FR2343987A1 - Tubular primer for artillery ammunition propellant - has axial bore and side vents through combustible ensuring uniform ignition - Google Patents
Tubular primer for artillery ammunition propellant - has axial bore and side vents through combustible ensuring uniform ignitionInfo
- Publication number
- FR2343987A1 FR2343987A1 FR7606456A FR7606456A FR2343987A1 FR 2343987 A1 FR2343987 A1 FR 2343987A1 FR 7606456 A FR7606456 A FR 7606456A FR 7606456 A FR7606456 A FR 7606456A FR 2343987 A1 FR2343987 A1 FR 2343987A1
- Authority
- FR
- France
- Prior art keywords
- propellant
- charge
- combustible
- block
- primer
- 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
Links
- 239000003380 propellant Substances 0.000 title abstract 5
- 238000002485 combustion reaction Methods 0.000 abstract 3
- 230000037452 priming Effects 0.000 abstract 2
- 239000008187 granular material Substances 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 229920003002 synthetic resin Polymers 0.000 abstract 1
- 239000000057 synthetic resin Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/08—Primers; Detonators
- F42C19/0823—Primers or igniters for the initiation or the propellant charge in a cartridged ammunition
- F42C19/0826—Primers or igniters for the initiation or the propellant charge in a cartridged ammunition comprising an elongated perforated tube, i.e. flame tube, for the transmission of the initial energy to the propellant charge, e.g. used for artillery shells and kinetic energy penetrators
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
Abstract
A tubular primer esp. for artillery ammunition comprising a projectile and a charge of propellant, has a back block with a location for a detonator. A combustion bore from the location for the detonator leads to a tubular arrangement fixed to the other side of the back block, in which there is a combustible charge for the priming of the propellant. At least one longitudinal ignition channel passes through the priming charge, extending practically the whole length and parallel to the axis of the tube. The combustible charge includes >=1 cylindrical block inside the tube or there may be two blocks placed end to end and formed so that there is a gap between them through which combustion is transmitted radially outwards. The tubular body has an internal transverse profile surrounding each cylindrical block so as to create >=1 lengthways extending ignition channel, externally to the block. Each block is formed by two symmetrical components joined axially and the tubular body is similarly formed by two shells of moulded synthetic resin, joined axially. The primer may have the form of granules filled into the tubular body with the longitudinal ignition passaged formed by a tube of combustible material down the centre. Ensures a high ballistic yield from the propellant charge by a uniform combustion of the primer throughout its whole length, and a brief and uniform ignition of the propellant. Wear on the artillery piece is reduced and a flame at the mouth of the barrel is prevented, bringing advantages, esp. at night.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7606456A FR2343987A1 (en) | 1976-03-08 | 1976-03-08 | Tubular primer for artillery ammunition propellant - has axial bore and side vents through combustible ensuring uniform ignition |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7606456A FR2343987A1 (en) | 1976-03-08 | 1976-03-08 | Tubular primer for artillery ammunition propellant - has axial bore and side vents through combustible ensuring uniform ignition |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2343987A1 true FR2343987A1 (en) | 1977-10-07 |
FR2343987B1 FR2343987B1 (en) | 1980-05-23 |
Family
ID=9170060
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7606456A Granted FR2343987A1 (en) | 1976-03-08 | 1976-03-08 | Tubular primer for artillery ammunition propellant - has axial bore and side vents through combustible ensuring uniform ignition |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2343987A1 (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3217976A1 (en) * | 1982-05-13 | 1983-11-17 | Bundesamt für Wehrtechnik u. Beschaffung, 5400 Koblenz | Propellant-charge igniter for propellant charges of extremely high charging density |
US4492167A (en) * | 1982-07-14 | 1985-01-08 | Dynamit Nobel Aktiengesellschaft | Partially combustible propellant charge igniter |
US4495866A (en) * | 1981-12-28 | 1985-01-29 | Dynamit Nobel Aktiengesellschaft | Flash guide tube arrangement for propellant charge igniters |
EP0163886A2 (en) * | 1984-05-07 | 1985-12-11 | Dynamit Nobel Aktiengesellschaft | Primer for a propellant charge |
FR2593905A1 (en) * | 1986-02-03 | 1987-08-07 | France Etat Armement | Destructible igniter for propellant charges |
EP0314547A1 (en) * | 1987-10-29 | 1989-05-03 | GIAT Industries | Propulsive charge for munition comprising a finned projectile, and manufacturing method thereof |
EP0364833A1 (en) * | 1988-10-15 | 1990-04-25 | DIEHL GMBH & CO. | Projectile comprising an ejecting charge |
US5005486A (en) * | 1989-02-03 | 1991-04-09 | Trw Vehicle Safety Systems Inc. | Igniter for airbag propellant grains |
US5192829A (en) * | 1991-07-31 | 1993-03-09 | Giat Industries | Initiation device for the propulsive charge of ammunition, for example telescoped ammunition, and ammunition ignited by such an ignition device |
FR2725781A1 (en) * | 1994-10-18 | 1996-04-19 | Giat Ind Sa | Propulsive charge igniter esp. for projectile |
US5895881A (en) * | 1996-08-02 | 1999-04-20 | Rheinmetall Industrie Ag | Propellant charge igniter |
WO2001016553A1 (en) * | 1999-08-31 | 2001-03-08 | Alliant Techsystems Inc. | Bayonet primer |
WO2001071274A1 (en) | 2000-03-23 | 2001-09-27 | Giat Industries | Igniter tube for artillery ammunition |
US6708621B1 (en) * | 1999-10-13 | 2004-03-23 | Giat Industries | Igniting device for a propellant charge |
EP1577634A1 (en) * | 2004-03-17 | 2005-09-21 | Rheinmetall Waffe Munition GmbH | Igniter for propulsive charge |
-
1976
- 1976-03-08 FR FR7606456A patent/FR2343987A1/en active Granted
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4495866A (en) * | 1981-12-28 | 1985-01-29 | Dynamit Nobel Aktiengesellschaft | Flash guide tube arrangement for propellant charge igniters |
DE3217976A1 (en) * | 1982-05-13 | 1983-11-17 | Bundesamt für Wehrtechnik u. Beschaffung, 5400 Koblenz | Propellant-charge igniter for propellant charges of extremely high charging density |
US4492167A (en) * | 1982-07-14 | 1985-01-08 | Dynamit Nobel Aktiengesellschaft | Partially combustible propellant charge igniter |
EP0163886A2 (en) * | 1984-05-07 | 1985-12-11 | Dynamit Nobel Aktiengesellschaft | Primer for a propellant charge |
US4669383A (en) * | 1984-05-07 | 1987-06-02 | Dynamit Nobel Aktiengesellschaft | Propellant charge igniter |
EP0163886A3 (en) * | 1984-05-07 | 1989-12-06 | Dynamit Nobel Aktiengesellschaft | Primer for a propellant charge |
FR2593905A1 (en) * | 1986-02-03 | 1987-08-07 | France Etat Armement | Destructible igniter for propellant charges |
EP0314547A1 (en) * | 1987-10-29 | 1989-05-03 | GIAT Industries | Propulsive charge for munition comprising a finned projectile, and manufacturing method thereof |
FR2622687A1 (en) * | 1987-10-29 | 1989-05-05 | France Etat Armement | PROPULSIVE LOADING FOR AMMUNITION COMPRISING AN EMPENNE PROJECTILE AND ITS IMPLEMENTATION METHOD |
US5000095A (en) * | 1988-10-15 | 1991-03-19 | Diehl Gmbh & Co. | Projectile with an ejecting charge |
EP0364833A1 (en) * | 1988-10-15 | 1990-04-25 | DIEHL GMBH & CO. | Projectile comprising an ejecting charge |
US5005486A (en) * | 1989-02-03 | 1991-04-09 | Trw Vehicle Safety Systems Inc. | Igniter for airbag propellant grains |
US5192829A (en) * | 1991-07-31 | 1993-03-09 | Giat Industries | Initiation device for the propulsive charge of ammunition, for example telescoped ammunition, and ammunition ignited by such an ignition device |
FR2725781A1 (en) * | 1994-10-18 | 1996-04-19 | Giat Ind Sa | Propulsive charge igniter esp. for projectile |
US5895881A (en) * | 1996-08-02 | 1999-04-20 | Rheinmetall Industrie Ag | Propellant charge igniter |
EP1039260A3 (en) * | 1996-08-02 | 2000-11-15 | Rheinmetall W & M GmbH | Primer for propulsive charge |
WO2001016553A1 (en) * | 1999-08-31 | 2001-03-08 | Alliant Techsystems Inc. | Bayonet primer |
US6708621B1 (en) * | 1999-10-13 | 2004-03-23 | Giat Industries | Igniting device for a propellant charge |
WO2001071274A1 (en) | 2000-03-23 | 2001-09-27 | Giat Industries | Igniter tube for artillery ammunition |
FR2806789A1 (en) | 2000-03-23 | 2001-09-28 | Giat Ind Sa | IGNITION TUBE FOR ARTILLERY AMMUNITION |
US6543363B2 (en) * | 2000-03-23 | 2003-04-08 | Giat Industries | Primer tube for artillery ammunition |
EP1577634A1 (en) * | 2004-03-17 | 2005-09-21 | Rheinmetall Waffe Munition GmbH | Igniter for propulsive charge |
Also Published As
Publication number | Publication date |
---|---|
FR2343987B1 (en) | 1980-05-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TP | Transmission of property |