US2157737A - Fuel delivery apparatus for injection internal combustion engines - Google Patents

Fuel delivery apparatus for injection internal combustion engines Download PDF

Info

Publication number
US2157737A
US2157737A US154874A US15487437A US2157737A US 2157737 A US2157737 A US 2157737A US 154874 A US154874 A US 154874A US 15487437 A US15487437 A US 15487437A US 2157737 A US2157737 A US 2157737A
Authority
US
United States
Prior art keywords
fuel
pipe
valve
air
chamber
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
US154874A
Inventor
Janssen Johann Friedrich
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.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
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 Robert Bosch GmbH filed Critical Robert Bosch GmbH
Application granted granted Critical
Publication of US2157737A publication Critical patent/US2157737A/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
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M55/00Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
    • F02M55/007Venting means

Definitions

  • the invention relates to fuel delivery apparatus for injection internal combustion engines 'of the type having an air separator which is arranged between the delivery pump and the injection pumps; and from which the separator air, and in certain cases a portion of the excess fuel delivered by the delivery pump, discharges into an overflow pipe for the rest of the excess fuel which branches oil" from the suction chamber of the injection pump and leads back to the fuel container.
  • an overflow valve to provided which is previously adjusted to the I paratively low pressure desired in the suction chamber of the pump.
  • a corresponding resistance must be opposed to the outflow of the fuel through the air discharge pipe of the air separator. This can be done without supplementary members and pipe lines in a very simple way by ensuring that the air discharge pipe merges into the overflow pipe in ilront of the overflow valve so that the fuel returning in certain cases through the air discharge pipe does not find more favourable conditions for flowing away than the excess fuel which is flowing back via the suctionchamber of the pump.
  • an injection pump is attached to the injection nozzles of an internal combustion engine (not shown) by pressure pipes 2.
  • a fuel container 3 situated remote from the injection apparatus is connected by pipes with two delivery pumps t, which .take fuel from the-container in all running positions by means of a swinging pipe 3a.
  • the pipes are controlled by taps B.
  • Each of the two delivery pumps delivers rather more fuel than is taken at full load setting from the suction chamber la of the multi cylinder injection pump.
  • H denotes a hand pump for.filling the pipe line when the engine is at rest.
  • the delivery pumps deliver fuel through a common delivery pipe 5 to an air separator 6, which is connected with the suction chamber la through a pipe 1.
  • an overflow pipe 8 leads from the chamber la into a valve casing 9.
  • a pipe Ill provided with a throttle- Illa establishes communication between the air separator and a chamber 90. of the valve casing 9. The air separated by the air separator or part of the excess fuel delivered by the delivery pump flows through this pipe to the valve casing, from the chamber 9b of which a pipe H returns to the fuel container 3.
  • a back pressure valve i2 Adjacent the inlet of the overflow pipe 8 in the housing chamber 911 a back pressure valve i2 is arranged, the spindle of which is guided in a ring I3 and the plate of which is pressed on to its seat against the pipe 8 by a weakspring It.
  • the free end of the spring M abuts against the ring H! which is perforated.
  • the thicker shaft In the chamber 9a is guided the thicker shaft, provided with longitudinal passages, of a second or overflow valve l5 opening towards the casing chamber 912.
  • the plate of this overflow valve is pressed on its seat at the junction of the chambers 9a, 912, by means of a spring Hi.
  • This spring is tensioned to maintain a predetermined desired pressure in' the suction chamber Ia, by allowing the free end of l the spring It to abut against a screw cap H which closes the casing and can be adjusted externally.
  • the greater part of the fuel delivered thereby flows towards the suction chamber la via the pipe I.
  • the excess fuel not taken up by the separate pumps of the injection apparatus then flows back to the container 3 via the pipe 8, the back pressure valve l2, the overflow valve l5 and the pipe II.
  • valve l2 provides a definite though very small resistance to the return flow of the fuel from the suction chamber la, nevertheless the greatest part of the fuel delivered by both pumps leaves the air separator B via'the pipe 1. This is to be ascribed to the fact that in the other route, which leads through the air separator and the pipe ill to the valve casing 9, a means of resistance to the flow is provided, e. g., the throttle indicated in Ilia, which offers more resistance to the discharge of the fuel than the valve II.
  • the throttle I00 only permits a small portion of the excess fuel to flow back by avoiding the suction-chamber la.
  • the opposition offered to the fiow of the fuel stream must thus be less in the route through separator 6, the suction chamber la and the valve l2 than in the route through the separator and the pipe I 0.
  • the valve I2 is loaded accordingly.
  • Fuel delivery apparatus for injection internal combustion engines comprising, in combination, a fuel injection pump, a supply tank and a fuel delivery pump for pumping fuel from said supply tank to the inlet chamber of said injec- 5 tion pump, an air separator between the delivery pump and said inlet chamber, a pipe leading from the lower fuel-containing portion of the separator to the inlet chamber, an overflow conduit, connected with said inlet chamber and said 10 supply tank, a weakly-loaded back pressure valve arranged in said overflow conduit, said valve opening in the direction of the overflow, an additional higher-loaded back-pressure valve arranged in the overflow conduit between said flrst- 15 mentioned valve and the supply tank, and a connection between the upper part of said sep-' arator and that part of the overflow conduit situated between the two valves, the first weeklyloaded valve preventing the injection pump from .sucking air into the inlet chamber out of the space between the two valves while the second valve is so loaded that the desired fuel pressure is maintained within the system under working conditions.
  • Fuel delivery apparatus in which the connection between the upper part of the separator and that part of the overflow conduit situated between the two valves is so dimensioned, that the resistance ofiered by it to the flow of fuel is higher than the total resistance oflered to the flow of fuel by said pipe, said inlet chamber and said first-mentioned valve.
  • Fuel delivery apparatus in which two fuel delivery pumps are arranged for pumping fuel from supply to the inlet chamber of said one injection pump, each'of said fuel delivery pumps being so dimensioned that it pumps an amount of fuel which is greater 4 than the maximum fuel amount required by said injection pump at full load of the engine.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Description

y 9, 1939- J. F. JANSSEN 7 2,157,737
FUEL DELIVERY APPARATUS FOR INJECTION INTERNAL COMBUSTION ENGINES Filed July 21, 1937 Ill ate-rated ay 9, i939 FUEL DELIVERY APPARATUS FOR INJEC- TION EXTERNAL COUSTION ENGINES Joh Friedrich .l'anssen, Stuttgart, Germany, assignor to Robert Bosch Gesellschaft mit beschriinkter Haftung Application .iuly 21, 1937, Serial No. 154,874
i In Germany July 15, 1936 3 Eiaims. (Cl. 123139) The invention relates to fuel delivery apparatus for injection internal combustion engines 'of the type having an air separator which is arranged between the delivery pump and the injection pumps; and from which the separator air, and in certain cases a portion of the excess fuel delivered by the delivery pump, discharges into an overflow pipe for the rest of the excess fuel which branches oil" from the suction chamber of the injection pump and leads back to the fuel container.
In this overflow pipe an overflow valve to provided which is previously adjusted to the I paratively low pressure desired in the suction chamber of the pump. In order that the desired pressure may be maintained in the suction chamber of the injection pump a corresponding resistance must be opposed to the outflow of the fuel through the air discharge pipe of the air separator. This can be done without supplementary members and pipe lines in a very simple way by ensuring that the air discharge pipe merges into the overflow pipe in ilront of the overflow valve so that the fuel returning in certain cases through the air discharge pipe does not find more favourable conditions for flowing away than the excess fuel which is flowing back via the suctionchamber of the pump. It has however been noticed that in apparatus of this kind, particularly when they are used for engines, such as aircraft engines, which are variable in position, air bubbles from the overflow pipe reach the suction chamber of the injection pump and lead to interruptions in delivery. To prevent such air bubbles reaching the suction chamber of the injection pump a back pressure .valve is provided according to the invention before the point where the air discharge pipe of the air separator merges into the overflow pipe; this valve opens even when there is only a very small flow back to the fuel container, but prevents a flowback from the branch of the overflow pipe situated behind it to the suction chamber of the injection pipe.
The invention is more particularly described with reference to the accompanying drawing which shows diagrammatically one form of fuel delivery apparatus with an air separator according to this invention.
In the drawing an injection pump is attached to the injection nozzles of an internal combustion engine (not shown) by pressure pipes 2. A fuel container 3 situated remote from the injection apparatus is connected by pipes with two delivery pumps t, which .take fuel from the-container in all running positions by means of a swinging pipe 3a. The pipes are controlled by taps B. Each of the two delivery pumps delivers rather more fuel than is taken at full load setting from the suction chamber la of the multi cylinder injection pump. H denotes a hand pump for.filling the pipe line when the engine is at rest.
The delivery pumps deliver fuel through a common delivery pipe 5 to an air separator 6, which is connected with the suction chamber la through a pipe 1. From the side of the suction chamber opposite to the mouth of the pipe I, an overflow pipe 8 leads from the chamber la into a valve casing 9. A pipe Ill provided with a throttle- Illa establishes communication between the air separator and a chamber 90. of the valve casing 9. The air separated by the air separator or part of the excess fuel delivered by the delivery pump flows through this pipe to the valve casing, from the chamber 9b of which a pipe H returns to the fuel container 3.
Adjacent the inlet of the overflow pipe 8 in the housing chamber 911 a back pressure valve i2 is arranged, the spindle of which is guided in a ring I3 and the plate of which is pressed on to its seat against the pipe 8 by a weakspring It. The free end of the spring M abuts against the ring H! which is perforated. In the chamber 9a is guided the thicker shaft, provided with longitudinal passages, of a second or overflow valve l5 opening towards the casing chamber 912. The plate of this overflow valve is pressed on its seat at the junction of the chambers 9a, 912, by means of a spring Hi. This spring is tensioned to maintain a predetermined desired pressure in' the suction chamber Ia, by allowing the free end of l the spring It to abut against a screw cap H which closes the casing and can be adjusted externally. In the absence of air in the excess fuel delivered by both pumps to the air separator ii, the greater part of the fuel delivered thereby flows towards the suction chamber la via the pipe I. The excess fuel not taken up by the separate pumps of the injection apparatus then flows back to the container 3 via the pipe 8, the back pressure valve l2, the overflow valve l5 and the pipe II. The valve l2 provides a definite though very small resistance to the return flow of the fuel from the suction chamber la, nevertheless the greatest part of the fuel delivered by both pumps leaves the air separator B via'the pipe 1. This is to be ascribed to the fact that in the other route, which leads through the air separator and the pipe ill to the valve casing 9, a means of resistance to the flow is provided, e. g., the throttle indicated in Ilia, which offers more resistance to the discharge of the fuel than the valve II.
The throttle I00. only permits a small portion of the excess fuel to flow back by avoiding the suction-chamber la. The opposition offered to the fiow of the fuel stream must thus be less in the route through separator 6, the suction chamber la and the valve l2 than in the route through the separator and the pipe I 0. The valve I2 is loaded accordingly.
If air is contained in the fuel entering the air separator, such as for example inthe event of one of the two delivery pumps becoming slack, or because the container is nearly empty, the excess fuel diminishes corresponding to the air content, since of course the pump always delivers a constant quantity. Not a very great excess amount of fuel, therefore, can flow away through the pipe 8, for the air content of what the pump delivers is separated in the air separator and flows into the chamber 9a of the valve casing through the pipe Hi. The throttle Illa does not offer any material resistance to the discharging air. Thus the state may arise that the return flow through the pipe 8 decreases so sharply that separated air might penetrate into the suction chamber I a, if it were not prevented by the valve It is possible to imagine that even when the back pressure valve is open and a small return flow of fuel occurs through the pipe 8, particles of air might nevertheless float throughnthe valve opening towards the suction chamber against the return of fuel. To avoid this the exit end of the pipe 8 is made so narrow at least at the point where it opens into the chamber 9a, that only a speed of fuel flow, sufficient to prevent air particles floating through it, prevails irrespective of how small the amount of fuel overflow obtains at any time.
I declare that what If claim is:
1. Fuel delivery apparatus for injection internal combustion engines, comprising, in combination, a fuel injection pump, a supply tank and a fuel delivery pump for pumping fuel from said supply tank to the inlet chamber of said injec- 5 tion pump, an air separator between the delivery pump and said inlet chamber, a pipe leading from the lower fuel-containing portion of the separator to the inlet chamber, an overflow conduit, connected with said inlet chamber and said 10 supply tank, a weakly-loaded back pressure valve arranged in said overflow conduit, said valve opening in the direction of the overflow, an additional higher-loaded back-pressure valve arranged in the overflow conduit between said flrst- 15 mentioned valve and the supply tank, and a connection between the upper part of said sep-' arator and that part of the overflow conduit situated between the two valves, the first weeklyloaded valve preventing the injection pump from .sucking air into the inlet chamber out of the space between the two valves while the second valve is so loaded that the desired fuel pressure is maintained within the system under working conditions.
2. Fuel delivery apparatus according to claim 1, in which the connection between the upper part of the separator and that part of the overflow conduit situated between the two valves is so dimensioned, that the resistance ofiered by it to the flow of fuel is higher than the total resistance oflered to the flow of fuel by said pipe, said inlet chamber and said first-mentioned valve.
3. Fuel delivery apparatus according to claim 1, in which two fuel delivery pumps are arranged for pumping fuel from supply to the inlet chamber of said one injection pump, each'of said fuel delivery pumps being so dimensioned that it pumps an amount of fuel which is greater 4 than the maximum fuel amount required by said injection pump at full load of the engine.
JOHANN FRIEDRICH JAIiSSEN.
US154874A 1936-07-15 1937-07-21 Fuel delivery apparatus for injection internal combustion engines Expired - Lifetime US2157737A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2157737X 1936-07-15

Publications (1)

Publication Number Publication Date
US2157737A true US2157737A (en) 1939-05-09

Family

ID=7987760

Family Applications (1)

Application Number Title Priority Date Filing Date
US154874A Expired - Lifetime US2157737A (en) 1936-07-15 1937-07-21 Fuel delivery apparatus for injection internal combustion engines

Country Status (1)

Country Link
US (1) US2157737A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2438311A (en) * 1944-05-15 1948-03-23 Carter Carburetor Corp Pump discharge fitting
US2513992A (en) * 1942-04-03 1950-07-04 Borg Warner High altitude fuel system
US2521270A (en) * 1945-01-10 1950-09-05 Sebem S A Apparatus for feeding liquid fuel to internal-combustion engines
US2580696A (en) * 1945-11-13 1952-01-01 Gen Motors Corp Engine fuel system
US2599699A (en) * 1947-05-13 1952-06-10 Gen Motors Corp Fuel system for combustion apparatus
US2608247A (en) * 1947-01-20 1952-08-26 Dowty Equipment Ltd Fuel supply system for spill type burners
US2740469A (en) * 1950-04-14 1956-04-03 Chrysler Corp Flow control apparatus
US2818111A (en) * 1954-12-10 1957-12-31 Ralph R Ross Automatic fuel control
US2983311A (en) * 1955-11-15 1961-05-09 Daimler Benz Ag Fuel-tank connecting assembly
US3267987A (en) * 1962-11-30 1966-08-23 Webasto Werk Baier Kg W Supply of fuel to burners more especially for vehicle heaters
US5015160A (en) * 1988-06-18 1991-05-14 Robert Bosch Gmbh Injection pump for internal combustion engines

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2513992A (en) * 1942-04-03 1950-07-04 Borg Warner High altitude fuel system
US2438311A (en) * 1944-05-15 1948-03-23 Carter Carburetor Corp Pump discharge fitting
US2521270A (en) * 1945-01-10 1950-09-05 Sebem S A Apparatus for feeding liquid fuel to internal-combustion engines
US2580696A (en) * 1945-11-13 1952-01-01 Gen Motors Corp Engine fuel system
US2608247A (en) * 1947-01-20 1952-08-26 Dowty Equipment Ltd Fuel supply system for spill type burners
US2599699A (en) * 1947-05-13 1952-06-10 Gen Motors Corp Fuel system for combustion apparatus
US2740469A (en) * 1950-04-14 1956-04-03 Chrysler Corp Flow control apparatus
US2818111A (en) * 1954-12-10 1957-12-31 Ralph R Ross Automatic fuel control
US2983311A (en) * 1955-11-15 1961-05-09 Daimler Benz Ag Fuel-tank connecting assembly
US3267987A (en) * 1962-11-30 1966-08-23 Webasto Werk Baier Kg W Supply of fuel to burners more especially for vehicle heaters
US5015160A (en) * 1988-06-18 1991-05-14 Robert Bosch Gmbh Injection pump for internal combustion engines

Similar Documents

Publication Publication Date Title
US2157737A (en) Fuel delivery apparatus for injection internal combustion engines
US7303378B2 (en) Apparatus for delivering fuel from a tank to an internal combustion engine
KR101696498B1 (en) Fuel system for an internal combustion engine
JP2002526716A (en) Pump device that generates high fuel pressure
US11073058B2 (en) Device for supplying a fluid at risk of freezing to the combustion chambers of an internal combustion engine
US7082931B2 (en) Fuel module
US2215469A (en) Fuel delivery pump system for injection internal combustion engines
US7219659B2 (en) Fuel injection system comprising a pressure intensifier and a delivery rate-reduced low-pressure circuit
US3635604A (en) Equipment for delivering liquid, particularly oil burners
US2521270A (en) Apparatus for feeding liquid fuel to internal-combustion engines
US4546745A (en) Fuel pumping apparatus
US3181468A (en) Fuel supply system
US2950709A (en) Injection devices including a reciprocating piston injection pump
CN208595026U (en) Fuel injection system and its fuel feeding pump assembly
US2215756A (en) Fuel delivery apparatus for injection internal combustion engines
CN1304747C (en) Priming system for an engine carburetor
US3066922A (en) Carburetors
US2874766A (en) Liquid fuel supply systems for gas turbine engines
US2991055A (en) Fuel injection system
US5806560A (en) Aircraft fuel transfer pump with auxiliary fuel line scavenge pump
US2214766A (en) Injection pump for internal combustion engines
US1944320A (en) Fuel pump for internal combustion engines
US3427981A (en) Gear pump with valve mechanism
US2839000A (en) Fuel injection device
US4846308A (en) Liquid feed pump system