EP0327706A2 - Fusée pour projectiles - Google Patents

Fusée pour projectiles Download PDF

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Publication number
EP0327706A2
EP0327706A2 EP88120682A EP88120682A EP0327706A2 EP 0327706 A2 EP0327706 A2 EP 0327706A2 EP 88120682 A EP88120682 A EP 88120682A EP 88120682 A EP88120682 A EP 88120682A EP 0327706 A2 EP0327706 A2 EP 0327706A2
Authority
EP
European Patent Office
Prior art keywords
rotor
spring
leg
recoil
detonator
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP88120682A
Other languages
German (de)
English (en)
Other versions
EP0327706B1 (fr
EP0327706A3 (en
Inventor
Wolfgang Schillinger
Andreas Hälssig
Wolfgang Zehnder
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.)
Gebrueder Junghans GmbH
Original Assignee
Gebrueder Junghans GmbH
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 Gebrueder Junghans GmbH filed Critical Gebrueder Junghans GmbH
Publication of EP0327706A2 publication Critical patent/EP0327706A2/fr
Publication of EP0327706A3 publication Critical patent/EP0327706A3/de
Application granted granted Critical
Publication of EP0327706B1 publication Critical patent/EP0327706B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • F42C15/24Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by inertia means

Definitions

  • the invention relates to a detonator for low-swirl and for swirl projectiles with a recoil pin system consisting of two recoil pins coupled to one another via a ball, with a rotor or slide for receiving a detonator and with an inhibitor controlling the focus of the rotor or slide in a housing of the detonator.
  • An igniter of the type mentioned is known from DE-PS 31 07 110.
  • This is a safety device for a detonator of swirl projectiles with a recoil pin system, which is arranged within the rotor. Due to the launch acceleration of a projectile, a recoil bolt is moved backwards against the pressure of a spring. Due to the translational acceleration, the ball mounted on a cone of the second recoil bolt is pushed against an opposite cone of the first recoil bolt. The spring on the first recoil pin, via its cone and the ball used, locks the recoil pin system in the unlocked position, as a result of which the rotor is finally unlocked by the second recoil pin.
  • this object is achieved in that a spring is provided, the first leg of which rests securely on the lower end of a cone of an axially movable recoil bolt and the second leg of which engages with its end on a pin or in a recess in the lateral surface of the slide or rotor.
  • the spring is a leg spring bent around the bolt in a U-shape.
  • the second leg of this spring lies against a shorter wall of the recess lying on the radius of the rotor in the rotational drive direction.
  • a spring tensioning system is provided for the rotor arming on a detonator when the projectile is fired, which prestresses a spring which turns the rotor into the arming position after its release.
  • the basic requirement of such a detonator is thus advantageously met in a simple manner, that no potential energy is used for the removal of the spark plug lock device.
  • the spring is in the fully secured position when the system is secured and only receives its operating energy when the first spring arm is tensioned by the axial movement of the second recoil bolt.
  • the rear-firing pin system 1 is mounted between two plates 14 and 15 arranged at a fixed distance from one another.
  • This recoil pin system consists of a first recoil pin 5, which is inserted with its upper shaft 16 in the upper plate 14 and axially against a spring 17 supported on the lower plate 15.
  • This recoil bolt 5 also has a cone 4, which is located between an upper collar 18 and a lower collar 19.
  • another recoil pin 20 is inserted in the housing, which in turn is axially supported against a spring 21 supported on the lower plate 15.
  • the two recoil bolts 5 and 20 are coupled to one another by a ball 11.
  • a U-shaped leg spring 2 is inserted around a bolt 12 arranged in the housing, the first spring leg 3 of which rests with its end on the lower part of the cone 4 of the recoil pin 5 in the securing of the igniter.
  • the second spring leg 6 of the leg spring lies in a recess 7 on the outer surface of the rotor 8. This spring leg 6 is supported in particular on the shorter wall 13 lying on the radius of the rotor 8.
  • the rotor 8 also has a focus lock 9 and is in drive connection with an inhibitor 10 formed from a plurality of wheels.
  • a slide can also be used.
  • a correspondingly arranged pin can be provided, against which the spring leg 6 of the leg spring 2 rests.
  • the leg spring 2 In securing the detonator, the leg spring 2 is not under tension and is protected against unintentional tension by securing the recoil pin system 1. There is therefore no spring force at the rotor 8. This meets STANAG 3525's requirement that no potential energy be used to remove the spark plug lock device.
  • the recoil pin system 1 triggers and the recoil pin 5 biases the spring leg 3 of the U-shaped leg spring 2 as it moves downward through the cone 4.
  • the spring leg 6 of the U-shaped leg spring 2 moves against the wall 13 in the recess 7 of the rotor 8. The rotor 8 is thus turned into the arming position, where it is fixed via the arming lock 9 becomes.
  • the escapement 10 connected to the rotor controls the rotary movement of the rotor in the arming position.
  • the inhibitor 10 itself consists of the armature 22, which is rotatably arranged on the shaft 23 and is in engagement with the star wheel 24.
  • the pinion 25, which is rotationally fixed on the same shaft with the star wheel 24, meshes with the intermediate wheel 26, which in turn is arranged on the same shaft with the second pinion 27 in a rotationally fixed manner.
  • the pinion 27 is operatively connected to the toothed segment 28, as a result of which the disk 29, which is rotationally fixed on the same shaft as the toothed segment, performs a limited rotational movement.
  • the rotor 8 When the disk 29 rotates, the rotor 8 is uncoupled from the inhibitor mechanism 10 when the flattened area of the disk 29 is above the recess 30 of the rotor. The rotor then swivels into its focus position, the spring leg 6 serving as the drive.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP88120682A 1987-12-16 1988-12-10 Fusée pour projectiles Expired - Lifetime EP0327706B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19873742575 DE3742575A1 (de) 1987-12-16 1987-12-16 Zuender
DE3742575 1987-12-16

Publications (3)

Publication Number Publication Date
EP0327706A2 true EP0327706A2 (fr) 1989-08-16
EP0327706A3 EP0327706A3 (en) 1989-11-08
EP0327706B1 EP0327706B1 (fr) 1992-11-04

Family

ID=6342703

Family Applications (1)

Application Number Title Priority Date Filing Date
EP88120682A Expired - Lifetime EP0327706B1 (fr) 1987-12-16 1988-12-10 Fusée pour projectiles

Country Status (3)

Country Link
US (1) US4876960A (fr)
EP (1) EP0327706B1 (fr)
DE (2) DE3742575A1 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0510396A2 (fr) * 1991-04-20 1992-10-28 Gebrüder Junghans Gmbh Dispositif de sécurité pour une fusée de projectile
EP1826527A1 (fr) 2006-02-25 2007-08-29 Junghans Feinwerktechnik GmbH & Co.KG Allumeur de fusée mécanique
EP2060868A3 (fr) * 2007-11-16 2013-02-20 JUNGHANS Microtec GmbH Dispositif de sécurisation pour une amorce
KR101666217B1 (ko) 2016-01-27 2016-10-24 주식회사 풍산에프앤에스 포탄용 신관의 시간차 관성 감응식 안전장전구조

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3934573A1 (de) * 1989-10-17 1991-04-25 Diehl Gmbh & Co Schalteinrichtung fuer endstellungs-detektion
US5271327A (en) * 1992-06-19 1993-12-21 Alliant Techsystems Inc. Elecro-mechanical base element fuze
US5275107A (en) * 1992-06-19 1994-01-04 Alliant Techsystems Inc. Gun launched non-spinning safety and arming mechanism
FR2702414B1 (fr) * 1993-03-12 1996-07-05 Helverep Sa Procédé de fabrication en continu de corps tubulaires de boîtes notamment en carton.
ES2138474B1 (es) * 1995-07-10 2000-10-01 Garcia Jose Garcia Espoleta de maxima seguridad y explosion elevada para mortero y armas lisas.
US5693906A (en) * 1995-09-28 1997-12-02 Alliant Techsystems Inc. Electro-mechanical safety and arming device
US6170397B1 (en) * 1998-08-20 2001-01-09 The United States Of America As Represented By The Secretary Of The Navy Energetic transmission line completion/interruption mechanism
DE10000177A1 (de) * 2000-01-05 2001-07-12 Junghans Feinwerktechnik Gmbh Zündeinrichtung, insbesondere für eine Mörsergranate
US6920826B2 (en) * 2000-09-15 2005-07-26 Junghans Feinwerktechnik Gmbh & Co. Kg Energy supply device having a shaft rotatably supported on a polytetrafluroethylene bearing surface
US7398734B1 (en) * 2006-03-09 2008-07-15 The United States Of America As Represented By The Secretary Of The Navy MEMS resettable timer
DE102008053990B4 (de) * 2008-10-30 2010-07-22 Junghans Microtec Gmbh Zünder für ein Geschoss
DE202009008861U1 (de) * 2009-06-27 2010-11-11 Junghans Microtec Gmbh Sicherungseinrichtung für ein Geschoss
US8869700B2 (en) * 2009-09-01 2014-10-28 Omnitek Partners Llc Impulse-based compact mechanical G-switch with modular design
KR101191170B1 (ko) 2010-01-29 2012-10-15 국방과학연구소 기어열을 로타에 내장시킨 안전장전장치

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2900913A (en) * 1958-10-02 1959-08-25 Eugene N Sheeley Fail-safe time delay fuze
US3139828A (en) * 1962-03-08 1964-07-07 Ferranti Ltd Inertia responsive fuze
US4216723A (en) * 1975-01-08 1980-08-12 The United States Of America As Represented By The Secretary Of The Air Force Bomblet fuze
GB2068088A (en) * 1980-01-29 1981-08-05 Mefina Sa Projectile fuzes
US4407201A (en) * 1981-05-04 1983-10-04 Honeywell Inc. Retard sensor and energy converter

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE413657A (fr) * 1935-02-11
US3170404A (en) * 1955-03-17 1965-02-23 Frank H Swaim Acceleration sensitive variable clock
US2863393A (en) * 1955-06-09 1958-12-09 Eugene N Sheeley Safety and arming mechanism
US2882826A (en) * 1955-08-05 1959-04-21 Billings John Harland Set-back device for fuze
US3376820A (en) * 1957-09-17 1968-04-09 Army Usa Safety and arming mechanism
DE1924025C3 (de) * 1969-05-10 1979-10-18 Gebrueder Junghans Gmbh, 7230 Schramberg Sicherungseinrichtung für Zünder dralloser Geschosse
DE2643828C3 (de) * 1976-09-29 1980-09-11 Gebrueder Junghans Gmbh, 7230 Schramberg Zünder für drallarm zu verschießende Geschosse
DE3107110C2 (de) * 1981-02-26 1984-03-29 Gebrüder Junghans GmbH, 7230 Schramberg Sicherungsvorrichtung für Zünder von Drallgeschossen

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2900913A (en) * 1958-10-02 1959-08-25 Eugene N Sheeley Fail-safe time delay fuze
US3139828A (en) * 1962-03-08 1964-07-07 Ferranti Ltd Inertia responsive fuze
US4216723A (en) * 1975-01-08 1980-08-12 The United States Of America As Represented By The Secretary Of The Air Force Bomblet fuze
GB2068088A (en) * 1980-01-29 1981-08-05 Mefina Sa Projectile fuzes
US4407201A (en) * 1981-05-04 1983-10-04 Honeywell Inc. Retard sensor and energy converter

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0510396A2 (fr) * 1991-04-20 1992-10-28 Gebrüder Junghans Gmbh Dispositif de sécurité pour une fusée de projectile
EP0510396A3 (en) * 1991-04-20 1993-06-16 Gebrueder Junghans Gmbh Safety device for a projectile fuse
EP1826527A1 (fr) 2006-02-25 2007-08-29 Junghans Feinwerktechnik GmbH & Co.KG Allumeur de fusée mécanique
EP2060868A3 (fr) * 2007-11-16 2013-02-20 JUNGHANS Microtec GmbH Dispositif de sécurisation pour une amorce
KR101666217B1 (ko) 2016-01-27 2016-10-24 주식회사 풍산에프앤에스 포탄용 신관의 시간차 관성 감응식 안전장전구조

Also Published As

Publication number Publication date
US4876960A (en) 1989-10-31
EP0327706B1 (fr) 1992-11-04
DE3742575A1 (de) 1989-07-06
DE3875718D1 (de) 1992-12-10
EP0327706A3 (en) 1989-11-08

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