EP0410064A1 - Self disarming fuze for cargo munition grenades - Google Patents

Self disarming fuze for cargo munition grenades Download PDF

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Publication number
EP0410064A1
EP0410064A1 EP89600019A EP89600019A EP0410064A1 EP 0410064 A1 EP0410064 A1 EP 0410064A1 EP 89600019 A EP89600019 A EP 89600019A EP 89600019 A EP89600019 A EP 89600019A EP 0410064 A1 EP0410064 A1 EP 0410064A1
Authority
EP
European Patent Office
Prior art keywords
fuze
grenades
disarming
self
slider
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Withdrawn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
EP89600019A
Other languages
German (de)
French (fr)
Inventor
Panagiotis Karamanolis
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of EP0410064A1 publication Critical patent/EP0410064A1/en
Withdrawn legal-status Critical Current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
    • 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
    • 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
    • F42C15/44Arrangements for disarming, or for rendering harmless, fuzes after arming, e.g. after launch

Definitions

  • the invention is referring to a self disarming fuze that can be used in grenades of artillery cargo munition, as well as in rotating mortars, bombs, and rockets.
  • the unexploded grenades are dangerous for the troops that will go through the bombarded areas, as well as for the field cleaning personel.
  • the armies that are currently using cargo munitions demand the use of a fuze, for the grenades, that will be self-destructive in the case that they will not operate, for any reason, after the impact on the target.
  • the described fuze, that constitutes the opject of the invention is self disarming, in the occasion that it will not operate after the impact on the target, making the grenade entirely harmless.
  • the fuze For the rare occasion that the fuze will not operate explosively and it will not self disarm after the impact of the grenade on the target, the fuze is again harmless for the troops that will go through the field and accidentally step on a grenade.
  • the detonator (7) and the striker (3) are off line.
  • the slider (2) cannot move in the armed position, because the end of the striker (3) is inside an opening of the slider (2),and retained in this position by the safety (5).
  • the entire system of the slider (2) and the striker (3) and the safety (5), is inside the shell (1) and enclosed with the metal plate (11).
  • the fuze is shown in the armed position.
  • the safety (5) of figure 1 is separated and the striker (3) has been retracted from the slider (2) because of the expansion of the spring (4) of figures 1 and 2.
  • the slider (2) because of the centrifugal force, has moved in a way that the detonator (7) is on line with the striker (3) making the spring (6) be compressed.
  • the upright position of the grenade during the fall is assured by the ribbon (13), that is firmly attached on the top of the fuze with the metal straps (9) and (14).
  • the metal straps (9a) and (9b), in the ribbon ends, during the rotation maintain the ribbon in an almost horizontal position, simulating in this maner the helicopter blades.
  • the metal straps (9a) and (9b) can be omitted if the ribbon, when rotating, has enough weight to maintain its horizontal position during the rotation of the grenade.
  • figure 3 side view
  • the striker (3) because of the inertia, has struck the detonator (7), causing its explosion.
  • the slider (2) is shown in top and side view.
  • location (1) the detonator (7) of figures 1,2,3 is placed.
  • location (3) the end of the striker (3) figures 1,2,3 is inserted when the fuze is in safe position.
  • the groove (4) is making the movement of the slider (2) easier during the arming procedure.
  • the movable cylinder or sphere (6), is located in groove (5).
  • the reason for the cylinder of sphere (6) is to maintain the slider (2) in armed position when the spin of the fuze is reduced or stopped.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)

Abstract

The self disarming fuze, for cargo munition that is used on grenades that are being carried above the target by cargo munitions and dis­persed in a great area, and exploding after the impact on the ground, sea, or any other target. The fuze is being armed during the rota­tion of the grenade immediately after its expulsion from the project­ile, and in an adequate height above the ground.
In case the grenade hits the target, or the ground and the fuze will not operate,(remotest possibility), then the fuze will immediately return to the disarmed position, making the grenade completely safe for handling, or for the occasion that a truck, or any other vehicle, or even personnel, will go through the bombarded area.

Description

  • The invention is referring to a self disarming fuze that can be used in grenades of artillery cargo munition, as well as in rotating mortars, bombs, and rockets.
  • The fuzes in use today, in cargo munitions, do not solve the signifi­cant problem of not exploded granades in the battlefield, or in the training field.
  • The unexploded grenades are dangerous for the troops that will go through the bombarded areas, as well as for the field cleaning personel.
  • The armies that are currently using cargo munitions, demand the use of a fuze, for the grenades, that will be self-destructive in the case that they will not operate, for any reason, after the impact on the target.
  • The only way of self distruction, that has been devised up to now is pyrotechnical. This solution is not acceptable by the users, because, besides the high cost, in a case that the self destruction mechanism will not operate, even to a low percentage, it will render the grena­des more hazardous than the ones that are using common fuzes.
  • The described fuze, that constitutes the opject of the invention is self disarming, in the occasion that it will not operate after the impact on the target, making the grenade entirely harmless.
  • For the rare occasion that the fuze will not operate explosively and it will not self disarm after the impact of the grenade on the target, the fuze is again harmless for the troops that will go through the field and accidentally step on a grenade.
  • In figure 1, an overall picture of the fuze is given, with the slider (2) of the detonator (7), in a safe position that is achieved by the pressure of the spring (6).
  • In this case, the detonator (7) and the striker (3), are off line. In addition the slider (2) cannot move in the armed position, because the end of the striker (3) is inside an opening of the slider (2),and retained in this position by the safety (5). The entire system of the slider (2) and the striker (3) and the safety (5), is inside the shell (1) and enclosed with the metal plate (11). In figure 2 (side section) the fuze is shown in the armed position. By the rotation of the fuze, the safety (5) of figure 1 is separated and the striker (3) has been retracted from the slider (2) because of the expansion of the spring (4) of figures 1 and 2. The slider (2), because of the centrifugal force, has moved in a way that the detonator (7) is on line with the striker (3) making the spring (6) be compressed.
  • The exact position of the slider (2), is determined by the end stop­per (2a), that is freely sliding in an opposite groove (12) of the shell (1).
  • The upright position of the grenade during the fall is assured by the ribbon (13), that is firmly attached on the top of the fuze with the metal straps (9) and (14). The metal straps (9a) and (9b), in the ribbon ends, during the rotation maintain the ribbon in an almost horizontal position, simulating in this maner the helicopter blades. The metal straps (9a) and (9b) can be omitted if the ribbon, when rotating, has enough weight to maintain its horizontal position during the rotation of the grenade.
  • In figure 3 (side view) is shown the fuze when the grenade is hitting the target. The striker (3), because of the inertia, has struck the detonator (7), causing its explosion. In figure (4) the slider (2) is shown in top and side view. In location (1) the detonator (7) of figures 1,2,3 is placed. In location (3) the end of the striker (3) figures 1,2,3 is inserted when the fuze is in safe position.
  • The groove (4) is making the movement of the slider (2) easier during the arming procedure. The movable cylinder or sphere (6), is located in groove (5).
  • The reason for the cylinder of sphere (6) is to maintain the slider (2) in armed position when the spin of the fuze is reduced or stopped.
  • In figure 5 (down view of the shell (1) of figures 1,2, and 3) are shown:
  • -The groove (12) in which the stopper (2a) of figures 1,2 and 3 can slide freely.
  • -The two holes (16) and (16a), are used to mount the fuze on the gre­nade.
  • -The cylindrical cavity (10) inside which the striker (3) can move in figures 1,2, and 3.
  • -The opening (15) that is used for partial entry of the cylinder (6) of figure 4 when due to the centrifugal force, the slider (2) of the detonator of figure 4 has stopped in the armed position.
  • The section of the cylinder (6) in figure 4 that has moved in to gro­ove (15) restricts the movement of the slider to the safe position, despite the pressure of the spring (16) in figures 1,2, and 3.
  • If during the impact, and for any reason, the detonator (7) of figu­res 1,2,3 will not explode, then, because of the shock, the small cylinder (6) of figure 4, is retract toward the groove (5) of figure 4 and the slider (2) with the pressure of the spring (6) of figures 1,2 and 3 returns to the safe position as in figure 1.
  • In figurs 6,7 and 8, are shown the above mentioned metal plates (14) (9) and (11) of figures 1 and 2.
  • In figure 9,is shown the fuze as it will be assembled and ready for shipping. The safety pin (17), is holding the ribbon (13) tight in place and also helps the loading of the shell with grenades in a spe­cial order.

Claims (8)

1. The self disarming fuze for cargo munition grenades which consists of the following.
a. The cell (1), figure 1.
b. The slider, figure 4.
c. The striker (3), figure 1.
d. The safely pin (5), figure 1.
e. The spring (4), of the striker (3) figure 1.
f. The spring (6), of the slider (2) figure 1.
g. The ribbon (13), figure 2.
h. The metalsheet (9), in figure 2, which holds the ribbon.
i. The metal sheets (9a) and (9b), figure 2.
j. The cylinder or small sphere (6), figure 4.
k. The metal sheet (14), figure 6.
1. The metal sheet (11), figure 8.
2.The self disarming fuze for cargo munition grenades, as in claim 1, is distinguished from the ribbon (13), figure 2 which is securely attached on the top of the fuze, and rotates with the grenade, assu­ring this way the vertical fall of the granade to the ground or to the target.
3.The self disarming fuze for cargo munition grenades, as in claim 1, is distinguished from the striker (3) in figure 1, which is inde­pendent from the ribbon and is retracted from the detonator (7), figure 2 with the help of the spring (4) figure 2, after its impact to the detonator (7), figure 2.
4.The self disarming fuze for cargo munition grenades as in claim 1, which is distringuished from the fact that the slider (2) of the detomator (7), figure 2, (the details can be seen in figure 4 ) , moves to the armed position because of the centrifugal force, over­coming the spring (6) force, figures 1,2, and 3.
5.The shelf disarming fuze for cargo munition grenades as in clain 1, which is distinguished by the fact that the cylinder or sphere system (6) of figure 4 that enters the groove (15), figure 5, because of the centrifugal force and holds the slider (2), as in figure 2, in the armed position, even ifthe spin is reduced or stopped during the free fall of the grenade.
6.The shelf disarming fuze for cargo munition grenades as in claim 1, which is distinguished by fact that the safety (5), figure 1, is hol­ding the slider (2), figure 1, in a non armed position, until the expulsion of the grenades from the shell.
7.The self disarming fuze for cargo munition grenades as in claim 1, which is distinguished by the fact that the shell (1), figure 1, has certain grooves, that the slider (2), the striker (3), and the safe­ties operate properly. Top view of the shell can be seen in figure 5.
8.The self disarming fuze for cargo munition granades as in claim 1, which is distinguished by the fact that the metal sheets (14) and (11) of figures 6, and 8 respectively, are holding the fuze as an assembly, and also increasing the strength and endurance of the fuze in the extremely high accelerations of 15.000 Gs that are exerted on the projectile during the firing of the cannon.
EP89600019A 1989-07-20 1989-10-02 Self disarming fuze for cargo munition grenades Withdrawn EP0410064A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GR89100460 1989-07-20
GR89100460 1989-07-20

Publications (1)

Publication Number Publication Date
EP0410064A1 true EP0410064A1 (en) 1991-01-30

Family

ID=10939459

Family Applications (1)

Application Number Title Priority Date Filing Date
EP89600019A Withdrawn EP0410064A1 (en) 1989-07-20 1989-10-02 Self disarming fuze for cargo munition grenades

Country Status (3)

Country Link
EP (1) EP0410064A1 (en)
GR (1) GR890100460A (en)
WO (1) WO1992012396A1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992012396A1 (en) * 1989-07-20 1992-07-23 Panagiotis Karamanolis Self disarming fuze for cargo munition granades
DE4421353A1 (en) * 1994-06-17 1995-12-21 Junghans Gmbh Geb Bomblet fuse to make safe unexploded shells
GR1004597B (en) * 2003-05-09 2004-06-18 Ευαγγελος Ιωαννη Κωνστας Mechanical fuse for the self-destructionn og grenades of grenade-carrying munitions
EP2669619A1 (en) * 2012-05-30 2013-12-04 MBDA France Secured arming device for explosive charge

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3926122A (en) * 1972-08-11 1975-12-16 Us Army Grenade with fuze (U)
US3956992A (en) * 1974-08-01 1976-05-18 The United States Of America As Represented By The Secretary Of The Army Wide-angle inertial impact fuze
US4612858A (en) * 1983-09-15 1986-09-23 Rheinmetall Gmbh. Fuse for a satellite projectile
US4762066A (en) * 1986-07-22 1988-08-09 Diehl Gmbh & Co. Fuze for a parachute-stabilized or band-stabilized small bomb which rotates during flight

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3603259A (en) * 1968-06-26 1971-09-07 Avco Corp Fuze setback and angular acceleration detent
DE2358310C1 (en) * 1973-11-23 1979-12-06 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Safety device for tinder from explosive charges, in particular from jumping mines
US4242963A (en) * 1978-09-25 1981-01-06 General Electric Company Delayed arming fuze for a spinning projectile
GR890100460A (en) * 1989-07-20 1991-12-10 Panagiotis Karamanolis Selfdisarming fuze for cargo munition grenades

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3926122A (en) * 1972-08-11 1975-12-16 Us Army Grenade with fuze (U)
US3956992A (en) * 1974-08-01 1976-05-18 The United States Of America As Represented By The Secretary Of The Army Wide-angle inertial impact fuze
US4612858A (en) * 1983-09-15 1986-09-23 Rheinmetall Gmbh. Fuse for a satellite projectile
US4762066A (en) * 1986-07-22 1988-08-09 Diehl Gmbh & Co. Fuze for a parachute-stabilized or band-stabilized small bomb which rotates during flight

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1992012396A1 (en) * 1989-07-20 1992-07-23 Panagiotis Karamanolis Self disarming fuze for cargo munition granades
DE4421353A1 (en) * 1994-06-17 1995-12-21 Junghans Gmbh Geb Bomblet fuse to make safe unexploded shells
DE4421353C2 (en) * 1994-06-17 1998-02-05 Junghans Gmbh Geb Self-neutralizing bomb detonator
GR1004597B (en) * 2003-05-09 2004-06-18 Ευαγγελος Ιωαννη Κωνστας Mechanical fuse for the self-destructionn og grenades of grenade-carrying munitions
EP2669619A1 (en) * 2012-05-30 2013-12-04 MBDA France Secured arming device for explosive charge
WO2013178889A1 (en) * 2012-05-30 2013-12-05 Mbda France Safety arming system for an explosive charge
FR2991447A1 (en) * 2012-05-30 2013-12-06 Mbda France SECURE ARMING SYSTEM FOR EXPLOSIVE LOAD
US9435624B2 (en) 2012-05-30 2016-09-06 Mbda France Safety arming system for an explosive charge

Also Published As

Publication number Publication date
WO1992012396A1 (en) 1992-07-23
GR890100460A (en) 1991-12-10

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