EP1367358B1 - Flugzeugbombe mit einer Nasenumhüllung - Google Patents
Flugzeugbombe mit einer Nasenumhüllung Download PDFInfo
- Publication number
- EP1367358B1 EP1367358B1 EP03019851A EP03019851A EP1367358B1 EP 1367358 B1 EP1367358 B1 EP 1367358B1 EP 03019851 A EP03019851 A EP 03019851A EP 03019851 A EP03019851 A EP 03019851A EP 1367358 B1 EP1367358 B1 EP 1367358B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- bomb
- penetrating body
- shroud
- aerial bomb
- shrouded
- 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
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/06—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with hard or heavy core; Kinetic energy penetrators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B25/00—Fall bombs
Definitions
- the present invention relates to aerial bombs, that is, bombs dropped from aircraft, and more particularly, to aerial bombs for penetrating hard targets.
- a bomb typically includes a hard casing having an interior hollow space for containing an explosive material.
- the physical characteristics of the bomb including the weight, center of gravity, moments or inertia, and the aerodynamic shape, all affect the free-fall response of the bomb, whether or not a guidance package is included with the bomb.
- Bombs delivered from aircraft including free-fall guided or unguided bombs, glide bombs, and boosted bombs, must pass rigorous field testing which includes the safe release from a deploying aircraft and accuracy of delivery to the target. These tests must be conducted for each type of aircraft that will carry the bomb. The development of new weapons, therefore, is subject to significant delay and expense before the weapon is qualified for use.
- the ability of a bomb, or other projectile, to penetrate a target is proportional to the mass and the velocity of impact of the projectile and inversely proportional to the cross-sectional area of the bomb. That is, the greater the kinetic energy and the smaller the cross-sectional area, the greater the penetration that can be expected.
- To adapt an existing bomb for greater penetration by reducing the external diameter of the bomb can also result, however, in changes in the mass properties such as weight, center of gravity, moment of inertia, and in the aerodynamic properties, all of which can affect the flight characteristics of the bomb. These changes also require that the adapted bomb be qualified for use.
- the present invention provides an aerial bomb according to claim 1 that overcomes the difficulty in qualification by emulating the pertinent aerodynamic characteristics and mass properties of a qualified bomb, while providing a function not provided by that bomb.
- the present invention provides a bomb having an improved penetrating warhead, that is, a warhead that more deeply penetrates a protected target, however, the bomb is substantially identical in aerodynamic and mass properties to a qualified bomb.
- the bomb of the present invention may be readily qualified by similarity of function to the existing bomb for use on an aircraft.
- the bomb of the invention can use existing guidance packages available for the qualified bomb.
- the invention provides a bomb that emulates the free-fall properties of an existing bomb pertinent to qualification, while at the same time, providing a warhead with the desired improved penetrating capability.
- the warhead is a penetrating body shaped for improved target penetration through a smaller cross-sectional area compared to an existing qualified bomb.
- An aerodynamic shroud mounted around the warhead emulates the shape of the qualified bomb, and the weight, center of gravity and moments of inertia of the bomb (the penetrating body and shroud) closely approximate those properties of the existing bomb.
- FIG 1 is a side view of a shrouded bomb 20 in accordance with the invention.
- the bomb 20 includes a penetrating body 24 or warhead (shown in Figure 2 ) and a shroud 40 shaped to emulate the aerodynamic shape of an existing, qualified bomb.
- the bomb 20 is shaped to emulate the BLU-109/B bomb, that is, the outer shape of the shroud 40 is substantially identical to the outer shape of the hard case of the BLU-109/B.
- the weight, center of gravity, and moments of inertia of the bomb 20 are substantially identical to those physical characteristics of the BLU-109/B.
- the bomb 20 will therefore have the same free-fall and aerodynamic properties as the emulated bomb, and as a result can be carried on any aircraft for which the emulated bomb is qualified. Further, the bomb 20 can be used with any guidance package appropriate for the emulated bomb.
- the improved bomb 20, however, avoids the lengthy and costly flight qualification tests because it is qualified by similarity to the qualified bomb.
- the invention thus provides an aerial bomb that improves on the function of an existing bomb, but qualifies for use by emulating the handling and aerial delivery characteristics of the existing bomb.
- the invention is not limited to emulating a particular qualified bomb, such as the BLU-109/B, which is used as an example here, but, as will be appreciated by those skilled in the art from the following description, the invention may be directed to improvements in other existing bombs.
- the penetrating body 24 in the illustrative embodiment is designed for improved target penetrating capability.
- the penetrating body 24 includes a case formed of a hard, dense material, such as steel, tungsten, or depleted uranium.
- the penetrating body 24 is narrower than the case of the emulated bomb to provide a smaller cross sectional area.
- the penetrating body 24 has an interior hollow space 26 that may contain an explosive.
- the space 26 opens at the tail end of the body 28 and extends toward the nose 30, leaving a solid, nose section.
- a bulkhead 32 is attached to the penetrating body 24 to close the opening at the tail and to support mounting of a fuze that activates the warhead, as further described below.
- the penetrating body 24 is narrower than a BLU-109/B, but has thicker walls to maintain most of the weight of the BLU-109/B.
- the penetrating body 24 has a weight (loaded with an explosive charge) that is between 80% and 90% of the weight of the BLU-109/B.
- the reduced diameter with approximately the same weight increases the penetration ability of the penetrating body as compared to the BLU-109/B by focusing kinetic energy on a smaller impact area.
- the invention is not limited to a particular diameter or weight ratio as compared to an emulated bomb.
- the diameter and weight of the warhead are to be selected, for example, for the penetrating and explosive functions desired, within the constraint of the total weight of the warhead and shroud being approximately equal to that of the emulated weapon.
- the penetrating body 24 is shaped at the nose end 30 with an ogive having a variable radius of curvature.
- the nose end 30 outer shape leads to a cylindrical center portion 34.
- the outer diameter of the penetrating body 24, measured at the cylindrical center portion 34 is 27,178 cm (10.7 inches), as compared to an outer diameter of the BLU-109/B of 37,084 cm (14.6 inches) at a center portion.
- the thickness of the wall 36 of the penetrating body surrounding the bore 26 is 5,74 cm (2.26 inches).
- FIG 3 is an exploded view of the shroud 40 and penetrating body 24.
- the shroud 40 includes a forward clamp 42 and an aft clamp 44 that are fastened to the center portion 34 of the penetrating body 24 in spaced relationship.
- the clamps 42, 44 each are of two-part construction, each having a pair of semicylindrical members that are bolted together about the penetrating body 24.
- the clamps 42, 44 are sized on the inner diameter to closely fit the penetrating body 24 to provide supporting locations for ground handling and storage pallets.
- Shear pins (not illustrated) are mounted in holes in the penetrating body 24 and extend outward therefrom to engage mating holes in the clamps 42, 44. The shear pins prevent the clamps 42, 44 from moving longitudinally and rotating relative to the penetrating body 24 during ground handling of the bomb and while carried on an aircraft.
- clamps 42,44 could be used to prevent movement of the clamps 42,44 on the penetrating body 24.
- longitudinal grooves formed in the penetrating body 24 could engage ribs extending from the clamps 42, 44, or the outer surface of the penetrating body 24 and the inner surfaces of the clamps 42, 44 could be formed as roughened surfaces to provide increased friction between the surfaces.
- the shear pins and the clamps are designed to have a material strength so that they break under the force of impact of the bomb on a target to help the penetrating body 24 shed the shroud 40 for better penetration into the target.
- each clamp 42, 44 includes mounting holes for lugs 48, 50 to mount the bomb on an aircraft hanger system.
- the spacing of the lugs 48, 50 and their position relative to the center of gravity of the bomb 20 is identical to that for the selected weapon, in the illustrated embodiment, the BLU-109/B.
- a single clamp may be used, depending for example, on space and load carrying requirements.
- the shroud 40 also includes skin members that form the outer surface and are shaped to have the aerodynamic characteristics of the emulated bomb.
- the skin members include a nose cone 60 mounted at the nose 30 of the penetrating body 24, and a forward tube 62 mounted between the nose cone 60 and the forward clamp 42.
- the nose cone 60 and forward tube 62 are fastened together, and the forward tube 62 is fastened to the forward clamp 42.
- a nose ring 64 helps secure the nose cone 60 in place and provides a mounting structure for a nose guidance unit, shown in Figures 4 and 5 .
- the forward end 61 of the nose cone 60 is cylindrically shaped and extends longitudinally forward from the penetrating body 24.
- the forward-extending cylinder end 61 is designed upon impact of the warhead on a target to break away from the penetrating body 24, to assist the penetrating body 24 in shedding the forward portion of the shroud.
- an upper shell 70 and a lower shell 72 are fastened.
- the lower shell 72 is made sufficiently thick, typically about 0.5 inches, to help support the weight of the bomb during ground handling by conventional lift equipment, and for resting the bomb on storage pallets.
- the upper shell 70 includes a switch plate 74 which cooperates with a release-indicating switch on the aircraft, which is used to signal the release of the bomb from an aircraft.
- the skin is completed by an aft tube 76 and a tail tube 78.
- the tail tube 78 flares outward to emulate the tail shape of the BLU-109/B.
- a tail ring 80 is fastened on the tail end of the bomb and the shroud, and provides a mounting structure for an aerodynamic tail unit; exemplary tail units are shown in Figures 4 and 7 .
- the clamps 42, 44 provide support for ground handling and storage of the bomb on racks, pallets and lifts. Additional support is provided by support rings which are installed between the penetrating body 24 and the skin elements at the support locations 82, 83 shown by the arrows.
- the support rings may, for example, be "T” or "H” profiled rings, and are positioned to bridge the space between the skin and the penetrating body 24 to help support the weight of the body.
- the unit 20 shown in Figure 1 is designed to have the same length, weight, center of gravity, and aerodynamic shape of the selected, qualified weapon.
- the weight and center of gravity can be adjusted by ballasting the penetrating body 24 or the shroud 40, by the addition or removal of material at selected locations.
- the length of the bore 26, or the thickness of the penetrating body walls 36 can be readily changed to adjust the weight and center of gravity.
- the shroud components, in particular, the clamps 42, 44 may also be adapted in weight and/or size to adjust the center of gravity and total weight
- FIG 4 is a side view of the shrouded bomb 20 with a guidance package attached.
- the guidance package includes a nose guidance unit 102 having target sensing devices (not illustrated), and a tail fin unit 104.
- the nose guidance unit 102 has fins 106 that are controllable by the nose guidance unit 102 for steering the bomb during free-fall and a folding fin stabilization assembly.
- the guidance package, including the fins, does not form a part of this invention, except that the shroud is designed to accept mounting of a guidance package, as explained below.
- the nose ring 64 sits on the nose end of the penetrating body 24, and is fastened to the front end of the penetrating body and to the nose cone 60 of the shroud.
- the nose ring 64 includes a circumferential groove 66 that accepts a mating rib 103 of the nose unit 102.
- a retaining ring 68 secures the nose unit 102 to the nose ring 64.
- FIG. 7 illustrates a tail fin mounting arrangement
- the tail ring 80 includes a v-shaped groove 84 that mates with a conventional ring clamp (not shown) of a tail fin unit
- a fuze 110 is installed in the tail end of the penetrating body 24.
- a power generator 45 a wind-driven turbine, is mounted in a seat 46 in the upper part of the forward clamp 42.
- the generator 45 is active when the bomb is in free-fall to generate electric power to activate the fuze 110.
- a cable 49 to connect the generator 45 to the fuze 110 is routed in a space between the shroud 40 and the penetrating body 24, thus passing under the mid shell 70, along the aft clamp 44 and under the aft tube 76 and tail tube 78.
- the cable 49 is then routed through a hole in the tail ring 80 and into the tail end of the penetrating body 24.
- a safe/arm device may be included with the fuze 110, and mounted in proximity to the fuze 110 within or on the shroud 40.
- the fuze 110 and power generator 45 are not a part of the bomb except that the warhead is designed to accommodate fuzing systems. Other suitable fuzing systems could be used with the bomb.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar Systems Or Details Thereof (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Claims (10)
- Ummantelte Fliegerbombe (20), umfassend:einen Eindringkörper (24), der einen spitzbogenförmigen Bugabschnitt (30) und eine hohle Bohrung umfasst, die eine Öffnung an einem Heckende aufweist und sich zum Bugabschnitt hin erstreckt;eine aerodynamische Ummantelung (40) die an einer Aussenfläche des Eindringkörpers angebracht ist, wobei die Ummantelung Mittel (42, 44, 82, 83) umfasst zum Befestigen der Ummantelung am Eindringkörper; undMittel (69, 66, 84) zum Anbringen eines Bugleitstücks (102) und eines Heckleitstücks (104) an der ummantelten Fliegerbombe;wobei die aerodynamische Form der Ummantelung im Wesentlichen identisch ist mit einer aerodynamischen Form einer ausgewählten, zugelassenen Fliegerbombe und wobei der Eindringkörper und die Ummantelung ein Gewicht, einen Schwerpunkt und Trägheitsmomente aufweisen, die im Wesentlichen gleich sind wie ein Gewicht, ein Schwerpunkt und Trägheitsmomente der ausgewählten, zugelassenen Fliegerbombe.
- Ummantelte Fliegerbombe (20) nach Anspruch 1, wobei ein Außendurchmesser des Eindringkörpers (24) kleiner ist als ein Außendurchmesser der ausgewählten, zugelassenen Fliegerbombe.
- Ummantelte Fliegerbombe (20) nach Anspruch 1, wobei ein Sprengstoff in die Bohrung (26) des Eindringkörpers (24) gepackt ist.
- Ummantelte Fliegerbombe (20) nach Anspruch 1, wobei der Eindringkörper (24) aus Wolfram gebildet ist.
- Ummantelte Fliegerbombe (20) nach Anspruch 1, wobei der Eindringkörper (24) aus abgereichertem Uran gebildet ist.
- Ummantelte Fliegerbombe (20) nach Anspruch 1, wobei die Ummantelung (40) aus einem Material gebildet ist, das eine Stärke aufweist, die geringer ist als eine Stärke eines den Eindringkörper (24) bildenden Materials, so dass die Ummantelung (40) vom Eindringkörper (24) ablösbar ist beim Einschlag an einem Ziel.
- Ummantelte Fliegerbombe (20) nach Anspruch 1, wobei die Mittel (42, 44, 82, 83) zum Befestigen der Ummantelung (40) am Eindringkörper (24) wenigstens eine Klemme (42, 44) umfassen, die an einem mittleren Abschnitt des Eindringkörpers (24) angebracht ist.
- Ummantelte Fliegerbombe (20) nach Anspruch 7, ferner umfassend Anbringungsbügel (48, 50), die an der wenigstens einen Klemme (42, 44) befestigt sind, um die Bombe (20) an einer Tragvorrichtung an einem Flugzeug anzubringen.
- Ummantelte Fliegerbombe (20) nach Anspruch 1, ferner umfassend einen Zünder (110), der am Heckende des Eindringkörpers (24) angebracht ist.
- Ummantelte Fliegerbombe (20) nach Anspruch 9, ferner umfassend eine Sicherheitsarmvorrichtung, die in der Nähe des Zünders (110) angeordnet ist.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE69739004T DE69739004D1 (de) | 1997-12-11 | 1997-12-11 | Flugzeugbombe mit einer Nasenumhüllung |
ES03019851T ES2312702T3 (es) | 1997-12-11 | 1997-12-11 | Bomba aerea provista de una cubierta. |
EP03019851A EP1367358B1 (de) | 1997-12-11 | 1997-12-11 | Flugzeugbombe mit einer Nasenumhüllung |
PT03019851T PT1367358E (pt) | 1997-12-11 | 1997-12-11 | Bomba aérea blindada |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP03019851A EP1367358B1 (de) | 1997-12-11 | 1997-12-11 | Flugzeugbombe mit einer Nasenumhüllung |
PCT/US1997/023112 WO1999030106A1 (en) | 1997-12-11 | 1997-12-11 | Shrouded aerial bomb |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97955029A Division EP1038152B1 (de) | 1997-12-11 | 1997-12-11 | Flugzeugbombe mit einer nasenumhüllung |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1367358A2 EP1367358A2 (de) | 2003-12-03 |
EP1367358A3 EP1367358A3 (de) | 2004-02-25 |
EP1367358B1 true EP1367358B1 (de) | 2008-09-17 |
Family
ID=40551250
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP03019851A Expired - Lifetime EP1367358B1 (de) | 1997-12-11 | 1997-12-11 | Flugzeugbombe mit einer Nasenumhüllung |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP1367358B1 (de) |
PT (1) | PT1367358E (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2521140C1 (ru) * | 2013-02-26 | 2014-06-27 | Олег Иванович Озерецковский | Унифицированная система управляемых авиационных бомб малого калибра |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2671610T3 (es) | 2014-02-11 | 2018-06-07 | Raytheon Company | Munición con múltiples capas de fragmentos |
US9810513B2 (en) | 2014-08-04 | 2017-11-07 | Raytheon Company | Munition modification kit and method of modifying munition |
US9739583B2 (en) | 2014-08-07 | 2017-08-22 | Raytheon Company | Fragmentation munition with limited explosive force |
US9909848B2 (en) | 2015-11-16 | 2018-03-06 | Raytheon Company | Munition having penetrator casing with fuel-oxidizer mixture therein |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4638737A (en) * | 1985-06-28 | 1987-01-27 | The United States Of America As Represented By The Secretary Of The Army | Multi-warhead, anti-armor missile |
DE19535218C1 (de) * | 1995-09-22 | 1997-02-27 | Diehl Gmbh & Co | Ballistisches Geschoß |
-
1997
- 1997-12-11 PT PT03019851T patent/PT1367358E/pt unknown
- 1997-12-11 EP EP03019851A patent/EP1367358B1/de not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2521140C1 (ru) * | 2013-02-26 | 2014-06-27 | Олег Иванович Озерецковский | Унифицированная система управляемых авиационных бомб малого калибра |
Also Published As
Publication number | Publication date |
---|---|
EP1367358A3 (de) | 2004-02-25 |
EP1367358A2 (de) | 2003-12-03 |
PT1367358E (pt) | 2008-10-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AU748098B2 (en) | Shrouded aerial bomb | |
US6276277B1 (en) | Rocket-boosted guided hard target penetrator | |
EP1377792B1 (de) | Basis für ein stabilisiertes präzisionsgeführtes langstrecken projektil | |
EP0718590B1 (de) | Splittergeschoss mit Radialausstoss mit niedriger Geschwindigkeit und bestimmtem Muster | |
US6389977B1 (en) | Shrouded aerial bomb | |
EP3186583B1 (de) | Splittermunition mit begrenzter explosiver kraft | |
US4444117A (en) | Stacked tube submunition dispenser | |
AU2002323387A1 (en) | Precision guided extended range artillery projectile tactical base | |
WO2005026654A2 (en) | Weapon and weapon system employing the same | |
US6408762B1 (en) | Clamp assembly for shrouded aerial bomb | |
US8689694B2 (en) | Flying bomb | |
GB2384291A (en) | General purpose bomb | |
WO2002018865A9 (en) | Shrouded bomb | |
EP1367358B1 (de) | Flugzeugbombe mit einer Nasenumhüllung | |
US5067410A (en) | Flexible wing | |
US4460137A (en) | Ballistic artillery projectile, that is initially spin-stabilized | |
RU2274823C1 (ru) | Танковый противовертолетный снаряд | |
US5649488A (en) | Non-explosive target directed reentry projectile | |
KR101449738B1 (ko) | 복수 폭발분리장치들의 전단파괴 작동에 의한 발사체 분리구조 | |
AU763036B2 (en) | Shrouded aerial bomb | |
AU755006B2 (en) | Shrouded aerial bomb | |
US8590453B2 (en) | Extending boom for stabilizing projectiles launched from an apparatus | |
WO1994023267A1 (en) | Explosive actuated acoustic underwater decoy | |
JP2001264000A (ja) | シュラウドによって囲まれた航空機用爆弾 | |
ES2312702T3 (es) | Bomba aerea provista de una cubierta. |
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: 20030901 |
|
AC | Divisional application: reference to earlier application |
Ref document number: 1038152 Country of ref document: EP Kind code of ref document: P |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: WOOTEN, RONALD L. Inventor name: SCHMACKER, BRUCE E. |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: 7F 42B 12/06 B Ipc: 7F 42B 12/44 A Ipc: 7F 42B 12/62 B Ipc: 7F 42B 25/00 B |
|
AKX | Designation fees paid |
Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
17Q | First examination report despatched |
Effective date: 20050721 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AC | Divisional application: reference to earlier application |
Ref document number: 1038152 Country of ref document: EP Kind code of ref document: P |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE CH DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: PT Ref legal event code: SC4A Free format text: AVAILABILITY OF NATIONAL TRANSLATION Effective date: 20080926 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
REF | Corresponds to: |
Ref document number: 69739004 Country of ref document: DE Date of ref document: 20081030 Kind code of ref document: P |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: BOHEST AG |
|
REG | Reference to a national code |
Ref country code: GR Ref legal event code: EP Ref document number: 20080403443 Country of ref document: GR |
|
REG | Reference to a national code |
Ref country code: DK Ref legal event code: T3 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: PT Payment date: 20081219 Year of fee payment: 12 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2312702 Country of ref document: ES Kind code of ref document: T3 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20081223 Year of fee payment: 12 |
|
BERE | Be: lapsed |
Owner name: LOCKHEED MARTIN CORP. Effective date: 20081231 |
|
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 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081231 Ref country code: FI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081211 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: DK Ref legal event code: EBP |
|
EUG | Se: european patent has lapsed | ||
26N | No opposition filed |
Effective date: 20090618 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20081217 |
|
NLV4 | Nl: lapsed or anulled due to non-payment of the annual fee |
Effective date: 20090701 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
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: 20081231 |
|
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: 20090701 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081231 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081231 Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081211 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20081217 Year of fee payment: 12 |
|
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: 20090701 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081217 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20090105 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20090703 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20081212 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20081212 |
|
REG | Reference to a national code |
Ref country code: PT Ref legal event code: MM4A Free format text: LAPSE DUE TO NON-PAYMENT OF FEES Effective date: 20100611 |
|
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: 20081211 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081211 Ref country code: PT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100611 Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081212 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20100831 |
|
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: 20091231 |
|
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: 20091211 |