[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

EP0111198B1 - Fusée à percussion - Google Patents

Fusée à percussion Download PDF

Info

Publication number
EP0111198B1
EP0111198B1 EP83111613A EP83111613A EP0111198B1 EP 0111198 B1 EP0111198 B1 EP 0111198B1 EP 83111613 A EP83111613 A EP 83111613A EP 83111613 A EP83111613 A EP 83111613A EP 0111198 B1 EP0111198 B1 EP 0111198B1
Authority
EP
European Patent Office
Prior art keywords
percussion
inertia
sleeve
needle
fuse
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
Application number
EP83111613A
Other languages
German (de)
English (en)
Other versions
EP0111198A2 (fr
EP0111198A3 (en
Inventor
Robert Apothéloz
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.)
Rheinmetall Air Defence AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
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 Werkzeugmaschinenfabrik Oerlikon Buhrle AG filed Critical Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Priority to AT83111613T priority Critical patent/ATE23634T1/de
Publication of EP0111198A2 publication Critical patent/EP0111198A2/fr
Publication of EP0111198A3 publication Critical patent/EP0111198A3/de
Application granted granted Critical
Publication of EP0111198B1 publication Critical patent/EP0111198B1/fr
Expired 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, with an ignition capsule which can be pierced from behind by an ignition pin, with locking bodies which are in their locking position on the one hand in a recess in the ignition pin and on the other hand rest on a bolt fastened in the ignition housing and on a displaceable inertia sleeve, to hold the firing pin and with a spring, which is supported with its rear end on the inertial sleeve and tends to hold the inertial sleeve in its rearmost position.
  • a mechanical delay device is provided so that the projectile can penetrate as deep as possible into the target.
  • a device for delayed ignition is provided in addition to a momentary detonator, with an inertial ignition pin which is supported directly by a weak flight safety spring and is held in its initial position during the flight.
  • the delay i. H. Braking of the projectile is initially so small that the inertial firing pin hits the primer at too low a piercing speed and is therefore unable to ignite it properly.
  • the object that is to be achieved with the present invention is now to provide a detonator in which the detonator pin is retained during the penetration process of the projectile into soft earth or snow until the projectile has penetrated on a harder ground.
  • the delay of the floor, i. H. its braking is then so great that when the firing pin is released, it now hits the primer at a sufficiently high piercing speed to ensure proper ignition.
  • the invention also aims to provide a detonator that can be destroyed relatively safely if the detonator has not responded and the projectile has become a dud.
  • the detonator according to the invention differs in that it uses a much stronger flight safety spring. This stronger spring means that if the primer capsule is not pierced correctly, it is more likely that the firing pin will be pushed back and a pricking, e.g. B. is practically avoided by clumsy handling of the dud.
  • the inertial piercing system according to the invention can be used both with an instantaneous capsule as a "double igniter", for example with an additional ignition delay, and with a delayed primer.
  • the igniter is provided with a device which enables the instantaneous -Lock the surcharge system.
  • the impact detonator according to the invention has a housing 10 with a bore 11 and a channel 12.
  • a slide 13 is slidably mounted in the channel 12.
  • this slide 13 contains a primer 14.
  • the primer 14 consists in the usual way of a prick-sensitive primer 15, which is located in a capsule housing 16.
  • This capsule housing 16 has an opening 17 at the bottom through which an ignition pin 18 can pierce the ignition compound 15.
  • the carriage 13 can be moved from a safety position, in which the primer 14 is not in the area of the firing pin 18, to an arming position, in which the primer 14 is located in the area of the firing pin 18.
  • a safety position in which the primer 14 is not in the area of the firing pin 18, to an arming position, in which the primer 14 is located in the area of the firing pin 18.
  • Fig. 1 the safety position and in Fig. 2 and 3 the focus is shown.
  • a sleeve 19 is slidably mounted in the mentioned bore 11 of the housing 10. 1, in the safety position of the slide 13, this sleeve 19 abuts with its front end against this slide 13 and with its rear end against a flange 20 of a bolt 21.
  • This flange 20 abuts a shoulder 22 of the bore 11 and is on the other hand held by a flange 23 in the bore 11.
  • the sleeve 19 is thus secured against any displacement in the safety position of the slide 13. However, as soon as the carriage 13 is in its focused position, the sleeve 19 can be pushed forward against the force of a strong spring 24, as can be seen from FIGS. 2 and 3. In this foremost position of the sleeve 19, a shoulder 25 of the sleeve 19 bears against a ring 26 which is fastened in the housing 10 of the impact detonator. In this sleeve 19, the ignition pin 18 is slidably mounted. At the rear end of the firing pin 18 there is a longitudinal bore 27 and a transverse bore 28.
  • the firing pin 18 has an annular shoulder 31 in the central region, which interacts with a corresponding annular shoulder 32 in the interior of the sleeve 19. As can be seen from FIG. 3, the shoulder 31 of the ignition pin 18 abuts against the shoulder 32 inside the sleeve 19 as soon as the tip of the ignition pin 18 penetrates into the ignition capsule 14.
  • the spring 24 is able, when the delay disappears, to push the sleeve 19 back into its starting position according to FIG. H. 3, the sleeve 19 is pushed back by the amount a. Since the shoulder 31 of the ignition pin 18 rests on the shoulder 32 of the sleeve 19 (FIG. 3), the ignition pin 18 is also pushed back by the amount a. Thus, after the impact delay has disappeared, the firing pin 18 can no longer pierce the squib 14. Since the impact deceleration is relatively large, a correspondingly strong spring 24 can be used. If, therefore, the firing pin 18 is no longer secured against displacement by the locking body 29, as shown in FIG. 1, the firing pin 18 is still secured by the relatively strong spring 24 - after an ignition failure - against undesired puncturing of the primer 14 .

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Electrophonic Musical Instruments (AREA)
  • Toys (AREA)
  • Thermistors And Varistors (AREA)

Claims (7)

1. Fusée à percussion comportant une amorce (14) susceptible d'être percutée par l'arrière, par un percuteur (18), et des organes de verrouillage (29) qui en position de verrouillage pénètre d'une part dans une cavité (28), du percuteur (18), et d'autre part s'appuie contre un goujon (21) fixé au boîtier (10) de la fusée et s'appuie contre une douille à inertie (19) coulissante pour maintenir fixe le percuteur (18) et un ressort (24) qui s'appuie d'une part contre la douille à inertie (19) et a tendance à maintenir la douille à inertie (19) dans sa position la plus à l'arrière, caractérisée en ce que le ressort (24) s'appuie par ailleurs sur le boîtier (10) du percuteur et en ce que le déplacement du percuteur (18) vers l'amorce (14) est assuré exclusivement par la force d'inertie s'exerçant sur le percuteur (18).
2. Fusée à percussion selon la revendication 1, caractérisée en ce que le percuteur (18) comporte un épaulement (31) qui coopère avec un épaulement (32) de la face intérieure de la douille à inertie (19) pour éviter toute avancée du percuteur (18) vers l'amorce (14) au cas où la douille à inertie (19) ne se trouverait pas dans sa position la plus avancée.
3. Fusée à percussion selon la revendication 1, caractérisée en ce que la douille à inertie (19) comporte un deuxième épaulement (30) sur sa face interne, épaulement sur lequel s'appuient les organes de verrouillage (29) lorsqu'ils sont dans leur position de verrouillage et en ce que le goujon (21) fixé au boîtier (10) du percuteur présente une surface supérieure cylindrique lisse afin que sous l'effet de la force d'inertie, la douille à inertie (19) et le percuteur (18) se déplacent ensemble.
4. Fusée à percussion selon la revendication 1, caractérisée par un équipage mobile (13) contenant l'amorce (14) et qui peut se déplacer transversalement au percuteur (18), équipage susceptible d'être coulissé d'une position de sécurité dans une position d'armement, évite lorsqu'il est en position de sécurité, la translation de la douille à inertie (19) et du percuteur (18).
5. Fusée à percussion selon la revendication 1, caractérisée en ce que la douille à inertie (19) comporte sur son côté extérieur un épaulement (25) qui lorsque la douille à inertie (19) occupe sa position la plus avancée, s'appuie contre une bague fixe (26) du boîtier de fusée (10).
6. Fusée à percussion selon la revendication 1, caractérisée en ce que l'amorce (14) est une amorce pyrotechnique temporisée.
7. Fusée à percussion selon la revendication 1, caractérisée en ce que seule la force d'inertie agit sur le percuteur (18).
EP83111613A 1982-12-10 1983-11-21 Fusée à percussion Expired EP0111198B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT83111613T ATE23634T1 (de) 1982-12-10 1983-11-21 Aufschlagzuender.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH7207/82 1982-12-10
CH720782 1982-12-10

Publications (3)

Publication Number Publication Date
EP0111198A2 EP0111198A2 (fr) 1984-06-20
EP0111198A3 EP0111198A3 (en) 1984-09-12
EP0111198B1 true EP0111198B1 (fr) 1986-11-12

Family

ID=4321549

Family Applications (1)

Application Number Title Priority Date Filing Date
EP83111613A Expired EP0111198B1 (fr) 1982-12-10 1983-11-21 Fusée à percussion

Country Status (4)

Country Link
EP (1) EP0111198B1 (fr)
AT (1) ATE23634T1 (fr)
CA (1) CA1242609A (fr)
DE (1) DE3367673D1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3535854A1 (de) * 1985-10-08 1987-04-09 Diehl Gmbh & Co Aufschlagzuender mit einer zuendkapsel

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL22031C (fr) * 1923-10-25
US3425351A (en) * 1954-12-21 1969-02-04 Us Army Setback-responsive igniter for ordnance projectiles
NL236971A (fr) * 1958-03-28

Also Published As

Publication number Publication date
EP0111198A2 (fr) 1984-06-20
EP0111198A3 (en) 1984-09-12
DE3367673D1 (en) 1987-01-02
CA1242609A (fr) 1988-10-04
ATE23634T1 (de) 1986-11-15

Similar Documents

Publication Publication Date Title
DE1086594B (de) Zerlegerzuender
DE2907308C2 (de) Geschoß mit mindestens einem ausstoßbaren Tochtergeschoß
DE2550093C3 (de) Beharrungszünder für Drallgeschosse mit Selbstzerlegereinrichtung
DE2621488C3 (de) Sperrvorrichtung für einen Aufschlagzünder
DE2838381C2 (de) Sicherheitsvorrichtung für Zündvorrichtungen
DE3149346A1 (de) Aufschlagzuender
DE3119369C2 (de) Beharrungszünder für Drallgeschosse mit Selbstzerlegereinrichtung
DE2132106A1 (de) Aufschlagzueder fuer Geschosse
DE450061C (de) Zuender mit Vorrichtung zum Verhindern des Rueckschlagens des Zuendstrahls
EP0111198B1 (fr) Fusée à percussion
DE560525C (de) Mechanischer Verzoegerungszuender fuer Drallgeschosse
DE1155695B (de) Aufschlagzuender fuer Raketen
EP0602632A2 (fr) Fusée à sécurité de bouche et projectile comportant une telle fusée
DE304247C (fr)
DE2842882C3 (de) Aufschlagzünder mit einer Zündkapsel
DE729174C (de) Aufschlagzuender
DE480272C (de) Aufschlagzuender fuer Geschosse, Luftbomben o. dgl.
DE309791C (fr)
DE2242956A1 (de) Zuender fuer drallose geschosse
AT228098B (de) Aufschlagzünder für Geschosse
EP0139173B1 (fr) Dispositif de sécurité pour une fusée à percussion d'un projectile
DE952875C (de) Aufschlagzuender fuer Drallgeschosse, Bomben od. dgl.
AT374584B (de) Sicherungseinrichtung bei einer granate
CH663277A5 (en) Centrifugal lock on an impact fuze for a spinning projectile
DE3344009A1 (de) Aufschlagzuender fuer bombletts

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

Designated state(s): AT BE CH DE FR GB IT LI

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Designated state(s): AT BE CH DE FR GB IT LI

17P Request for examination filed

Effective date: 19840927

17Q First examination report despatched

Effective date: 19860129

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

ITF It: translation for a ep patent filed
AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH DE FR GB IT LI

REF Corresponds to:

Ref document number: 23634

Country of ref document: AT

Date of ref document: 19861115

Kind code of ref document: T

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

Ref country code: AT

Payment date: 19861209

Year of fee payment: 4

REF Corresponds to:

Ref document number: 3367673

Country of ref document: DE

Date of ref document: 19870102

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

Ref country code: AT

Effective date: 19871121

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

Ref country code: LI

Effective date: 19871130

Ref country code: CH

Effective date: 19871130

Ref country code: BE

Effective date: 19871130

BERE Be: lapsed

Owner name: WERKZEUGMASCHINENFABRIK OERLIKON-BUHRLE A.G.

Effective date: 19871130

GBPC Gb: european patent ceased through non-payment of renewal fee
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

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

Effective date: 19880729

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

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

Ref country code: DE

Effective date: 19880802

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

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

Ref country code: GB

Effective date: 19881122