EP0452538B1 - Propulseur à réaction pour bateaux et avions ainsi que pompes - Google Patents

Propulseur à réaction pour bateaux et avions ainsi que pompes Download PDF

Info

Publication number
EP0452538B1
EP0452538B1 EP19900118422 EP90118422A EP0452538B1 EP 0452538 B1 EP0452538 B1 EP 0452538B1 EP 19900118422 EP19900118422 EP 19900118422 EP 90118422 A EP90118422 A EP 90118422A EP 0452538 B1 EP0452538 B1 EP 0452538B1
Authority
EP
European Patent Office
Prior art keywords
propulsion
characteristic
jet
pipe
casing
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.)
Expired - Lifetime
Application number
EP19900118422
Other languages
German (de)
English (en)
Other versions
EP0452538A1 (fr
Inventor
Reinhard Gabriel
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to EP19900118422 priority Critical patent/EP0452538B1/fr
Publication of EP0452538A1 publication Critical patent/EP0452538A1/fr
Application granted granted Critical
Publication of EP0452538B1 publication Critical patent/EP0452538B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H5/00Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/14Arrangements on vessels of propulsion elements directly acting on water of propellers characterised by being mounted in non-rotating ducts or rings, e.g. adjustable for steering purpose
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H11/00Marine propulsion by water jets
    • B63H11/02Marine propulsion by water jets the propulsive medium being ambient water
    • B63H11/04Marine propulsion by water jets the propulsive medium being ambient water by means of pumps
    • B63H11/08Marine propulsion by water jets the propulsive medium being ambient water by means of pumps of rotary type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/18Rotors
    • F04D29/186Shaftless rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H1/00Propulsive elements directly acting on water
    • B63H1/02Propulsive elements directly acting on water of rotary type
    • B63H1/12Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
    • B63H1/14Propellers
    • B63H1/16Propellers having a shrouding ring attached to blades
    • B63H2001/165Hubless propellers, e.g. peripherally driven shrouds with blades projecting from the shrouds' inside surfaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H2023/005Transmitting power from propulsion power plant to propulsive elements using a drive acting on the periphery of a rotating propulsive element, e.g. on a dented circumferential ring on a propeller, or a propeller acting as rotor of an electric motor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H23/00Transmitting power from propulsion power plant to propulsive elements
    • B63H23/02Transmitting power from propulsion power plant to propulsive elements with mechanical gearing
    • B63H2023/0208Transmitting power from propulsion power plant to propulsive elements with mechanical gearing by means of endless flexible members
    • B63H2023/0216Transmitting power from propulsion power plant to propulsive elements with mechanical gearing by means of endless flexible members by means of belts, or the like
    • B63H2023/0225Transmitting power from propulsion power plant to propulsive elements with mechanical gearing by means of endless flexible members by means of belts, or the like of grooved belts, i.e. with one or more grooves in longitudinal direction of the belt

Definitions

  • the invention relates to a jet drive for water and aircraft and circulation pumps, in which the fluid flowing into a jet pipe (11) is accelerated against the intended direction of travel by at least one propulsion element such as a rotor (17), in which the outer edge of the Screw (17) is firmly connected to the inner jacket of the jet pipe (11) and the inner edge of the screw delimits a central axis-parallel opening and screw and jet pipe (11) rotate together, in which the jet pipe (11) is driven to its outer jacket.
  • a propulsion element such as a rotor (17)
  • the outer edge of the Screw (17) is firmly connected to the inner jacket of the jet pipe (11) and the inner edge of the screw delimits a central axis-parallel opening and screw and jet pipe (11) rotate together, in which the jet pipe (11) is driven to its outer jacket.
  • Such a jet drive is previously known from US-A-3482402.
  • two separately driven jet drives are connected in series in terms of flow.
  • the flow is accelerated in the opposite direction of rotation by constriction of the grids consisting of a larger number of propulsion elements than that of the first.
  • the larger grid area in the second jet pipe however, much greater friction losses and thus turbulent separation phenomena of the flow can be expected, so that the jet drive has a narrow bandwidth.
  • jet drives of this type have thrust generation efficiencies which can only be used in a certain speed range.
  • the invention seeks to remedy this.
  • the object is therefore to create a jet drive of the type described above which is particularly suitable for water and aircraft and which is effective in all other necessary speed ranges.
  • the object of the invention is achieved in a particularly simple manner in that at least one additional propulsion element such as screw propeller (18) is arranged on an outer casing section which is kept free from the mounting of the jet pipe.
  • at least one additional propulsion element such as screw propeller (18) is arranged on an outer casing section which is kept free from the mounting of the jet pipe.
  • boat drives and a circulating pump The boat jacks can also be used in aircraft with a corresponding adjustment.
  • the subject of registration works as follows:
  • the fluid located in the jet pipe 11 is set in rotation by the edge worm 17 and strikes with the still sucked-in fluid on the fluid located in the free central passage and also accelerates it in the direction of passage, as a result of which a strong driving force acting almost over the length of the jet pipe 11 by delivering part of the kinetic energy from the blades to the central flow.
  • the fluid on the front face is continuously drawn in without eddy formation.
  • the central flow compensates for the torque exerted on the overall arrangement, so that, in addition to the vortex-free inflow and the avoidance of eddy formation at the exit, a propulsive force not previously achieved results.
  • An empennage at the output end of the jet pipe 11 is also generally saved in an advantageous manner.
  • jet pipes 11 of a jet drive 10 are each rotatably mounted in a cladding tube housing 12 on bearing rings 13.
  • the cladding tube housing 12 are integrally formed with brackets 14.
  • the jet pipes 11 are driven by toothed belts 15, the teeth 15a of which mesh with a toothed ring 16 arranged on their outer jacket.
  • An auger 17 serves as the propulsion element, which is attached with its outer edge to the inner jacket of the jet pipe 11 and only covers an outer field of the interior of the jet pipe according to the sectional view II-II in FIG. 1a. The same arrangement is shown in FIG. 2.
  • FIG. 3 shows a drive pinion 19 of a motor indicated by its drive shaft 20 for the drive of the jet pipe 11 already described; 4, the pinion 19 meshes directly with the ring gear 16 of the jet pipe 11.
  • the jet pipe 11 is designed as a rotor of an electric motor and carries an armature winding 21 which is supplied with current via a collector 22. A magnetic winding 23 is indicated on the outside.
  • FIG. 6 shows a pressure medium drive with a feed line 24 and a return line 25 and the turbine 26.
  • the two types of drive discussed last are shown in more detail in FIGS. 7 and 8 and above all show the cladding tube housing 12 more clearly.
  • the magnetic winding 23 is accommodated in an embedded chamber 12a in the cladding tube housing 12.
  • the pressure medium acts on blades 28 on the jet tube 11 via nozzles 27 guiding it.
  • FIG. 9 illustrates the arrangement of a jet engine 10 according to the invention in a boat 1.
  • an outlet pipe 29 projecting aft at the rear 1b is held on a stand 2 arranged on the floor by means of a bracket 3a engaging around the outlet pipe 29.
  • Another tube 30 is held at the other end of the stand 2 with its end in a bracket 3b and connected to a water inlet opening 1c in the bilge 1a.
  • the drive shaft 20 of a motor 31 is mounted, the drive pinion 19 of which engages on the ring gear 16 of the jet pipe 11. It is obvious that instead of the drive pinion 19 a larger drive spur gear is used and around it e.g. can drive several jet pipes 11 in a pitch circle. This is indicated schematically in FIGS. 10 and 11 by toothed belts 15.
  • the drive shaft 20 of a boat 1 is inserted into a housing 10a which surrounds the jet engine 10 with the jet pipe 11 and gearbox.
  • FIG. 13 shows an outboard motor 34 which represents a motor 31 and the above-described jet engine 10 as a unit and which can be detached from the stern 1b of the boat 1 with a flange connection 34a.
  • the outboard motor 34 can also be designed to be pivotable about a rudder shaft.
  • the jet pipe 11 is constructed in principle as in Figure 7, with the difference that here Cladding tube housing 12 is designed as a fitting with flange connections 35 and thus serves as a circulation pump in a liquid circuit, for example in a hot water line. It is obvious that both the lubrication and the cooling are not as prophematic as in conventional circulating pumps and that a quiet and therefore less noisy run is guaranteed, as a result of which the jet drive according to the invention is particularly distinguished here.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Claims (14)

  1. Propulseur par réaction pour engins de navigation maritime ou aérienne et pompes de circulation caractérisé en ce que le fluide pénétrant dans la tuyère d'échappement (11) subit dans au moins un élément moteur, par exemple un rotor en forme d'hélice (17), une accélération opposée à la direction de propulsion voulue, en ce que la bordure extérieure de l'hélice (17) est solidement liée à l'enveloppe intérieure de la tuyère d'échappement (11) et la bordure intérieure de l'hélice représents une ouverture centrale parallèle à l'axe, en ce que l'hélice et la tuyère d'échappement (11) rotent en phase, en ce que la tuyère d'échappement (11) est entraînée par son enveloppe extérieure, et en ce qu'il est pourvu d'au moins un élément moteur supplémentaire, telle qu'une hélice propulsive (18), agencé sur un segment de l'enveloppe extérieure ne faisant pas partie de la suspension (12) de la tuyère d'échappement (11).
  2. Propulseur par réaction selon la revendication 1., se caractérisant par la position de l'hélice propulsive (18) à la sortie de la tuyère d'échappement (11).
  3. Propulseur par réaction selon la revendication 1., caractérisé en ce que la tuyère d'échappement (11) est montée dans un tube de gainage, un boîtier tubulaire (12) ou une pièce semblable.
  4. Propulseur par réaction selon la revendication 1., se caractérisant par les convergences de la tuyère d'échappement (11) entre l'entrée (11b) et la sortie (11a) ou sur certains segments de celle-ci.
  5. Propulseur par réaction selon la revendication 1., se caractérisant par l'absence d'élémentes moteurs sur l'enveloppe intérieure à l'entrée (11b) et éventuellement à la sortie (11a) de la tuyère d'échappement (11).
  6. Propulseur par réaction selon la revendication 1., caractérisé en ce que la sortie (11a) de la tuyère d'échappement (11) a la forme d'une tuyère de poussée (32).
  7. Propulseur par réaction selon la revendication 1., caractérisé en ce que l'épaisseur de matériau constituant l'hélice (17) augmente au-delà de la sortie (11a).
  8. Propulseur par réaction selon la revendication 1., caractérisé en ce que le boîtier tubulaire (12) est pourvu au niveau de la suspension d'orifices permettant l'entrée d'eau.
  9. Propulseur par réaction selon la revendication 1., caractérisé en ce que le boîtier tubulaire (12) est fixé à un montant (2) ou à une console (14).
  10. Propulseur par réaction selon la revendication 1., caractérisé en ce que le boîtier tubulaire (12) et la console (14) sont assemblés en un seul élément.
  11. Propulseur par réaction selon au moins l'une quelconque des revendications précédentes, caractérisé en ce que, entre les suspensions (13), la tuyère d'échappement (11) a la forme d'un élément d'entraînement tel que, par exemple, une couronne dentée (16), une ancre (21) ou des pales (28).
  12. Propulseur par réaction selon au moins l'une quelconque des revendications précédentes, caractérisé en ce qu'à l'élément d'entraînement (16, 21, 18) correspond un élément moteur telle qu'une courroie dentée (15), un pignon d'entraînement (19), une bobine électro-magnétique (23) ou une turbine (26), y compris des tuyères (27) pourvues de conduites d'arrivée et d'échappement (24, 25), et en ce que celui-ci est agencé dans la boîtier tubulaire (12) et/ou dans la console (14).
  13. Système de conduites avec pompe de circulation conçue selon au moins l'une quelconque des revendications 1 à 12.
  14. Bateau pourvu d'une propulseur par réaction conçu selon l'une quelconque ou plusieurs des revendications 1 à 12.
EP19900118422 1990-02-06 1990-09-26 Propulseur à réaction pour bateaux et avions ainsi que pompes Expired - Lifetime EP0452538B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP19900118422 EP0452538B1 (fr) 1990-02-06 1990-09-26 Propulseur à réaction pour bateaux et avions ainsi que pompes

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP90102293 1990-02-06
EP90102293 1990-02-06
EP19900118422 EP0452538B1 (fr) 1990-02-06 1990-09-26 Propulseur à réaction pour bateaux et avions ainsi que pompes

Publications (2)

Publication Number Publication Date
EP0452538A1 EP0452538A1 (fr) 1991-10-23
EP0452538B1 true EP0452538B1 (fr) 1994-12-21

Family

ID=26124932

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19900118422 Expired - Lifetime EP0452538B1 (fr) 1990-02-06 1990-09-26 Propulseur à réaction pour bateaux et avions ainsi que pompes

Country Status (1)

Country Link
EP (1) EP0452538B1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5484266A (en) * 1993-02-03 1996-01-16 Murga; Jose High speed electrically driven axial-flow pump and boat driven thereby
WO1998048167A2 (fr) * 1997-04-18 1998-10-29 Centriflow Llc Mecanisme permettant de produire une force motrice pour des applications de pompage
US5951262A (en) * 1997-04-18 1999-09-14 Centriflow Llc Mechanism for providing motive force and for pumping applications
DE10002657A1 (de) * 2000-01-21 2001-07-26 Lothar Bieschewski Elektromotor
DE10002655A1 (de) * 2000-01-21 2001-07-26 Lothar Bieschewski Motorischer Schiffsantrieb

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5490768A (en) * 1993-12-09 1996-02-13 Westinghouse Electric Corporation Water jet propulsor powered by an integral canned electric motor
US6068454A (en) * 1998-04-06 2000-05-30 Ford Motor Company Fuel pump with helical impeller
DE10044101A1 (de) * 2000-09-07 2002-04-04 Schottel Gmbh & Co Kg Antrieb für schnelle Wasserfahrzeuge
EP2370314A2 (fr) * 2008-12-05 2011-10-05 Schottel GmbH Entraînement marin comportant un gicleur de pompe

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1387416A (en) * 1921-03-07 1921-08-09 John M Lemieux Propeller
DE806766C (de) * 1948-10-02 1951-06-18 Luebbe Schnitger Duesen-Propeller
US2656809A (en) * 1951-06-25 1953-10-27 James W Frasure Combination rudder and propulsion device
US2997015A (en) * 1960-07-25 1961-08-22 Harvey E Richter Marine propulsion device
US3482402A (en) * 1967-07-31 1969-12-09 Herbert A Anthoney Sr Fluid propulsion system
BE901181A (fr) * 1984-11-30 1985-03-15 Bulatov Georges Helice de propulsion ou roue de pompe rotative.
DE3508203A1 (de) * 1985-03-08 1986-09-11 Rudolf Dr. 6800 Mannheim Wieser Schiffsantrieb
CH673445A5 (en) * 1987-09-21 1990-03-15 Sicommerce Ag Medium-delivery mechanism - comprises hub-less blade ring with external drive and inside annular housing

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5484266A (en) * 1993-02-03 1996-01-16 Murga; Jose High speed electrically driven axial-flow pump and boat driven thereby
WO1998048167A2 (fr) * 1997-04-18 1998-10-29 Centriflow Llc Mecanisme permettant de produire une force motrice pour des applications de pompage
US5951262A (en) * 1997-04-18 1999-09-14 Centriflow Llc Mechanism for providing motive force and for pumping applications
US6000915A (en) * 1997-04-18 1999-12-14 Centiflow Llc Mechanism for providing motive force and for pumping applications
GB2338516A (en) * 1997-04-18 1999-12-22 Centriflow Llc Mechanism for providing motive force and for pumping applications
GB2338516B (en) * 1997-04-18 2001-11-28 Centriflow Llc Mechanism for providing motive force and for pumping applications
DE10002657A1 (de) * 2000-01-21 2001-07-26 Lothar Bieschewski Elektromotor
DE10002655A1 (de) * 2000-01-21 2001-07-26 Lothar Bieschewski Motorischer Schiffsantrieb
EP1122165A2 (fr) 2000-01-21 2001-08-08 Lothar Bieschewski Propulsion à reaction avec moteur électrique

Also Published As

Publication number Publication date
EP0452538A1 (fr) 1991-10-23

Similar Documents

Publication Publication Date Title
DE60033850T2 (de) Reibungsrotorkomponenten für pumpen, turbinen und getriebe
DE3207852C2 (fr)
EP0115045B1 (fr) Propulseur sous-marin à hélice dont la bague reliant les pales comporte le rotor du moteur électrique entraînant l'hélice
DE102009040471B4 (de) Mechanisch angetriebener Schiffpropulsor mit hohem Wirkungsgrad
EP2279112A1 (fr) Turbomachine présentant au moins deux rotors tournant en sens opposés et une compensation mécanique du couple
EP0452538B1 (fr) Propulseur à réaction pour bateaux et avions ainsi que pompes
EP0241730B1 (fr) Dispositif de propulsion, notamment pour des bateaux à faible tirant d'eau
EP2028102A1 (fr) Hélice de shpadi (et variantes) et développante de ces pales
WO1998019907A1 (fr) Systeme de propulsion a double helice pour navires
DE2757454B2 (de) Wasserstrahlantrieb zum Antrieb und Steuern von insbesondere flachgehenden Wasserfahrzeugen
DE69200164T2 (de) Verbesserung an einer hohlstrahlantriebsvorrichtung.
DE19747561A1 (de) Wasserstrahlsystem
DE3912910C2 (fr)
DE19648417A1 (de) Schiffsantrieb mit einem Ruderpropeller
DE102006028226A1 (de) Gegenläufige koaxiale Luftschrauben und Getriebe hierfür
DE20121672U1 (de) Schiffsantrieb
US3998177A (en) Outboard motor
DE10158320A1 (de) Schiffsantrieb
DE10044101A1 (de) Antrieb für schnelle Wasserfahrzeuge
DE102015111291A1 (de) Strömungsmaschine mit gegenläufigen Schaufelrädern
AT525998B1 (de) Antriebseinheit für ein Wasserfahrzeug mit Wasserleitelementen
EP2948366B1 (fr) Arrangement de propulsion pour bateaux
DE2610257B1 (de) Kraftuebertragungseinrichtung fuer schiffsantriebe
DE112005002761B4 (de) Kombinationspumpe
DE1528855C3 (de) Wasserstrahlantrieb

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: 19910601

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE ES FR GB GR IT LI NL SE

17Q First examination report despatched

Effective date: 19920220

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH DE ES FR GB GR IT LI NL SE

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

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 19941221

Ref country code: ES

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

Effective date: 19941221

Ref country code: BE

Effective date: 19941221

REF Corresponds to:

Ref document number: 115929

Country of ref document: AT

Date of ref document: 19950115

Kind code of ref document: T

REF Corresponds to:

Ref document number: 59008087

Country of ref document: DE

Date of ref document: 19950202

ITF It: translation for a ep patent filed
ET Fr: translation filed
GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 19950324

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: CH

Payment date: 20010830

Year of fee payment: 12

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

Ref country code: AT

Payment date: 20010928

Year of fee payment: 12

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: SE

Payment date: 20020808

Year of fee payment: 13

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

Ref country code: AT

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

Effective date: 20020926

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: 20020930

Ref country code: CH

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

Effective date: 20020930

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

Ref country code: FR

Payment date: 20030926

Year of fee payment: 14

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

Ref country code: SE

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

Effective date: 20030927

EUG Se: european patent has lapsed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

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

Effective date: 20050531

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

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

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.

Effective date: 20050926

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

Ref country code: GB

Payment date: 20061004

Year of fee payment: 17

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

Ref country code: NL

Payment date: 20061017

Year of fee payment: 17

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

Ref country code: DE

Payment date: 20070930

Year of fee payment: 18

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

Effective date: 20070926

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: 20080401

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

Effective date: 20080401

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: 20080401

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: 20070926