EP0162335A2 - Dispositif de sécurité d'un détonateur - Google Patents

Dispositif de sécurité d'un détonateur Download PDF

Info

Publication number
EP0162335A2
EP0162335A2 EP85105119A EP85105119A EP0162335A2 EP 0162335 A2 EP0162335 A2 EP 0162335A2 EP 85105119 A EP85105119 A EP 85105119A EP 85105119 A EP85105119 A EP 85105119A EP 0162335 A2 EP0162335 A2 EP 0162335A2
Authority
EP
European Patent Office
Prior art keywords
slide
protection device
detonator
safety slide
ignition protection
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
EP85105119A
Other languages
German (de)
English (en)
Other versions
EP0162335A3 (en
EP0162335B1 (fr
Inventor
Werner Rüdenauer
Wilhelm Fürst
Norbert Liebl
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 EP0162335A2 publication Critical patent/EP0162335A2/fr
Publication of EP0162335A3 publication Critical patent/EP0162335A3/de
Application granted granted Critical
Publication of EP0162335B1 publication Critical patent/EP0162335B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/24—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by inertia means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/28—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
    • F42C15/295—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids operated by a turbine or a propeller; Mounting means therefor

Definitions

  • the invention relates to an ignition protection device according to the preamble of claim 1.
  • Such an ignition protection device is known from DE-AS 22 34 849.
  • it has significant functional disadvantages in that mechanical locking in the movable wind turbine generator itself must act as the first securing criterion.
  • the second unlocking process provided there in the form of an explosion pressure application of the wind turbine generator appears to be particularly susceptible to faults; to irreversibly deform a locking member by pushing the wind turbine generator further out of the projectile from its first position.
  • this process cannot be readily predicted kinetically, the explosion pressure applied to the carriage displacing the wind turbine generator can lead to malfunctions in the generator, and the further displacement of the wind turbine generator laterally out of the projectile leads to undesirable influences on the flight dynamics of the projectile and on the inflow conditions of the generator. If the generator is to run for the entire flight time, it is cheaper to leave it in one position.
  • the object of the invention is an ignition protection device To further develop the generic type in such a way that, with a small construction volume, the safety functions of the safety functions that can be clearly differentiated from each other can be implemented in such a way that malfunctions of the wind turbine generator (in the course of the safety function) and of the projectile, particularly in the course of its critical initial or stabilization flight phase, are largely avoided ; while the criteria of the safety standard with regard to two mutually independent environmental releasing criteria and also with regard to the avoidance of prestressed spring force elements on the releasing elements should be fulfilled in the installation and securing phase.
  • the ejection of the projectile from its carrier provides the first environmentally dependent unlocking criterion, which only leads to the tension compression spring for the detonator safety slide being tensioned and, at the same time, to its unlocking.
  • a control circuit operating independently of the operation of the wind turbine generator provides an electrical unlocking criterion for releasing the wind turbine generator for the shift into its working position.
  • the flow towards the environment as the second environmentally dependent release criterion finally unlocks the safety slide, whereupon the detonator is moved into its focus.
  • an ignition protection device 11 in order to avoid repetition, reference is made in full to the description of claims and summary of the aforementioned parallel application with the same priority.
  • that ignition protection device 11 is provided, in the secured state, not yet to provide a loaded pressure accumulator (in the form of a prestressed feed compression spring 27). Instead, this compression spring 27 is only tensioned when the locking action of the blocker 31 on the detonator safety slide 25 is released by means of an acceleration-dependent unlocking mechanism 50.
  • the release mechanism 50 is accordingly also oriented in this transverse direction.
  • it consists of the tried-and-tested so-called double pushback pin system, which responds to the ejection acceleration 51 as the first environmentally-dependent release criterion.
  • the inertia of a response pin 53 thus causes the projectile 12 to be ejected laterally from its support (not shown) relative to the ignition protection device 11, the direction of the ejection acceleration 51 and the force of a spring 54, until the end of the bolt 55 has the lateral displacement possibility of a locking ball 56 releases.
  • the force element 43 is actuated from the control circuit 42, which is provided with a separate energy source for this purpose, in order to pull the locking pin 19 out of the slide 16.
  • This is therefore pushed forward by its prestressed compression spring 17 until the lamellar wheel 22 of the wind turbine generator 21, which is designed for radial inflow, projects beyond the periphery of the projectile wall 14 after passing through the housing opening 23.
  • the ambient flow against the projectile 12, which is free-flying after being ejected, is the second environmental safety criterion that is functionally independent of the first.
  • the wind turbine generator 21 After a certain operating time, the wind turbine generator 21 has supplied the energy required to control the force element 44 for pulling the locking pin 26 out of the sliding guide 24 for the detonator 28. Since the release mechanism 50 acting as a function of acceleration, which provided the first environmentally dependent release criterion, also tensioned the compression spring 27, the safety slide 25 is now advanced to its arming position (not shown in the drawing), in which the detonator 28 with the transfer charge 29 in front of it Battle charge 13 is aligned and a bypass switch 30 (for the electrical short circuit of the detonator control in the safety position) is open.
  • the detonator 28 is acted upon by the control circuit 42 with ignition energy supplied by the wind turbine generator 21 when ignition sensors (not taken into account in the drawing) respond due to the approach or target impact, or, if a target is missed, an inertial sensor 61 responds.
  • the locking pin 26 for the detonator safety slide 25 should come out of engagement too early, namely before the first environmentally-dependent unlocking criterion in the form of the operational sequence of the unlocking mechanism 50 has taken place - and thus before its compression spring 27 has been tensioned and before its locking ball 59 can dodge sideways in front of the beveled front of its flange 37 -, the detonator safety slide 25 is shifted backwards by a tension spring 62; until then a locking member 63, for example a pin loaded by a compression spring 64, engages as a lock between the safety slide 25 and a surrounding fixed component of the ignition safety device 11.
  • the safety slide 25 can no longer be advanced, so the detonator 28 can no longer be moved in front of the transfer charge 29; the projectile 12 is thus securely locked as a dud.
  • the direction of advance of the wind turbine generator slide 16 differs from that of the detonator safety slide 25 in this exemplary embodiment.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Air Bags (AREA)
  • Spark Plugs (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
EP85105119A 1984-05-19 1985-04-26 Dispositif de sécurité d'un détonateur Expired - Lifetime EP0162335B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3418759 1984-05-19
DE3418759A DE3418759A1 (de) 1984-05-19 1984-05-19 Zuendsicherungseinrichtung

Publications (3)

Publication Number Publication Date
EP0162335A2 true EP0162335A2 (fr) 1985-11-27
EP0162335A3 EP0162335A3 (en) 1987-10-07
EP0162335B1 EP0162335B1 (fr) 1990-08-08

Family

ID=6236380

Family Applications (1)

Application Number Title Priority Date Filing Date
EP85105119A Expired - Lifetime EP0162335B1 (fr) 1984-05-19 1985-04-26 Dispositif de sécurité d'un détonateur

Country Status (6)

Country Link
US (1) US4679503A (fr)
EP (1) EP0162335B1 (fr)
CA (1) CA1267565A (fr)
DE (2) DE3418759A1 (fr)
DK (1) DK194185A (fr)
NO (1) NO164865C (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3828949A1 (de) * 1988-08-26 1990-03-08 Messerschmitt Boelkow Blohm Sicherheitseinrichtung
DE10000177A1 (de) * 2000-01-05 2001-07-12 Junghans Feinwerktechnik Gmbh Zündeinrichtung, insbesondere für eine Mörsergranate

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3631078A1 (de) * 1986-09-12 1988-03-24 Diehl Gmbh & Co Submunitionskoerper mit seitlich herausbewegbarer zieldetektionseinrichtung
DE3934573A1 (de) * 1989-10-17 1991-04-25 Diehl Gmbh & Co Schalteinrichtung fuer endstellungs-detektion
US4986184A (en) * 1989-10-26 1991-01-22 Honeywell Inc. Self-sterilizing fire-on-the-fly bi-stable safe and arm device
DE4240809A1 (de) * 1992-12-04 1994-06-09 Diehl Gmbh & Co Sicherungsvorrichtung für eine Munition
US6389976B1 (en) * 2000-05-08 2002-05-21 The United States Of America As Represented By The Secretary Of The Army Hard target fuze
US6634301B1 (en) * 2002-09-26 2003-10-21 The United States Of America As Represented By The Secretary Of The Navy Enclosed ignition flare igniter
US7798064B1 (en) 2007-04-26 2010-09-21 Dse, Inc. Command and arm fuze assembly having small piston actuator

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2775941A (en) * 1946-12-23 1957-01-01 Harold J Plumley Magnetic inertia controlled fuze
US2985105A (en) * 1947-05-27 1961-05-23 Rabinow Jacob Wind-operated delayed arming fuze
DE1927911A1 (de) * 1969-05-31 1970-12-03 Uhrenfabrik Stowa Gmbh Sprengkapselsicherung
US3677186A (en) * 1969-10-01 1972-07-18 Us Navy Velocity discriminating time mechanical ordnance fuze
US3757695A (en) * 1969-12-19 1973-09-11 Us Army Charging system for electric bomb fuzes (u)
FR2180159A5 (fr) * 1972-04-10 1973-11-23 Nathan Guy
DE2234849C3 (de) * 1972-07-15 1979-11-22 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Von einem Windradgenerator gespeiste Zündeinrichtung, insbesondere für aus Flugzeugen abwerfbare Bomblets
US3967556A (en) * 1975-03-31 1976-07-06 The United States Of America As Represented By The Secretary Of The Army Pneumatic fuze for safing and arming missiles
US3961577A (en) * 1975-05-12 1976-06-08 The United States Of America As Represented By The Secretary Of The Navy Air driven energy storing fuze safing and arming mechanism
US4027593A (en) * 1976-02-12 1977-06-07 The United States Of America As Represented By The Secretary Of The Army Multi-directional system for electrical bomb fuzes
US4031827A (en) * 1976-03-04 1977-06-28 The United States Of America As Represented By The Secretary Of The Air Force Pop-up cover for slipstream generator
FR2438819A1 (fr) * 1978-10-13 1980-05-09 Matra Perfectionnements aux dispositifs d'activation pour charges largables a partir d'un vehicule porteur
DE3015424A1 (de) * 1980-04-22 1981-10-29 Diehl GmbH & Co, 8500 Nürnberg Sicherungsvorrichtung fuer zuender von drallosen oder drallarmen geschossen
DE3126288A1 (de) * 1981-07-03 1983-05-26 Diehl GmbH & Co, 8500 Nürnberg Sicherungseinrichtung fuer geschosszuender
US4393780A (en) * 1981-08-17 1983-07-19 The United States Of America As Represented By The Secretary Of The Army Omni directional fuze
DE3418745A1 (de) * 1984-05-19 1985-11-21 Diehl GmbH & Co, 8500 Nürnberg Zuendsicherungseinrichtung

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3828949A1 (de) * 1988-08-26 1990-03-08 Messerschmitt Boelkow Blohm Sicherheitseinrichtung
US4932325A (en) * 1988-08-26 1990-06-12 Messerschmitt-Bolkow-Blohm Gmbh Safety device for an aerodynamic body fuse
DE10000177A1 (de) * 2000-01-05 2001-07-12 Junghans Feinwerktechnik Gmbh Zündeinrichtung, insbesondere für eine Mörsergranate
US6463855B2 (en) 2000-01-05 2002-10-15 Junghans Feinwerktechnik Gmbh & Co. Kg Fuse device for a mortar shell
AU774459B2 (en) * 2000-01-05 2004-06-24 Junghans Feinwerktechnik Gmbh & Co. Kg Fuse device in particular for a mortar shell

Also Published As

Publication number Publication date
DE3579035D1 (de) 1990-09-13
NO164865C (no) 1990-11-21
EP0162335A3 (en) 1987-10-07
DE3418759A1 (de) 1985-11-21
NO164865B (no) 1990-08-13
US4679503A (en) 1987-07-14
EP0162335B1 (fr) 1990-08-08
DE3418759C2 (fr) 1989-10-05
NO851449L (no) 1985-11-20
DK194185A (da) 1985-11-20
CA1267565A (fr) 1990-04-10
DK194185D0 (da) 1985-04-30

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