GB743366A - Improvements in or relating to igniter cartridges - Google Patents
Improvements in or relating to igniter cartridgesInfo
- Publication number
- GB743366A GB743366A GB21728/53A GB2172853A GB743366A GB 743366 A GB743366 A GB 743366A GB 21728/53 A GB21728/53 A GB 21728/53A GB 2172853 A GB2172853 A GB 2172853A GB 743366 A GB743366 A GB 743366A
- Authority
- GB
- United Kingdom
- Prior art keywords
- charge
- per cent
- base
- ignition
- weight
- 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
Links
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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or arrangements
-
- 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
Abstract
743,366. Cartridges for igniting fuels. OLIN MATHIESON CHEMICAL CORPORATION. Aug. 6, 1953 [Aug. 20, 1952], No. 21728/53. Class 9(1) An igniter cartridge 20 for igniting the fuel in the combustion chamber 42 of a jet engine has a casing 22 of paper, cardboard or metal, with a brass base 34 housing a primer 24 as in a shot-cartridge. At the forward end of the casing is an ignition charge 26 adapted to be ignited by flash from the primer 24 through a flash tube 30, which is surrounded by the main gas-producing charge 28. The main charge extends from base wads 35 to the ignition charge over which is a, closure wad 36 on to which the casing is crimped. The flash tube, which has a press-fit in the base 34, has an enlarged end to receive the primer 24. Fuel is injected into the combustion chamber 42 through a nozzle 44 where it mixes with compressed air entering through the inlet 46 to form a combustible mixture. On actuation, by remote control, of a trigger 52, a percussion pin 50 fires the cartridge 20 in a mounting 48-on the engine and a, stream of hot gases and molten metal is projected into the chamber 42 to ignite the fuel-air mixture. The main charge 28 may be made up of a slow-burning base charge 56 and a faster burning intermediate charge 58 which is a blend of the base charge and the ignition charge compositions. The base charge may be about 25 per cent by weight of powdered magnesium, 60 per cent by weight of a pulverulent oxidizing agent such as alkaline earth peroxide or nitrate with small quantities of fuels such as oxalates and binders such as metal soaps, e.g., calcium resinate. The ignition mixture may consist of 15 per cent by weight of powdered magnesium and about 85 per cent by weight of an alkaline earth peroxide with small amounts of insoluble metal soap. The intermediate charge is preferably a blend of 80 per cent of the base charge composition and 20 per cent of the ignition mixture, while the ignition charge is 80 per cent by weight of the igniter mixture and 20 per cent of the base charge. The flash tube 30 is made of a combustible metal such as aluminium, magnesium, zinc or alloys thereof. Before firing, the forward end of the tube is closed by pressing equal portions 64 of the wall inwardly to form radial fins 66, Fig. 9. On firing, flash from the primer forces the fins apart. These fins may be sealed by dipping in lacquer.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US743366XA | 1952-08-20 | 1952-08-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB743366A true GB743366A (en) | 1956-01-11 |
Family
ID=22119012
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB21728/53A Expired GB743366A (en) | 1952-08-20 | 1953-08-06 | Improvements in or relating to igniter cartridges |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB743366A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5000479A (en) * | 1988-09-21 | 1991-03-19 | Bayern-Chemie Gesellschaft Fuer Flugchemische Antriebe Mbh | Housing for a gas generator |
-
1953
- 1953-08-06 GB GB21728/53A patent/GB743366A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5000479A (en) * | 1988-09-21 | 1991-03-19 | Bayern-Chemie Gesellschaft Fuer Flugchemische Antriebe Mbh | Housing for a gas generator |
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