IL41998A - Electro-mechanical proximity fuse for projectiles - Google Patents
Electro-mechanical proximity fuse for projectilesInfo
- Publication number
- IL41998A IL41998A IL41998A IL4199873A IL41998A IL 41998 A IL41998 A IL 41998A IL 41998 A IL41998 A IL 41998A IL 4199873 A IL4199873 A IL 4199873A IL 41998 A IL41998 A IL 41998A
- Authority
- IL
- Israel
- Prior art keywords
- striker
- detonator
- weight
- cap
- fuse
- Prior art date
Links
- 238000010304 firing Methods 0.000 claims 4
- 229920003023 plastic Polymers 0.000 claims 2
- 239000004033 plastic Substances 0.000 claims 2
- 239000000463 material Substances 0.000 claims 1
- 230000005855 radiation Effects 0.000 claims 1
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
- F42C15/18—Arming-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
- F42C15/184—Arming-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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C13/00—Proximity fuzes; Fuzes for remote detonation
- F42C13/02—Proximity fuzes; Fuzes for remote detonation operated by intensity of light or similar radiation
-
- 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
- F42C19/00—Details of fuzes
- F42C19/06—Electric contact parts specially adapted for use with electric fuzes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C9/00—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
- F42C9/14—Double fuzes; Multiple fuzes
- F42C9/148—Proximity fuzes in combination with other fuzes
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
- Radar Systems Or Details Thereof (AREA)
- Nozzles (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Claims (3)
1. A proximity fuse for missiles, including a body fitted on the nose of the missile and a cap revolvably carried by the body and provided with a cover forming a radome permeable to hyperfrequency radiation, said fuse being characterized by the fact that the radome is made of a deformable material and encloses a detecting aerial rigid with the compact electronic section adapted to slide inside the cap so as to form a striking plunger, while the mechanism includes a detonator-carrier adapted to slide transversely in the body under the action of a spring or of centrifugal force, said detonator-carrier being normally held in an inoperative position by the end of rod of an axial striker the fron tail-piece of which carries slidingly a striker weight urged forwardly by a spring and locked when inoperative by a first ball engaging an annular groove in said tailnpiece and held in its turn in position by a second ball or the like member adapted to move transversely and locked in its normal position by an arming weight adapted to move inside the cap along a line parallel with the striker and urged forwardl by a ferther spring, said arming weight including a rearward extension passing through said further spring, the weight on the striker being locked by means such as a circlips adapted to engage a further groove in the striker tail-piece after the striker weight has travelled sufficiently in a rearward direction upon firing of the missile and after the arming weight has itself bee shifted rearwardly through inertia and has thus released the balls whereby, the striker weight having first returned forwardly under the action of its spring, the front end of the striker tail-piece engages the striking plunger while the 41998/2 ^J striker rear tip releases the transverse movement of the detonator-carrier, so as to bring' the detonator in front of said tip and to close at the end of its stroke a switch controlling the electronic circuit, while an electric primer arranged in parallelism with the s riker communicates through channels formed in the ca and i the body with the main detonator when brought into its operative axial position, said primer being connected with the electronic detecting means through a delaying condenser, the whole arrangement being such that after a rotation through say 90° of the cap with reference to the fuse body, the channel in the cap connected with the electric .primer is out of registry with the corresponding channel in the fuse body whereby the first sequence of firing means is broken, while the rear tail-piece on the arming weight is out of registry with the port provided in the f se body for its collapse, so that the second sequence of firing means is also broken by the looking of the striker in its rearmost position, which, as a second safety, prevents the transverse movement of the detonator carrier and thereby breaks both pyrotechnical chains of sequential firing means and also the electric circuit.
2. A fuse as claimed in claim 1, wherein the electric circuit includes a general switch constituted by two elastic conductive blades into the interval between which may be inserted a conductive member provided with an annular retaining groove and rigid with the detonator-carrier.
3. A f se as claimed in claim 1, wherein the cap carries a block of plastics molded over the general switch controlling the electric circuit, over the condenser, over the electric primer and over their connections , said block extending rearwardly through an opening in the fuse body, which provides abutments for the rotation of the cap with reference to the body, the rearward extension of the block ending with connectihgyplugs engaging a further block of plastics molded over the battery and revolvably surrounding a tube forming a pyrotechnical relay between the detonator and a rear booster. For the Applicants DR. NERS HE:mr
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7212527A FR2180159A5 (en) | 1972-04-10 | 1972-04-10 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IL41998A0 IL41998A0 (en) | 1973-06-29 |
| IL41998A true IL41998A (en) | 1976-09-30 |
Family
ID=9096601
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IL41998A IL41998A (en) | 1972-04-10 | 1973-04-10 | Electro-mechanical proximity fuse for projectiles |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US3839963A (en) |
| JP (1) | JPS4948200A (en) |
| DE (1) | DE2318039A1 (en) |
| FR (1) | FR2180159A5 (en) |
| GB (1) | GB1371480A (en) |
| IL (1) | IL41998A (en) |
| IT (1) | IT983756B (en) |
| NL (1) | NL7304993A (en) |
| NO (1) | NO135446C (en) |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3977329A (en) * | 1974-10-25 | 1976-08-31 | Motorola, Inc. | Shock-acceleration activated function selector |
| US4451960A (en) * | 1979-03-15 | 1984-06-05 | Molitor Industries, Inc. | Method of producing multiple coil, multiple tube heat exchanger |
| DE3418759A1 (en) * | 1984-05-19 | 1985-11-21 | Diehl GmbH & Co, 8500 Nürnberg | IGNITION PROTECTION DEVICE |
| US4930419A (en) * | 1989-05-23 | 1990-06-05 | Serby Victor M | Ordnance fuze power source |
| EP0758737A1 (en) * | 1995-08-16 | 1997-02-19 | Schweizerische Eidgenossenschaft vertreten durch die Eidg. Munitionsfabrik Thun der Gruppe für Rüstungsdienste | Method and device for securing and arming a fuse and/or ammunition body to be fired mechanically |
| DE19926754C2 (en) * | 1999-06-11 | 2001-08-23 | Buck Neue Technologien Gmbh | Safety device for ammunition with an electrochemical cell as an energy source |
| DE102007060567B4 (en) * | 2007-12-15 | 2009-08-27 | Junghans Microtec Gmbh | Safety device for an igniter of a projectile |
| IL189692A (en) * | 2008-02-21 | 2014-07-31 | Rafael Advanced Defense Sys | Guided munition unit with in-flight switchable multiple fuze modes |
| US7819061B2 (en) * | 2008-09-08 | 2010-10-26 | Raytheon Company | Smart fuze guidance system with replaceable fuze module |
| CO2017008406A1 (en) | 2017-08-17 | 2017-09-20 | Tobon Trujillo Luis Eduardo | Electromechanical percussion fuze for multipurpose aerial ammunition |
| US10935357B2 (en) | 2018-04-25 | 2021-03-02 | Bae Systems Information And Electronic Systems Integration Inc. | Proximity fuse having an E-field sensor |
| RU2767809C1 (en) * | 2021-07-30 | 2022-03-22 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") | Safety and arming device of fuse |
| DE102021123375A1 (en) | 2021-09-09 | 2023-03-09 | Rwm Schweiz Ag | Ignition device for ammunition, in particular medium-caliber ammunition, and associated method for detonating or self-destructing ammunition, in particular medium-caliber ammunition |
| DE102022106883A1 (en) | 2022-03-23 | 2023-09-28 | Rheinmetall Air Defence Ag | Fuse unit for a detonator, use of the fuse unit and method for activating a detonator with this fuse unit |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2900911A (en) * | 1943-11-30 | 1959-08-25 | Louis D Statham | Fuze |
| US2870713A (en) * | 1955-06-09 | 1959-01-27 | Saloranta Arvo Ensio | Fuse for shells |
| US2951444A (en) * | 1958-09-12 | 1960-09-06 | Jr Clayton E Hunt | Fuze arming and safety mechanism |
| FR1274980A (en) * | 1960-08-08 | 1961-11-03 | Percussion fuze for rocket |
-
1972
- 1972-04-10 FR FR7212527A patent/FR2180159A5/fr not_active Expired
-
1973
- 1973-04-09 NO NO1444/73A patent/NO135446C/no unknown
- 1973-04-09 US US00349124A patent/US3839963A/en not_active Expired - Lifetime
- 1973-04-10 GB GB1722473A patent/GB1371480A/en not_active Expired
- 1973-04-10 IL IL41998A patent/IL41998A/en unknown
- 1973-04-10 NL NL7304993A patent/NL7304993A/xx unknown
- 1973-04-10 IT IT22823/73A patent/IT983756B/en active
- 1973-04-10 DE DE2318039A patent/DE2318039A1/en active Pending
- 1973-04-10 JP JP48040781A patent/JPS4948200A/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| NO135446B (en) | 1976-12-27 |
| IL41998A0 (en) | 1973-06-29 |
| JPS4948200A (en) | 1974-05-10 |
| FR2180159A5 (en) | 1973-11-23 |
| NO135446C (en) | 1977-04-05 |
| IT983756B (en) | 1974-11-11 |
| US3839963A (en) | 1974-10-08 |
| DE2318039A1 (en) | 1973-10-31 |
| GB1371480A (en) | 1974-10-23 |
| NL7304993A (en) | 1973-10-12 |
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