spring loaded piston or diaphragm may be provided in the chamber 7 for supporting the by-pass valve m.
  • This valve controls communication between the chamber 7' and a passage p leading from the inlet D.
  • a fuel can pass to an outlet q for connection to the pilot burner.
  • the chamber :i communicates with the main fuel outlet 0 by way of a passage 1' extending between this outlet and the chamber outlet q, this passage being controlled by a spring loaded non-return valve s.
  • a relief passage t controlled by a spring loaded valve u is provided in communication with the chamber 7.
  • the supply to the pilot burner is cut off by another valve (not shown), and the supply of fuel to the main burner is regulated as required by means of the manually operable valve d above described.
  • the manually operable valve d is closed.
  • the required restricted supply to the main burner is then maintained by flow past the by-pass valve m and through the above mentioned passage 1' containing the non-return valve s.
  • the manually operable valve (1 and its seating i are contained in a housing 1; which is separate and may be arranged at any convenient distance from the body part a containing the by-pass valve m and the chamber
  • the housing 1 is provided with an inlet b for connection by piping w to the delivery side of a fuel supply pump or, and with an outlet c for connection by piping y to the main burner 2.
  • the by-pass valve m comprises a closure member adapted to .co-operate with an annular seating at the inner end of an inlet passage p leading to the interior of the chamber 7' the outer end of this passage being adapted for connection to the piping w communicating with the delivery side of the pump a:.
  • the closure member of the by-pass valve m is formed on or secured to a lever 2 which at one end is pivoted to the body part a, and at the other end is connected to the capsule is in the chamber 7' this capsule being open to the atmosphere, or wholly or partially evacuated, as in the previously described example.
  • the chamber 7' is provided with an outlet q for connection by a pipe 3 to the pilot burner 4, this pipe having associated with it any convenient valve 5 for interrupting the supply of liquid fuel to the pilot burner after the prime mover has been started.
  • the chamber is provided with a passage r for connection with the piping 1 leading to the main burner a, this passage being controlled by a nonretum valve s
  • the chamber i is also provided with a pressure relief passage t for connection by a pipe 6 to the inlet side of the pump :0, this passage being controlled by a spring loaded valve al
  • the pump a: may be of the swash-plate or other suitable type, and may be controllable by barometric pressure through the medium of any convenient and known device I which is connected to the pump by pipes 8.
  • Means for controlling the supply of liquid fuel to a prime mover of the kind specified comprising in combination an inlet passage for liquid fuel under pressure, a main outlet passage for liquid fuel from said inlet passage, a subsidiary outlet passage for liquid fuel from said inlet passage, a manually operable valve for controlling liquid fuel flow from said inlet passage to said main outlet passage, a bypass valve for controlling liquid fuel flow from said inlet passage to said subsidiary outlet passage, a non-return valve operable by liquid fuel pressure at the outlet side of said by-pass valve for admitting a restricted supply of liquid fuel from the outlet side of said by-pass valveto said main outlet passage, and means for actuating said by-pass valve in response to liquid fuel pressure at the outlet side of said by-pass valve.

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

LIQUID FUEL CONTROLLING MEANS Filed March 25, 1947 Patented Oct. 4, 1949 2,483,907 LIQUID FUEL CONTROLLING MEANS Richard Joseph Ifield, Birmingham, England, assignor to Joseph Lucas Limited, Birmingham,
England Application March 25, 1947, Serial No. 737,030 In Great Britain February 25, 1946 Section 1, Public Law 690, August 8, 1946 Patent expires February 25, 1966 3 Claims.
This invention relates to means for controlling the supply of liquid fuel to the burner nozzles of .a combustion chamber formin part of a prime mover, the latter being of the kind in which the combustion chamber is provided with a main burner and also with a pilot burner for effecting ignition of the main combustible mixture in the chamber. The use of a pilot burner avoids the necessity for arranging the required igniting device in the vicinity of the main burner, and thereby subjecting the device to undesirable heating efiects. In cases where a pilot burner is not employed, it is known to make the igniting device retractible so that it can be moved away from the main burner after ignition has been effected, but this entails complication of the igniting-device, and it is more usual to provide a pilot burner which enables the igniting device to be arranged away from the main burner, and which can project a flame for effecting ignition of the main combustible mixture. In order to attain satisfactory atomisation at the pilot burner, it is desirable that fuel shall be supplied thereto at a substantially constant pressure. The object of the invention is to provide improved means for controlling the supply of fuel to the main and pilot burners, such that the supply to the pilot burner is effected at a substantially constant pressure.
p In the accompanying sheet of explanatory drawings:
Figure 1 is a diagrammatic sectional side view of means constructed in accordance with the invention for controlling the supply of liquid fuel to a prime mover of the kind specified.
Figure 2 is a part sectional side view illustrating a modified form of the invention.
In carrying the invention into effect as shown in Figure 1, I employ a hollow body part a. having an inlet b for connection to a fuel supply pump and an outlet for connection to the main burner. Between the inlet b and outlet 0 there is arranged in the body part a a manually controllable valve d of any convenient form. Preferably and as shown the valve d is of the slidable-plunger type, and is operable by a lever e through the medium of a rack j and pinion ,q, the plunger having a conical end which co-operates with an annular seating i in the body part a to control the flow of liquid fuel from the inlet b to the outlet 0. In the body part a is formed a cylindrical or other chamber 9 containing a deformable capsule k 2 phere through an opening 0 in the chamber, or being wholly or partially evacuated. Instead of the capsule is a spring loaded piston or diaphragm may be provided in the chamber 7 for supporting the by-pass valve m. This valve controls communication between the chamber 7' and a passage p leading from the inlet D. From the chamber a fuel can pass to an outlet q for connection to the pilot burner. Also the chamber :i communicates with the main fuel outlet 0 by way of a passage 1' extending between this outlet and the chamber outlet q, this passage being controlled by a spring loaded non-return valve s. Moreover, a relief passage t controlled by a spring loaded valve u is provided in communication with the chamber 7.
Starting of the prime mover is usually effected by an auxiliary motor. Assuming the manually operable valve 11 to be open the pump then supplies fuel past this valve to the main burner. At the same time fuel flows past the by-pass valve m and through the chamber 7' to the pilot burner. Should the pressure of the fuel supplied by the pump exceed some predetermined amount, the action of the pressure on the capsule k (or the piston or diaphragm) in the chamber 7' causes the same to move and allow the by-pass valve m to be moved by its spring n to close or restrict the fuel flow to the chamber and thus to the pilot burner. Consequently the supply of fuel to the pilot burner is effected at a substantially constant pressure. After ignition has been effected, the supply to the pilot burner is cut off by another valve (not shown), and the supply of fuel to the main burner is regulated as required by means of the manually operable valve d above described. When it is required to supply to the main burner only sumcient fuel to maintain combustion, as when the prime mover is idling, the manually operable valve d is closed. The required restricted supply to the main burner is then maintained by flow past the by-pass valve m and through the above mentioned passage 1' containing the non-return valve s.
In the modification shown in Figure 2, in which parts similar or analogous to those above described are indicated by the same reference characters sufiixed by l the manually operable valve (1 and its seating i are contained in a housing 1; which is separate and may be arranged at any convenient distance from the body part a containing the by-pass valve m and the chamber The housing 1: is provided with an inlet b for connection by piping w to the delivery side of a fuel supply pump or, and with an outlet c for connection by piping y to the main burner 2. The by-pass valve m comprises a closure member adapted to .co-operate with an annular seating at the inner end of an inlet passage p leading to the interior of the chamber 7' the outer end of this passage being adapted for connection to the piping w communicating with the delivery side of the pump a:. The closure member of the by-pass valve m is formed on or secured to a lever 2 which at one end is pivoted to the body part a, and at the other end is connected to the capsule is in the chamber 7' this capsule being open to the atmosphere, or wholly or partially evacuated, as in the previously described example. The chamber 7' is provided with an outlet q for connection by a pipe 3 to the pilot burner 4, this pipe having associated with it any convenient valve 5 for interrupting the supply of liquid fuel to the pilot burner after the prime mover has been started. Also the chamber is provided with a passage r for connection with the piping 1 leading to the main burner a, this passage being controlled by a nonretum valve s Moreover, the chamber i is also provided with a pressure relief passage t for connection by a pipe 6 to the inlet side of the pump :0, this passage being controlled by a spring loaded valve al The pump a: may be of the swash-plate or other suitable type, and may be controllable by barometric pressure through the medium of any convenient and known device I which is connected to the pump by pipes 8.
In operation the example shown in Figure 2 is essentially similar to that shown in Figure 1.
By this invention I am able to effect the required control of the supply of fuel to the main and pilot burners in a simple and satisfactory manner. The invention is not, however, limited to the examples described as subordinate details may be varied to suit different requirements.
Having thus described my invention what I claim as new and desire to secure by Letters Patent is:
1. Means for controlling the supply of liquid fuel to a prime mover of the kind specified, comprising in combination an inlet passage for liquid fuel under pressure, a main outlet passage for liquid fuel from said inlet passage, a subsidiary outlet passage for liquid fuel from said inlet passage, a manually operable valve for controlling liquid fuel flow from said inlet passage to said main outlet passage, a bypass valve for controlling liquid fuel flow from said inlet passage to said subsidiary outlet passage, a non-return valve operable by liquid fuel pressure at the outlet side of said by-pass valve for admitting a restricted supply of liquid fuel from the outlet side of said by-pass valveto said main outlet passage, and means for actuating said by-pass valve in response to liquid fuel pressure at the outlet side of said by-pass valve.
2. Means as claimed in claim 1 and having a hollow body part containing the manually operable valve, the by-pass valve, the non-return valve, and the means for actuating said by-pass valve. j
3. Means as claimed in claim 1 and having in combination a housing containing the manually operable valve and communicating with the inlet passage and main outlet passage, and a hollow body part containing the by-pass valve and its actuating means and communicating with the inlet passage and subsidiary outlet passage, the non-return valve being arranged between said main outlet passage and the interior of said hollow body part.
RICHARD JOSEPH IFIELD.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,394,807 Blanchard Oct. 25, 1921 1,554,869 McAndrews Sept. 22, 1925 FOREIGN PATENTS Number Country Date 645,284 France June 26. 1928
US737030A 1946-02-25 1947-03-25 Liquid fuel controlling means Expired - Lifetime US2483907A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2483907X 1946-02-25

Publications (1)

Publication Number Publication Date
US2483907A true US2483907A (en) 1949-10-04

Family

ID=10908086

Family Applications (1)

Application Number Title Priority Date Filing Date
US737030A Expired - Lifetime US2483907A (en) 1946-02-25 1947-03-25 Liquid fuel controlling means

Country Status (1)

Country Link
US (1) US2483907A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2698632A (en) * 1949-04-26 1955-01-04 Parker Appliance Co Control valve for single acting fluid motors

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1394807A (en) * 1920-12-04 1921-10-25 George N Blanchard Igniting and controlling device for hydrocarbon generators and burners
US1554869A (en) * 1923-12-20 1925-09-22 Mcandrews John Joseph Automatic fire-control and fuel-economizer system
FR645284A (en) * 1927-11-19 1928-10-23 Safety device for boilers heated by liquid or gaseous fuels

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1394807A (en) * 1920-12-04 1921-10-25 George N Blanchard Igniting and controlling device for hydrocarbon generators and burners
US1554869A (en) * 1923-12-20 1925-09-22 Mcandrews John Joseph Automatic fire-control and fuel-economizer system
FR645284A (en) * 1927-11-19 1928-10-23 Safety device for boilers heated by liquid or gaseous fuels

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2698632A (en) * 1949-04-26 1955-01-04 Parker Appliance Co Control valve for single acting fluid motors

Similar Documents

Publication Publication Date Title
US3177920A (en) Priming and venting arrangement for fuel feed system
US2668415A (en) Means for automatically controlling the supply of liquid fuel to prime movers
US2593884A (en) Oil burner nozzle
US3847537A (en) Air-atomizing fuel burner
US4388047A (en) Solenoid-operated pump
US2483907A (en) Liquid fuel controlling means
US2643915A (en) Oil burner nozzle
US2683485A (en) Liquid fuel controlling means for jet-engines, gas turbines, or like prime movers
US1488238A (en) Combustion apparatus
US2334220A (en) Fuel system
US3056257A (en) Rocket ignitor construction
US2552658A (en) Nozzle for gas turbines
US3591081A (en) Process and installation for burning liquified hydrocarbons
US2880790A (en) Starting fuel control for gas turbine engines
US2016449A (en) Carburetor
US2912696A (en) Combination oil and gas burner
US2012128A (en) Device for injecting fuel into internal combustion engines
US1752167A (en) Apparatus for preparing hydrocarbon mixtures for combustion
US1858264A (en) Device for burning liquid fuels
US3447315A (en) Fuel systems for gas turbine engines
US1648573A (en) Burner
US1483577A (en) Engine preheater
US2399783A (en) Fuel preheating device
US2197476A (en) Carburetor
US3397030A (en) Gas generating system