EP2095059B1 - Ummantelte penetrationsfliegerbombe - Google Patents

Ummantelte penetrationsfliegerbombe Download PDF

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Publication number
EP2095059B1
EP2095059B1 EP07872427A EP07872427A EP2095059B1 EP 2095059 B1 EP2095059 B1 EP 2095059B1 EP 07872427 A EP07872427 A EP 07872427A EP 07872427 A EP07872427 A EP 07872427A EP 2095059 B1 EP2095059 B1 EP 2095059B1
Authority
EP
European Patent Office
Prior art keywords
bomb
hollow
penetrating body
outer casing
bomb according
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.)
Not-in-force
Application number
EP07872427A
Other languages
English (en)
French (fr)
Other versions
EP2095059A1 (de
Inventor
Christian Martin
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.)
Ateliers Mecaniques De Pont Sur Sambre Ste
Original Assignee
Ateliers Mecaniques De Pont Sur Sambre Ste
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 Ateliers Mecaniques De Pont Sur Sambre Ste filed Critical Ateliers Mecaniques De Pont Sur Sambre Ste
Publication of EP2095059A1 publication Critical patent/EP2095059A1/de
Application granted granted Critical
Publication of EP2095059B1 publication Critical patent/EP2095059B1/de
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F42B12/04—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
    • 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
    • F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • 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 an aerial penetration bomb.
  • a bomb is known to FR2688304
  • An object of the present invention is therefore to solve the problems mentioned above with the aid of a simple solution to implement, reliable and inexpensive.
  • the invention proposes to reduce the dimensions of the penetration body while maintaining the characteristics of a general purpose bomb according to claim 1.
  • FIGS 1 to 4 represent an aerial penetration bomb 1 according to the present invention. This bomb is intended to be integrated under an aircraft to which it is suspended.
  • This bomb 1 comprises a hollow penetration body 10 made for example by forging in a high elastic limit material, high density and high hardness, such as steel.
  • the material chosen to make the penetration hollow body also ensures a natural fragmentation thereof during the detonation of the active ingredient after penetration of a hard target.
  • the hollow penetration body 10 has a generally cylindrical shape comprising a front portion 11, a central portion 12 and a rear portion 13.
  • the front part 11, or nose has two successive warheads 11a and 11b ending in a penetration point 11c.
  • the double-warped shape of the front portion 11 facilitates penetration of the penetration body 10 into the hard targets and allows an optimal distribution of the stresses generated during the penetration phase.
  • An internal empty zone or hollow 14 is defined inside the trunk 12. This hollow 14 extends over the entire length of the latter and contains an active material 20.
  • the rear portion 13 of the penetration body 10, or base has a tapered conical shape to ensure its continuity with the central portion 12.
  • the base 13 provides the interface with the guide systems or is protected in storage by a hood rear guard 15 which is removable.
  • a sheath 30 is inserted inside the hollow 14 of the penetration body 10, more precisely inside the active material 20.
  • This sheath 30 encloses, for example, detonation initiation means (not shown) and possibly guide means and / or propulsion means.
  • An inner sheath 31 also passes through the active material 20.
  • the sheath 31 allows in particular the passage of cables (not shown) for cooperating with the detonation means.
  • the sheath 31 is connected on the one hand to a sleeve tip 32 fixed to the sheath 30 by means of a tip nut 33, and to an accessory shaft 40. In order to ensure a level of safety sufficient, the fasteners of the sleeve 31 to the accessory well 40 and the sheath 30 are perfectly sealed.
  • the sheath 31 is also made of a material resistant on the one hand to the chemical attack of the various elements constituting the active ingredient and on the other hand to the mechanical forces generated during the life of the product (storage, handling, transport, catapulting,
  • the sheath 30 is connected on the one hand to the tip nut 33 and on the other hand to a closure plate 34 by means of a sheath nut 35 protected by a removable protective cap 36 for the storage of the bomb. Since the bomb 1 is intended for the penetration of hard targets, the sheath 30 is therefore capable of withstanding the decelerations generated by the penetration and the stresses generated by all the elements with which it is interfaced under all the conditions of use applicable to this type of material. Furthermore, the sheath 30 is designed to best ensure the transmission of shock waves between the detonation means and the active or inert material.
  • the accessory shaft 40 is fixed directly on the penetration body 10, more precisely on its trunk 12, by means of screws 42 provided to be sheared during an impact of the bomb 1 against an obstacle generating a deceleration exceeding a determined value, for example of the order of 500 G negative.
  • Accessory well 40 meets the military standards of the general skilled use bomb, particularly in terms of its positioning.
  • the accessory well 40 allows the assembly of a generator necessary for the operation of the cocking system when it is not directly connected to the aircraft, and is protected by a waterproof and removable protective plug 43 in the part of the storage of the bomb.
  • Each suspension ring well 50 and 51 are fixed on the penetration body 10, at its trunk 12.
  • Each suspension ring well is fixed to the trunk 12 by means of screws 52 provided to be sheared during impact of the bomb 1 against an obstacle generating a deceleration exceeding a determined value, for example of the order of 500 G negative.
  • the distance between the center of the suspension ring wells is normalized and is identical to that of a qualified general purpose spray. This makes it possible to hang the bomb 1 of the present invention under many types of aircraft.
  • the suspension of the bomb 1 is for example made using NATO standard suspension rings which are the interface with the aircraft.
  • the front suspension ring well 50 and the accessory well 40 are made in one piece, the three wells being made of a strong metallic material. Furthermore, the two suspension ring wells 50 and 51 are each closed by a waterproof and removable protective cap 53 for storing the bomb.
  • An aerodynamic outer coating 60 is disposed around the penetration body 10.
  • the outer coating 60 is integral with the penetration body 10, that is to say that it is not removable once installed and that it can not be removed. to be separated from the penetrating body 10 only after a violent shock capable of destroying it, in particular during the penetration of the bomb into a hard target.
  • the outer liner 60 is generally cylindrical in shape. It extends over the entire length of the penetrating hollow body 10.
  • the outer coating 60 has an outer profile, a mass and a spatial arrangement around the penetration body 10 determined so as to give the bomb 1, provided with said coating, the same dimensional, volume, mechanical, aerodynamic and inertial characteristics (mass, center of gravity and moments of inertia) as a qualified general purpose bomb, for example an Mk82 model.
  • the outer coating 60 comprises three identical longitudinal elements 62 each fixed directly on the entire length of the penetration body 10.
  • each of these elements 62 extends integrally from one end to the other of the penetration body 10.
  • Each longitudinal element 62 covers one-third of the circumference of the penetration body, that is to say 120 °.
  • the longitudinal members 62 are thermoformed and made of a fiber-reinforced plastics material, such as a Sheet Molding Compound (SMC), for example a polyester and graphite filled fiberglass blend. More specifically, according to a particular embodiment, the longitudinal elements 62 consist of a polyester resin in a proportion by weight ranging from 50% to 100%, glass fibers in a proportion by weight included in the present invention. range from 0% to 30%, for example 10%, the remainder (at most 20%) consisting of graphite and additives ensuring the lightness of the material (density of 0.74 to 0.86 g / dm 3 ) and its electrical conductivity.
  • SMC Sheet Molding Compound
  • Each longitudinal element 62 has a housing 64 receiving a balancing flange 70 made of a high density material, for example greater than or equal to that of steel, and contributing to impart to the bomb 1 said volumetric, dimensional, mechanical characteristics , aerodynamic and inertial identical to those of a general purpose bomb. More precisely, these flanges 70 make it possible to move the mass of inertia around the periphery of the bomb for a better distribution of the masses with respect to its main axes of inertia.
  • a balancing flange 70 made of a high density material, for example greater than or equal to that of steel, and contributing to impart to the bomb 1 said volumetric, dimensional, mechanical characteristics , aerodynamic and inertial identical to those of a general purpose bomb. More precisely, these flanges 70 make it possible to move the mass of inertia around the periphery of the bomb for a better distribution of the masses with respect to its main axes of inertia.
  • Each balancing flange 70 is fixed directly to the hollow penetration body 10 by means of screws 72 intended to be sheared during an impact of the bomb 1 against an obstacle generating a deceleration exceeding a determined value, for example of the order of 500 G negative.
  • One of the flanges 70 has three orifices 75 for the passage of the two suspension ring wells 50 and 51 and the accessory well 40.
  • Each longitudinal element 62 is bonded directly to the hollow penetration body 10, for example using an adhesive polyurethane. Once stuck, they can not be separated unless they are destroyed. Similarly, each flange 70 is locally bonded to an area of the corresponding longitudinal element 62 with the same polyurethane adhesive.
  • the outer coating 60 further comprises a thin protective coating 80 surrounding it integrally.
  • the protective coating 80 is made of a material capable of withstanding shocks defined by the aeronautical standard Gam EG13, in particular handling or transport shocks, or in the event of a fall when the bomb is suspended on the aircraft.
  • the protective coating 80 also resists abrasion.
  • the material chosen is, for example, a monolayer elastomeric polyurethane which is cast directly around the longitudinal elements 62 and flanges 70, over a thickness of a few millimeters, for example 3 millimeters, so that the profile of the bomb 1, once coated by the protective coating 80, is identical to that of the general purpose spray.
  • the protective coating 80 also has three orifices 85 facing the three orifices 75 of one of the flanges 70 so that the accessory well 40 and the suspension ring wells 50 and 51 are accessible from the outside the bomb 1 and flush with said protective coating 80.
  • the bomb 1 comprises a hollow front sleeve 90 intended to enclose equipment participating in its operation, for example laser guiding means, a gyroscope or an accelerometer.
  • the hollow sleeve 90 is fixed directly to the penetrating hollow body 10, more precisely on the front portion 11 of the latter.
  • the front sleeve 90 has a rear internal thread 91 intended to cooperate with an external thread 11d located between the zones 11a and 11b of the front portion 11 of the penetrating hollow body 10.
  • the front sleeve 90 also has an internal thread. before 92 which interfaces with the guidance systems and is protected, for the storage of the bomb, by a removable protective cap 95.
  • the coating provides the bomb 1 with the same dimensional, volume, mechanical, aerodynamic and inertial characteristics as a general purpose bomb, for example of the Mk82 type, it is not necessary to make it pass through. full qualification tests that are long and costly.
  • thermoformed elements and flanges around the penetration body there may be more or less than three thermoformed elements and flanges around the penetration body.
  • plastics used are mentioned for information only and may be replaced by other materials with identical or similar characteristics, including mechanical and resistance to chemical attack or fire.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Pens And Brushes (AREA)
  • Materials For Medical Uses (AREA)
  • Coating Apparatus (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Fertilizers (AREA)

Claims (11)

  1. Penetrationsfliegerbombe (1), umfassend:
    - einen ein aktives Material (20) oder ein inertes Material enthaltenden Penetrationshohlkörper (10) von generell zylindrischer Form,
    - wenigstens einen Aufhängringschacht (50 ; 51), um das Aufhängen der Bombe an einem Flugzeug zu ermöglichen, und
    - einen Schacht (40), der Zubehöre enthält, die das Funktionieren der Bombe (1) ermöglichen,
    - eine Außenverkleidung von generell zylindrischer Form (60), die mit dem Penetrationshohlkörper (10) fest verbunden ist, sich über dessen gesamte Länge erstreckt und ein Außenprofil, eine Masse und eine solche räumliche Anordnung um den Penetrationskörper herum aufweist, dass die genannte mit ihrer Außenverkleidung versehene Bombe die gleichen dimensionellen, volumenbezogenen, mechanischen, aerodynamischen und inertialen Charakteristika wie eine qualifizierte universell verwendbare Bombe besitzt,
    dadurch gekennzeichnet, dass die Außenverkleidung (60) identische warmgeformte Längselemente (62) umfasst, jedes über die gesamte Länge des Penetrationshohlkörpers (10) direkt befestigt, wobei jedes Element (62) aus faserverstärktem Kunststoff, etwa einer vorimprägnierten Matte (SMC), zum Beispiel einem Gemisch aus Polyester und graphithaltigen Glasfasern, ist.
  2. Bombe nach Anspruch 1, dadurch gekennzeichnet, dass jedes Längselement (62) einen Sitz (64) zur Aufnahme eines Gleichgewichtsflansches (70) aufweist, der hergestellt ist aus einem Material von hoher Dichte, zum Beispiel höher oder gleich derjenigen des Stahls, und der dazu beiträgt, der Bombe die genannten volumenbezogenen, dimensionellen, mechanischen, aerodynamischen und inertialen Charakteristika zu verleihen.
  3. Bombe nach Anspruch 2, dadurch gekennzeichnet, dass jeder Gleichgewichtsflansch (70) direkt auf dem Penetrationshohlkörper mit Hilfe von Schrauben (72) befestigt ist, die dazu bestimmt sind, abgeschert zu werden bei einem Einschlag der Bombe auf einem Hindernis, bei dem eine einen bestimmten Wert überschreitende Verzögerung erzeugt wird.
  4. Bombe nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass jedes Längselement (62) und/oder jeder Gleichgewichtsflansch (70) direkt auf den Penetrationshohlkörper (10) geklebt ist, zum Beispiel mit Hilfe eines Polyurethan-Klebstoffs.
  5. Bombe nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Außenverkleidung (60) außerdem eine die Längselemente (62) ganz umschließende dünne Schutzhülle (80) umfasst.
  6. Bombe nach Anspruch 5, dadurch gekennzeichnet, dass die Schutzhülle (80) aus einem Material ist, das durch die Luftfahrtnorm GAM EG13 definierte Stöße, Abrasion und Feuer aushält, wobei dieses Material zum Beispiel ein einschichtig gegossenes Polyurethan ist.
  7. Bombe nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass sie Aufhängringschächte (50, 51) und einen Zubehörschacht (40) umfasst, wobei die genannten Schächte (40 ; 50, 51) mit Hilfe von Schrauben (42 ; 52) direkt auf dem Penetrationshohlkörper (10) befestigt und dazu
    bestimmt sind, abgeschert zu werden bei einem Einschlag der Bombe auf einem Hindernis, bei dem eine einen bestimmten Wert überschreitende Verzögerung erzeugt wird.
  8. Bombe nach Anspruch 7, dadurch gekennzeichnet, dass wenigstens einer (50) der Aufhängringschächte aus einem Stück mit dem Zubehörschacht (40) ist.
  9. Bombe nach Anspruch 8, dadurch gekennzeichnet, dass sie außerdem eine Hülse (31) für die Durchführung von Kabeln umfasst, die Zubehöre des Zubehörschachts (40) mit den Detonationseinrichtungen verbinden, wobei die genannte Hülse (31) in das aktive oder inerte Material (20) eingebettet ist und aus einem Material ist, das den chemischen Angriffen dieses Letzteren widersteht.
  10. Bombe nach einem der Ansprüche 1 bis 9, dadurch gekennzeichnet, dass die Außenverkleidung (60) lokal Zugänge (75 ; 85) zu den Schächten (40 ; 51, 52) aufweist, so dass sie von der Außenseite der Bombe (1) zugänglich sind.
  11. Bombe nach einem der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass der Penetrationshohlkörper (10) einen Rumpf (12) mit einem spitzbogenförmigen vorderen Ende (11) und einem sockelförmigen, insbesondere die Detonationseinrichtungen umschließenden hinteren Ende (13) umfasst, wobei das vordere Ende (11) ein Außengewinde (11d) aufweist, das mit einem Innengewinde (91) eines Kopfelements (90) kooperiert, das als Schnittstelle mit wenigstens einer am Funktionieren der Bombe beteiligten Einrichtung, etwa einem Lenksystem, dient.
EP07872427A 2006-12-21 2007-12-20 Ummantelte penetrationsfliegerbombe Not-in-force EP2095059B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0655788A FR2910612B1 (fr) 2006-12-21 2006-12-21 Bombe aerienne de penetration munie d'un revetement externe.
PCT/FR2007/002143 WO2008096069A1 (fr) 2006-12-21 2007-12-20 Bombe aerienne de penetration munie d'un revetement externe

Publications (2)

Publication Number Publication Date
EP2095059A1 EP2095059A1 (de) 2009-09-02
EP2095059B1 true EP2095059B1 (de) 2010-06-09

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP07872427A Not-in-force EP2095059B1 (de) 2006-12-21 2007-12-20 Ummantelte penetrationsfliegerbombe

Country Status (10)

Country Link
EP (1) EP2095059B1 (de)
KR (1) KR20090113827A (de)
CN (1) CN101578492B (de)
AT (1) ATE470835T1 (de)
BR (1) BRPI0720586A2 (de)
DE (1) DE602007007118D1 (de)
ES (1) ES2346817T3 (de)
FR (1) FR2910612B1 (de)
WO (1) WO2008096069A1 (de)
ZA (1) ZA200905070B (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2016022181A1 (en) * 2014-08-07 2016-02-11 Raytheon Company Fragmentation munition with limited explosive force
US9816793B2 (en) 2014-02-11 2017-11-14 Raytheon Company Shock-resistant fuzewell for munition

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2496908B1 (de) 2009-11-04 2013-09-11 Diehl BGT Defence GmbH & Co.KG Fliegerbombe
US9810513B2 (en) 2014-08-04 2017-11-07 Raytheon Company Munition modification kit and method of modifying munition
US9909848B2 (en) 2015-11-16 2018-03-06 Raytheon Company Munition having penetrator casing with fuel-oxidizer mixture therein
US10101139B1 (en) * 2016-12-15 2018-10-16 The United States Of America As Represented By The Secretary Of The Navy Cook-off mitigation systems
WO2019048914A1 (de) * 2017-09-09 2019-03-14 Ruag Ammotec Ag Vollmantel-sicherheitsgeschoss, insbesondere für mehrzweckanwendungen

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GB168837A (en) * 1917-01-08 1921-09-12 Vicente Almonacid Improvements in or relating to projectiles particularly for use on aircraft
US1557082A (en) * 1921-09-01 1925-10-13 Newton Henry Shell and bomb
US2968244A (en) * 1948-05-07 1961-01-17 Jr Leo Maas Jet accelerated missile
FR2155008A5 (de) * 1971-10-04 1973-05-18 Mulleman Michel
FR2688304B1 (fr) * 1992-03-05 1995-12-08 Michel Mulleman Corps de bombe perfectionne, procede de fabrication de tels corps de bombe, et bombes de divers types equipees d'un tel corps.
US6227096B1 (en) * 1999-06-22 2001-05-08 The Boeing Company Universal warhead adapter, and missile and method incorporating same
US7261042B1 (en) * 2004-07-08 2007-08-28 Lockheed Martins Corporation Insensitive munition design for shrouded penetrators
CN1731073A (zh) * 2005-08-29 2006-02-08 陈嘉农 一种可以调节损伤毁坏威力的航空炸弹

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9816793B2 (en) 2014-02-11 2017-11-14 Raytheon Company Shock-resistant fuzewell for munition
US10184763B2 (en) 2014-02-11 2019-01-22 Raytheon Company Munition with nose kit connecting to aft casing connector
US10267607B2 (en) 2014-02-11 2019-04-23 Raytheon Company Munition with outer enclosure
US10520289B2 (en) 2014-02-11 2019-12-31 Raytheon Company Munition with multiple fragment layers
WO2016022181A1 (en) * 2014-08-07 2016-02-11 Raytheon Company Fragmentation munition with limited explosive force
US9739583B2 (en) 2014-08-07 2017-08-22 Raytheon Company Fragmentation munition with limited explosive force

Also Published As

Publication number Publication date
KR20090113827A (ko) 2009-11-02
BRPI0720586A2 (pt) 2014-03-18
WO2008096069A1 (fr) 2008-08-14
ES2346817T3 (es) 2010-10-20
ATE470835T1 (de) 2010-06-15
FR2910612A1 (fr) 2008-06-27
DE602007007118D1 (de) 2010-07-22
CN101578492B (zh) 2012-12-05
EP2095059A1 (de) 2009-09-02
FR2910612B1 (fr) 2009-10-02
CN101578492A (zh) 2009-11-11
ZA200905070B (en) 2010-07-28

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