US1081950A - Process for removing carbon deposited in internal-combustion engines. - Google Patents

Process for removing carbon deposited in internal-combustion engines. Download PDF

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US1081950A
US1081950A US74435913A US1913744359A US1081950A US 1081950 A US1081950 A US 1081950A US 74435913 A US74435913 A US 74435913A US 1913744359 A US1913744359 A US 1913744359A US 1081950 A US1081950 A US 1081950A
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carbon
oxygen
ignited
particles
combustion engines
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US74435913A
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Harley M Eller
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NORFOLK Manufacturing Co
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NORFOLK Manufacturing Co
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Assigned to CONGRESS FINANCIAL CORPORATION (NEW ENGLAND) A MASSACHUSETTS CORPORATION reassignment CONGRESS FINANCIAL CORPORATION (NEW ENGLAND) A MASSACHUSETTS CORPORATION SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GREAT NORTHERN PAPER, INC A DELAWARE CORPORATION
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  • the object of my invention is to provide a method whereby carbon formed upon the piston head and the walls of the combustion chamber of an internal combustion engine,
  • the combustible fluid upon a particle of carbon while it is being. consumed by combining with the oxygen of the jet, the combustible fluid ignites and burns sufliciently long" to enable the operator to find and burn other ignited but unconsumed particles, and also to ignite more combustible fluid that maybe sprayed on another portion of the wall of the cylinder, to detect particles there, if any there be; and so on throughout the combustion'chamber.
  • the carbon-destroying torch is of the following construction :A copper tube 1, Figs. 1 and 2, which has been annealed for the purpose of giving itthe desired flexibility, see Fig. .3, is in communication with a supply of oxygen through a channel 2 provided in a brass fitting 3 which has a suitable hose connection 4, connected'to a source ofoxygen, not shown. of this tube 1, which may be termed the oxygen tube, is formed a combustible fluid reservoir 5, comprising a cylindrical piece of sheet brass 6 connected with and sol.-
  • a pump 8 the mouth of which lies within the reservoir 5, and is controlled by a check valve 9 that permits the inflow, but prevents the outflow, of the liquid pumped by means of a piston 10, a piston rod 11 and pump handle 12.
  • a i -combustible fluid tube 14 of annealed copper lying in parallelism with the oxygen tubel, but terminating a short distance from the end thereof; the joints formed between the oxygen tube, the combustible fluid tube, and the end fitting 7 of the reservoir, being closed as by soldering.
  • a valve 16 to control the feed of oxygen. It is operated and extending forward-lyin operative parallelism with the reservoir, and connected with I the valve stem 18 by a yoke 19 embracing the stem and capable of adjustment by a nut Surrounding one end portion] and continues for a few moments.
  • valve 16 secured to the outer end of the stem, and in engagement with the outside part of the yoke of the .valve lever.
  • This valve 16 is mounted in a metallic casing 21 in screw ongagement with the fittingfi; the bearings for the valve stem 18 being a threaded ring 22, screwed into the outer end portion of this casing; and an opening in the bottom of the casing, abutting a leather packing 23.
  • the valve is formed of india rubber, and
  • a coil spring 25 surrounds the valve stem 18 and presses against both the bottom of the valve casing 21, and the threaded bearing ring 22 in the opposite end of the casing.
  • valve finger lever 17 being parallel with the reservoir handle 6, it is within the grasp of the operator, and
  • the pump may be refilled by pulling the handle 12 outward, thereby drawing in a charge of fluidfrom the reservoir, past the check valve 9, which closes the moment the pump piston ceases its outward movement.
  • the first and old step consists in a general burning off of the carbon.
  • the torch is introduced into the chamber, through the sparkplug opening, the end of the oxygen tube being brought close to some of the carbon, say that visible to the operator.
  • the oxygen control lever 17 ofthe torch is then slightly pressed toward the handle 6 of the reservoir, thereby permitting a small atmosphere of oxygen oxygen insuring and hastening theignition'.
  • this torch has found in using this torch that after a small supply of-alcohol has been actually delivered to the ignited carbon, there remains in the tube a sullicient amount to ignite and burn at the end of the combustible fluid tube. ⁇ Vhile this flame may be made constant, and is not essential to theperformance of my process, I do find that it greatly assists not only in preventing the above mentioned collection of combustible fluid, in case there is no ignited carbon at hand, but also in starting the combustion entirely anew in the combustion chamber, as where ignited carbon has ceased burning, but before the process is completed.
  • bustible liquid for the purpose of igniting the llquid. and unignit'ed carbon, to show

Description

H. M. ELLBR. PROCESS FOR REMOVING CARBON DEPOSITBD IN INTERNAL COMBUSTION ENGINES.
APPLICATION FILED JAN. 27, 1913 3. m m v Zn .1 3 6 J D (Q w m T O W M Z 1. a r l UNITED STAClTiEiPATENT oFFIoF..
HARLEY M. ELLER, OF WoLnnsToN, MASSACHUSETTS, ASSIGNOIR, T NORFOLK MANUFACTURING COMPANY, OF BOSTON, MASSACHUSETTS, .A. CORPORATION OF MAINE.
rnoonss roe nmvrovxne CARBON :onrosrrnn IN IN'rERNAt-ooMBUsTIoN ENGINES.
Specification of Letters Patent.
Application filed January 27,1913. Serial No. 744,359.
To all whom it may concern Be it known that I, HARLEY M. ELLER,1-
. siding at Wollaston. in the county of Norfolk and State of .Massachusetts, have invented a certain new and useful Process for 'Removing Carbon Deposited in -Internal Combustion Engines, of which the following is a specification, reference being had therein to the accompanying drawings. 7 The object of my invention is to provide a method whereby carbon formed upon the piston head and the walls of the combustion chamber of an internal combustion engine,
may be more successfully removed than has been the case heretofore. As is well known,.
sumed; more or less carbon in the form of particles and patches being left in a glowing state. This step may be termed the be. located. But even with great care, a
preliminary burning out. Next, a jet of oxygen is supplied successively to the ignited patches, for the purpose of entirely consuming them. If for any reason the ignition of the carbon ceases, combustion has to be again started; often with great difficulty, because of the absence of the easily ignitible oil present-at the first lighting, and also because the match or'.taper burns out quickly, and, oftener than not, not only before the visible carbon can be lighted, butbefore the carbon, concealed upon the invisible wall surfaces of the cylinder, can
complete removal of the carbon is diificult, for, as much of the wall surface of the combustion chamber is invisible to the operator,
. 'it is impossible to see what there is, or-what is taking place, thereon. While any of the unseen particles glow and light up the ignited particles go out,the operator is not sure whether all have been consumed or not; if he decides yes, and they have been, all
particles left, it is very hard, even if found, to reignite them. Consequently, their removal is oftener than not, incomplete; and if they or any of them have become separated from the cylinder walls, as by the blast of the oxygen jet, and are scattered throughout the cylinder, they are extremely difficult to locate, and, being free, are likely to score the piston rings and the wall of the cylinder, when the engine is started.
But in all events, the carbon has, by this inefiicient method, to be lighted and reli hted many times, andall with the result, 0 loss of'time and patience; a great waste of oxygen; and an incomplete removal of the car- Now by my method, I obviate the necessity of frequent and difficult relighting of mtentetlDec. 23,1913.
"well and good; if no, and there are oilless' the carbon, with tapers and oxygen; and I i do so by injecting upon a considerable wall surface containing an ignited patch or particleof carbon, a spray of combustible fluid, say, a volatile hydrocarbon, as alcohol, kerosene, or oil, which at once becomes ignited,
and starts combustion of the adjacent unconsumed carbon. The glow and sparks from the ignited carbon, show its location,
whether it can be actually seen or not, and enable the operator to bring his oxygen jet into direct contact with the glowing patch or particles of carbon until it is completely consumed. In short, by the additional step of introducing a combustible fluid upon a particle of carbon while it is being. consumed by combining with the oxygen of the jet, the combustible fluid ignites and burns sufliciently long" to enable the operator to find and burn other ignited but unconsumed particles, and also to ignite more combustible fluid that maybe sprayed on another portion of the wall of the cylinder, to detect particles there, if any there be; and so on throughout the combustion'chamber. Obviously, during the pe formance of the process, there is always glowing carbon to combine with the continuous jet of oxygen; there is no relighting of matches or tapers; there is no waste of oxygen; and the operator, knowing he has gone over the by a finger lever 17, pivoted to the fitting piston head and all of the wall surfaces of the chamber, with no glow or sparks showing, restsfassured that there is no unconsumed carbon left.
While the successful operation of my new process is not'dependent upon any particular form of apparatus, I make use of a new and useful device which is called a carbon-.
carbon from the interior walls of the comcylinder of an internal bustion chamber of a combustion engine. I
The carbon-destroying torch is of the following construction :A copper tube 1, Figs. 1 and 2, which has been annealed for the purpose of giving itthe desired flexibility, see Fig. .3, is in communication with a supply of oxygen through a channel 2 provided in a brass fitting 3 which has a suitable hose connection 4, connected'to a source ofoxygen, not shown. of this tube 1, which may be termed the oxygen tube, is formed a combustible fluid reservoir 5, comprising a cylindrical piece of sheet brass 6 connected with and sol.-
dered to said fitting 3, and alsosimilarly connected and soldered to a fitting 7 sur-' rounding the mid-portion of the oxygen tube. In the top portion of the reservoir, is mounted a pump 8, the mouth of which lies within the reservoir 5, and is controlled by a check valve 9 that permits the inflow, but prevents the outflow, of the liquid pumped by means of a piston 10, a piston rod 11 and pump handle 12.- Between the piston and thevalve, in the side of the pump, is an opening 13 to serve as a communication between the'pump, and what may be called a i -combustible fluid tube 14, of annealed copper lying in parallelism with the oxygen tubel, but terminating a short distance from the end thereof; the joints formed between the oxygen tube, the combustible fluid tube, and the end fitting 7 of the reservoir, being closed as by soldering. Access to the reservoir is controlled by means of athreaded plug 15. The outside of this cylindrical reservoir serves as a handle for conveniently holding and operating the torch, as clearly appears in Fig. 2. In -the fitting 3, at the inner end of the reservoir, is a valve 16 to control the feed of oxygen. It is operated and extending forward-lyin operative parallelism with the reservoir, and connected with I the valve stem 18 by a yoke 19 embracing the stem and capable of adjustment by a nut Surrounding one end portion] and continues for a few moments.
20 secured to the outer end of the stem, and in engagement with the outside part of the yoke of the .valve lever. This valve 16 is mounted in a metallic casing 21 in screw ongagement with the fittingfi; the bearings for the valve stem 18 being a threaded ring 22, screwed into the outer end portion of this casing; and an opening in the bottom of the casing, abutting a leather packing 23. The valve is formed of india rubber, and
engages a suitable seat 24 formed at the mouth of the channel 2 connected with the source of oxygen supply. In order that the valve may constantly tend to find its seat 24, a coil spring 25 surrounds the valve stem 18 and presses against both the bottom of the valve casing 21, and the threaded bearing ring 22 in the opposite end of the casing.
As appears in Fig. 2, the valve finger lever 17 being parallel with the reservoir handle 6, it is within the grasp of the operator, and
may be easily manipulated simply by pres-' sure of the fingers, when desired; while he may from time to time, discharge from the pump 8 small quantities of combustible fluid,
by pushing down the handle 12, short spaces,
until the charge is exhausted. The pump may be refilled by pulling the handle 12 outward, thereby drawing in a charge of fluidfrom the reservoir, past the check valve 9, which closes the moment the pump piston ceases its outward movement.
I will now describe how my process is carried out, reference being had again to Fig. 3, showing in section, an internal combustion engine cylinder 26, its spark plug and cap having been removed; and the piston 27 at the upper end of its stroke. The walls of the combustion chamber 28 and the piston head are assumed to be covered with asomewhat evenly distributed mass of carbon moistened with oil of the cylinder. The first and old step consists in a general burning off of the carbon. The torch is introduced into the chamber, through the sparkplug opening, the end of the oxygen tube being brought close to some of the carbon, say that visible to the operator. The oxygen control lever 17 ofthe torch is then slightly pressed toward the handle 6 of the reservoir, thereby permitting a small atmosphere of oxygen oxygen insuring and hastening theignition'. I
Combustion rapidly spreads over the walls of the combustion chamber and piston head While much of'the carbon is thus consumed, unburned patches, and 'particles, remain. Until now, combustion has been assisted by continuing a small supply of oxygen; but before this preliminary burning off has been completed, a small amount of a combustible ignited particles of carbon and they are wholly consumed 'one after another; but when the sparks almost cease, indicating to the operator that this patch has almost been removed, a small additional supply of alcohol is sprayed upon the glowing carbon, and
. adjacent non-ignited carbon; it instantly lights, and, in rapidly burning, starts a'new mass of carbon to burning. I The jet of oxygen from the torch is then directed toward these glowing particles, and they are consumed in the manner described; the above sequence of operation being repeated until all of the carbon Within sight has been done away with, speedily and; easily. When, however, the carbon is not visible, greater difficulties are encountered, but easily overcome by means of my process. Continuous glow of particles concealed from view in the combustion chamber, may be brought about by introducing another small charge of alcohol upon some particles which are lighted, let
us suppose, at B on a portion of the roof'of the combustion chamber. It will be remembered .that these oxygen and combustible fluid tubes 1, 14, Figs. 1 and 2, are of copper which has been annealed, consequently, they may be bent into any form adapted to direct the current of oxygen and that of the com-' bustible fluid to that or any other portion of the unseen roof surface; such a bending of the tubes is shown in Fig. 3. Particles of carbon, as B, upon this roof surface be ing, as already assumed, ignited, a small charge of alcohol or combustible. fluid is delivered upon them, but it must not beforgotten, that after each spraying, the liquid extends over a considerable area of unburned carbon, and, consequently starts all of the carbon in that area, aglowing. By a somewhat rapid movement of the oxygen nozzle from place to place, with occasional sprayings of alcohol, alarge portion of the remaining carbon may be destroyed. How ever, in thus going somewhat rapidly over the entire wall surface of the combustion chamber and the piston head, there will be left particles and patches here and there, which must be found and burned. Obviously, these tubes are such that they may be bent and forced into form whereby their nozzles may be brought into close proximity with all of the surfaces making up the combustion chamber these surfaces themselves aiding in giving to the inwardly pressed tubes the desired form. After all of these surfaces have been gone over, in this somewhat general. way, with the torch, the operator can again apply his torch nozzle to all of these surfacesyand, by a careful and systematic introduction of small charges of the combustible fluid, as often as the glow of'the ignited particles seems to diminish,'andby a constant supply of oxygen. .forconsumlngvarious particles of unconsumed'carbon, he may continue this combustion until all particles or patches of carbon are consumed. .In short, there is always some glowin carbon to ignite the new supply of com ustible fluid, which, in
turn, starts any unconsumed carbon to glowing for the purpose of indicating to the operator the presence and location of carbon to be consumed; and, further, all of the first mentioned benefits flowing from the use of by process, are attained.
In using alcohol or other combustible fluid that vaporizes quickly, to spray unconsumed carbon, care should be taken in not delivering too much of it, for if the supply is large, there is likely to be a violent explosion, not dangerous to the operator, but extremelyannoying. This might be well illustrated by assuming the combustion chamber to have been cleared of carbon, when as a fact at the extreme inner side, there happens to be a glowing particle or patch; it the operator, under these conditions. introduces successive small charges, which later become ignited by this particle, the large atmosphere of combustible gas would explode with violence. have found in using this torch that after a small supply of-alcohol has been actually delivered to the ignited carbon, there remains in the tube a sullicient amount to ignite and burn at the end of the combustible fluid tube. \Vhile this flame may be made constant, and is not essential to theperformance of my process, I do find that it greatly assists not only in preventing the above mentioned collection of combustible fluid, in case there is no ignited carbon at hand, but also in starting the combustion entirely anew in the combustion chamber, as where ignited carbon has ceased burning, but before the process is completed.
Having fully described my process and desiring to protect the same in the broadest manner legally possible, what I claim is r'- 1. In the method of removing carbon from the combustion chamber of internal combustion engines; discharging upon ignited carbon and unigni-ted carbon, combustible liquid for the purpose of igniting the liquid and carbon, to show the presence of the latter.
2. The method of removing carbon from the combustion chamber walls of anintcrnal combustion engine, consisting, in igniting a portion of said carbon; supplying an artificial supply of oxygen to the ignited the combustion chamber of internal combustion engines, consisting, in igniting a portion of sald carbon; 1n dlrectlng an artificial supply of oxygen upon sald carbon;
in discharging upon an area including the ignited carbon, a combustible liquid which at once ignites, and m so dolng ignites and discloses other carbon W1th1n the area, that must be supplied with oxygen, and be consumed.
4. In the method of removing carbon from the combustion 'chamber of internal combustion engines; discharging upon ig nited carbon and unignited carbon separated by Wall space free from carbon, com- F. UNIAo, F. A. MCCARTHY.
bustible liquid, for the purpose of igniting the llquid. and unignit'ed carbon, to show
US74435913A 1913-01-27 1913-01-27 Process for removing carbon deposited in internal-combustion engines. Expired - Lifetime US1081950A (en)

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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2443373A (en) * 1943-08-20 1948-06-15 Victor N Borsoff Method of removing carbon and carbonaceous matter
US2538057A (en) * 1943-12-06 1951-01-16 William C Steele Method of cleaning circulating heaters
US2633428A (en) * 1949-01-22 1953-03-31 Alexander H Kerr & Company Inc Process of removing size from glass fibers and the subsequent coating thereof
US2828163A (en) * 1956-04-23 1958-03-25 Gen Am Transport Conveyors for pulverulent materials
US4377420A (en) * 1980-03-06 1983-03-22 United Technologies Corporation Removal of carbonaceous material from gas turbine cavities
US5634598A (en) * 1994-09-20 1997-06-03 Minerals Technologies, Inc. Abrasion resistant lined sweep nozzle
US20060156733A1 (en) * 2005-01-14 2006-07-20 Pratt & Whitney Canada Corp. Integral heater for fuel conveying member
US20060277913A1 (en) * 2005-06-14 2006-12-14 Pratt & Whitney Canada Corp. Internally mounted fuel manifold with support pins
US20080016869A1 (en) * 2005-01-14 2008-01-24 Jason Fish Gas turbine internal manifold mounting arrangement
US20080053096A1 (en) * 2006-08-31 2008-03-06 Pratt & Whitney Canada Corp. Fuel injection system and method of assembly
US20080072600A1 (en) * 2006-09-22 2008-03-27 Oleg Morenko Internal fuel manifold and fuel inlet connection
US20080072601A1 (en) * 2006-09-22 2008-03-27 Oleg Morenko Internal fuel manifold and fuel fairing interface
US20080072599A1 (en) * 2006-09-26 2008-03-27 Oleg Morenko Heat shield for a fuel manifold
US20080092545A1 (en) * 2006-10-24 2008-04-24 Jason Fish Gas turbine internal manifold mounting arrangement
US20090072051A1 (en) * 2007-05-16 2009-03-19 Jason Fish Redundant mounting system for an internal fuel manifold
US7514015B2 (en) 2004-06-17 2009-04-07 Uvtech Systems Method for surface cleaning
US20090126368A1 (en) * 2006-08-31 2009-05-21 Patel Bhawan B Fuel injection system for a gas turbine engine
US20100281881A1 (en) * 2006-08-18 2010-11-11 Pratt & Whitney Canada Corp. Gas turbine combustor and fuel manifold mounting arrangement
US8051664B2 (en) 2007-07-23 2011-11-08 Pratt & Whitney Canada Corp. Pre-loaded internal fuel manifold support

Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2443373A (en) * 1943-08-20 1948-06-15 Victor N Borsoff Method of removing carbon and carbonaceous matter
US2538057A (en) * 1943-12-06 1951-01-16 William C Steele Method of cleaning circulating heaters
US2633428A (en) * 1949-01-22 1953-03-31 Alexander H Kerr & Company Inc Process of removing size from glass fibers and the subsequent coating thereof
US2828163A (en) * 1956-04-23 1958-03-25 Gen Am Transport Conveyors for pulverulent materials
US4377420A (en) * 1980-03-06 1983-03-22 United Technologies Corporation Removal of carbonaceous material from gas turbine cavities
US5634598A (en) * 1994-09-20 1997-06-03 Minerals Technologies, Inc. Abrasion resistant lined sweep nozzle
US5884851A (en) * 1994-09-20 1999-03-23 Minerals Technologies Inc. Abrasion resistant lined sweep nozzle
US7514015B2 (en) 2004-06-17 2009-04-07 Uvtech Systems Method for surface cleaning
US20110120142A1 (en) * 2005-01-14 2011-05-26 Lev Alexander Prociw Gas turbine engine fuel conveying member
US20080016869A1 (en) * 2005-01-14 2008-01-24 Jason Fish Gas turbine internal manifold mounting arrangement
US8276387B2 (en) 2005-01-14 2012-10-02 Pratt & Whitney Canada Corp. Gas turbine engine fuel conveying member
US20060156733A1 (en) * 2005-01-14 2006-07-20 Pratt & Whitney Canada Corp. Integral heater for fuel conveying member
US7721546B2 (en) 2005-01-14 2010-05-25 Pratt & Whitney Canada Corp. Gas turbine internal manifold mounting arrangement
US8171739B2 (en) 2005-06-14 2012-05-08 Pratt & Whitney Canada Corp. Internally mounted fuel manifold with support pins
US20060277913A1 (en) * 2005-06-14 2006-12-14 Pratt & Whitney Canada Corp. Internally mounted fuel manifold with support pins
US7540157B2 (en) 2005-06-14 2009-06-02 Pratt & Whitney Canada Corp. Internally mounted fuel manifold with support pins
US20100281881A1 (en) * 2006-08-18 2010-11-11 Pratt & Whitney Canada Corp. Gas turbine combustor and fuel manifold mounting arrangement
US8353166B2 (en) 2006-08-18 2013-01-15 Pratt & Whitney Canada Corp. Gas turbine combustor and fuel manifold mounting arrangement
US20090126368A1 (en) * 2006-08-31 2009-05-21 Patel Bhawan B Fuel injection system for a gas turbine engine
US20080053096A1 (en) * 2006-08-31 2008-03-06 Pratt & Whitney Canada Corp. Fuel injection system and method of assembly
US8033113B2 (en) 2006-08-31 2011-10-11 Pratt & Whitney Canada Corp. Fuel injection system for a gas turbine engine
US20080072601A1 (en) * 2006-09-22 2008-03-27 Oleg Morenko Internal fuel manifold and fuel fairing interface
US20080072600A1 (en) * 2006-09-22 2008-03-27 Oleg Morenko Internal fuel manifold and fuel inlet connection
US7703286B2 (en) 2006-09-22 2010-04-27 Pratt & Whitney Canada Corp. Internal fuel manifold and fuel fairing interface
US7743612B2 (en) 2006-09-22 2010-06-29 Pratt & Whitney Canada Corp. Internal fuel manifold and fuel inlet connection
US7559142B2 (en) 2006-09-26 2009-07-14 Pratt & Whitney Canada Corp. Method of manufacturing a heat shield for a fuel manifold
US7926286B2 (en) 2006-09-26 2011-04-19 Pratt & Whitney Canada Corp. Heat shield for a fuel manifold
US20080072599A1 (en) * 2006-09-26 2008-03-27 Oleg Morenko Heat shield for a fuel manifold
US20080078080A1 (en) * 2006-09-26 2008-04-03 Patel Bhawan B Method of manufacturing a heat shield for a fuel manifold
US9068508B2 (en) 2006-10-24 2015-06-30 Pratt & Whitney Canada Corp. Gas turbine internal manifold mounting arrangement
US8171738B2 (en) 2006-10-24 2012-05-08 Pratt & Whitney Canada Corp. Gas turbine internal manifold mounting arrangement
US20080092545A1 (en) * 2006-10-24 2008-04-24 Jason Fish Gas turbine internal manifold mounting arrangement
US7856825B2 (en) 2007-05-16 2010-12-28 Pratt & Whitney Canada Corp. Redundant mounting system for an internal fuel manifold
US20090072051A1 (en) * 2007-05-16 2009-03-19 Jason Fish Redundant mounting system for an internal fuel manifold
US8051664B2 (en) 2007-07-23 2011-11-08 Pratt & Whitney Canada Corp. Pre-loaded internal fuel manifold support

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Owner name: CONGRESS FINANCIAL CORPORATION (NEW ENGLAND) A MAS

Free format text: SECURITY INTEREST;ASSIGNOR:GREAT NORTHERN PAPER, INC A DELAWARE CORPORATION;REEL/FRAME:011485/0044

Effective date: 20010118