EP0733876A1 - Sicherheitsbehälter für selbstangetriebene Flugkörper - Google Patents

Sicherheitsbehälter für selbstangetriebene Flugkörper Download PDF

Info

Publication number
EP0733876A1
EP0733876A1 EP96460013A EP96460013A EP0733876A1 EP 0733876 A1 EP0733876 A1 EP 0733876A1 EP 96460013 A EP96460013 A EP 96460013A EP 96460013 A EP96460013 A EP 96460013A EP 0733876 A1 EP0733876 A1 EP 0733876A1
Authority
EP
European Patent Office
Prior art keywords
missile
envelope
container according
cradle
door
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
EP96460013A
Other languages
English (en)
French (fr)
Other versions
EP0733876B1 (de
EP0733876B8 (de
Inventor
Francky Le Mezo
Loic Dugor
Patrick Parneix
Roger Le Chenadec
Didier Beninca
Christian Lamamy
Yves Leclerc
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.)
Etat Francais En Daher Lhotellier Csi
Original Assignee
LHOTELLIER MONTRICHARD (SA)
Delegation Generale pour lArmement
Gouvernement de la Republique Francaise
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 LHOTELLIER MONTRICHARD (SA), Delegation Generale pour lArmement, Gouvernement de la Republique Francaise filed Critical LHOTELLIER MONTRICHARD (SA)
Publication of EP0733876A1 publication Critical patent/EP0733876A1/de
Publication of EP0733876B1 publication Critical patent/EP0733876B1/de
Application granted granted Critical
Publication of EP0733876B8 publication Critical patent/EP0733876B8/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/073—Silos for rockets, e.g. mounting or sealing rockets therein
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
    • F42B39/14—Explosion or fire protection arrangements on packages or ammunition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
    • F42B39/20—Packages or ammunition having valves for pressure-equalising; Packages or ammunition having plugs for pressure release, e.g. meltable ; Blow-out panels; Venting arrangements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
    • F42B39/24—Shock-absorbing arrangements in packages, e.g. for shock waves

Definitions

  • the present invention relates to a container for self-propelled ammunition, in particular of the missile type.
  • the current missile containers make it possible to provide the conventional functions of transport, storage and handling of ammunition. They protect them against untimely shocks and the natural environment: high humidity, salty air, etc. On the other hand, they have the major drawback of not having a security function with regard to more severe aggressions such as fire, detonation by influence, impacts of bullets or shrapnel, etc.
  • the invention was carried out with the aim of overcoming this lack, that is to say of securing a container for ammunition and more particularly for missile, and it therefore relates to a container for missile which, while presenting the all the qualities of known containers, and while remaining within acceptable weight and size limits, ensures a safety function by preventing or at least limiting the reactions of the munition contained inside when it is attacked, as well as the effects on the neighborhood of an accidental initiation of this munition.
  • the main object of the invention is to secure such a container against attack.
  • They can be external: impacts of fragments from the outside; local jet of combustion gas attacking the container on one of its walls; fire outside the container; free fall ; particle fields or magnetic field.
  • Securing also concerns the internal aggressions generated by the missile itself by limiting the thrust in the event of the thruster's operation and by limiting, in the event of detonation of the military charge, the external effects and especially the risk of detonation by influence of the charges military stored in neighboring secure containers.
  • the container preferably has a thermal shield on its two side walls. he it is advantageously a layer of ablative material, added, for example by gluing, on the outer skin of the envelope.
  • the ballistic shielding consists of elements separated from the external layer of the envelope by an air space, in order to prevent the direct transmission of shocks to the envelope and to limit thermal transfer phenomena.
  • the use of an intumescent paint as a finish increases the resistance of the container to thermal attack.
  • a secure missile container consists of a sealed envelope formed by an elongated parallelepipedic body 2, closed at the rear by a removable panel 4, and at the front by a door 3 intended for loading and when the missile was unloaded.
  • the body 2 of the container is provided with laying pads 5 ensuring the interface with the ground or another container during stacking, as well as palletizing tunnels 6.
  • the reference 7 designates front and rear belts carrying accessories necessary for handling and stowage.
  • the container body 2 is made of a sandwich, Figs. 2, 3, comprising an inner skin 20 of stainless steel, a balsa core 21 and an outer skin 22 of composite material such as glass-resin composite (CVR).
  • the thickness of the internal skin 20 of stainless steel can be of the order of 2 mm. It provides sealing, mechanical resistance, electromagnetic protection and attachment of elements including a chassis which will be mentioned below.
  • the thickness of the balsa core 21 can be close to 50 mm. It acts as a thermal insulator and gives the sandwich inertia allowing it to withstand the mechanical forces due to the pressure or the thrust of a jet of propellant.
  • the outer skin 22 can have a thickness of the order of 5 mm. It protects the balsa climatically and serves as an interface for mounting the above-mentioned equipment on the outside of the container body 2. All these thicknesses are given by way of example but are in no way limiting.
  • the internal skin 20 is locally reinforced by another layer of highly resistant steel 23, FIG. 4, the layer 23 constituting a splinter protection device.
  • the container body 2 On its upper face, as best seen in Figs. 2 and 3, the container body 2 is provided with ballistic shielding 24 made of metal or composite material, intended to ensure the impact resistance of fragments. Made up of planar elements fixed on profiles, the shield 24 is separated from the external skin 22 by an enclosed space of air, to prevent the direct transmission of shocks and limit the phenomena of thermal transfer.
  • ballistic shielding 24 made of metal or composite material, intended to ensure the impact resistance of fragments.
  • the shield 24 Made up of planar elements fixed on profiles, the shield 24 is separated from the external skin 22 by an enclosed space of air, to prevent the direct transmission of shocks and limit the phenomena of thermal transfer.
  • thermal shielding 25 intended to ensure the resistance to the secondary jet of a propellant.
  • the thermal shielding 25 is an ablative coating such as phenolic carbon, phenolic glass or charged silicone, fixed for example by bonding to the external skin 22. In practice, it can have a thickness of the order of 5 mm.
  • the door 3 is made of a sandwich of the same kind as that constituting the container body 2. It is a door with multi-point closure controlled by a removable central handle 35.
  • the door 3 has a peripheral groove 31 into which a climatic seal 32 is inserted.
  • the seal 32 cooperates with a seal plane 26 mounted at the end of the walls of the container body 2.
  • a second thermal protection seal, not shown, is mounted externally relative to the climate seal 32.
  • the door has externally a central hollow region or bowl 33 at the bottom of which are located the closure system as well as various organs such as pressure gauge, valve, humidity indicator, shock indicators, etc.
  • the handle 35 of the door closing system can be pressed against the bottom of the bowl 33, in the storage position, as shown in solid lines in FIG. 4 and in broken lines in FIG. 5.
  • the cover 34 is produced in a sandwich of the same kind as that constituting the door and the container body.
  • the panel 4 closing the rear of the container, FIG. 1.
  • the panel 4 has internally a peripheral groove 41 containing a climate seal 42, while a thermal seal, not shown, is mounted externally relative to the climate seal 42.
  • the rear panel 4 is fixed to the body of the container by a fixing system ensuring its embrittlement in the event of accidental firing of the missile's propellant.
  • this fixing system can consist of a plurality of thermally protected screws.
  • the container is equipped to receive an assembly formed by a missile and its cradle. To this end, it is provided internally with a chassis 8 mounted on metal cable dampers 81, themselves mounted on supports 82 fixed to the internal steel skin 20.
  • the chassis 8 essentially comprises two metal rails 80, FIGS. 2 and 3, providing support and guidance for the missile's cradle.
  • the cradle 9 comprises a central beam 90 on which are mounted a front collar 91 and a rear collar 92, FIG. 1, the collars 91 and 92 also being joined together above by a bar 93.
  • the wedging material providing the interface between the missile and the front collar can provide additional thermal protection by wrapping the military load.
  • the cradle 9 is provided with an anti-thrust device for the case of accidental firing of the missile thruster: the beam 90 of the cradle is extended beyond the rear collar 92 to carry a plate d stop 94 appearing in FIG. 1.
  • a folding bar 95 provides the upper connection between the rear collar 92 and the stop plate 94.
  • the link bar 95 has not been locked beforehand.
  • the recovery of the forces generated by the thrust of the missile engine is obtained by the mechanical connection of the bars 93 and 95 with the hooking fittings of the missile under aircraft.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Pressure Vessels And Lids Thereof (AREA)
  • Packages (AREA)
  • Burglar Alarm Systems (AREA)
  • Laminated Bodies (AREA)
EP96460013A 1995-03-20 1996-03-19 Sicherheitsbehälter für selbstangetriebene Flugkörper Expired - Lifetime EP0733876B8 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9503522A FR2732106B1 (fr) 1995-03-20 1995-03-20 Conteneur securise pour munition autopropulsee notamment pour missile
FR9503522 1995-03-20

Publications (3)

Publication Number Publication Date
EP0733876A1 true EP0733876A1 (de) 1996-09-25
EP0733876B1 EP0733876B1 (de) 2002-08-14
EP0733876B8 EP0733876B8 (de) 2003-01-02

Family

ID=9477420

Family Applications (1)

Application Number Title Priority Date Filing Date
EP96460013A Expired - Lifetime EP0733876B8 (de) 1995-03-20 1996-03-19 Sicherheitsbehälter für selbstangetriebene Flugkörper

Country Status (4)

Country Link
EP (1) EP0733876B8 (de)
AT (1) ATE222348T1 (de)
DE (1) DE69622901T2 (de)
FR (1) FR2732106B1 (de)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1009979C2 (nl) * 1998-09-01 2000-03-02 Fokker Special Products Lanceerbuis uit composietmateriaal.
CN110921108A (zh) * 2019-12-25 2020-03-27 常州中航泰克船舶装备有限公司 一种长圆柱或长条类物品专用贮运箱
CN111595199A (zh) * 2020-05-14 2020-08-28 湖北三江航天万峰科技发展有限公司 一种发射箱加热控制装置
KR102222030B1 (ko) * 2019-09-19 2021-03-02 주식회사 한화 이동식 유도탄 검사 장치
CN116697833A (zh) * 2023-07-28 2023-09-05 北京爱思达航天科技有限公司 一种复合材料包装箱及其制备方法
RU239116U1 (ru) * 2025-04-14 2025-11-24 Федеральное государственное казённое военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-Морского Флота "Военно-морская академия имени Адмирала Флота Советского Союза Н.Г. Кузнецова" Полуприцеп-фургон для бескрановой перегрузки и боевого оснащения ракет в транспортно-пусковых стаканах

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3368452A (en) * 1965-04-19 1968-02-13 Martin Marietta Corp Shock isolation system
US3823903A (en) * 1972-03-03 1974-07-16 Menasco Mfg Co Dual length pendulum shock absorbing system
US4055247A (en) * 1976-10-22 1977-10-25 The United States Of America As Represented By The United States Energy Research And Development Administration Explosion containment device
EP0284777A1 (de) * 1987-04-02 1988-10-05 Howaldtswerke-Deutsche Werft Ag Ausbildung von Ablauf-, Ausstossrohren oder Behältnissen in U-Booten
EP0304345A1 (de) * 1987-08-04 1989-02-22 Constructions Industrielles De La Mediterranee C.N.I.M. Aufhängungssystem für zylindrische Elemente in Behältern, insbesondere Raketenaufhängungssysteme für Unterwasserlancierungen
FR2656085A1 (fr) * 1987-10-13 1991-06-21 Thomson Brandt Armements Munition explosive protegee contre l'elevation de temperature.
EP0530529A1 (de) * 1991-09-04 1993-03-10 Daimler-Benz Aerospace Aktiengesellschaft Transportbehälter

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3368452A (en) * 1965-04-19 1968-02-13 Martin Marietta Corp Shock isolation system
US3823903A (en) * 1972-03-03 1974-07-16 Menasco Mfg Co Dual length pendulum shock absorbing system
US4055247A (en) * 1976-10-22 1977-10-25 The United States Of America As Represented By The United States Energy Research And Development Administration Explosion containment device
EP0284777A1 (de) * 1987-04-02 1988-10-05 Howaldtswerke-Deutsche Werft Ag Ausbildung von Ablauf-, Ausstossrohren oder Behältnissen in U-Booten
EP0304345A1 (de) * 1987-08-04 1989-02-22 Constructions Industrielles De La Mediterranee C.N.I.M. Aufhängungssystem für zylindrische Elemente in Behältern, insbesondere Raketenaufhängungssysteme für Unterwasserlancierungen
FR2656085A1 (fr) * 1987-10-13 1991-06-21 Thomson Brandt Armements Munition explosive protegee contre l'elevation de temperature.
EP0530529A1 (de) * 1991-09-04 1993-03-10 Daimler-Benz Aerospace Aktiengesellschaft Transportbehälter

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL1009979C2 (nl) * 1998-09-01 2000-03-02 Fokker Special Products Lanceerbuis uit composietmateriaal.
WO2000012952A1 (en) * 1998-09-01 2000-03-09 Fokker Special Products B.V. Launching tube made from composite material
KR102222030B1 (ko) * 2019-09-19 2021-03-02 주식회사 한화 이동식 유도탄 검사 장치
CN110921108A (zh) * 2019-12-25 2020-03-27 常州中航泰克船舶装备有限公司 一种长圆柱或长条类物品专用贮运箱
CN111595199A (zh) * 2020-05-14 2020-08-28 湖北三江航天万峰科技发展有限公司 一种发射箱加热控制装置
CN111595199B (zh) * 2020-05-14 2022-12-23 湖北三江航天万峰科技发展有限公司 一种发射箱加热控制装置
CN116697833A (zh) * 2023-07-28 2023-09-05 北京爱思达航天科技有限公司 一种复合材料包装箱及其制备方法
CN116697833B (zh) * 2023-07-28 2023-12-29 北京爱思达航天科技有限公司 一种复合材料包装箱及其制备方法
RU239116U1 (ru) * 2025-04-14 2025-11-24 Федеральное государственное казённое военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-Морского Флота "Военно-морская академия имени Адмирала Флота Советского Союза Н.Г. Кузнецова" Полуприцеп-фургон для бескрановой перегрузки и боевого оснащения ракет в транспортно-пусковых стаканах

Also Published As

Publication number Publication date
FR2732106A1 (fr) 1996-09-27
EP0733876B1 (de) 2002-08-14
DE69622901T2 (de) 2003-04-10
DE69622901D1 (de) 2002-09-19
ATE222348T1 (de) 2002-08-15
EP0733876B8 (de) 2003-01-02
FR2732106B1 (fr) 1997-05-30

Similar Documents

Publication Publication Date Title
US7520223B2 (en) Explosive effect mitigated containers
US5390580A (en) Lightweight explosive and fire resistant container
US20100257998A1 (en) System and method for protecting vehicle occupants
EP3027511B1 (de) Verfahren und vorrichtung zum verbinden und trennen von zwei elementen mittels verbindungsplatten
CA2426351C (fr) Systeme d'obturation pour un orifice d'un conduit, en particulier pour un orifice d'une voie d'introduction d'air dans la chambre de combustion d'un statoreacteur
US8783157B2 (en) System and method for protecting vehicle occupants
US8418597B2 (en) System and method for protecting vehicle occupants
EP0733876B1 (de) Sicherheitsbehälter für selbstangetriebene Flugkörper
US4041869A (en) Cook-off liner component
US7422102B1 (en) Container for ammunition
JPH05203398A (ja) 輸送容器
EP0578522B1 (de) Verschlusselement für ein Abschussrohr und ein mit diesem Verschlusselement versehenes Abschussrohr
US5611424A (en) Container fuse for enhanced survivability
RU2175457C2 (ru) Контейнер для перевозки опасных и ценных грузов
EP0988239B1 (de) Kastenförmiger behälter zum transport von zerbrechlichen und/oder wertvollen gegenständen
US4458483A (en) Rocket motor end flap
CA1191054A (en) Rapid de-icing system
US4885994A (en) Armor penetration resistance enhancement
EP1637830B1 (de) Vorrichtung zur Abkapselung einer Vielzahl von explosiven Gegenständen
KR20170038204A (ko) 추진장약 포장용기
EP3697703A1 (de) Einheit zum transportieren, aufbewahren und/oder handhaben eines pyrotechnischen produkts
EP0481851B1 (de) Schliess- und Schutzvorrichtung für ein Gasauslasssystem eines senkrechten Abschussmoduls
FR2853053A1 (fr) Blindage actif
GB1605450A (en) Protective systems
EP2956738B1 (de) Leichtes waffensystem

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

AK Designated contracting states

Kind code of ref document: A1

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

17P Request for examination filed

Effective date: 19970124

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

17Q First examination report despatched

Effective date: 20010726

RBV Designated contracting states (corrected)

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

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

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 DK ES FI GB IT LI NL SE

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20020814

Ref country code: FI

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: 20020814

Ref country code: AT

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: 20020814

REF Corresponds to:

Ref document number: 222348

Country of ref document: AT

Date of ref document: 20020815

Kind code of ref document: T

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

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

Effective date: 20020814

REF Corresponds to:

Ref document number: 69622901

Country of ref document: DE

Date of ref document: 20020919

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: DAHER LHOTELLIER CSI

Owner name: ETAT FRANCAIS REPRESENTE PAR LE DELEGUE GENERAL PO

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20021114

Ref country code: DK

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: 20021114

NLT2 Nl: modifications (of names), taken from the european patent patent bulletin

Owner name: ETAT FRANCAIS EN DAHER LHOTELLIER CSI

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

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: 20030228

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: 20030331

Ref country code: CH

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

Effective date: 20030331

Ref country code: BE

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

Effective date: 20030331

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

Effective date: 20030515

BERE Be: lapsed

Owner name: S.A. *LHOTELLIER MONTRICHARD

Effective date: 20030331

Owner name: ETAT FRANCAIS REPRESENTE PAR LE DELEGUE GENERAL PO

Effective date: 20030331

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: GB

Ref legal event code: 732E

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

Ref country code: IT

Payment date: 20140318

Year of fee payment: 19

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

Ref country code: GB

Payment date: 20140319

Year of fee payment: 19

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

Ref country code: DE

Payment date: 20140417

Year of fee payment: 19

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 69622901

Country of ref document: DE

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

Effective date: 20150319

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

Effective date: 20150319

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: 20150319

Ref country code: DE

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

Effective date: 20151001