US2996054A - Fuel containers in reciprocating cylinders of internal combustion engines - Google Patents

Fuel containers in reciprocating cylinders of internal combustion engines Download PDF

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US2996054A
US2996054A US822893A US82289359A US2996054A US 2996054 A US2996054 A US 2996054A US 822893 A US822893 A US 822893A US 82289359 A US82289359 A US 82289359A US 2996054 A US2996054 A US 2996054A
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fuel
chamber part
piston
pump
internal combustion
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US822893A
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Lang Anton
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Delmag Maschinenfabrik Reinhold Dornfeld GmbH and Co
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Delmag Maschinenfabrik Reinhold Dornfeld GmbH and Co
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B7/00Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
    • F01B7/20Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders with two or more pistons reciprocating one within another, e.g. one piston forming cylinder of the other
    • EFIXED CONSTRUCTIONS
    • E02HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
    • E02DFOUNDATIONS; EXCAVATIONS; EMBANKMENTS; UNDERGROUND OR UNDERWATER STRUCTURES
    • E02D7/00Methods or apparatus for placing sheet pile bulkheads, piles, mouldpipes, or other moulds
    • E02D7/02Placing by driving
    • E02D7/06Power-driven drivers
    • E02D7/12Drivers with explosion chambers
    • E02D7/125Diesel drivers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B59/00Internal-combustion aspects of other reciprocating-piston engines with movable, e.g. oscillating, cylinders

Definitions

  • This invention relates to a system for removing gas from the fuel in reciprocating fuel'containers of internal combustion engines, more particularly fuel containers of; internal combustion hammers, which containers communi-- cate with the injection pump.
  • the internal chamber of the fuel container is subdivided into two'chamber parts.
  • her part and'which completely fills this part is free from 40 air. Moreover the narrow passages prevent the. fuel. located in the lower chamber part from flowingupwards unchecked as soon as the hammer body duringits rapid. ascent has its upward movement retarded by picking up the hammer piston or by frictional resistancesof the inclination and separating the two chambers parts, and.
  • Tlie passages disposedin the bottom. region of fth'e. intermediate. walll may advantageously be; formed by a narrow annular gap located .between the bot-.- tom endof the intermediate walland a.holder of. the. injectionipump.
  • the additional passages-disposed in. the. top region of theintermediate wall are preferablyformed; as narrow bores merging into widened portionsextend ing towards the lower chamberpart. But.the..additional passages can also be united to form .a .narrowannular gap. which widens towards the lower chamber part.
  • the inter-- mediate wall surrounding, the holder of the injection pump: and 'extendingdownwards towards th'isholder may advantageously have conical bounding; surfaces... Alterna tively, however, this wall 'mayconsist of a.disc inserted: into the fuel'container and forming narrow. gaps in come binationwith the holder of 'theinjecti-onpump. andwithz the vlateral"boundary wall of' the fuel container.
  • Thelbottom. boundary surface of the-lower chamber part mayprefer. ablyhave a region which descends-towards theJateral. boundary wall of that part and;advantageously-:iswfm conical shape, and'is downwardly ofl'set, through..a.certain distance, with respect to thefuelsupply b'oresof the: injection pump.
  • injection pump By meansof this construction,..maintenance of "the flow of 'fuel'to the supply bores-oftheline. jection pump is ensured even duringtheretardation that. takes place during the laststage. of the rapid-ascentof. the hammer body, since only a very smallkpartlofthe.
  • 1 is a hammer body surroundinga fuel container and having a lower part .1 in. whichwa-t piston 2 of an internal combustion.
  • hammer isguidede
  • An injection pump 3 is secured, by means of a holder. 3. screwed into the hammer body 1, in.a-.cylinder.head formed by the upper part of the hammer. body. 3.! is"; the piston of the injection pump.
  • the injection pump, .of..' which the axis coincides with that ofthe hammer body and of the fuel container in the'ambodiments illustrated, may alternatively be arranged eccentrically,' i.e.
  • the internal chamber of the fuel container is subdi- 3 vided into two chamber parts A and A which are disposed one above the other and communicate with one another through narrow passages 7.
  • the passages may be formed by one or more narrow bores arranged for instance in a ring or may alternatively be constructed as a narrow annular gap.
  • additional narrow passages 11 are provided which are located in the top region 10 of this intermediate Wall.
  • the passages 7 disposed in the bottom region 8 of the intermediate wall 9 are formed by a narrow annular gap located between the bottom end of the intermediate wall and the holder 3 of the injection pump 3, whereas the additional passages 11 located in the top region 10 of the intermediate wall 9 consist of a ring of narrow bores merging into widened portions 12 extending towards the lower chamber part A.
  • the intermediate wall 9 surrounding the holder 3' of the injection pump 3 and extending downwards towards this holder has conical bounding surfaces 13 and 14.
  • the strength of the spring shown in the drawing, which bears at one end against the plate-shaped end of the large piston and at the other end against the holder 3, is made such that the spring permits relative displacement between the said large piston and the hammer body as indicated above, but subsequently brings the said large piston and therefore the pump piston 3" back into the position, relative to the hammer body 1, which is shown in the drawing.
  • the additional passages 11' are also united to form a narrow annular gap which widens towards the lower chamber part A.
  • the intermediate wall consists of a disc 9' inserted into the fuel container and forming narrow gaps 7 and 11' in combination with the holder 3' of the injection pump 3 and with the lateral boundary wall 15 of the fuel container; the disc has ribs 16 which project beyond its outer periphery, and is supported, through the intermediary of these ribs, on a projection 17 formed on the lateral boundary wall 15 of the container.
  • a compression spring 18 arranged for instance between the injection pump holder 3' and the ribs 16 secures the disc 9 in the position shown in the drawing.
  • the bottom boundary surface 19 of this chamber part has a region 20 which descends towards the lateral boundary wall 15 of this part and advantageously is of conical shape, and is downwardly offset, through a distance h, with respect to the fuel supply bores 6.
  • the hammer body After expansion has ended, the hammer body is retarded by the piston friction and still more by picking up the piston, but this retardation of the hammer body mainly atfects the fuel located in the upper chamber part A.
  • the magnitude of the retardation exceeds that of gravitational acceleration, the liquid level in the upper chamber part A is reversed, and intensive intermingling with air takes place.
  • the fuel enclosed in the lower chamber part A only a small portion of this fuel can pass through the passages 7 and 11 or 11 into the upper chamber part A, and at the same time a vacuum v (FIGURE 2) lasting only a brief period of time is formed;
  • an upwardly and downwardly reciprocable power cylinder a power piston slidably mounted in said cylinder, a cylinder head on said power cylinder above said piston, a fuel chamber formed in said cylinder head, a downwardly and inwardly inclined annular intermediate wall having an upper and a lower extremity and dividing said chamber into an upper chamber part above said wall and a lower chamber part beneath said wall, first permanently narrow passage means disposed adjacent said upper extremity and providing communication between said upper and lower chamber parts, second permanently narrow passage means disposed adjacent said lower extremity and providing communication between said upper and lower chamber parts, and an injection pump adapted to communicate with said lower chamber part and to inject fuel into said power cylinder.
  • annular disc forming said intermediate wall, a holder accommodating said injection pump and extending through said disc, a first annular gap located between said disc and said cylinder head and constituting said first narrow passage means, and a second annular gap located between said disc and said holder and constituting said second narrow passage means.
  • an upwardly and downwardly reciprocable power cylinder a power piston slidably mounted in said power cylinder, a cylinder head on said power cylinder above said power piston, a fuel chamber formed in said cylinder head and divided into an upper chamber part and a lower chamber part beneath said upper chamber part, said lower chamber part having a bottom surface which is adjacent to said piston and comprises a downwardly and outwardly inclined frusto conical portion, and a top surface adjacent to said upper chamber part, passage means providing communication between said upper and lower parts, said passage means being at all times sufliciently narrow to prevent bubbles from passing from said upper part into said lower part, an injection pump having an injection cylinder and an injection piston accommodated in said injection cylinder and slidable relatively to said injection cylinder, and duct means disposed wholly above said bottom surface of said lower chamber part and adapted to provide communication between said lower chamber part and said injection cylinder, whereby retardation of said power cylinder during upward movement thereof will cause said injection cylinder to be filled with fuel under pressure.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Mining & Mineral Resources (AREA)
  • Paleontology (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Fuel-Injection Apparatus (AREA)

Description

2,996,054 IPROCATING CYLINDERS USTION ENGINES Aug. 15, 1961 A. LANG FUEL CONTAINERS IN REC OF INTERNAL COMB Filed June FIG. 7
United States. Patent f h FUEL CONTAINERS IN RECIIPRD'CAIING'CYLIN-' DERS OF INTERNAL COMBUSTION EN Anton Lang,.Hartberg, Steiermark,.Austria,- assignor to' 5 Delmag MaschinenfabrikReinhold Dornfeld, Esslingen (Neckar), Germany.
Filed June 25, 1959', Sen-No. 822,893 Claims priority, application Austria July.10,-.195 8 7 Claims. (Cl. 1239- 139) This invention relates to a system for removing gas from the fuel in reciprocating fuel'containers of internal combustion engines, more particularly fuel containers of; internal combustion hammers, which containers communi-- cate with the injection pump.
In internal combustion hammers and stampers, in which: both the fuel container and alsothemembers usedfor inje'cting the fuel into the workingcylindenare accommodated in parts that jump during operation, the problem of.
the removal of gas from the fuel is particularlyim-.
portant, because the fuel is shaken together with air toaparticularly large extent owing to the reciprocatingmovement of the fuel container, and any airor. gas bubble.in-.- volves the risk of trouble in operation. Experiencehas.
shown. that filters placed in front of thefuel supply bores provided in the injection pump cannot obviate. these. defects.
Accordingto-the invention, the internal chamber of the fuel container is subdivided into two'chamber parts.
disposed one above the other and communicating with one another through-narrow passages; in certaincases the. passages maybe united to form a narrow annular gap.. The fuel which is in the upper chamber part and which. during operation is permeated by air owing to the .con-
tinuous reciprocating movement, gives up its air bubbles on passing into the lower chamber part, so that the small; air bubblesremain'behind in the upper chamber part, and the liquid fuel which has passed through the narrowpassages or through the annular gap into the lower cham:
her part and'which completely fills this part, is free from 40 air. Moreover the narrow passages prevent the. fuel. located in the lower chamber part from flowingupwards unchecked as soon as the hammer body duringits rapid. ascent has its upward movement retarded by picking up the hammer piston or by frictional resistancesof the inclination and separating the two chambers parts, and.
additional passages may be provided in the topregion of this intermediate wall. This construction not only prevents air bubbles from getting from theupperintothe lower chamber part but also at the same time ensures the.
separation of any air or gas particles that may have gotten.
into the lower chamber part in any way. For instance it is quite possible even if the internal combustion engine of the hammer is operating satisfactorily in other respects, that compressed air or combustion gases may occasionally get out'ofthe combustion chamber, past the non-return valveoftheinjection pump and through the fuel supply boresofthis-pump, into the lower chamber part of the container. The air or gas bubbles expanding in this chamber: partrise in the fuel to the top region ofthe intermediatewall-and from there pass out through the. 7 0
additional narrowpassages into theupperrchamben'part," whereby re-entry of these air or gas bubbles into the in- Patented Aug, 1.5.;v 1 9.61-.
2 jection pump-is prevented; this re-entry would cause. troublein operation. Tlie passages disposedin the bottom. region of fth'e. intermediate. walllmay advantageously be; formed by a narrow annular gap located .between the bot-.- tom endof the intermediate walland a.holder of. the. injectionipump. The additional passages-disposed in. the. top region of theintermediate wall are preferablyformed; as narrow bores merging into widened portionsextend ing towards the lower chamberpart. But.the..additional passages can also be united to form .a .narrowannular gap. which widens towards the lower chamber part. The inter-- mediate wall surrounding, the holder of the injection pump: and 'extendingdownwards towards th'isholdermay advantageously have conical bounding; surfaces... Alterna tively, however, this wall 'mayconsist of a.disc inserted: into the fuel'container and forming narrow. gaps in come binationwith the holder of 'theinjecti-onpump. andwithz the vlateral"boundary wall of' the fuel container.
In order to vensure that any compressed. air or com bustion gases. getting through during temporarily faulty. operation of "the non-return valve of the injection pump,- can fi'ow away unhindered into. the. upper. chamber part,. itis advisable to make the fuel supply ductsof the injec tion pump, which extends through the lower chamber part, lead directly from this lower chamberpart, whereby. the. distance from the internal chamber. of..the.- pump. to. the fuel container is reduced to a minimum, .in-contra-.- distinction to. constructions used heretofore inwhich the: communication between the fuel container and. the inter.-. nal chamber of'the pump, was usuallyestablished... by means of'ditferent bores which were relativelyrlong. and in some cases bent at.angles to one another. Thelbottom. boundary surface of the-lower chamber part mayprefer. ablyhave a region which descends-towards theJateral. boundary wall of that part and;advantageously-:iswfm conical shape, and'is downwardly ofl'set, through..a.certain distance, with respect to thefuelsupply b'oresof the: injection pump. By meansof this construction,..maintenance of "the flow of 'fuel'to the supply bores-oftheline. jection pump is ensured even duringtheretardation that. takes place during the laststage. of the rapid-ascentof. the hammer body, since only a very smallkpartlofthe. fuel' that completely fills the lowerchamber. part.-.and-.. is .pressed. against the. intermediate wall during .the..reev tardation period, passes through thenarrow passages-into: the upper chamber part, whereby a vacuum'lasting only for a brief length of time is formed in theregion of thelower boundary surface of the lower chamber part, but extends only over" the preferably. comically descending, boundary surface region and'is unable, because, of, the. fact that this region is vertically offset with. respectuto the fuel supply bores, to spread as far as thesesupply. bores.
Vertical sections throughtwo embodiments of the;.in.-. vention chosen by way of'example are shbwn:in ..FIG.- URES l and 2' of the accompanyingdrawings.
In these drawings, 1 is a hammer body surroundinga fuel container and having a lower part .1 in. whichwa-t piston 2 of an internal combustion. hammer isguidede An injection pump 3 is secured, by means of a holder. 3. screwed into the hammer body 1, in.a-.cylinder.head formed by the upper part of the hammer. body. 3.! is"; the piston of the injection pump. The injection pump, .of..' which the axis coincides with that ofthe hammer body and of the fuel container in the'ambodiments illustrated, may alternatively be arranged eccentrically,' i.e. offset: laterally.- 4 is a non-returnvalve'provided'attheinjec tion pump nozzle, and 5 is the internal chamber oftheinjection pump, which chamber is locatedbetween that valve: andsthe pump 'piston ii fuel supplybores=-6 lead into .this'xchamber.
The internal chamber of the fuel container is subdi- 3 vided into two chamber parts A and A which are disposed one above the other and communicate with one another through narrow passages 7. The passages may be formed by one or more narrow bores arranged for instance in a ring or may alternatively be constructed as a narrow annular gap. In addition to the passages 7 disposed in the bottom region 8 of the intermediate wall 9 separating the two chamber parts A and A and extending at an inclination, additional narrow passages 11 are provided which are located in the top region 10 of this intermediate Wall. In the embodiment illustrated in FIGURE 1, the passages 7 disposed in the bottom region 8 of the intermediate wall 9 are formed by a narrow annular gap located between the bottom end of the intermediate wall and the holder 3 of the injection pump 3, whereas the additional passages 11 located in the top region 10 of the intermediate wall 9 consist of a ring of narrow bores merging into widened portions 12 extending towards the lower chamber part A. The intermediate wall 9 surrounding the holder 3' of the injection pump 3 and extending downwards towards this holder has conical bounding surfaces 13 and 14.
The large piston above and integral with pump piston 3 is guided in the hollow cylindrical holder 3', so that the pump piston 3" connected to this large piston is satisfactorily alined. The pump piston 3" therefore does not need to be guided'in the cylinder of the injection pump 3:, that is to say, this cylinder does not have to perform the function of maintaining the piston 3" in correct alinement. The piston 3" can therefore slide up and down in the pump cylinder, making sealing contact with the inside surface of the cylinder, and does not have to be supported by the pump cylinder against any transverse forces that may arise, since these forces are absorbed by the holder 3" surrounding the large piston integral with piston 3". The pump piston 3" therefore wears only to a practically negligible extent, and therefore continues always to ensure a constant injection pressure and therefore a correct quantity of injected fuel, even after this piston 3" has been in use for a long time.
' During upward movement of the said large piston, fuel is sucked into the annular space between the pump piston 3" and the internal surface of the holder 3', through the transverse bores shown in the drawing, which are provided between the said annular space and the chamber part A. During subsequent descent of the large piston, the pressure in said annular space rises, whereby the fuel that has been sucked in is mostly forced back into the chamber part A, but some of this fuel is forced upwards into the sliding clearance between the large piston and the holder 3. This ensures very satisfactory lubrication of the large piston.
In addition to this, the said large piston has another special function. This large piston causes injection to occur, in the following manner.
The downward movement of the hammer body 1 is retarded as soon as the power piston 2 strikes against the pile that is being hammered. The air in the combustion chamber above the piston 2 is then compressed, and this brakes the further downward movement of the hammer body 1. But the large piston integral with the piston 3 is slidable in the hammer body and tends to follow the force of gravity, i.e. to continue its descent. The strength of the spring, shown in the drawing, which bears at one end against the plate-shaped end of the large piston and at the other end against the holder 3, is made such that the spring permits relative displacement between the said large piston and the hammer body as indicated above, but subsequently brings the said large piston and therefore the pump piston 3" back into the position, relative to the hammer body 1, which is shown in the drawing.
In the embodiment illustrated in FIGURE 2, the additional passages 11' are also united to form a narrow annular gap which widens towards the lower chamber part A. The intermediate wall consists of a disc 9' inserted into the fuel container and forming narrow gaps 7 and 11' in combination with the holder 3' of the injection pump 3 and with the lateral boundary wall 15 of the fuel container; the disc has ribs 16 which project beyond its outer periphery, and is supported, through the intermediary of these ribs, on a projection 17 formed on the lateral boundary wall 15 of the container. A compression spring 18 arranged for instance between the injection pump holder 3' and the ribs 16 secures the disc 9 in the position shown in the drawing.
The fuel supply bores 6 of the injection pump 3, which extends through the lower chamber part A, lead directly from this lower chamber part. The bottom boundary surface 19 of this chamber part has a region 20 which descends towards the lateral boundary wall 15 of this part and advantageously is of conical shape, and is downwardly offset, through a distance h, with respect to the fuel supply bores 6.
The manner of operation of the apparatus is as follows:
When the fuel container is stationary, that is to say,
when the hammer body in the present embodiments is stationary, fuel introduced into the upper chamber part A is freed from gas on passing through the narrow passages, so that only fuel that is completely free from air can get into the lower chamber part A, the fuel supply bores 6 and the internal chamber 5 of the pump and down to the non-return valve 4. Since the level of the liquid in the upper chamber part A then descends because of the consumption of fuel during the operation of the hammer, as a rule the upper chamber part is only partly full of fuel. By the retardation of the downward 1 movement of the hammer body 1 and subsequent upthe chamber parts A and A is forced with considerable pressure, by its own inertia, against the container walls surrounding the fuel, whereby air or gas bubbles in the fuel are urged rapidly upwards. Because of the inclined direction of the intermediate wall 9 of the disc 9', the
r rising air or gas bubbles in the lower chamber part A are guided towards the top region of the intermediate wall or disc, and from there the bubbles pass through the additional narrow passages 11 or the narrow annular gap 11' into the upper chamber part A, and at the same time fuel flows from the upper to the lower chamber part through the narrow annular gaps 7. Furthermore, during the reciprocating movement of the hammer body and the consequent alternation between acceleration and retardation, the displacement of the the air and gas bubbles towards the lateral boundary wall 15 of the lower chamber part A is also assisted by the conical region 20 of the lower boundary surface 19 of the chamber A, which region is inclined downwards towards that boundary wall. As indicated in FIGURE 1, the liquid column H causes gas bubbles, which occasionally expand into the lower chamber part A through the injection pump, to rise through the narrow passages 11 or 11.
After expansion has ended, the hammer body is retarded by the piston friction and still more by picking up the piston, but this retardation of the hammer body mainly atfects the fuel located in the upper chamber part A. When the magnitude of the retardation exceeds that of gravitational acceleration, the liquid level in the upper chamber part A is reversed, and intensive intermingling with air takes place. But as regards the fuel enclosed in the lower chamber part A, only a small portion of this fuel can pass through the passages 7 and 11 or 11 into the upper chamber part A, and at the same time a vacuum v (FIGURE 2) lasting only a brief period of time is formed;
scending region 20 of the lower boundary surface 19 of the lower chamber part A and does not extend as far as the fuel supply bores 6 of the injection pump 3, whereby the filling of the injection pump without air bubbles is ensured.
The liquid level in the upper chamber part A will have returned to normal before the hammer body 1 falls back, so that during the descent fuel can again flow from A to A at the beginning of the compression period, whereby the lower chamber part A is again completely filled with fuel and any air or gas bubble that may be present are forced through the additional passages 11 or 11' into the upper chamber part A. Therefore, however abrupt the alternation between acceleration and retardation may be, the apparatus according to the invention ensures steady uninterrupted feeding of the injection pump with fuel that is completely freed from gas, and consequently also ensures completely satisfactory operation of the equipment.
What is claimed is:
1. In an internal combustion engine, an upwardly and downwardly reciprocable power cylinder, a power piston slidably mounted in said cylinder, a cylinder head on said power cylinder above said piston, a fuel chamber formed in said cylinder head, a downwardly and inwardly inclined annular intermediate wall having an upper and a lower extremity and dividing said chamber into an upper chamber part above said wall and a lower chamber part beneath said wall, first permanently narrow passage means disposed adjacent said upper extremity and providing communication between said upper and lower chamber parts, second permanently narrow passage means disposed adjacent said lower extremity and providing communication between said upper and lower chamber parts, and an injection pump adapted to communicate with said lower chamber part and to inject fuel into said power cylinder.
2. In an internal combustion engine as claimed in claim 1, a holder extending through said intermediate wall and accommodating said injection pump, and a narrow annular gap located between said lower extremity of said intermediate wall and said holder and constituting said second permanently narrow passage means.
3. In an internal combustion engine as claimed in claim 1, narrow bores formed in said intermediate wall near said upper extremity thereof and merging into widened portions extending towards said lower chamber 6 part, said bores constituting said first permanently narrow passage means.
4. In an internal combustion engine as claimed in claim 1, an annular gap widening towards said lower chamber part and constituting said first passage means.
5. In an internal combustion engine as claimed in claim 1, an upper and a lower frusto-conical bounding surface on said intermediate wall.
'6. In an internal combustion engine as claimed in claim 1, an annular disc forming said intermediate wall, a holder accommodating said injection pump and extending through said disc, a first annular gap located between said disc and said cylinder head and constituting said first narrow passage means, and a second annular gap located between said disc and said holder and constituting said second narrow passage means.
7. In an internal combustion engine, an upwardly and downwardly reciprocable power cylinder, a power piston slidably mounted in said power cylinder, a cylinder head on said power cylinder above said power piston, a fuel chamber formed in said cylinder head and divided into an upper chamber part and a lower chamber part beneath said upper chamber part, said lower chamber part having a bottom surface which is adjacent to said piston and comprises a downwardly and outwardly inclined frusto conical portion, and a top surface adjacent to said upper chamber part, passage means providing communication between said upper and lower parts, said passage means being at all times sufliciently narrow to prevent bubbles from passing from said upper part into said lower part, an injection pump having an injection cylinder and an injection piston accommodated in said injection cylinder and slidable relatively to said injection cylinder, and duct means disposed wholly above said bottom surface of said lower chamber part and adapted to provide communication between said lower chamber part and said injection cylinder, whereby retardation of said power cylinder during upward movement thereof will cause said injection cylinder to be filled with fuel under pressure.
References Cited in the file of this patent UNITED STATES PATENTS
US822893A 1958-07-10 1959-06-25 Fuel containers in reciprocating cylinders of internal combustion engines Expired - Lifetime US2996054A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3105473A (en) * 1960-09-06 1963-10-01 Minnie B Johns Spherical ball rotary liquid sealed internal combustion engine
US4054248A (en) * 1976-07-01 1977-10-18 General Motors Corporation Fuel injector pump for a unit fuel injector

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1531382A (en) * 1921-01-21 1925-03-31 William S Franklin Valve-operating device for internal-combustion engines
US2846987A (en) * 1956-03-13 1958-08-12 Nettel Frederick Reciprocating internal combustion engine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1531382A (en) * 1921-01-21 1925-03-31 William S Franklin Valve-operating device for internal-combustion engines
US2846987A (en) * 1956-03-13 1958-08-12 Nettel Frederick Reciprocating internal combustion engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3105473A (en) * 1960-09-06 1963-10-01 Minnie B Johns Spherical ball rotary liquid sealed internal combustion engine
US4054248A (en) * 1976-07-01 1977-10-18 General Motors Corporation Fuel injector pump for a unit fuel injector

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