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US1394850A - Internal-combustion engine - Google Patents

Internal-combustion engine Download PDF

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US1394850A
US1394850A US325977A US32597719A US1394850A US 1394850 A US1394850 A US 1394850A US 325977 A US325977 A US 325977A US 32597719 A US32597719 A US 32597719A US 1394850 A US1394850 A US 1394850A
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fuel
cylinders
cylinder
conduit
pressure
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US325977A
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Albert R Long
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B13/00Engines characterised by the introduction of liquid fuel into cylinders by use of auxiliary fluid
    • F02B13/10Use of specific auxiliary fluids, e.g. steam, combustion gas
    • 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
    • F02M69/00Low-pressure fuel-injection apparatus ; Apparatus with both continuous and intermittent injection; Apparatus injecting different types of fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B2075/1804Number of cylinders
    • F02B2075/1808Number of cylinders two
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2720/00Engines with liquid fuel
    • F02B2720/15Mixture compressing engines with ignition device and mixture formation in the cylinder
    • F02B2720/151Mixture compressing engines with ignition device and mixture formation in the cylinder with fuel supply and pulverisation by air or gas under pressure during the suction or compression stroke

Definitions

  • This invention relates to improvements in internal combustion engines, especially those of the twocycle type and it is an object of the invention to provide an engine of two cycle type with a novel form of fuel feed and vaporizing means whereby the fuel from whic'lrfpoweris to be derived will be thorouglily vaporized and discharged into one of a pair of cylinders by functioning of the remaining cylinder and connection of the same thereto in a manner to permit the shunting of a portion of the burning gases in said remaining cylinder through the connection into the first cylinder, such shunted gas carrying with it a gaseous charge delivered thereunto.
  • Another important characteristic feature of the invention resides in manner in which a scavenging current of fresh air is delivered into the cylinders of the engine whereby to expedite exhaustion of spent or burnt gases from the same immediately'subsequently to the completion of the power stroke of each cylinder and previous to the intake of the highly combustible vaporized gases thereinto.
  • Other features of the invention will be in part obvious and in part described hereinafter.
  • 1 and 2 indicate the several cylinders of the engine having their respective pistons 3 and 4 mounted for operation therein and having connection through pitmen to a crank shaft 5 journaled in bearings and arranged within the engine crank case 6 in the usual manner.
  • Said pair of cylinders 1 and 2 are connected by a fuel feeding conduit 7 the opposite ends of which discharge into the adjacent cylinders while its intermediate portion is formed with a valve seat 8 into which a needle valve 9 is turned; a fuel supply conduit 10 being connected to the valve andadapted to have the passage of fuel therefrom, into the conduit regulated to the desired degree by the same.
  • the needle valve 9 is provided with a knurled head 11 which is conveniently located to enable adjustment thereof with ease and despatch.
  • exhaust ports 13 and 141 are formed on the opposite sides of the walls of said cylinders, serving, as will be appreciated, as outlets for the spent gases.
  • Other ports 15 and 16 are formed in the cylinders and are arranged thereabout in spaced relation, and afford means for permitting the intaking of fresh air to the crank case 6 in order that the scavenging of the cylinders subsequent to a working stroke of each, may
  • Ports 15 and 16 are also formed in the adjacent walls of the cylinders and have communication with the particular compartments of the crank case of their respective cylinders, thus affording passages for the discharge of scavenging air currents into said cylinders at predetermined intervals Ignition means (not shown) are of course, engaged in the heads of the cylinders 1 and 2 through the openings 17 therein and serve to ignite the gasessubsequent to COIIIPIGS? slon.
  • piston 4 is on the upper center, in whichrelative positions the following functions occur:
  • the exhaust port 13 is wide open and the burned gases are exhausting from cylinder 1.
  • the air transfer port 15 is open and air under pressure, (due to the down stroke of the piston 3) in the crank-case is passing into cylinder 1 as the exhaust-gases passout, supplying the cylinder 1 with a fresh charge of air for another power cycle.
  • Piston 4 being on its upper center; port 16 is open and air is allowed to flow into the crank case replacing the partial vacuum caused by the up stroke of piston 4.
  • Fuel conduit 7 is closed to the cylinder 2 by piston 4, and the fuel passing by the adjustingneedle valve 9, will collect in conduit 7, there being no force present aside from its own volume to carry it out.
  • The-ignition means has fired the charge in cylinder 2 above piston 4, which was compressed on the upstroke of piston 4, and this charge, due to its burning will rise to a much higher pressure than its compression pressure, therefore delivering to the pistona much higher pressure and giving-to it-a working stroke on its down motion.
  • Ports l3 and 15' are closed by piston 3 in cylinder 1, and the compression begins and also a reduced pressure in crank case has begun to be set up.
  • the piston 1 in cylinder 2 will have uncovered the small port to the fuel conduit and as the power stroke is less than half completed, the pressure in cylinder 2 is still high.
  • the pressure in cylinder 2 is still high.
  • the size of theconduit 7 is so proportioned that the amount desired only will pass through the conduit. Furthermore it is desired that a small amount of the hot gases should pass from one cylinder to the other in order to clean'the conduit of its fuel and add enough limited, and as the ratio of fuel to air in the To determine the size of the conduit 7 tests similar to those made in determining the size of a nozzle on the present day automobile gasolene engine carbureters of certain makes are made, in which case a proportion of 8000 to 1 in column of the liquid fuel and air is sought.
  • the ratio of fuel to air to form a. burning mixture is very small conduit is many, many times too rich to support a flame, no flame can exist.
  • the fuel in being changed from a liquid to a gas absorbs a certain amount of heat without a rise in temperature and as this heat is taken from the hot gases forcing the fuel into the cylinder,'these gases are cooled by that amount.
  • a flame cannot be supported through asmall pipe unless the temperature of the pipe is-held constant at the temperature of the flame. This, it will be remembered, was done in the first gas engines which were ignited by a hot tube heated by a Bunsen burner.
  • the amount of fuel introduced into the conduit 7, and in consequence into the cylinders 1 and 2 may be varied, such as conditions or preference saving in cost of operating the engine providedtherewith.
  • an unobstructed valveless fuel conduit connecting each pair of cylinders, a fuel supply means common to each pair of cylinders, exhaust means for the cylinders, and means in proximity to said exhaust means for supplying a scavenging current of air to said cylinders and partially exhausting the same therefrom, the fuel supply means and fuel conduit being so arranged and the pistons so timed in their cycle of operation that the pressure created by the explosion in one cylinder will act as the injection means for the fuel through said conduit into the other cylinder, when the pressure within the latter is near its minimum.
  • an unobstructed valveless fuel conduit connecting each pair of cylinders, a fuel supply means common to each pair of cylinders, regulating means cooperable with said supply means, and means in 'proximityto the exhaust means of the cylinders for supplying a scavenging current of air thereto and partially exhausting the same therefrom, the fuel supply means and fuel conduit being so arranged and the pistons so timed in their cycle of operation that the pressure created by the explosion in one cylinderwill act as the injection means for the fuel through said conduit into the other cylinder, whenthe pressure within the latter is near its minimum.
  • an unobstructed valveless fuel conduit connecting each pair of cylinders, a fuel supply means common to said cylinders, and operable upon opening of the exhaust ports of the cylinders for allowing a scavenging current of air to pass through said cylinders, the fuel supply means and fuel conduit being so arranged and the pistons so timed in their cycle of operation that the pressure created by the explosion in one cylinder will act as the injection means for the fuel through said conduit into the other cylinder, when the pressure within the latter is near its minimum.
  • I 4 In a two cycle two cylinder engine, an unobstructed valveless fuel conduit connecting each pair of cylinders, a fuel supply means common to said cylinders, and means in proximity to the exhaust ports of said cylinders for supplying a scavenging current of air to said cylinders and partially exhausting the same, and fuel conduit being so arranged and the pistons So timed in their cycle-0f operation that the pressure created by the explosion in one cylinder will act as the injection means for the fuel through said conduit into the other cylinder, when the pressure within the latter is near its minimum.
  • the fuel supply means an unobstructed valveless fuel conduit connecting each pair of cylinders.
  • a fuel supply means common to each pair of cylinders, and communicating with the firing chambers thereof, means for regulating the passage of fuel through said supply means, said cylinders having air intake and exhaust ports therein in proximity to. the gas exhaust ports thereof controlled by movement of the pistons in their cylinders, and positioned below the fuel supply means, the fuel supply means and fuel conduit being so arranged and the pistons so timed in their cycle of operation that the pressure created by the explosion in one cylinder will act as the injection means for the fuel through said conduitinto the other cylinder, when the pressure within the latter is near its minimum.
  • an unobstructed valveless fuel conduit connecting each pair of cylinders, a fuel supply means common to each pair of cylinders, the exhaust ports of said cylinders being arranged below the supply means, and controlled by the pistons in said cylinders, said cylinders also having air intake and exhaust ports therein in proximity to said first exhaust ports adapted to be controlled by said pistons, the fuel supply means and fuel conduit being 'soarranged and the pistons so timed in their cycle of operation that the pressure created b the explosion in one cylmder willa'ct as t e injection means for the fuel through said conduit into the other cylinder, when the pressure within the latter is near its minimum.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Fuel-Injection Apparatus (AREA)

Description

ALBERT R. LONG, 0F BALLSTON, VIRGINIA.
INTERNAL-COMBUSTION ENGINE.
Specification of Letters Patent. Patented Oct. 25, 1921,
Application filed September 24, 1919. Serial No. 325,977.
i To all whom it may concern:
Be it known that I, ALBERT R.-L oNc, a citizen of the United States of America, re-
siding at Ballston, in the county of Alexandria and State of Virginia, have invented certain new and useful Improvements in Internal-Combustion Engines, of which the following is a specification.
This invention relates to improvements in internal combustion engines, especially those of the twocycle type and it is an object of the invention to provide an engine of two cycle type with a novel form of fuel feed and vaporizing means whereby the fuel from whic'lrfpoweris to be derived will be thorouglily vaporized and discharged into one of a pair of cylinders by functioning of the remaining cylinder and connection of the same thereto in a manner to permit the shunting of a portion of the burning gases in said remaining cylinder through the connection into the first cylinder, such shunted gas carrying with it a gaseous charge delivered thereunto.
Another important characteristic feature of the invention resides in manner in which a scavenging current of fresh air is delivered into the cylinders of the engine whereby to expedite exhaustion of spent or burnt gases from the same immediately'subsequently to the completion of the power stroke of each cylinder and previous to the intake of the highly combustible vaporized gases thereinto. Other features of the invention will be in part obvious and in part described hereinafter.
In order that the invention and the manner of its application may be readily under-- stood by workers skilled in the art, I have in the accompanying illustrative drawings and in the following detailed description based thereon set out a preferred embodi ment of the same.
In these drawings I haveshown a vertical section through a pair of cylinders of a twocycle engine, clearly indicatingtherein the relative positions of the pistons of the several cylinders.
Having more particular reference to the drawings in connection with which like reference characters will refer to corresponding parts throughout, 1 and 2 indicate the several cylinders of the engine having their respective pistons 3 and 4 mounted for operation therein and having connection through pitmen to a crank shaft 5 journaled in bearings and arranged within the engine crank case 6 in the usual manner. Said pair of cylinders 1 and 2 are connected by a fuel feeding conduit 7 the opposite ends of which discharge into the adjacent cylinders while its intermediate portion is formed with a valve seat 8 into which a needle valve 9 is turned; a fuel supply conduit 10 being connected to the valve andadapted to have the passage of fuel therefrom, into the conduit regulated to the desired degree by the same.
Obviously, the needle valve 9 is provided with a knurled head 11 which is conveniently located to enable adjustment thereof with ease and despatch.
Below the connection of the conduit 7 with the cylinders 1 and 2, exhaust ports 13 and 141 are formed on the opposite sides of the walls of said cylinders, serving, as will be appreciated, as outlets for the spent gases. Other ports 15 and 16 are formed in the cylinders and are arranged thereabout in spaced relation, and afford means for permitting the intaking of fresh air to the crank case 6 in order that the scavenging of the cylinders subsequent to a working stroke of each, may
be effected. Ports 15 and 16 are also formed in the adjacent walls of the cylinders and have communication with the particular compartments of the crank case of their respective cylinders, thus affording passages for the discharge of scavenging air currents into said cylinders at predetermined intervals Ignition means (not shown) are of course, engaged in the heads of the cylinders 1 and 2 through the openings 17 therein and serve to ignite the gasessubsequent to COIIIPIGS? slon.
When the piston 3 is on the lower center,
piston 4: is on the upper center, in whichrelative positions the following functions occur: The exhaust port 13 is wide open and the burned gases are exhausting from cylinder 1. The air transfer port 15 is open and air under pressure, (due to the down stroke of the piston 3) in the crank-case is passing into cylinder 1 as the exhaust-gases passout, supplying the cylinder 1 with a fresh charge of air for another power cycle. Piston 4 being on its upper center; port 16 is open and air is allowed to flow into the crank case replacing the partial vacuum caused by the up stroke of piston 4. Fuel conduit 7 is closed to the cylinder 2 by piston 4, and the fuel passing by the adjustingneedle valve 9, will collect in conduit 7, there being no force present aside from its own volume to carry it out. The-ignition means has fired the charge in cylinder 2 above piston 4, which was compressed on the upstroke of piston 4, and this charge, due to its burning will rise to a much higher pressure than its compression pressure, therefore delivering to the pistona much higher pressure and giving-to it-a working stroke on its down motion.
Now, to complete any portion of the power stroke, which is less than a half stroke, such a position is shown in the drawings and the following are the conditions at this position:
Ports l3 and 15' are closed by piston 3 in cylinder 1, and the compression begins and also a reduced pressure in crank case has begun to be set up. The piston 1 in cylinder 2 will have uncovered the small port to the fuel conduit and as the power stroke is less than half completed, the pressure in cylinder 2 is still high. Now as there is very. little if any pressure in cylinder 1, the only thing separating the two cylinders through the small fuel conduit 7, is the fuel collected in the conduit while one end was out off. Now as the pressure is cylinder 2 in several times that of cylinder 1, the fuel will be forced with great velocity into cylinder 1. Now, as either heat or velocity applied to a liquid fuel in space, (the fuel is suspended in space when it. passes into the cylinder) will vaporize it, the fuel will be vaporized. It
- is understood that the working of one of the cylinders is identical with the other.
It willbe noted that the moment piston 4 in cylinder 2 opens the port to fuel duct 7,
- piston 3 in cylinder 1 hasonly just closed its ports and there could be no pressure in cylinder 1. As the conduit 7 must'be high enough above what is the mid stroke of-the piston to insure opening enough to allow fuel to pass into cylinder 1, the piston 2 on its working stroke will not have made its half stroke before the conduit 7 is opened, and as the volume above the piston 4 is less and as the cylinders are filled with equal volumes of air the pressure would be higher in cylinder 2 and consequently there would be a flow through conduit 7 toward cylinder 1, thereby carrying the fuel into cylinder 1.
Now asto a portion of the expanding gases being orced into the other cylinder the size of theconduit 7 is so proportioned that the amount desired only will pass through the conduit. Furthermore it is desired that a small amount of the hot gases should pass from one cylinder to the other in order to clean'the conduit of its fuel and add enough limited, and as the ratio of fuel to air in the To determine the size of the conduit 7 tests similar to those made in determining the size of a nozzle on the present day automobile gasolene engine carbureters of certain makes are made, in which case a proportion of 8000 to 1 in column of the liquid fuel and air is sought.
It will also be noted that the ratio of fuel to air to form a. burning mixture is very small conduit is many, many times too rich to support a flame, no flame can exist. Second, due to the latent heat of evaporation, the fuel in being changed from a liquid to a gas absorbs a certain amount of heat without a rise in temperature and as this heat is taken from the hot gases forcing the fuel into the cylinder,'these gases are cooled by that amount. Third, a flame cannot be supported through asmall pipe unless the temperature of the pipe is-held constant at the temperature of the flame. This, it will be remembered, was done in the first gas engines which were ignited by a hot tube heated by a Bunsen burner.
By regulating the valve 9 the amount of fuel introduced into the conduit 7, and in consequence into the cylinders 1 and 2 may be varied, such as conditions or preference saving in cost of operating the engine providedtherewith.
Manifestly, the construction shown, 1s
capable dqf considerable modification, and such mo fication as is within the scope of my claims, I consider within the spirit of my invention.
What I claim is: p
1. In a two cycle multiple cylinder engine, an unobstructed valveless fuel conduit connecting each pair of cylinders, a fuel supply means common to each pair of cylinders, exhaust means for the cylinders, and means in proximity to said exhaust means for supplying a scavenging current of air to said cylinders and partially exhausting the same therefrom, the fuel supply means and fuel conduit being so arranged and the pistons so timed in their cycle of operation that the pressure created by the explosion in one cylinder will act as the injection means for the fuel through said conduit into the other cylinder, when the pressure within the latter is near its minimum.
2. In a two cycle multiple cylinder engine, an unobstructed valveless fuel conduit connecting each pair of cylinders, a fuel supply means common to each pair of cylinders, regulating means cooperable with said supply means, and means in 'proximityto the exhaust means of the cylinders for supplying a scavenging current of air thereto and partially exhausting the same therefrom, the fuel supply means and fuel conduit being so arranged and the pistons so timed in their cycle of operation that the pressure created by the explosion in one cylinderwill act as the injection means for the fuel through said conduit into the other cylinder, whenthe pressure within the latter is near its minimum.
.3. Ina two cycle multiple cylinder engine, an unobstructed valveless fuel conduit connecting each pair of cylinders, a fuel supply means common to said cylinders, and operable upon opening of the exhaust ports of the cylinders for allowing a scavenging current of air to pass through said cylinders, the fuel supply means and fuel conduit being so arranged and the pistons so timed in their cycle of operation that the pressure created by the explosion in one cylinder will act as the injection means for the fuel through said conduit into the other cylinder, when the pressure within the latter is near its minimum.
I 4. In a two cycle two cylinder engine, an unobstructed valveless fuel conduit connecting each pair of cylinders, a fuel supply means common to said cylinders, and means in proximity to the exhaust ports of said cylinders for supplying a scavenging current of air to said cylinders and partially exhausting the same, and fuel conduit being so arranged and the pistons So timed in their cycle-0f operation that the pressure created by the explosion in one cylinder will act as the injection means for the fuel through said conduit into the other cylinder, when the pressure within the latter is near its minimum.
5. In a two cycle multiple cylinder engine,
the fuel supply means an unobstructed valveless fuel conduit connecting each pair of cylinders. a fuel supply means common to each pair of cylinders, and communicating with the firing chambers thereof, means for regulating the passage of fuel through said supply means, said cylinders having air intake and exhaust ports therein in proximity to. the gas exhaust ports thereof controlled by movement of the pistons in their cylinders, and positioned below the fuel supply means, the fuel supply means and fuel conduit being so arranged and the pistons so timed in their cycle of operation that the pressure created by the explosion in one cylinder will act as the injection means for the fuel through said conduitinto the other cylinder, when the pressure within the latter is near its minimum.
6; In a two cycle multiple cylinder engine, an unobstructed valveless fuel conduit connecting each pair of cylinders, a fuel supply means common to each pair of cylinders, the exhaust ports of said cylinders being arranged below the supply means, and controlled by the pistons in said cylinders, said cylinders also having air intake and exhaust ports therein in proximity to said first exhaust ports adapted to be controlled by said pistons, the fuel supply means and fuel conduit being 'soarranged and the pistons so timed in their cycle of operation that the pressure created b the explosion in one cylmder willa'ct as t e injection means for the fuel through said conduit into the other cylinder, when the pressure within the latter is near its minimum.
In testimony whereof I afiix my signature in presence of a witness.
ALBERT R. LONG.
Witness:
Emu J Aims Smmnr.
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2446094A (en) * 1944-07-05 1948-07-27 Harold E Mattice Supercharging and scavenging internal-combustion engine
US2476816A (en) * 1944-06-14 1949-07-19 Crossley Brothers Ltd Internal-combustion engine
FR2627228A1 (en) * 1988-02-12 1989-08-18 Outboard Marine Corp FUEL INJECTION SYSTEM FOR MULTI-CYLINDER TWO-STROKE ENGINE

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2476816A (en) * 1944-06-14 1949-07-19 Crossley Brothers Ltd Internal-combustion engine
US2446094A (en) * 1944-07-05 1948-07-27 Harold E Mattice Supercharging and scavenging internal-combustion engine
FR2627228A1 (en) * 1988-02-12 1989-08-18 Outboard Marine Corp FUEL INJECTION SYSTEM FOR MULTI-CYLINDER TWO-STROKE ENGINE
DE3903493A1 (en) * 1988-02-12 1989-08-24 Outboard Marine Corp INTERNAL COMBUSTION ENGINE
US4862857A (en) * 1988-02-12 1989-09-05 Outboard Marine Corporation Fuel injection system for multi cylinder two-stroke engine

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