EP0218947B1 - Fusée d'impact comportant une amorce à percussion - Google Patents

Fusée d'impact comportant une amorce à percussion Download PDF

Info

Publication number
EP0218947B1
EP0218947B1 EP86112969A EP86112969A EP0218947B1 EP 0218947 B1 EP0218947 B1 EP 0218947B1 EP 86112969 A EP86112969 A EP 86112969A EP 86112969 A EP86112969 A EP 86112969A EP 0218947 B1 EP0218947 B1 EP 0218947B1
Authority
EP
European Patent Office
Prior art keywords
fuze
firing pin
impact
balls
sleeve
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
Application number
EP86112969A
Other languages
German (de)
English (en)
Other versions
EP0218947A1 (fr
Inventor
Adolf Weber
Hans Strauss
Adolf Bankel
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 EP0218947A1 publication Critical patent/EP0218947A1/fr
Application granted granted Critical
Publication of EP0218947B1 publication Critical patent/EP0218947B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C1/00—Impact fuzes, i.e. fuzes actuated only by ammunition impact
    • F42C1/02—Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze
    • F42C1/04—Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze operating by inertia of members on impact

Definitions

  • the invention relates to an impact detonator for barrel weapon projectiles according to the preamble of claim 1.
  • Such an impact detonator is already known from US-A-3,718,093.
  • an impact detonator with a detonator which can be pierced from the back of the detonator with a spring-operated firing pin.
  • the impact detonator has a mechanical delay device with a blocking body which, in its blocking position, lies on the one hand in recesses in the firing pin and on the other hand in recesses of a stationary detonator part.
  • two inertial sleeves arranged one behind the other coaxially to the igniter part, which release the blocking bodies after the impact delay has ended.
  • the tapping energy required for initiation is no longer available via an inertia-dependent hammer with a defined ignition delay time. Accordingly, a preloaded compression spring is provided in the aforementioned patent. After the locking body is unlocked, it strikes the firing pin against the primer.
  • a impact detonator is known from FR-A 599 412, in which a firing pin is mounted separately in a securing sleeve.
  • the mass of the firing pin is relatively small. With thin targets, its kinetic energy is often not sufficient to ignite a detonator. An ignition delay time is not provided.
  • US-A-3 718 093 relates to an impact detonator for exercise bombs, particularly when it is turned at an angle.
  • a firing pin and a securing sleeve are connected to one another via locking members in a securing manner, however, the locking sleeve is displaced in the ignition direction against the force of a spring upon impact and is finally locked by the locking members.
  • the firing pin then slides into the ignition position, supported by spring force.
  • the detonator is suitable for bombs, but not for missiles at long range and with thin targets. Since an ignition delay necessary for the projectile to penetrate sufficiently into the target is not achieved.
  • the object of the invention is therefore to create a impact detonator for a mechanical, highly sensitive ignition system which initiates initiation with sufficient ignition delay time in the case of thin targets, flat angles of incidence and long combat distances.
  • the firing pin has the mass required for inertia-dependent ignition with high impact energy.
  • the proportion of the spring's propulsive force is negligible.
  • the preloaded compression spring in conjunction with low friction losses during the movement of the firing pin ensures that the firing takes place safely with the firing pin.
  • the ignition delay time which is decisive for the degree of destruction of the target, can be determined in a simple manner. With a low impact energy there is a longer ignition delay time than with a high impact energy. This is due to the fact that when the impact energy is low, the securing sleeve only has to be at the rear, housing-fixed stop so that the locking bolt can pierce the primer with the required energy. In contrast, with a high impact energy, the shorter ignition delay time is ensured by the distance of the recess fixed to the housing from the securing or basic position of the mechanical delay device.
  • FIG. 1 shows a simplified cross-section through an igniter in the "safe" position
  • FIG. 2 shows the igniter according to FIG. 1 in the ignition position.
  • An impact detonator 1 consists of a housing 2 with recesses 3, 4 and bore 5, a cover 7 screwed at 6, a base body 8, a cup-shaped securing sleeve 9, a centrifugal securing device 10, a rotor 11 with a detonator 12 and a firing pin 13.
  • the firing pin 13 consists of a piston sleeve 14 with a riveted firing needle 15 and a compression spring 16 which is clamped between a collar 17 and a plate 18.
  • the piston sleeve 14 also has a stop 20, a space 21 for a compression spring 22 and recesses 23 for balls 24.
  • the compression spring 22 fixes the piston sleeve 14 on the balls 24 in the starting position.
  • the balls 24 are arranged in recesses 30. They are delimited on the outside by a guide wall 31 and on the inside by the compression spring 22.
  • the securing sleeve 9 is provided with a bottom 33 and a bore 34. Their mass is approx. 30% less than that of the firing pin 13.
  • annular recess 40 is provided at a distance 41, with a depth 42 and a length 43.
  • the distance 41 corresponds approximately to the diameter 44 of the balls 24 and lies between the surfaces of the cutouts 30, 40 on the igniter bottom side.
  • the depth 42 is somewhat greater than the diameter 44 of the balls.
  • the length 43 corresponds approximately to twice the diameter 44 of the balls 24.
  • an axial stroke of the securing sleeve 9 and the firing pin 13 coupled via the balls 24 takes place in the direction of arrow 45.
  • the axial stroke ends in a first phase when the balls 24 enter the recess 40 Tip 46 has reached the position labeled 50 at the end of the first phase.
  • the compression spring 22 telescopes the securing sleeve 9 and the piston sleeve 14 apart, counter to the direction of the arrow 45 up to the stop on the cover 7, and then in the third phase causes the firing pin 13 to advance until the detonator 12 is tapped 2.
  • the ignition delay time is added up from the times of phases 1 to 3.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)

Claims (4)

  1. Allumeur à percussion (1) pour projectile d'armes à tube comportant une amorce (12) qui peut être percutée de l'arrière au moyen d'un percuteur (14,15) actionné sous l'action d'un ressort, comportant un dispositif de retardement mécanique (9,14,15,22) qui comporte des corps de blocage (24) qui, dans leur position de blocage, se trouvent d'une part dans des évidements (23) du percuteur (14,15), d'autre part dans des évidements (30) d'un élément allumeur (9), l'élément allumeur étant réalisé sous la forme d'un manchon de sûreté (9) mobile axialement et un autre évidement (40) annulaire recevant les corps de blocage (24), étant prévu dans un corps de base (8) côté boîtier à une distance (41) de l'évidement (30) du manchon de sûreté (9) situé dans la direction d'allumage (45), distance (41) qui existe entre les surfaces des évidements (30,40) situées du côté du fond de l'allumeur, de sorte que les évidements (30,40) sont décalés entre eux de la distance (41).
  2. Allumeur à percussion selon la revendication 1, caractérisé en ce que les billes (24) verrouillent un manchon de piston (14) avec le manchon de sûreté (9) de telle sorte que, lors de l'impact sur la cible, le manchon de sûreté (9) effectue, en même temps que le percuteur (13) et un ressort de compression (22) une course axiale correspondant à la distance (41) au cours d'une première phase, puis le déverrouillage se produit, sur quoi , au cours d'une seconde phase, le ressort de compression (22) écarte d'abord télescopiquement le manchon de sûreté (9) et le manchon de piston (14) jusqu'à ce que le manchon de sûreté (9) soit immobile côté boîtier (couvercle 7), pour entraîner alors, au cours d'une troisième phase, le manchon de piston (14) vers l'avant (flèche 45) jusqu'au percement d'un détonateur (12).
  3. Allumeur à percussion selon la revendication 2, caractérisé en ce que le manchon de sûreté (9) présente une masse inférieure d'environ 30% à celle du percuteur (13).
  4. Allumeur à percussion selon la revendication 3, caractérisé en ce que le diamètre (14) des billes (24) correspond à la distance (41).
EP86112969A 1985-10-08 1986-09-19 Fusée d'impact comportant une amorce à percussion Expired - Lifetime EP0218947B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3535854 1985-10-08
DE19853535854 DE3535854A1 (de) 1985-10-08 1985-10-08 Aufschlagzuender mit einer zuendkapsel

Publications (2)

Publication Number Publication Date
EP0218947A1 EP0218947A1 (fr) 1987-04-22
EP0218947B1 true EP0218947B1 (fr) 1991-03-27

Family

ID=6283036

Family Applications (1)

Application Number Title Priority Date Filing Date
EP86112969A Expired - Lifetime EP0218947B1 (fr) 1985-10-08 1986-09-19 Fusée d'impact comportant une amorce à percussion

Country Status (4)

Country Link
US (1) US4693180A (fr)
EP (1) EP0218947B1 (fr)
CA (1) CA1285176C (fr)
DE (2) DE3535854A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3933436A1 (de) * 1989-10-06 1991-04-18 Diehl Gmbh & Co Bodenzuender fuer rohrwaffengeschosse mit aufschlagfunktion
US5872324A (en) * 1997-07-07 1999-02-16 The United States Of America As Represented By The Secretary Of The Navy Trimode fuze
DE19901045B4 (de) * 1999-01-14 2007-06-06 Junghans Feinwerktechnik Gmbh & Co. Kg Aufschlageinrichtung für einen elektronischen Annäherungszünder mit einem ein Anzündstück tragenden Aufschlagkörper
US7587979B2 (en) * 2006-08-02 2009-09-15 Omnitek Partners Llc Multi-stage mechanical delay mechanisms for inertial igniters for thermal batteries and the like
FR2991447B1 (fr) * 2012-05-30 2017-04-07 Mbda France Systeme d'armement securise pour charge explosive

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR579672A (fr) * 1923-05-26 1924-10-21 Allumeur pour grenades à main, projectiles de minenwerfer ou autres
FR599412A (fr) * 1924-06-09 1926-01-12 Fusée à répulsion
US2376332A (en) * 1941-06-14 1945-05-22 Adelman Arthur Antitank mine fuse
US2513536A (en) * 1947-01-03 1950-07-04 Us Sec War All angle of impact inertia fuse
US2701527A (en) * 1948-07-06 1955-02-08 Louis P Granath Selective delayed-action fuze
FR1017844A (fr) * 1950-03-29 1952-12-19 Soc Tech De Rech Ind Fusée pour amorçage des projectiles
BE508953A (fr) * 1951-02-08
CH402672A (de) * 1962-08-02 1965-11-15 Oerlikon Buehrle Holding Ag Selbstzerlegerzünder für Drallgeschosse
NL123881C (fr) * 1963-02-07
US3638501A (en) * 1970-04-27 1972-02-01 Gen Motors Corp Sensor
US3718093A (en) * 1971-04-22 1973-02-27 Us Army Firing pin assembly
CH585891A5 (fr) * 1974-11-20 1977-03-15 Oerlikon Buehrle Ag
CH623408A5 (fr) * 1977-10-20 1981-05-29 Oerlikon Buehrle Ag
EP0068534B1 (fr) * 1981-06-30 1985-01-23 Werkzeugmaschinenfabrik Oerlikon-Bührle AG Dispositif de sécurité pour la fusée d'un projectile stabilisé par rotation
AT374584B (de) * 1982-08-03 1984-05-10 Oregon Ets Patentverwertung Sicherungseinrichtung bei einer granate
ATE23634T1 (de) * 1982-12-10 1986-11-15 Oerlikon Buehrle Ag Aufschlagzuender.

Also Published As

Publication number Publication date
EP0218947A1 (fr) 1987-04-22
DE3535854A1 (de) 1987-04-09
US4693180A (en) 1987-09-15
DE3678380D1 (de) 1991-05-02
CA1285176C (fr) 1991-06-25

Similar Documents

Publication Publication Date Title
EP0364670B1 (fr) Grenade
EP0583642B1 (fr) Engin explosif emportant deux charges placées en tandem
DE69015046T2 (de) Zündvorrichtung einer Zündkette für Submunitionskörpern.
DE3624713A1 (de) Zuender fuer ein fallschirm- oder bandstabilisiertes, im flug rotierendes bomblett
EP0158700B1 (fr) Fusée pour projectile secondaire
EP0218947B1 (fr) Fusée d'impact comportant une amorce à percussion
EP0318995A2 (fr) Allumeur pyrotechnique pour projectiles
EP0156763B1 (fr) Méthode et dispositif pour augmenter l'énergie dans une amorce électromagnétique
EP0104138B1 (fr) Dispositif pour armer et neutraliser une fusée électrique pour munition
DE4303128C2 (de) Zündvorrichtung für Geschosse, Raketen, Bomblets und Minen mit einer pyrotechnischen Selbstzerlegervorrichtung
EP0318996B1 (fr) Allumeur pyrotechnique pour projectiles, roquettes bombes et mines
CH657450A5 (de) Beharrungszuender fuer drallgeschosse mit selbstzerlegereinrichtung.
DE854314C (de) Aufschlagzuender fuer Geschosse
EP0227919B1 (fr) Fusée d'impact pour projectile
CH656001A5 (de) Zuender sowie geschoss mit einem zuender.
DE4127023A1 (de) Treibladungsanzuender
DE7928929U1 (de) Aufschlagzuendkopf fuer ein explosivgeschoss
EP0421334B1 (fr) Fusée de culot pour projectiles fonctionnant à l'impact
DE2918039A1 (de) Mechanischer aufschlagzerlegerzuender fuer drallstabilisierte geschosse
AT407575B (de) Sicherungsvorrichtung für zünder von drallgeschossen
DE3533753A1 (de) Boden-aufschlagzuender mit geteiltem schlagstueck
AT214812B (de) Mechanischer Aufschlagzünder für Geschosse mit doppelter und mehrfacher Anfeuerung
DE250697C (fr)
DE1158876B (de) Mechanischer Aufschlagzuender fuer ein Raketengeschoss
DE3507392A1 (de) Gefechtskopf

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

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): CH DE GB IT LI NL

17P Request for examination filed

Effective date: 19870326

17Q First examination report despatched

Effective date: 19881024

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): CH DE GB IT LI NL

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRE;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.SCRIBED TIME-LIMIT

Effective date: 19910327

Ref country code: GB

Effective date: 19910327

REF Corresponds to:

Ref document number: 3678380

Country of ref document: DE

Date of ref document: 19910502

GBV Gb: ep patent (uk) treated as always having been void in accordance with gb section 77(7)/1977 [no translation filed]
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

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 19960930

Year of fee payment: 11

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: 19980401

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 19980401

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20031017

Year of fee payment: 18

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20031126

Year of fee payment: 18

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20040930

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20040930

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: 20050401

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL