EP0441942A1 - Verfahren und vorrichtung zur verbrennung von giftigen sauerstoffarmen abgasen. - Google Patents

Verfahren und vorrichtung zur verbrennung von giftigen sauerstoffarmen abgasen.

Info

Publication number
EP0441942A1
EP0441942A1 EP90913706A EP90913706A EP0441942A1 EP 0441942 A1 EP0441942 A1 EP 0441942A1 EP 90913706 A EP90913706 A EP 90913706A EP 90913706 A EP90913706 A EP 90913706A EP 0441942 A1 EP0441942 A1 EP 0441942A1
Authority
EP
European Patent Office
Prior art keywords
gas
combustion
tunnel
combustion zone
dart
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP90913706A
Other languages
English (en)
French (fr)
Other versions
EP0441942B1 (de
Inventor
Serge Carpentier
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Societe Generale pour les Techniques Nouvelles SA SGN
Original Assignee
Societe Generale pour les Techniques Nouvelles SA SGN
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Societe Generale pour les Techniques Nouvelles SA SGN filed Critical Societe Generale pour les Techniques Nouvelles SA SGN
Publication of EP0441942A1 publication Critical patent/EP0441942A1/de
Application granted granted Critical
Publication of EP0441942B1 publication Critical patent/EP0441942B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G7/00Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
    • F23G7/06Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases
    • F23G7/061Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases with supplementary heating
    • F23G7/065Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases with supplementary heating using gaseous or liquid fuel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23JREMOVAL OR TREATMENT OF COMBUSTION PRODUCTS OR COMBUSTION RESIDUES; FLUES 
    • F23J15/00Arrangements of devices for treating smoke or fumes
    • F23J15/02Arrangements of devices for treating smoke or fumes of purifiers, e.g. for removing noxious material
    • F23J15/022Arrangements of devices for treating smoke or fumes of purifiers, e.g. for removing noxious material for removing solid particulate material from the gasflow
    • F23J15/025Arrangements of devices for treating smoke or fumes of purifiers, e.g. for removing noxious material for removing solid particulate material from the gasflow using filters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23GCREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G2209/00Specific waste
    • F23G2209/14Gaseous waste or fumes
    • F23G2209/142Halogen gases, e.g. silane

Definitions

  • the invention relates to a method and an installation for the destruction by combustion of toxic oxygen-free gaseous effluents.
  • a known treatment method consists in burning
  • the combustion products are not toxic or can be easily eliminated (for example by filtration for arsenious oxide).
  • the patent FR 87 03 729 published under the number 2 612 606 describes such a process with its associated device.
  • the effluent is brought into a combustion zone by a central duct surrounded by a tube bringing the combustible gas, itself surrounded by three annular conduits bringing the combustion air.
  • the gas injection rates and speeds are adjusted for this purpose.
  • the combustible gas stream constitutes a protective sheath for the effluent vis-à-vis the oxidizing gas.
  • the Applicant currently offers a combustion process in which, unlike the prior art, significant turbulence is created.
  • the subject of the invention is a process for the combustion of toxic gaseous effluents devoid of oxygen in a flame comprising a dart supplied with combustible gas and in so-called primary oxidizing gas, process implemented in vacuum and in which said gaseous effluent and a so-called secondary oxidizing gas are introduced separately at said dart, said secondary oxidizing gas being introduced in the form of at least one jet directed towards the axis of said dart at a rate and speed sufficient to ensure an excess by oxidizing. Maintaining the temperature and creating a turbulent gas mass at the level of said dart; The toxic gaseous effLuent being introduced into said turbulent gaseous mass.
  • the invention therefore consists of a process for combustion of toxic gaseous effluents, devoid of oxygen. Such effluent is not, in itself, exposible. They can become so in the presence of oxygen.
  • Said carrier gas consist of Hydrogen, Nitrogen, or a mixture of gases. Air and oxygen are obviously excluded.
  • Said gaseous effluents to be burned according to the process of the invention can, as indicated above, come from the electronic industry.
  • Such effluent is loaded with hydride, in particular phosphines, arsines "and / or si Lanes ... and / or other chemical compounds containing in particular atoms B, P, As, Te, Se, CL, F.
  • Said gaseous effluents can also come from the nuclear industry. It can be pyroLysis gas and / or radioactive gas loaded with tritium.
  • the stinger is obtained from a conventional burner placed at the head of the combustion zone, supplied with combustible gas (natural gas for example) and oxidizing gas (air for example).
  • This oxidizing gas is called primary in the text of the present application to distinguish it from the other oxidizing currents.
  • the flow rate of this primary oxidizing gas is adjusted so as to ensure combustion, with a small excess of oxidizing gas (approximately 10%).
  • so-called secondary oxidizing gas is sent to the dart in the form of a jet (s), at a rate sufficient to ensure an excess of oxidizer, relative to the quantity necessary for the combustion of the toxic effluent, and at a speed sufficient to create a turbulent gas mass at the level of the stinger.
  • the secondary oxidizing gas is, for example, air.
  • the flow rate and the speed of the secondary oxidizing gas are such that the appearance of the sting is modified: it changes color, its shape is disturbed and we observe perverse movements. It is said then that the gas mass is turbulent. This phenomenon is known to those skilled in the art.
  • the flow rate and speed of the secondary oxidant gas must also be determined to ensure temperature maintenance in the combustion zone and excess oxidant.
  • the speeds can go up to several tens of m / s.
  • the secondary oxidizing gas is introduced in the form of one or more jets directed towards the axis of said dart. These jets can converge towards the axis of the dart or else be directed so as to create a peat LLonnai re movement of the oxidizer around said dart; in this case also, the orientation of the jet contributes to the creation of turbulence.
  • the method of the invention is implemented, under vacuum with respect to the atmosphere outside the combustion zone (ambient atmosphere). Such a depression prevents the formation of gas pockets, avoids possible dispersion of the gases to the outside.
  • IT IS EASY BY ELSEWHERE The extraction of gases from the installation in which the process is implemented.
  • This depression is of the order of 0.5 to 6 mbar (or 50 to 600 Pa).
  • the secondary oxidizing gas is brought in by two different circuits producing:
  • the modulable (secondary) oxidant gas stream cools the gas mass and allows the temperature of the combustion zone to be lowered, if necessary. By the absence of said current, the temperature rises, which can be accelerated by adjusting the flow rate of combustible gas / primary oxidant.
  • the toxic gaseous effluent it is sufficient, within the framework of the invention, for the toxic gaseous effluent to be introduced in the form of a jet into the turbulent gas mass (one or more jets). Regardless of where the effluent jet (s) arrives (s) in relation to the arrival of secondary oxidant gas, it is sufficient that turbulence is created on the gas mass .
  • the toxic effluent is of a different nature, it can be introduced in the form of separate jets at the level of the stinger, or else it can be mixed before being introduced.
  • the toxic effLuent can be introduced occasionally.
  • the flow of secondary oxidant gas is generally controlled by the measurement of the temperature in the combustion zone.
  • the method of the invention makes it possible, advantageously, to treat effLuents whose flow and speed are not controlled; It is enough then to regulate the flow rates and speeds of oxidizing gas to result in combustion.
  • the temperature in the combustion zone is generally higher than 900 C for the treatment of the aforementioned toxic gases. Said temperature is advantageously chosen so as to obtain at least 99% destruction of the toxic gases over the whole of the installation - that is to say, a possible complete combustion zone of a post-combustion zone.
  • LaqueLLe the reaction ends- in LaqueLLe
  • the process of the invention is implemented.
  • a so-called post-combustion zone containing a lining of refractory materials.
  • Said lining is advantageously brought to a temperature above the combustion temperature in the combustion zone. Said lining also ensures gas filtration and better distribution of calories in the installation.
  • Said post-combustion zone is obviously, too, in depression (0.5 to 6 mbar preferably).
  • the flow rates and speeds of the oxidizing gases are regulated so as to obtain a temperature of 900 to 1,200 ° C., approximately 1,000 ° C., in the post-combustion zone, within the framework of an application to the toxic effluents listed above. above.
  • the gases leaving can be discharged directly into the atmosphere or be treated, depending on the quantity of toxic residues and the standards of discharge in force.
  • the present invention also relates to an installation for the combustion of toxic gaseous effluents devoid of oxygen, in which the process described above can be implemented.
  • Said installation comprises:
  • tunneL or combustion zone the bottom of which consists of a conical wall open on said tunneL and of the same axis as Him; a burner supplied with combustible gas and gas primary oxidant being disposed on this axis so that the base of the dart is located near the bottom of the tunnel,
  • the (said) tube (s) being oriented (s) so that said oxidant gas is directed in jet (s) towards the dart ,
  • tubing to bring the toxic gaseous effluent to the bottom of said tunnel, the so-called tubing (s) being oriented so that the effLuent is directed in convergent jet (s) ( s) towards the axis of the da rd.
  • tunneL a gas extraction device
  • the installation according to the invention comprises a combustion tunnel, the bottom of which consists of a conical wall.
  • This wall is generally made up of refractory materials over a thickness sufficient to ensure the thermal insulation of
  • the facility vis-à-vis the outside.
  • the burner includes a pipe for the supply of combustible gas and another pipe for the supply of primary oxidizing gas.
  • the burner comprises two concentric tubes, and the tube bringing the fuel is placed back from the bottom of the tunnel cone, in order to facilitate the primary fuel / oxidizer mixture before the development of the dart, the base of the dart being practically at the bottom of the cone of the combustion tunnel.
  • Flow control means are provided on these pipes; they are preferably bonded to the measurement of the temperature in 1 L installation.
  • the secondary oxidant gas is supplied by one or more tubes which pass through the conical wall over its entire thickness.
  • the tubes are dimensioned so that the gas escapes in the form of a jet.
  • These tubes can be given a slit shape so as to cover the jets with a larger surface.
  • a more favorable embodiment consists of providing several pipes, for example three or four, regularly arranged around the circumference of the conical wall.
  • the tubes are arranged so that the jets converge towards the axis of the dart substantially at the same point, or else they are identically inclined around the periphery of the conical wall so as to create a rotary movement of the oxidant gas introduced. .
  • the tubing (s ) bringing the effluent also crosses the conical wall and is (are) arranged so as to direct the jet (s) of effluent towards the axis of the dart sensibly at the same point.
  • tubes separated into two parts by a wall, the jets then opening substantially in the same place.
  • the dimensions of the combustion tunnel are determined by a person skilled in the art depending on the products treated, the combustion temperature to be obtained, the residence time, etc.
  • a device for example an extraction fan, is mounted on the gas extraction pipe to create the vacuum in the installation.
  • An interesting installation comprises a combustion tunnel followed by a post-combustion zone, said zone also comprising refractory walls and its axis advantageously forming an angle with that of the combustion tunnel.
  • the bottom of said zone is provided with a lining of refractory material and a lateral tube allows the outlet of the gases having passed through said lining.
  • an intake valve can be fitted, allowing the passage of oxidant (tertiary oxidant) to the bottom of said post-combustion zone.
  • said valve is used as an expansion valve, to compensate for accidental overpressures.
  • Figures 2A, 2B and 3A show in section (view along the axis of the combustion tunnel) The bottom of the tunnel with the burner and the gas pipes, Figure 3B shows a section view of
  • FIG. 1A shows an installation comprising a combustion tunnel 1 of axis (D) followed by a post-combustion zone 2 disposed perpendicularly to said tunnel.
  • the bottom of the tunneL 1 is constituted by a conical wall 3 open on the tunneL.
  • the tunnel with its bottom is surrounded by a thickness 4 of refractory bricks (or other material) to ensure thermal insulation.
  • a recess is arranged along the axis (D) and over the entire thickness of the conical wall.
  • a dart 8 grows in the bottom of the tunnel.
  • the base of the stinger is at the bottom of the cone of
  • the conical wall in FIG. 1B, it is located in the opening placed on the recess arranged in the bottom of the cone.
  • Tubes 9 and 10 pass through the conical wall to supply the secondary oxidizing gas (air) and the toxic effluent respectively.
  • the tubes 9 are arranged so that their axes converge on the axis (D) of the tunnel at a point A,
  • the tubes 10 in point B and point B is located beyond point A.
  • the tubes 9 converge at points A1 and A2, the tubes 10 at point B and Points A1 and A2 are located beyond point B.
  • the pipes 9 supplying the secondary oxidizing gas have a slit shape while the pipes 10 have a recirculated shape.
  • FIG. 3A presents a preferred variant, in which the tubes 9 are separated into two parts by a partition 11.
  • part 12 the closest to the burner, circulates the secondary oxidizing gas with fixed jet and in part 13 the oxidizing gas. secondary with modular jet.
  • the two parts are then supplied by different pipes. On the supply pipes, there are suitable means of regulating flow and speed.
  • FIG. 1B shows separate tubes 9A and 9B for supplying the secondary oxidizing gas in the form of a modulable and fixed jet respectively.
  • FIG. 2B shows in section Tubings 9B incined so as to create a rotary movement of the secondary oxidizing gas known as a fixed jet around the dart.
  • Tubing 10 is divided into three groups of three tubing 10A, 10B, 10C which each bring a toxic effluent of a different nature, for example.
  • the group pipes are regularly arranged around the circumference of the conical wall.
  • the post-combustion zone 2 which contains at its bottom a lining 14 (in silicon carbide for example) which can be evacuated by a withdrawal door 15 and brought by a door 16.
  • the door 16 may include a cLapet 17 by LequeL arrives then tertiary oxidant (air) which is entrained with the combustion gases towards the lining. The gases which have passed through the lining, leave the installation via the pipe 18.
  • the invention is illustrated by the example below.
  • the cylindrical combustion chamber of which has an external diameter of approximately 1,200 mm, an internal diameter of approximately 400 mm, an approximate internal length of 1,600 mm and of which the post- combustion - which follows said combustion chamber - contains silicon carbide aggregates a gas loaded with arsine, at 6000 ppm in volume, was treated at a flow rate of 14 Nm / h.
  • the carrier gas loaded with arsine is sent in the quarry to the combustion tunnel. It is composed of :
  • the fuel used is natural gas, delivered at a rate of 1.1 Nm / h at the nose of the burner, previously mixed in the burner at 6 Nm / h of primary air (primary oxidant).
  • the air / gas ratio was kept constant, regardless of the burner flame size, with a 10% excess of air compared to stoichiometry.
  • Through the burner outlet also arrives at a speed of 12 m / s
  • the secondary oxidizing gas composed of:
  • the depression in Tunisia is 5 mbar.
  • the temperature measured before the silicon carbide packing is 1000 C.
  • the volume of the fumes at this temperature is 90 Nm 3 / h.
  • Said fumes are then cooled from 1000 C to 700 C in a heat exchanger and then undergo a dilution, by ambient air, of a factor of 4 (325 Nm / h ) to be brought back to a temperature of 100-120 C before a very high efficiency filtration (to stop 99.99% of particles of the order of 0.3 ⁇ m) aimed at retaining the arsenious acid, solid, formed, before rejection to the chimney.
  • the arsine charge is no more than 0.5 ppm by volume.
  • the purification yield provided by the installation is therefore 99.966%, higher than the 99.95% required (after taking into account the dilution on cooling).
  • composition of the fumes at the chimney was approximately as follows:

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Environmental & Geological Engineering (AREA)
  • Incineration Of Waste (AREA)
  • Treating Waste Gases (AREA)
  • Air Supply (AREA)
EP90913706A 1989-09-04 1990-09-04 Verfahren und vorrichtung zur verbrennung von giftigen sauerstofffreien abgasen Expired - Lifetime EP0441942B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR8911548 1989-09-04
FR8911548A FR2651561B1 (fr) 1989-09-04 1989-09-04 Procede et installation pour la combustion d'effluents gazeux toxiques.
PCT/FR1990/000641 WO1991003685A1 (fr) 1989-09-04 1990-09-04 Procede et installation pour la combustion d'effluents gazeux toxiques depourvus d'oxygene

Publications (2)

Publication Number Publication Date
EP0441942A1 true EP0441942A1 (de) 1991-08-21
EP0441942B1 EP0441942B1 (de) 1995-03-22

Family

ID=9385109

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90913706A Expired - Lifetime EP0441942B1 (de) 1989-09-04 1990-09-04 Verfahren und vorrichtung zur verbrennung von giftigen sauerstofffreien abgasen

Country Status (7)

Country Link
US (1) US5169605A (de)
EP (1) EP0441942B1 (de)
JP (1) JPH0816527B2 (de)
CA (1) CA2039727C (de)
DE (1) DE69018059T2 (de)
FR (1) FR2651561B1 (de)
WO (1) WO1991003685A1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1248599B (it) * 1991-05-10 1995-01-19 Bono En S P A Procedimento ed apparecchiatura per la distruzione termica di reflui industriali inquinanti
US5271908A (en) * 1992-04-07 1993-12-21 Intel Corporation Pyrophoric gas neutralization chamber
US5310334A (en) * 1992-06-03 1994-05-10 Air Duke Australia, Ltd. Method and apparatus for thermal destruction of waste
DE4310011C1 (de) * 1993-03-27 1994-05-05 Ltg Lufttechnische Gmbh Verfahren und Vorrichtung zum Verbrennen von Abluft
US6021723A (en) * 1997-06-04 2000-02-08 John A. Vallomy Hazardous waste treatment method and apparatus
FR2782377B1 (fr) * 1998-08-13 2000-09-22 Leces Equipement de post-combustion pour reacteurs industriels
US6969250B1 (en) * 1998-12-01 2005-11-29 Ebara Corporation Exhaust gas treating device
JP4528141B2 (ja) * 2005-01-14 2010-08-18 東京瓦斯株式会社 難燃性物質分解バーナ
JP4619798B2 (ja) * 2005-01-14 2011-01-26 日本パイオニクス株式会社 有害ガスの浄化装置
DE102008037418B3 (de) * 2008-10-07 2010-02-18 Reicat Gmbh Verfahren zur Reinigung von Abgasen durch generative Nachverbrennung
WO2013126452A2 (en) 2012-02-20 2013-08-29 Avery Dennison Corporation Multilayer film for multi-purpose inkjet systems

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3311456A (en) * 1963-03-21 1967-03-28 Universal Oil Prod Co Apparatus for incinerating a waste gas stream
US4199549A (en) * 1964-05-07 1980-04-22 Salem Corporation Method of operating an incinerator
US3552334A (en) * 1969-01-31 1971-01-05 Helmut Springer Incinerator
US4033725A (en) * 1972-02-24 1977-07-05 John Zink Company Apparatus for NOx control using steam-hydrocarbon injection
US4154567A (en) * 1977-01-07 1979-05-15 Continental Carbon Company Method and apparatus for the combustion of waste gases
US4145979A (en) * 1978-01-23 1979-03-27 Envirotech Corporation Afterburner assembly
JPS5546302A (en) * 1978-09-26 1980-04-01 Hitachi Plant Eng & Constr Co Ltd Combustion furnace for methyl bromide gas
DE2857224A1 (de) * 1978-09-28 1980-04-17 Bayer Ag Verfahren und vorrichtung zur verbrennung explosibler gase
JPS62134414A (ja) * 1985-12-04 1987-06-17 Nippon Sanso Kk 半導体製造排ガスの燃焼方法及び同燃焼装置
US4801437A (en) * 1985-12-04 1989-01-31 Japan Oxygen Co., Ltd. Process for treating combustible exhaust gases containing silane and the like
FR2612606B1 (fr) * 1987-03-18 1990-09-14 Air Liquide Procede et dispositif de destruction d'effluents gazeux toxiques
US4920898A (en) * 1988-09-15 1990-05-01 Trw Inc. Gas turbine slagging combustion system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9103685A1 *

Also Published As

Publication number Publication date
FR2651561B1 (fr) 1991-12-27
DE69018059T2 (de) 1995-08-10
DE69018059D1 (de) 1995-04-27
CA2039727A1 (en) 1991-03-05
EP0441942B1 (de) 1995-03-22
JPH04502957A (ja) 1992-05-28
JPH0816527B2 (ja) 1996-02-21
FR2651561A1 (fr) 1991-03-08
WO1991003685A1 (fr) 1991-03-21
US5169605A (en) 1992-12-08
CA2039727C (en) 1998-12-01

Similar Documents

Publication Publication Date Title
EP0441942B1 (de) Verfahren und vorrichtung zur verbrennung von giftigen sauerstofffreien abgasen
CH629886A5 (fr) Procede de combustion d'un combustible carbone.
EP0012091B1 (de) Verfahren und Anlage zur Behandlung von Industriemüll
EP1458902B1 (de) Verfahren und vorrichtung zur verdichtung poröser substrate mittels chemischer dampfinfiltration
EP0524880B1 (de) Verfahren und Anlage für pulsierende Verbrennung
EP2504624B1 (de) Verfahren und vorrichtung zur thermischen zerstörung von organischen verbindungen mit einem induktionsplasma
CN100549526C (zh) 用于能反应形成固态产品的气体燃烧的燃烧器与方法
WO2008148994A2 (fr) Injecteur mixte a bas nox
EP0033285B1 (de) Vorrichtung zum Mischen mit Turbulenz von Gas enthaltenden Fluida und festen Partikeln
SE453120B (sv) Anordning for efterbrenning av med framfor allt kolvatten bemengda avgaser fran destruktionsanleggningar eller liknande
KR20070086017A (ko) 프로세스 저감 동안 입자 침착을 감소시키는 반응 장치
EP0707558A1 (de) Verfahren zur behandlung von verbrennungsrückständen und vorrichtung dafür
WO2015097389A1 (fr) Procédé intégré d'oxycombustion et de production d'oxygène
EP2153128B1 (de) Verdünnte verbrennung
EP0754924A1 (de) Vorrichtung und Verfahren zum Kalzinieren von Rohmehl mit verminderter Stickoxydemission
JPH04504613A (ja) 気流の中の不純物を完全に酸化するための焼却炉
WO2002097327A1 (fr) Generateur thermique et procede de combustion permettant de limiter les emissions d'oxydes d'azote par recombustion des fumees
WO2006117336A1 (fr) Procede de fusion d'une charge ferreuse
EP0336087B1 (de) Verfahren und Vorrichtung zur Behandlung eines Gasstromes, der pyrophorischen Staub enthält
Yang et al. Some experiments on free droplet combustion at low gravity
WO1997024470A1 (fr) Procede de revetement d'un substrat en metal
BE648130A (de)
FR2683620A1 (fr) Enceinte thermique pour le traitement de produits industriels et four a chaux industriel comportant une telle enceinte.
WO2000009947A1 (fr) Equipement de post-combustion pour reacteurs industriels
EP0834042A1 (de) Verfahren und anlage zur verbrennung von krankenhausabfällen

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19910424

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): BE CH DE GB LI NL SE

17Q First examination report despatched

Effective date: 19920928

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): BE CH DE GB LI NL SE

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 19950316

REF Corresponds to:

Ref document number: 69018059

Country of ref document: DE

Date of ref document: 19950427

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 19980825

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 19980922

Year of fee payment: 9

Ref country code: CH

Payment date: 19980922

Year of fee payment: 9

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: THE PATENT HAS BEEN ANNULLED BY A DECISION OF A NATIONAL AUTHORITY

Effective date: 19990929

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19990930

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19990930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20000401

EUG Se: european patent has lapsed

Ref document number: 90913706.9

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 20000401

REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20020827

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20020911

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 20021011

Year of fee payment: 13

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20030904

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20030930

BERE Be: lapsed

Owner name: SOC. GENERALE POUR LES TECHNIQUES NOUVELLES *SGN

Effective date: 20030930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20040401

GBPC Gb: european patent ceased through non-payment of renewal fee