EP0256320A2 - Fusée double à autodestruction pour bombe aérienne - Google Patents

Fusée double à autodestruction pour bombe aérienne Download PDF

Info

Publication number
EP0256320A2
EP0256320A2 EP87110330A EP87110330A EP0256320A2 EP 0256320 A2 EP0256320 A2 EP 0256320A2 EP 87110330 A EP87110330 A EP 87110330A EP 87110330 A EP87110330 A EP 87110330A EP 0256320 A2 EP0256320 A2 EP 0256320A2
Authority
EP
European Patent Office
Prior art keywords
slide
needle
detonator
housing
ignition
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.)
Withdrawn
Application number
EP87110330A
Other languages
German (de)
English (en)
Other versions
EP0256320A3 (fr
Inventor
Werner Rüdenauer
Fritz Müller
Dieter Küfner
Joachim Furtmayr
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.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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 Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of EP0256320A2 publication Critical patent/EP0256320A2/fr
Publication of EP0256320A3 publication Critical patent/EP0256320A3/fr
Withdrawn legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C9/00Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
    • F42C9/14Double fuzes; Multiple fuzes
    • F42C9/142Double fuzes; Multiple fuzes combined time and percussion fuzes in which the timing is caused by combustion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/18Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved
    • F42C15/184Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved using a slidable carrier

Definitions

  • the invention relates to an igniter for a parachute or band-stabilized, rotating in flight bombed according to the preamble of claim 1.
  • an ignition and safety device for launching ammunition in which a slide under spring tension can be released via an ignition button that can be moved in a thread.
  • a stabilizing band connected to the firing needle brakes the firing needle with respect to the rotating ammunition, so that the firing needle tip lifts off the slide.
  • a self-dismantling device is not provided in this ignition and safety device.
  • the object of the invention is to propose a detonator for bomblets, which ensures that the detonator is ignited in any case in the absence of an ignition-relevant impact pulse.
  • the igniter should be highly sensitive and simple.
  • the pyrotechnic set serving as a timing element is arranged in the slide in a space-saving manner, together with the detonator and a disassembly needle biased by spring force.
  • This spring is the only energy storage element in the igniter. It only supports the centrifugal forces caused by the rotation, which also act on the cutting needle, for piercing the pyrotechnic block.
  • the firing needle fulfills a double function, it secures both the slide in the safe position and the disassembly needle in the safe position. This means that the self-disassembly activation is only coupled to the ignition needle, so that the pyrotechnic charge is ignited even when the ignition needle is unscrewed.
  • the time-delayed detonator firing caused by the kit runs over a period of time that is significantly greater than the flight time normally required to combat a target.
  • the required bore lengths for the pyrotechnic set in the slide are achieved in a small space, without the risk of undesired over-ignition of the set already burning in the first hole on the set arranged in the second hole.
  • a determination of the disassembly needle consisting of a few existing parts is achieved according to claim 4.
  • the ignition needle according to the invention is supported twice by the housing-side guide length and by the collar of a box-shaped sheet metal guide, so that a central ignition of the detonator is ensured.
  • a detonating needle that evades the centric ignition of the detonator cannot occur.
  • the detonator detonation achieved in a cost-effective manner is achieved by the firing needle sealing the collar of the box-shaped sheet metal guide with its cone opening. This contributes to the safe ignition of the explosive-side transmission set.
  • a single, lateral engagement of a safety slide mounted on the housing on the slide having the detonator is sufficient. Therefore, in the event of assembly errors in which, for example, the installation of the firing needle has been forgotten - within a group of several bobbins placed one on top of the other - undesired ignition of the detonator by the self-dismantling device cannot occur.
  • a spring force is not exerted on the slide.
  • the slide remains in the safe position - even if the ignition needle is missing. If the safety slide is possibly extended, it moves back into the safety hole when the impact pulse has subsided and positively fixes the slide again.
  • an additional securing of the slide is ensured in a structurally simple manner.
  • the positive locking of the slide in the association of bomblets is achieved by means of simple construction.
  • a relatively small impact pulse is sufficient for the ignition of the detonator upon impact.
  • An igniter 1 consists of a housing 2 with a guide length 11, a square opening 3, a bearing bush 4 designed as a square nut, an ignition needle 5 with thread 6, ring 7, cone opening 8, a non-rotatably fastened stabilizing band 9, a cap 10, a Safety slide 15, a bearing bore 17, a sheet metal guide 18 with a collar 19, a slide 20 with bores 25 to 29, a detonator 30, an approximately U-shaped pyrotechnic, time-delaying set 31, a disc 32, a disassembly needle 33, a spring 34, a sheet 35, a stop 36 and from a locking device, not shown, for the focusing of the slide 20th
  • the housing 2 is connected via screw connections 37 to an explosive shell 40 which has a transmission set 41.
  • Bombblets are combined in an association not shown, for example within a floor.
  • the stop 36 is located on the wall 38 of the housing.
  • the bomblets After ejection of the bomblets from a storey with swirl, the bomblets separate from one another, i.e. the bomblett bandage is dissolved and the stabilizing band 9 unfolds.
  • the sleeve 42 has released the slide 20.
  • the braking force of the stabilizing band 9 causes, compared to the rotating bomblet, that the firing needle 5 is unscrewed from the igniter housing 2 until the ring 7 rests on the bearing bush 4.
  • the ignition needle 5 unlocks the disassembly needle 33 and the safety slide 15 releases the slide 20.
  • the disassembly needle 33 ignites the pyrotechnic set 31, which burns up relatively slowly.
  • the firing needle 5 is then above the detonator 30. If the bomblet is now relevant to ignition, the firing needle 5 stings the detonator 30, which then ignites the transmission set 41 via a channel 46 in order to initiate the detonation of the bomblet.
  • the detonator 30 is ignited via the pyrotechnic charge 31 which has burned down to the detonator 30.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Automotive Seat Belt Assembly (AREA)
  • Emergency Lowering Means (AREA)
EP87110330A 1986-07-22 1987-07-17 Fusée double à autodestruction pour bombe aérienne Withdrawn EP0256320A3 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3624713 1986-07-22
DE3624713A DE3624713C2 (de) 1986-07-22 1986-07-22 Aufschlagzünder mit Selbstzerlegeeinrichtung für einen Bomblet

Publications (2)

Publication Number Publication Date
EP0256320A2 true EP0256320A2 (fr) 1988-02-24
EP0256320A3 EP0256320A3 (fr) 1988-09-14

Family

ID=6305679

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87110330A Withdrawn EP0256320A3 (fr) 1986-07-22 1987-07-17 Fusée double à autodestruction pour bombe aérienne

Country Status (5)

Country Link
US (1) US4762066A (fr)
EP (1) EP0256320A3 (fr)
DE (1) DE3624713C2 (fr)
DK (1) DK368987A (fr)
NO (1) NO166816C (fr)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0284923A2 (fr) * 1987-03-31 1988-10-05 TAAS Israel Industries, Limited Fusée pour une sous-munition
EP0318996A2 (fr) * 1987-12-03 1989-06-07 DIEHL GMBH & CO. Allumeur pyrotechnique pour projectiles, roquettes bombes et mines
EP0318995A2 (fr) * 1987-12-03 1989-06-07 DIEHL GMBH & CO. Allumeur pyrotechnique pour projectiles
EP0318997A2 (fr) * 1987-12-03 1989-06-07 DIEHL GMBH & CO. Dispositif de sécurité pour une fusée à autodestruction par combustion pour utilisation dans des bombes
EP0393456A2 (fr) * 1989-04-18 1990-10-24 DIEHL GMBH & CO. Fusée d'allumage pour une bombe
FR2691796A1 (fr) * 1992-06-02 1993-12-03 Giat Ind Sa Système d'auto-destruction d'une munition en particulier d'une sous-munition d'obus cargo comprenant un générateur de gaz.
WO1996035095A1 (fr) * 1995-05-05 1996-11-07 Dixi S.A. Dispositif de securite pour fusee percutante
FR2801099A1 (fr) * 1999-11-17 2001-05-18 Giat Ind Sa Systeme d'amorcage de la charge explosive d'une sous- munition
DE102008032744A1 (de) * 2008-07-11 2010-01-14 Junghans Microtec Gmbh Zünder für ein Geschoss
FR3049056A1 (fr) * 2016-03-17 2017-09-22 Nexter Munitions Dispositif d'amorcage pour une charge pyrotechnique et munition incorporant un tel dispositif d'amorcage

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3901525A1 (de) * 1989-01-20 1990-07-26 Junghans Gmbh Geb Zuender fuer ein bomblet
GR890100460A (el) * 1989-07-20 1991-12-10 Panagiotis Karamanolis Αυτοαφοπλιζομενος πυροσωληνας βομβιδων βομβιδοφορων πυρομαχικων.
DE3925238A1 (de) * 1989-07-29 1991-01-31 Rheinmetall Gmbh Zuender fuer ein bombletgeschoss
DE3925235A1 (de) * 1989-07-29 1991-01-31 Rheinmetall Gmbh Bombletzuender
DE3925236A1 (de) * 1989-07-29 1991-01-31 Rheinmetall Gmbh Zuender fuer ein bombletgeschoss
US5067410A (en) * 1990-12-21 1991-11-26 The United States Of America As Represented By The Secretary Of The Army Flexible wing
FR2683035B1 (fr) * 1991-10-25 1993-12-24 Giat Industries Fusee pour bombelette munie d'un ruban stabilisateur.
EP0573328B1 (fr) * 1992-06-02 1997-10-29 GIAT Industries Système d'auto-destruction d'une munition d'obus cargo par attaque chimique
US5387257A (en) * 1994-01-05 1995-02-07 The United States Of America As Represented By The Secretary Of The Army Self-destruct fuze for improved conventional munitions
WO1996023194A1 (fr) * 1995-01-25 1996-08-01 Tari Michael T Fusible auto-destructeur pour munitions conventionnelles perfectionnees
DE19842541C2 (de) * 1998-09-17 2003-10-16 Rheinmetall W & M Gmbh Stabilisierungsbandbefestigung bei einer Abwurfmunition
DE19917121C2 (de) * 1999-04-15 2002-03-21 Rheinmetall W & M Gmbh Submunitionsgeschoss mit einem durch die Anströmkräfte der Luft aus der Sicherungsposition freigebbaren Schieber
DE19916775C2 (de) * 1999-04-15 2002-12-05 Rheinmetall W & M Gmbh Submunitionsgeschoß
FR2816400B1 (fr) * 2000-11-07 2003-04-04 Giat Ind Sa Dispositif d'amorcage de la charge explosive d'une sous-munition
US6968785B2 (en) * 2003-09-22 2005-11-29 The United States Of America As Represented By The Secretary Of The Army Locking and stabilizing device for grenades
KR101078153B1 (ko) * 2009-02-20 2011-10-28 주식회사 풍산 유탄의 자폭장치
CN111547269B (zh) * 2020-04-21 2021-06-15 哈尔滨工业大学 小行星探测勘察弹加旋释放装置

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3025795A (en) * 1958-02-12 1962-03-20 Thiokol Chemical Corp Time delay fuse element
US3371608A (en) * 1967-06-01 1968-03-05 Avco Corp Fuze with delay firing and impact firing features
DE3333667A1 (de) * 1983-09-17 1985-03-28 Honeywell Gmbh, 6050 Offenbach Zuend- und sicherungseinrichtung fuer abwurfmunition
EP0158700A2 (fr) * 1983-09-15 1985-10-23 Rheinmetall GmbH Fusée pour projectile secondaire
EP0205956A1 (fr) * 1985-06-28 1986-12-30 FRATELLI BORLETTI S.p.A. Fusée à autodestruction pour sous-projectiles lancés à partir d'une roquette
DE3539279A1 (de) * 1985-11-06 1987-05-07 Diehl Gmbh & Co Zuender fuer ein fallschirm- oder bandstabilisiertes bomblet

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1751616A (en) * 1925-03-02 1930-03-25 Secretary Of War Of The United Combination fuse
BE537367A (fr) * 1954-04-27
NL107545C (fr) * 1960-04-02
SE331438B (fr) * 1969-05-19 1970-12-21 Foersvarets Fabriksverk
US3926122A (en) * 1972-08-11 1975-12-16 Us Army Grenade with fuze (U)
US3998164A (en) * 1975-12-15 1976-12-21 The United States Of America As Represented By The Secretary Of The Army Self-destruct delay fuze
US4455940A (en) * 1982-06-28 1984-06-26 The United States Of America As Represented By The Secretary Of The Army Random time delay fuze

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3025795A (en) * 1958-02-12 1962-03-20 Thiokol Chemical Corp Time delay fuse element
US3371608A (en) * 1967-06-01 1968-03-05 Avco Corp Fuze with delay firing and impact firing features
EP0158700A2 (fr) * 1983-09-15 1985-10-23 Rheinmetall GmbH Fusée pour projectile secondaire
DE3333667A1 (de) * 1983-09-17 1985-03-28 Honeywell Gmbh, 6050 Offenbach Zuend- und sicherungseinrichtung fuer abwurfmunition
EP0205956A1 (fr) * 1985-06-28 1986-12-30 FRATELLI BORLETTI S.p.A. Fusée à autodestruction pour sous-projectiles lancés à partir d'une roquette
DE3539279A1 (de) * 1985-11-06 1987-05-07 Diehl Gmbh & Co Zuender fuer ein fallschirm- oder bandstabilisiertes bomblet

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0284923A2 (fr) * 1987-03-31 1988-10-05 TAAS Israel Industries, Limited Fusée pour une sous-munition
EP0284923A3 (en) * 1987-03-31 1990-04-04 The State Of Israel, Ministry Of Defence, Israel Military Industries Fuse for sub-munition warhead
EP0318996A2 (fr) * 1987-12-03 1989-06-07 DIEHL GMBH & CO. Allumeur pyrotechnique pour projectiles, roquettes bombes et mines
EP0318995A2 (fr) * 1987-12-03 1989-06-07 DIEHL GMBH & CO. Allumeur pyrotechnique pour projectiles
EP0318997A2 (fr) * 1987-12-03 1989-06-07 DIEHL GMBH & CO. Dispositif de sécurité pour une fusée à autodestruction par combustion pour utilisation dans des bombes
EP0318997A3 (en) * 1987-12-03 1989-11-02 Diehl Gmbh & Co. Safety device for a pyrotechnical self-destruction fuze safety device for a pyrotechnical self-destruction fuze for use with bomblets for use with bomblets
EP0318996A3 (en) * 1987-12-03 1989-11-15 Diehl Gmbh & Co. Pyrotechnical initiator for projectiles, rockets, bomblets and mines
EP0318995A3 (en) * 1987-12-03 1990-04-18 Diehl Gmbh & Co. Pyrotechnical initiator for projectiles
EP0393456A2 (fr) * 1989-04-18 1990-10-24 DIEHL GMBH & CO. Fusée d'allumage pour une bombe
EP0393456A3 (fr) * 1989-04-18 1992-01-02 DIEHL GMBH & CO. Fusée d'allumage pour une bombe
FR2691796A1 (fr) * 1992-06-02 1993-12-03 Giat Ind Sa Système d'auto-destruction d'une munition en particulier d'une sous-munition d'obus cargo comprenant un générateur de gaz.
WO1996035095A1 (fr) * 1995-05-05 1996-11-07 Dixi S.A. Dispositif de securite pour fusee percutante
FR2801099A1 (fr) * 1999-11-17 2001-05-18 Giat Ind Sa Systeme d'amorcage de la charge explosive d'une sous- munition
DE102008032744A1 (de) * 2008-07-11 2010-01-14 Junghans Microtec Gmbh Zünder für ein Geschoss
DE102008032744B4 (de) * 2008-07-11 2010-04-01 Junghans Microtec Gmbh Zünder für ein Geschoss
FR3049056A1 (fr) * 2016-03-17 2017-09-22 Nexter Munitions Dispositif d'amorcage pour une charge pyrotechnique et munition incorporant un tel dispositif d'amorcage

Also Published As

Publication number Publication date
NO166816C (no) 1991-09-04
NO872421L (no) 1988-01-25
US4762066A (en) 1988-08-09
DK368987A (da) 1988-01-23
DE3624713C2 (de) 1995-09-07
EP0256320A3 (fr) 1988-09-14
DE3624713A1 (de) 1988-01-28
NO166816B (no) 1991-05-27
DK368987D0 (da) 1987-07-15
NO872421D0 (no) 1987-06-10

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Inventor name: KUEFNER, DIETER