WO2009121384A1 - Procédé de combustion avec contrôle complet de tous les combustibles purifiés qui sont soumis à de l'air fortement comprimé - Google Patents

Procédé de combustion avec contrôle complet de tous les combustibles purifiés qui sont soumis à de l'air fortement comprimé Download PDF

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Publication number
WO2009121384A1
WO2009121384A1 PCT/EP2008/007011 EP2008007011W WO2009121384A1 WO 2009121384 A1 WO2009121384 A1 WO 2009121384A1 EP 2008007011 W EP2008007011 W EP 2008007011W WO 2009121384 A1 WO2009121384 A1 WO 2009121384A1
Authority
WO
WIPO (PCT)
Prior art keywords
pipe
fuel
air
shall
injector
Prior art date
Application number
PCT/EP2008/007011
Other languages
English (en)
Inventor
Iosif Ursut
Original Assignee
Campean, Romulus
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
Priority claimed from SE0800711A external-priority patent/SE0800711L/xx
Priority claimed from SE0801730A external-priority patent/SE0801730L/xx
Application filed by Campean, Romulus filed Critical Campean, Romulus
Publication of WO2009121384A1 publication Critical patent/WO2009121384A1/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00—Subject-matter not provided for in other groups of this subclass
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D1/00—Burners for combustion of pulverulent fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N3/00—Regulating air supply or draught
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24—HEATING; RANGES; VENTILATING
    • F24H—FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, e.g. HEAT PUMPS, IN GENERAL
    • F24H1/00—Water heaters, e.g. boilers, continuous-flow heaters or water-storage heaters
    • F24H1/10—Continuous-flow heaters, i.e. heaters in which heat is generated only while the water is flowing, e.g. with direct contact of the water with the heating medium
    • F24H1/12—Continuous-flow heaters, i.e. heaters in which heat is generated only while the water is flowing, e.g. with direct contact of the water with the heating medium in which the water is kept separate from the heating medium
    • F24H1/14—Continuous-flow heaters, i.e. heaters in which heat is generated only while the water is flowing, e.g. with direct contact of the water with the heating medium in which the water is kept separate from the heating medium by tubes, e.g. bent in serpentine form
    • F24H1/16—Continuous-flow heaters, i.e. heaters in which heat is generated only while the water is flowing, e.g. with direct contact of the water with the heating medium in which the water is kept separate from the heating medium by tubes, e.g. bent in serpentine form helically or spirally coiled
    • F24H1/165—Continuous-flow heaters, i.e. heaters in which heat is generated only while the water is flowing, e.g. with direct contact of the water with the heating medium in which the water is kept separate from the heating medium by tubes, e.g. bent in serpentine form helically or spirally coiled using fluid fuel

Definitions

  • This invention shall be used by all kinds of combustion contrivance forms which can burn up all kinds of pure fuels, including synthetic, in gas, fluid, solid form.
  • This invention shall apply to a total combustion under complete control of the combustion without any pollution, i.e. the outlet shall be H 2 O, CO 2 and N 2 that are recyclable.
  • the invention refers to how this (the fuels) shall be burned up with an INJECTOR with high compressed air and the air sucks in fuel which becomes homogeneously mixed with the air to give a total combustion.
  • Another field where this invention shall be used is for all different types of engines that are manufactured on earth.
  • the new engines shall take use of an INJECTOR with high compressed air that sucks in gas form or fuel fluid, ethanol, methanol, petrol, jet-fuel, diesel fuel, etc., that shall be ejected into the engine cylinder for combustion and the outlet shall be H 2 O, CO 2 and N 2 which can be recycled, please have a look at Annex 5.
  • the outlets from the new combustion process you can use a labyrinth for irrigation with H 2 CO 3 + N 2 .
  • the labyrinth will be used within agriculture for irrigation of plants with H 2 CO 3 + N 2 which are recycled according to the new combustion process.
  • Reactor R1,R2 and R3 Reactor Rl will be used to obtain vapors for turbine, Reactor R2 used for thermal power station for warmth water and reactor R3it is used for warm up private houses. These Reactors shall use an injector AF at 5 to 250 atm.
  • Figure in Annex 1 displays cylinder geometry with piston.
  • Figure in Annex 2 displays an air compressor connected with an injector.
  • Figure in Annex 3 displays an injector for mixture of air, fuel and coal.
  • Figure in Annex 4 displays the injector nozzle.
  • Figure in Annex 5 displays the recycle of the outlets H 2 O, CO 2 and N 2 .
  • Figure in Annex 6 displays the labyrinth for irrigation with H 2 CO 3 + N 2 of plants with leaves.
  • FIG. 7 displays a pipe with holes made by PVC (a kind of plastic).
  • Figure in Annex 8 displays an injector model AF.
  • Figure in Annex 9 displays a reactor Rl for vapor for a turbine.
  • Figure in Annex 10 displays a reactor R2 for warmth water for a thermal power station.
  • Figure in Annex 11 displays a reactor R3 for warmth water for private houses.
  • the new combustion process under a perfect control and with high compressed air ("jet air") between (5 to 200 or more) atm., for all kinds of purified fuels and with naught/zero outlet of pollutions.
  • jet air high compressed air
  • the high compressed air shall suck in all sorts of fuels until it will be saturated to a complete combustion of the fuel .By the sucking in of the fuel by a higher compressed air the fuel particles will become so fine distributed in the air that it will be homogeneous.
  • the quantity of the fuel that will be sucked in by the compressed air will be under a perfect control and adjusted from a tap that is assembled on the fuel pipe.
  • A The compressed air between (5 - 200 or more) atm., the pressure shall be chosen accordingly/in proportion to the conditions of the fuel viscosity.
  • F The fuel liquid as in Table 1 on page 4/16:
  • A The compressed air between (5 - 200 or more) arm., the pressure shall be chosen in relation to the solid fuel.
  • All the types of injectors described above shall be provided with a tap for both air flow (5 - 200 or more) atm. and the fuel flow.
  • the pressure shall be in relation with V 11 (the combustion chambers volume).
  • the mixture shall be regulated so that the combustion shall be complete and with that only let out H 2 O, CO 2 and N 2 that can be measured.
  • the tap for fuel shall be blocked up at the time of total saturation of the mixture of air under pressure and fuel and shall calibrate the pipe.
  • Mouthpiece through which the mixture of air and fuel is injected in to the engine.
  • Cylinder 11) The spring of the valve for out press of air in the pipes that binds the compressor with the injector. 12) Valve for out press of air in the pipes' injector. 13) Crank to the compressor for air. 14) Cylinder to compressor for air. 15) Air chamber. 16) Valve for intake of air. 17) Spring for intake valve. 18) Filter for air. 19) Roll. 20) Cam (eccentric) that together with a roll starts the crank. 21) Spring for needle. 22) Safety bolt.
  • the new engines shall be provided with INJECTOR model AF, G, that will not pollute the environment.
  • This model of injector will be used together with a compressor that has an equal amount of cylinders as the engine has, i.e. if the engine has 4 cylinders the compressor will also have 4 cylinders.
  • the compressor will replace the fuel pump and the injector shall be assembled into the axis of the cylinder in the cylinder head, and replaces the intake valve.
  • the injector will be opened by a solenoid.
  • A The air [ Compressed air between (20 - 200 or more) atm.]
  • N f the fuel speed
  • M a molecular mass for air
  • Compressed air shall be stored in the pipe that joins the compressor with the injector.
  • the pipe area will be calculated out in relation to the cylinders' (V c + V d ).
  • V t The pipe/tube hole volume
  • the air mass in the air pipe shall be in state with the density and the pressure.
  • ⁇ v volumetric efficiency
  • ni a /ni f is 15,1/1, i.e. to burn up
  • V t the volume of the air pipe.
  • B Bore, 4)
  • V d Displacement volume
  • V c clearance volume
  • Vj injector volume
  • TDC "the pistons' top dead center”
  • BDC "the pistons' bottom dead center”
  • r connecting rod length
  • ⁇ Crank angel
  • a crank offset
  • s the pistons' position.
  • crank angel (intake angel), ⁇ , shall be newly calculated. See Annex 1.
  • Jet- engines and rocket engines will use injector AF, G, plus they will suck in fuel through the compressor axis, the effect of the engine will then ascend.
  • the engines When there is a high compressed air, the engines will be able to work with fine filtrated crude oil, that becomes so homogenous and fine distributed fuel, and this fuel will be injected by the injector.
  • the compressor shall be installed on all the engines in the same position as the pump for fuel is installed in the diesel engines.
  • the furnaces for all the private houses shall be provided with INJECTOR AF, G with a pressure of 5 atm. from a compressor that can provide an entire residential district. This will minimise the consumption with more than half when using fuel (heating) oil.
  • INJECTOR AF, G shall be installed in hermetically sealed boilers/furnaces with outlet pipes.
  • This kind of injector is provided with three different canals, one for the outflow of air and the other two for sucking in of the liquid respective solid fuel.
  • the injectors' outflow, where these three materials already have been mixed, shall have a double conical shape so that you can get a better spreading out and mixture.
  • This principle is applicable on furnaces.
  • This INJECTOR AFS shall be installed in a hermetically sealed furnace or boiler. This kind of injector will mix:
  • the intake of fuel and coal shall be regulated with a tap.
  • the air will also be regulated with a tap that will be opened till maximum wide when it's time for combustion.
  • a 8 the pipe area for the compressed air flow.
  • a f the pipe area for the fuel flow.
  • a 5 the pipe area for the coal flow.
  • R 1 radius for the fuel pipe.
  • R 2 radius for the coal pipe.
  • R 3 radius for the compressed air pipe.
  • a a ⁇ R 3 2 - ⁇ R 2 2
  • V t the volume that streams out from the pipe in the kiln under a high pressure.
  • P 1 the compressed air that will be chosen, for example 30 atm.
  • V u the volume that is usable in the kiln.
  • the heating pan shall be constructed after the form of the flame, see Annex 3. This, so that the water, that will be warmed up will be able to absorb the warmth faster and give a result of maximum warmth action.
  • the labyrinth is good even for irrigation of woods nursery, and can even be used for irrigation in greenhouses.
  • the irrigation shall carry on daily, shorter than 20 minutes a day until the ground will be saturated, or maybe every two days. This is up to the agronomist to decide.
  • the labyrinth made out of pipes, see Annex 6, with holes, see Annex 7, is built under the ground to a deep (profoundly) of 80 centimeters. Round the pipe there shall be a radius of 100 mm where there will be arranged a gravel circular round the pipe, for the hole not to be stuffed up with soil.
  • REACTOR Rl is for vapour to a turbine, R2 for thermal power station and R3 as small as a boiler, with inside new combustion process between 5 to 250 atm, and without any pollution. These reactors will be used in a closed circuit to produce vapour and the water will be warmed up directly in contact with flames from the new combustion process, hi this situation water take up all heating value from the fuels.
  • the combustion in reactor Rl shall be made up of 16 INJECTOR model AF., placed in two row or more. This injector is seen in Annex 8. This INJECTOR model AF, will use 250 atm., compressed air, for combustion inside the REACTOR Rl. Through this new combustion process H 2 CO 3 + N 2 is obtain, which will be part of vapour in circuit. H 2 CO 3 +N 2 and will be recycled with a reservoir for 25 litres.
  • A air with high pressure between 5 to 250 atm.
  • F fuel liquid or gas
  • This Injector with high air pressure take in so many of fuel for an total combustion with the new combustion process.
  • the reactor Rl shall produce vapour for the turbine with a pressure of up to 200 atm or more, which will start the turbine.
  • the water that is used for vapour will be injected into the reactor with a pressure of 250 atm. through a system formed like a shower, which sprays water over the flames which is on the two rows.
  • the water in direct contact with the heat of the flames will rapidly take up all heating value and transform into vapour.
  • the size of the reactor is chosen in state to the quantity of vapour (or water) that is needed for starting up the turbine.
  • An example for a reactor with 2 m in diameter is that 4 m 3 will be used for flame space and the rest is for a volume for stockroom of vapours and spiral pipe.
  • the vapour shall be stored up to 200 atm. before it is used inside the turbine together with H 2 CO 3 + N 2 which is obtained from the new combustion process.
  • the reactor Rl for vapour (or warmth water) has a valve, on the pipe for the turbine, the valve unlocks at 200 atm..
  • This reactor Rl can also use injector AFS with coal that will have a shower that will be assembled under the flames. Example; for warming up 120 litre water to 100° degrees Celsius you need 1 litre of combustible oil.
  • Reactor Rl see in Annex 9.
  • the reactor Rl shall be hermetically isolated for a maximum efficiency and shall have a warning system for the maximum temperature of 110°C and for the pressure a maximum of 200 atm..
  • the thermal power station reactor R2 shall usel2 injector AF with compressed air of 50 atm. this work on two rows or more. For the warming up of the water that shall be injected into the reactor over the flames, there shall be a temperature of up till or more than 100°C with a pressure of 30 atm., but it may be lowered in a place to live or else it can be dangerous.
  • the reactor shall be used in a closed circuit and H 2 CO 3 + N 2 that were obtained through the new combustion process shall be recycled from the circuit.
  • the price for warmth shall be 80 % less than the actual price of today, because there is so little fuel that shall be used for heating up the water.
  • Example from the total space in the reactor the flame shall have a 3 m 3 space, and the remaining 8 m 3 space shall be stock for water and for spiral pipe.
  • This reactor has zero exhaust of pollution.
  • the reactor R2 is used to warming up water. This reactor R2 will be isolated thermally for maximum efficiency and assemble a warning system for temperature and pressure. Reactor R2 will be seen in Annex 10.
  • Reactor R3 is as big as a boiler and used for a private house.
  • the reactor will use injector AF and a pressure of air at 10 atm..
  • This reactor R3 shall warm up water to 100°C for the private house to be heated. . Water injected in through a shower directly on the flame
  • This reactor will consume two litre of combustible oil during 24 hours and will heat up 240 litres of water for a private house.
  • In the stockroom shall be assembled a spiral of pipes for warming up usually water for private houses.
  • the H 2 CO 3 + N 2 which is obtained from the new combustion process will be used for irrigation in the backyard with a labyrinth.
  • Reactor Rl in spiral pipe will be obtain 250°- 1000° degrees or more, if the new combustion process is regulate so, for warming will be used vapor and H 2 CO 3 +N 2 obtaining from new combustion process it work in close circle, example spiral pipe warming up crude oil for refine up it.
  • the flood for water, fuel, gas or air in a pipe is F or Q.
  • Pl pressure of water, or air in reactor Rl is 250 atm.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

L'invention porte sur un procédé de combustion avec contrôle complet sur tous les combustibles purifiés qui sont soumis à de l'air fortement comprimé (« jetluft ») entre (5 à 200 ou plus) atm., H2O, CO2 et N2 étant des sorties recyclables.
PCT/EP2008/007011 2008-03-31 2008-08-28 Procédé de combustion avec contrôle complet de tous les combustibles purifiés qui sont soumis à de l'air fortement comprimé WO2009121384A1 (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
SE0800711A SE0800711L (sv) 2008-03-31 2008-03-31 Ny förbrännings process under fullständig kontroll för all slags renat bränsle under hög tryckluft ("jetluft") mellan (5 till 200 eller mer) atm, med utsläpp H2O, CO2 och N2 som kan återvinnas
SE0800711-4 2008-03-31
SE0801730A SE0801730L (sv) 2008-07-21 2008-07-21 Irrigationssystem
SE0801730-3 2008-07-21

Publications (1)

Publication Number Publication Date
WO2009121384A1 true WO2009121384A1 (fr) 2009-10-08

Family

ID=40054016

Family Applications (2)

Application Number Title Priority Date Filing Date
PCT/EP2008/007011 WO2009121384A1 (fr) 2008-03-31 2008-08-28 Procédé de combustion avec contrôle complet de tous les combustibles purifiés qui sont soumis à de l'air fortement comprimé
PCT/EP2009/001838 WO2009121473A2 (fr) 2008-03-31 2009-03-16 Nouveau procédé de combustion

Family Applications After (1)

Application Number Title Priority Date Filing Date
PCT/EP2009/001838 WO2009121473A2 (fr) 2008-03-31 2009-03-16 Nouveau procédé de combustion

Country Status (2)

Country Link
EP (1) EP2107303A1 (fr)
WO (2) WO2009121384A1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012154070A1 (fr) * 2011-05-09 2012-11-15 Iosif Ursut Procédé pour obtenir une combustion totale à l'aide d'injecteurs, et injecteurs
DE102014210402A1 (de) * 2014-06-03 2015-12-03 Siemens Aktiengesellschaft Pumpenfreie Metall-Verdüsung und -Verbrennung mittels Unterdruckerzeugung und geeignete Materialflusskontrolle

Citations (14)

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US1157315A (en) * 1913-08-05 1915-10-19 Gen Electric Fuel-injector.
GB114069A (en) * 1917-05-17 1918-03-21 James Park Improvements in Means for Generating Combustion Products under Pressure for use in Motive-power Engines.
GB147240A (en) * 1918-11-16 1920-07-22 Herbert Atkins Improvements in or relating to burners for firing brick kilns, furnaces, or the like
US2484272A (en) * 1947-08-05 1949-10-11 Crowe John Marshall Fluid burner with auxiliary external oxygen supply
GB821467A (en) * 1956-02-24 1959-10-07 Jose Ylla Conte Improvements in or relating to the generation of steam
US3994281A (en) * 1973-09-25 1976-11-30 Ateliers J. Hanrez Societe Anonyme Heat generator of the combustion product condensation type and process for heating a heat-carrying fluid
US4116387A (en) * 1976-05-11 1978-09-26 Eastfield Corporation Mist generator
GB1590341A (en) * 1977-07-25 1981-06-03 Fredrick W L Apparatus and methods for enhancing combustibility of solid fuels
JPS5956605A (ja) * 1982-09-24 1984-04-02 Miura Eng Internatl Kk 重油の酸素燃焼方法
US4569484A (en) * 1984-08-31 1986-02-11 The United States Of America As Represented By The United States Department Of Energy Air blast type coal slurry fuel injector
US4895136A (en) * 1988-09-02 1990-01-23 Kemco Systems, Inc. High-temperature heaters, methods and apparatus
US5630368A (en) * 1993-05-24 1997-05-20 The University Of Tennessee Research Corporation Coal feed and injection system for a coal-fired firetube boiler
US6488496B1 (en) * 2001-09-06 2002-12-03 Hauck Manufacturing Co. Compact combination burner with adjustable spin section
WO2003036064A1 (fr) * 2001-10-26 2003-05-01 Alstom Technology Ltd Turbine a gaz adaptee pour etre utilisee avec un taux de recirculation de gaz d'echappement eleve et procede d'utilisation

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GB191509802A (en) * 1915-07-06 1916-03-30 Robur Motoren Ges M B H Improved Process and Apparatus for Introducing and Atomizing the Fuel of Internal Combustion Engines.
US4823756A (en) * 1988-03-24 1989-04-25 North Dakota State University Of Agriculture And Applied Science Nozzle system for engines
US5190216A (en) * 1991-04-19 1993-03-02 Deneke Carl F Fuel-injection apparatus for internal combustion engines
DE10150931A1 (de) * 2001-10-11 2003-04-30 Lueder Gerking Verbesserte Gemischbildung in Verbrennungskraftmaschinen
DE10212439B4 (de) * 2002-03-21 2004-10-07 Kaibel, Jens, Dipl.-Ing. Vorrichtung und Verfahren zum Erzeugen feiner Tropfen

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1157315A (en) * 1913-08-05 1915-10-19 Gen Electric Fuel-injector.
GB114069A (en) * 1917-05-17 1918-03-21 James Park Improvements in Means for Generating Combustion Products under Pressure for use in Motive-power Engines.
GB147240A (en) * 1918-11-16 1920-07-22 Herbert Atkins Improvements in or relating to burners for firing brick kilns, furnaces, or the like
US2484272A (en) * 1947-08-05 1949-10-11 Crowe John Marshall Fluid burner with auxiliary external oxygen supply
GB821467A (en) * 1956-02-24 1959-10-07 Jose Ylla Conte Improvements in or relating to the generation of steam
US3994281A (en) * 1973-09-25 1976-11-30 Ateliers J. Hanrez Societe Anonyme Heat generator of the combustion product condensation type and process for heating a heat-carrying fluid
US4116387A (en) * 1976-05-11 1978-09-26 Eastfield Corporation Mist generator
GB1590341A (en) * 1977-07-25 1981-06-03 Fredrick W L Apparatus and methods for enhancing combustibility of solid fuels
JPS5956605A (ja) * 1982-09-24 1984-04-02 Miura Eng Internatl Kk 重油の酸素燃焼方法
US4569484A (en) * 1984-08-31 1986-02-11 The United States Of America As Represented By The United States Department Of Energy Air blast type coal slurry fuel injector
US4895136A (en) * 1988-09-02 1990-01-23 Kemco Systems, Inc. High-temperature heaters, methods and apparatus
US5630368A (en) * 1993-05-24 1997-05-20 The University Of Tennessee Research Corporation Coal feed and injection system for a coal-fired firetube boiler
US6488496B1 (en) * 2001-09-06 2002-12-03 Hauck Manufacturing Co. Compact combination burner with adjustable spin section
WO2003036064A1 (fr) * 2001-10-26 2003-05-01 Alstom Technology Ltd Turbine a gaz adaptee pour etre utilisee avec un taux de recirculation de gaz d'echappement eleve et procede d'utilisation

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012154070A1 (fr) * 2011-05-09 2012-11-15 Iosif Ursut Procédé pour obtenir une combustion totale à l'aide d'injecteurs, et injecteurs
DE102014210402A1 (de) * 2014-06-03 2015-12-03 Siemens Aktiengesellschaft Pumpenfreie Metall-Verdüsung und -Verbrennung mittels Unterdruckerzeugung und geeignete Materialflusskontrolle

Also Published As

Publication number Publication date
WO2009121473A2 (fr) 2009-10-08
EP2107303A1 (fr) 2009-10-07
WO2009121473A3 (fr) 2010-05-20

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