FR2868351A1 - DEVICE FOR CUTTING A STRUCTURE IN A MOTOR VEHICLE - Google Patents
DEVICE FOR CUTTING A STRUCTURE IN A MOTOR VEHICLE Download PDFInfo
- Publication number
- FR2868351A1 FR2868351A1 FR0403469A FR0403469A FR2868351A1 FR 2868351 A1 FR2868351 A1 FR 2868351A1 FR 0403469 A FR0403469 A FR 0403469A FR 0403469 A FR0403469 A FR 0403469A FR 2868351 A1 FR2868351 A1 FR 2868351A1
- Authority
- FR
- France
- Prior art keywords
- tube
- pyrotechnic charge
- groove
- charge
- pyrotechnic
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B26—HAND CUTTING TOOLS; CUTTING; SEVERING
- B26F—PERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
- B26F3/00—Severing by means other than cutting; Apparatus therefor
- B26F3/04—Severing by squeezing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
- F42B15/38—Ring-shaped explosive elements for the separation of rocket parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B3/00—Blasting cartridges, i.e. case and explosive
- F42B3/006—Explosive bolts; Explosive actuators
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Forests & Forestry (AREA)
- Air Bags (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
- Body Structure For Vehicles (AREA)
- Harvester Elements (AREA)
Abstract
Description
Le domaine technique de l'invention est celui de la sécurité automobileThe technical field of the invention is that of automobile safety
impliquant des dispositifs de découpe d'une structure comme, par exemple, un tableau de bord, afin de mettre en action un dispositif de involving cutting devices of a structure such as, for example, a dashboard, in order to activate a
sécurité. Les dispositifs de découpe selon l'invention sont particulièrement adaptés à la mise en oeuvre de coussins de protection dans un véhicule automobile. security. The cutting devices according to the invention are particularly suitable for the implementation of protective cushions in a motor vehicle.
Les dispositifs de découpe de structure ont déjà fait l'objet de plusieurs brevets. Structural cutting devices have already been the subject of several patents.
On peut citer le brevet EP 0 273 061 qui décrit un joint de séparation entre deux structures et impliquant une charge explosive linéaire confinée dans un tube aplati. Les deux structures s'emboîtent l'une dans l'autre et la mise à feu de la charge explosive provoque une expansion du tube qui déforme alors l'une des deux structures entraînant leur désolidarisation. La charge explosive n'est pas spécifiquement décrite mais la description dévoile quelques indices qui laissent à penser qu'il s'agit d'une charge détonante. Patent EP 0 273 061 describes a separation joint between two structures and involves a linear explosive charge confined in a flattened tube. The two structures fit into each other and the firing of the explosive charge causes an expansion of the tube which then deforms one of the two structures causing their disengagement. The explosive charge is not specifically described but the description reveals some clues that suggest that it is a detonating charge.
De même, le dispositif de séparation divulgué dans le brevet US 6,170,400 ou dans le brevet US 5,372,071 met en jeu un cordeau détonant dont la mise à feu va provoquer la déformation du tube dans lequel il est logé afin de repousser un piston pour séparer deux sous- ensembles. Similarly, the separation device disclosed in US Patent 6,170,400 or in US Pat. No. 5,372,071 involves a detonating cord whose firing will cause the deformation of the tube in which it is housed in order to push a piston to separate two sub - sets.
Enfin on peut mentionner le brevet US 5,478,106 qui décrit un système d'ouverture pour le déploiement d'un airbag. Ce système d'ouverture comprend un tube déformé présentant une partie effilée et dans lequel est logée une charge pyrotechnique linéaire. La mise à feu de ladite charge provoque l'expansion du tube dont la partie effilée vient au contact de la structure pour la découper. Finally, mention may be made of US Pat. No. 5,478,106, which describes an opening system for the deployment of an airbag. This opening system comprises a deformed tube having a tapered portion and in which is housed a linear pyrotechnic charge. The firing of said load causes the expansion of the tube whose tapered portion comes into contact with the structure to cut it.
Les dispositifs de découpe selon l'invention font intervenir des cordeaux déflagrants, logés dans des tubes aplatis et leur mise à feu provoque une expansion de la section desdits tubes pour découper une structure. The cutting devices according to the invention involve explosion cords, housed in flattened tubes and their firing causes an expansion of the section of said tubes to cut a structure.
Les cordeaux déflagrants ont des vitesses de réactions plus lentes que celles des cordeaux détonants et par conséquent, les effets pyrotechniques associés sont moins violents et en particulier, les risques de projection d'éclats et d'émission d'une onde de choc aérienne vers l'extérieur desdits dispositifs deviennent négligeables. Les dispositifs de découpe selon l'invention sont particulièrement adaptés aux véhicules automobiles dans la mesure où ils sont fiables et efficaces, tout en présentant un niveau de sécurité accru en limitant l'intensité de la réaction et donc les possibilités de dommages corporels. Explosion cords have slower reaction speeds than those of detonating cords and therefore the associated pyrotechnic effects are less violent and in particular the risk of splintering and emission of an air-to-air shock wave. outside said devices become negligible. The cutting devices according to the invention are particularly suitable for motor vehicles to the extent that they are reliable and effective, while having an increased level of safety by limiting the intensity of the reaction and therefore the potential for bodily injury.
L'objet de la présente invention concerne un dispositif de découpe d'une structure dans une automobile comprenant une charge pyrotechnique linéaire placée dans un tube déformable aplati, la combustion de ladite charge entraînant la déformation du tube qui accroît sa section, ladite déformation provoquant la rupture de la structure, caractérisé en ce que la vitesse de combustion de la charge pyrotechnique est inférieure à 3000m/s. The object of the present invention relates to a device for cutting a structure in an automobile comprising a linear pyrotechnic charge placed in a flattened deformable tube, the combustion of said load causing the deformation of the tube which increases its section, said deformation causing the rupture of the structure, characterized in that the combustion rate of the pyrotechnic charge is less than 3000 m / s.
Dans cette demande de brevet, les expressions "charge déflagrante" et "charge dont la vitesse de combustion est inférieure à 3000m/s" sont équivalentes. In this patent application, the terms "explosion charge" and "charge whose combustion rate is less than 3000m / s" are equivalent.
Cette équivalence est souhaitable car une déflagration bien que définissant une réaction plus longue et moins violente qu'une détonation reste relativement peu déterminée quant à la valeur de certains paramètres qui la caractérisent. This equivalence is desirable because a deflagration although defining a reaction longer and less violent than a detonation remains relatively indeterminate as to the value of certain parameters which characterize it.
Préférentiellement, la vitesse de combustion de la charge pyrotechnique est comprise entre l000m/s et 2OOOm/s. Preferably, the combustion rate of the pyrotechnic charge is between 1000m / s and 20000m / s.
Les charges déflagrantes retenues pour les dispositifs de découpe selon l'invention sont suffisamment vives pour provoquer la découpe d'une structure dans un véhicule automobile, sans présenter les désagréments liés à l'utilisation d'une charge détonante comme par exemple, les risques de rupture du dispositif de découpe avec émission d'effets pyrotechniques indésirables tels que onde de choc aérienne et projection d'éclats. The explosive charges retained for the cutting devices according to the invention are sufficiently sharp to cause the cutting of a structure in a motor vehicle, without presenting the inconveniences associated with the use of a detonating charge, such as, for example, the risks of rupture of the cutting device with emission of undesirable pyrotechnic effects such as air shock wave and splinters projection.
Avantageusement, la charge pyrotechnique comprend une pluralité de brins comme par exemple, celles qui 15 sont décrites dans le brevet US 4,220, 087. Advantageously, the pyrotechnic charge comprises a plurality of strands, for example those described in US Pat. No. 4,220,087.
De façon préférentielle, le tube est métallique. Preferably, the tube is metallic.
De façon avantageusement, ledit tube présente une bonne aptitude à la déformation plastique. Advantageously, said tube has a good aptitude for plastic deformation.
Préférentiellement, le tube est obturé à chacune de 20 ses extrémités par un bouchon afin de contenir les effets pyrotechniques à l'intérieur dudit tube. Preferably, the tube is closed at each of its ends by a plug in order to contain the pyrotechnic effects inside said tube.
En effet, les exigences en matière de sécurité automobile étant particulièrement élevées, il est recommandé de minimiser les risques de propagation d'effets intempestifs à l'extérieur du dispositif de découpe. Indeed, the requirements for automotive safety being particularly high, it is recommended to minimize the risk of propagation of unwanted effects outside the cutting device.
De façon préférentielle, le tube est en aluminium. Preferably, the tube is aluminum.
De façon avantageuse, il existe un espace entre la charge pyrotechnique et le tube, ledit espace étant comblé par une mousse en élastomère destinée, d'une part, à maintenir ladite charge au centre dudit tube et, d'autre part, à augmenter la mise en pression dudit tube. De cette manière, cela permet avec une faible charge pyrotechnique et donc une faible quantité de gaz produit, de maximiser la contrainte dans des tubes même 2868351 4 résistants, pour qu'ils retrouvent leur forme cylindrique originale. Advantageously, there is a space between the pyrotechnic charge and the tube, said space being filled by an elastomer foam intended, on the one hand, to maintain said charge in the center of said tube and, on the other hand, to increase the pressurizing said tube. In this way, this makes it possible with a small pyrotechnic charge and therefore a small amount of gas produced, to maximize the stress in the same resistant tubes, so that they regain their original cylindrical shape.
Préférentiellement, un dispositif d'allumage de la charge pyrotechnique comprenant un allumeur, est placé à 5 l'une des extrémités du tube. Preferably, a device for igniting the pyrotechnic charge comprising an igniter, is placed at one end of the tube.
Avantageusement, le tube aplati est logé dans une rainure de la structure ayant une section en forme de Li, le fond de la rainure comportant une rainure secondaire et le tube étant maintenu au moyen d'un clip de fermeture. Advantageously, the flattened tube is housed in a groove of the structure having a section in the form of Li, the bottom of the groove having a secondary groove and the tube being held by means of a closing clip.
De façon préférentielle, la densité linéique de la charge pyrotechnique est inférieure à 4g/m. Preferably, the linear density of the pyrotechnic charge is less than 4 g / m.
Les dispositifs de découpe selon l'invention présentent l'avantage de ne pas être dangereux pour les personnes, que ce soit en fonctionnement normal ou erratique, dans la mesure où les effets produits restent de faible intensité. De plus, ils sont fiables car la mise à feu de telles compositions est parfaitement maîtrisée. Enfin de par la grande diversité des compositions déflagrantes pouvant être utilisées, les dispositifs de découpe selon l'invention peuvent s'adapter à un grand nombre de configurations liées notamment à l'épaisseur de la structure à découper, au matériau constitutif de ladite structure, à la surface à découper. The cutting devices according to the invention have the advantage of not being dangerous for people, whether in normal or erratic operation, insofar as the effects produced remain low intensity. In addition, they are reliable because the firing of such compositions is perfectly controlled. Finally, because of the great diversity of the explosive compositions that can be used, the cutting devices according to the invention can be adapted to a large number of configurations related in particular to the thickness of the structure to be cut, to the material constituting said structure, on the surface to be cut.
On donne, ci-après, la description détaillée d'un mode de réalisation préféré de l'invention en se référant aux figures 1 et 2. The following is a detailed description of a preferred embodiment of the invention with reference to FIGS. 1 and 2.
La figure 1 est une vue en coupe axiale latérale d'un dispositif de découpe selon l'invention, positionné par rapport à la structure à découper et n'ayant pas encore fonctionné. Figure 1 is a side axial sectional view of a cutting device according to the invention, positioned relative to the structure to be cut and has not yet worked.
La figure 2 représente le dispositif de découpe de 35 la figure 1 après fonctionnement. Figure 2 shows the cutting device of Figure 1 after operation.
En se référant à la figure 1 le dispositif de découpe 1 selon l'invention est inséré dans une rainure 2 de la structure 3 à découper, ladite rainure 2 ayant une section en forme de Li et dont le fond comporte une rainure secondaire en forme de v de manière à ce que l'épaisseur de la structure 3 au niveau de ladite rainure secondaire 4 soit minimum. Une charge pyrotechnique 5 linéaire constituée de trois brins est logée au centre d'un tube creux 6 déformable en aluminium, ledit tube 6 étant aplati de façon à présenter une section allongée possédant deux côtés plans, parallèles entre eux, et reliés entre eux par deux segments en arc de cercle, ladite charge 5 se retrouvant au contact des deux côtés plans du tube 6. Referring to Figure 1 the cutting device 1 according to the invention is inserted into a groove 2 of the structure 3 to be cut, said groove 2 having a section in the form of Li and whose bottom has a secondary groove in the form of v so that the thickness of the structure 3 at said secondary groove 4 is minimum. A linear pyrotechnic charge consisting of three strands is housed in the center of a deformable hollow aluminum tube 6, said tube 6 being flattened so as to have an elongated section having two planar sides, parallel to each other, and interconnected by two segments in an arc of circle, said load 5 being found in contact with both planar sides of the tube 6.
L'espace subsistant entre la charge pyrotechnique 5 et la paroi interne du tube 6 est comblé par une mousse en élastomère 7 pour contribuer ä maintenir ladite charge 5 au centre dudit tube 6. Le tube 6 occupe la rainure 2 sans jeu latéral, autrement dit, les deux côtés plans du tube 6 sont chacun au contact des parois de la rainure 2. La rainure 2 est pratiquée dans un bourrelet de la structure 3 et le tube 6 est maintenu dans la rainure 2 au moyen d'un clip 8 de fermeture recouvrant ladite rainure 2. Le tube 6 dans la rainure 2 se retrouve au contact à la fois du fond de ladite rainure 2 et du clip 8 de fermeture. Un dispositif d'allumage comprenant un simple allumeur est placé à proximité du tube 6. Deux bouchons obturent les extrémités dudit tube 6. The space remaining between the pyrotechnic charge 5 and the inner wall of the tube 6 is filled by an elastomer foam 7 to help maintain said load 5 at the center of said tube 6. The tube 6 occupies the groove 2 without lateral play, that is to say , the two planar sides of the tube 6 are each in contact with the walls of the groove 2. The groove 2 is formed in a bead of the structure 3 and the tube 6 is held in the groove 2 by means of a closure clip 8 covering the groove 2. The tube 6 in the groove 2 is in contact with both the bottom of said groove 2 and the closure clip 8. An ignition device comprising a single igniter is placed near the tube 6. Two plugs close the ends of said tube 6.
En se référant aux figures 1 et 2, le mode de 30 fonctionnement du dispositif de découpe selon l'invention est le suivant. Referring to FIGS. 1 and 2, the mode of operation of the cutting device according to the invention is as follows.
La mise à feu de la charge pyrotechnique 5 entraîne la production de gaz dans le tube 6 qui subit alors une pression interne importante. Le tube 6 réagit en se déformant pour adopter une section circulaire. The firing of the pyrotechnic charge 5 causes the production of gas in the tube 6 which then undergoes a significant internal pressure. The tube 6 reacts by deforming to adopt a circular section.
Cette expansion provoque la rupture de la structure 3 au niveau de son épaisseur la plus faible créée par la rainure secondaire 4, ainsi que celle du clip 8 de fermeture. La structure se retrouve ainsi découpée et 5 tous les effets pyrotechniques restent contenus dans le tube 6. This expansion causes the breaking of the structure 3 at its lowest thickness created by the secondary groove 4, and that of the closure clip 8. The structure is thus cut off and all the pyrotechnic effects remain contained in the tube 6.
Claims (2)
Priority Applications (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0403469A FR2868351B1 (en) | 2004-04-02 | 2004-04-02 | DEVICE FOR CUTTING A STRUCTURE IN A MOTOR VEHICLE |
| US11/065,444 US20050217466A1 (en) | 2004-04-02 | 2005-02-25 | Device for cutting a structure in a motor vehicle |
| JP2005076927A JP2005288686A (en) | 2004-04-02 | 2005-03-17 | Cutting device |
| DE602005000645T DE602005000645T2 (en) | 2004-04-02 | 2005-03-24 | Device for cutting through a vehicle structure |
| AT05290641T ATE355945T1 (en) | 2004-04-02 | 2005-03-24 | DEVICE FOR SEPARATING A VEHICLE STRUCTURE |
| EP05290641A EP1582321B1 (en) | 2004-04-02 | 2005-03-24 | Device for the cutting of an automotive structure |
| ES05290641T ES2281886T3 (en) | 2004-04-02 | 2005-03-24 | CUTTING DEVICE OF A CAR STRUCTURE. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0403469A FR2868351B1 (en) | 2004-04-02 | 2004-04-02 | DEVICE FOR CUTTING A STRUCTURE IN A MOTOR VEHICLE |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2868351A1 true FR2868351A1 (en) | 2005-10-07 |
| FR2868351B1 FR2868351B1 (en) | 2006-06-23 |
Family
ID=34878487
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR0403469A Expired - Fee Related FR2868351B1 (en) | 2004-04-02 | 2004-04-02 | DEVICE FOR CUTTING A STRUCTURE IN A MOTOR VEHICLE |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20050217466A1 (en) |
| EP (1) | EP1582321B1 (en) |
| JP (1) | JP2005288686A (en) |
| AT (1) | ATE355945T1 (en) |
| DE (1) | DE602005000645T2 (en) |
| ES (1) | ES2281886T3 (en) |
| FR (1) | FR2868351B1 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6097523B2 (en) * | 2012-10-26 | 2017-03-15 | 鹿島建設株式会社 | Charged drug and method of setting charged charge |
| CN108195236B (en) * | 2018-01-12 | 2019-03-22 | 北京航空航天大学 | A kind of separate type self-destruction security control device and rocket |
| FR3130363B1 (en) * | 2021-12-15 | 2024-03-01 | Pyroalliance | Set separable by pyrotechnic cutting |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0273061A1 (en) * | 1985-06-24 | 1988-07-06 | McDONNELL DOUGLAS CORPORATION | Separation system |
| US5372071A (en) * | 1993-07-13 | 1994-12-13 | Tracor, Inc. | Thrusting separation system |
| US6170400B1 (en) * | 1998-06-02 | 2001-01-09 | AEROSPATIALE Soci{acute over (e)}t{acute over (e)}Nationale Industrielle | Device for the cutting of nonmetallic parts by means of a pyrotechnic expansion tube |
| FR2806342A1 (en) * | 2000-03-15 | 2001-09-21 | Lacroix Soc E | Device, for controlled shockless rupture of structures, comprises fluid generator connected to energizing system, and flat tube connected to generator between two structure components |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3076408A (en) * | 1958-06-11 | 1963-02-05 | Borg Warner | Controlled fracturing of solids by explosives |
| US3698281A (en) * | 1970-02-27 | 1972-10-17 | Lockheed Aircraft Corp | Explosive system |
| US3741583A (en) * | 1970-06-25 | 1973-06-26 | Nissan Motor | Motor vehicle safety device |
| US4220087A (en) * | 1978-11-20 | 1980-09-02 | Explosive Technology, Inc. | Linear ignition fuse |
| US4301707A (en) * | 1979-10-29 | 1981-11-24 | Mcdonnell Douglas Corporation | Embedded explosive severance of non-metallic materials |
| US5392684A (en) * | 1993-06-25 | 1995-02-28 | The Ensign-Bickford Company | Explosive thrust-producing coupling |
| US5478106A (en) * | 1994-07-22 | 1995-12-26 | Tip Engineering Group, Inc. | Method and arrangement for forming an air bag deployment opening |
| DE69835077T3 (en) * | 1997-09-08 | 2012-01-26 | Zodiac Automotive Us Inc. | INFLATION DEVICE WITH DISTRIBUTED CHARGE |
| US6336611B1 (en) * | 1998-04-09 | 2002-01-08 | Certime Amsterdam B.V. | Collapsible panel and method for controlled collapsing thereof |
| US6454038B2 (en) * | 1998-04-09 | 2002-09-24 | Certime Amsterdam B.V. | Collapsible panel and method for controlled collapsing thereof |
| US6176517B1 (en) * | 1998-10-23 | 2001-01-23 | Autoliv Aspinc. | Gas generating apparatus |
| FR2799708B1 (en) * | 1999-09-24 | 2001-12-07 | Livbag Snc | INFLATABLE METAL STRUCTURE WITH INTEGRATED PYROTECHNIC LOADING |
| US6886469B2 (en) * | 2002-05-17 | 2005-05-03 | Zodiac Automotive Us Inc. | Distributed charge inflator system |
-
2004
- 2004-04-02 FR FR0403469A patent/FR2868351B1/en not_active Expired - Fee Related
-
2005
- 2005-02-25 US US11/065,444 patent/US20050217466A1/en not_active Abandoned
- 2005-03-17 JP JP2005076927A patent/JP2005288686A/en active Pending
- 2005-03-24 ES ES05290641T patent/ES2281886T3/en active Active
- 2005-03-24 AT AT05290641T patent/ATE355945T1/en not_active IP Right Cessation
- 2005-03-24 DE DE602005000645T patent/DE602005000645T2/en active Active
- 2005-03-24 EP EP05290641A patent/EP1582321B1/en not_active Not-in-force
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0273061A1 (en) * | 1985-06-24 | 1988-07-06 | McDONNELL DOUGLAS CORPORATION | Separation system |
| US5372071A (en) * | 1993-07-13 | 1994-12-13 | Tracor, Inc. | Thrusting separation system |
| US6170400B1 (en) * | 1998-06-02 | 2001-01-09 | AEROSPATIALE Soci{acute over (e)}t{acute over (e)}Nationale Industrielle | Device for the cutting of nonmetallic parts by means of a pyrotechnic expansion tube |
| FR2806342A1 (en) * | 2000-03-15 | 2001-09-21 | Lacroix Soc E | Device, for controlled shockless rupture of structures, comprises fluid generator connected to energizing system, and flat tube connected to generator between two structure components |
Also Published As
| Publication number | Publication date |
|---|---|
| DE602005000645D1 (en) | 2007-04-19 |
| EP1582321B1 (en) | 2007-03-07 |
| FR2868351B1 (en) | 2006-06-23 |
| EP1582321A1 (en) | 2005-10-05 |
| ATE355945T1 (en) | 2007-03-15 |
| JP2005288686A (en) | 2005-10-20 |
| US20050217466A1 (en) | 2005-10-06 |
| ES2281886T3 (en) | 2007-10-01 |
| DE602005000645T2 (en) | 2007-11-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| TP | Transmission of property | ||
| CA | Change of address |
Effective date: 20130213 |
|
| CD | Change of name or company name |
Owner name: HERAKLES, FR Effective date: 20130213 |
|
| PLFP | Fee payment |
Year of fee payment: 13 |
|
| PLFP | Fee payment |
Year of fee payment: 14 |
|
| PLFP | Fee payment |
Year of fee payment: 15 |
|
| CD | Change of name or company name |
Owner name: ARIANEGROUP SAS, FR Effective date: 20180621 |
|
| TP | Transmission of property |
Owner name: ARIANEGROUP SAS, FR Effective date: 20180621 |
|
| ST | Notification of lapse |
Effective date: 20191206 |