GB366704A - Improvements in or relating to the extinction and/or prevention of fires on aircraft - Google Patents
Improvements in or relating to the extinction and/or prevention of fires on aircraftInfo
- Publication number
- GB366704A GB366704A GB222531A GB222531A GB366704A GB 366704 A GB366704 A GB 366704A GB 222531 A GB222531 A GB 222531A GB 222531 A GB222531 A GB 222531A GB 366704 A GB366704 A GB 366704A
- Authority
- GB
- United Kingdom
- Prior art keywords
- container
- piercer
- cartridge
- casing
- cap
- 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
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C35/00—Permanently-installed equipment
- A62C35/58—Pipe-line systems
- A62C35/60—Pipe-line systems wet, i.e. containing extinguishing material even when not in use
- A62C35/605—Pipe-line systems wet, i.e. containing extinguishing material even when not in use operating and sounding alarm automatically
Landscapes
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Packages (AREA)
Abstract
366,704. Fire-extinguishing apparatus. BLAKEBOROUGH, R. A. and DENNE, R. A., Woodhouse Works, Brighouse, Yorkshire. Jan. 22, 1931, Nos. 2225 and 13457. [Class 47 (ii).] A fire-extinguisher comprises a collapsable container which, in use, is ruptured or pierced and is then collapsed by applied pressure to eject its contents. As shown, a casing a is subdivided by a perforated partition a<3>. A container e, of thin lead, for example, is placed in one end of the casing, and that end is closed by a cap a<2> provided with a sealing capsule f. The mouth of the container is reinforced by a ring e<1> and is soldered to the casing. The chamber b at the other end of the casing is charged with a fluid pressure medium through a valve c. The cap a<2> carries a tubular member g in which a spring-pressed hollow pierced h is restrained by a latch lever j. The latter is held in restraining position by a cartridge k adapted to be fired electrically. The piercer is connected to a pipe line by means, such as a coiled tube m, allowing movement of the piercer. In use, firing of the cartridge allows the piercer to rupture the capsule f. The pressure in chamber b then acts to collapse the container e. The cartridge may consist of a glass vessel or a two-part telescopic device housing an explosive charge. In a modification, the piercer is restrained by a catch on a spring adapted to be moved aside by explosion of the cartridge. In another modification, the member g is replaced by a cap provided with a nozzle and a hand-operated piercer. In another modification, the chamber b is connected to a suitable source of compressed fluid. In another modification, Fig. 4, the chamber b houses a combustible cartridge p adapted to be ignited electrically. The collapsable container e is closed at both ends, and the outer end is formed with a skirt and a flange c<3> nipped between the cap a<2> and a packing ring s. The cartridge is arranged first to burn quickly, to force the container e against a fixed piercer h<4>, and then to burn at a slow uniform rate, to generate pressure for collapsing the container. Where an extinguishing medium of a very volatile nature is employed, the container may be provided with a protective casing designed to resist deformation of the container by abnormal internal pressures, but to permit access to the container of the applied collapsing pressure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB222531A GB366704A (en) | 1931-01-22 | 1931-01-22 | Improvements in or relating to the extinction and/or prevention of fires on aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB222531A GB366704A (en) | 1931-01-22 | 1931-01-22 | Improvements in or relating to the extinction and/or prevention of fires on aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB366704A true GB366704A (en) | 1932-02-11 |
Family
ID=9735793
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB222531A Expired GB366704A (en) | 1931-01-22 | 1931-01-22 | Improvements in or relating to the extinction and/or prevention of fires on aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB366704A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2159707A (en) * | 1984-06-08 | 1985-12-11 | Abg Semca | Rapid discharge extinguisher |
-
1931
- 1931-01-22 GB GB222531A patent/GB366704A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2159707A (en) * | 1984-06-08 | 1985-12-11 | Abg Semca | Rapid discharge extinguisher |
US4637472A (en) * | 1984-06-08 | 1987-01-20 | Abg Semca | Rapid discharge extinguisher |
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