US2372264A - Bomb - Google Patents
Bomb Download PDFInfo
- Publication number
- US2372264A US2372264A US429541A US42954142A US2372264A US 2372264 A US2372264 A US 2372264A US 429541 A US429541 A US 429541A US 42954142 A US42954142 A US 42954142A US 2372264 A US2372264 A US 2372264A
- Authority
- US
- United States
- Prior art keywords
- bomb
- jacket
- partition
- chamber
- plugs
- 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 - Lifetime
Links
- 238000005192 partition Methods 0.000 description 10
- 239000007788 liquid Substances 0.000 description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 239000002360 explosive Substances 0.000 description 3
- 239000011521 glass Substances 0.000 description 2
- 108010010803 Gelatin Proteins 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 229920000159 gelatin Polymers 0.000 description 1
- 239000008273 gelatin Substances 0.000 description 1
- 235000019322 gelatine Nutrition 0.000 description 1
- 235000011852 gelatine desserts Nutrition 0.000 description 1
- 210000004907 gland Anatomy 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/46—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
- F42B12/50—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances by dispersion
- F42B12/52—Fuel-air explosive devices
Definitions
- the principal object of the present invention is to provide a bomb which employs gasoline or some other highly volatile fluid which when it reaches its objective releases a heavy cloud of gas which is then ignited, the bomb serving to be destructive both from an explosive standpoint and that of incendiarism.
- Figure 1 represents a side elevational view of the bomb.
- Figure 2 is a top plan view.
- Figure 3 is a bottom lan view.
- Figure 4 is a longitudinal section.
- Figure 5 is an enlarged cross-sectional view taken substantially on the line 5-5 of Figure 4.
- Figure 6 is an enlarged sectional viewtaken substantially on the line 6-6 of Figure 4.
- the bomb is made up of a jacket 5 having a closed upper end 6 and a conical-shaped lower end I. This end terminates in a rather snub thick end portion 8 having a threaded bore therethrough for high explosive l3.
- 2 has a packing gland l4 through which the rod is slidable.
- the lower end of the rod I has a pointed head l5 which will assist in piercing an objective or sticking in the ground to hold the bomb in upright position.
- acoiled compression spring l6 which serves to hold the upper end of the rod I normally from .the glass vial H which is held by suitable securing means l8 to the underside of a partition l9 situated a slight distance upwardly in the jacket 5 from the partition l2.
- This glass or fragile vial or container I! contains a load of carbide 20, the container being liquidproof depending into a volume 2
- the partition I9 has openings therein normally closed by plugs 22 which will yield only at a certain pressure, such as will be built up by contact of the carbide with the water 2
- Adjacent the top 6 is another partition 23 downwardly through which depends a stack 24,
- spouts 25 radiating therefrom and terminating at the side of the jacket 5 where openings 26 a e located. These openings are normally closed by small plugs 21 which are dislodged when a certain predetermined pressure is imposed thereon.
- the chamber 28 defined by the partitions l8 and 23 contains gasoline or some'other highly volatile liquid.
- the upper end of the jacket 5 is provided ,with fins 29.
- the gasoline under pressure dislodges the plugs 21 and the gasoline in both liquid and gaseous form will escape and leave a highly the upper end of which, that is, the portion beinflammable path which will be set off when the time fuse 9 goes off igniting the dynamite gelatin or other explosive l3.
- a bomb comprising a jacket having .a leading end, a plurality of transverse partitions in said jacket dividing the same into a front chamber and a rear chamber, one of the partitions separating said chambers, the front chamber being loaded with water, andthe rear chamber with volatile liquid, a rupturable container projecting from said one partition into said front chamber and being loaded with carbide for mixing with the water to form a gas for expelling the volatile liquid out of the rear chamber, a plunger in said leading end for rupturing said container under impact of the plunger against the target, plugs in said one partition displaceable by the pressure of gas formed in the front chamber to admit such gas to the rear chamber for expelling said volatile liquid, and a volatile liquid manifold leading from said rear chamber to the outside is claimed or the jacket and provided with pressure blowout plugs therein.
Description
S. W. FIRTH March 27, 1945.
BOMB
2 Sheets-Sheet 1 Filed Feb. 4, 1942 Inrentor 57'EPHEN w FIRTH,
March 27 1945. s. w. FIRTH BOIMYB Filed Feb.-4, 1942 2 Sheets-Sheet 2 Inventor g. L Q
that I AJInrneys Patented Mar. 27," 1945 Application February 4, 19-42, Serial No. 429,541 1 Claim. (Cl. 102-6) This invention relates to now and useful improvements in bombs'of the incendiary type.
The principal object of the present invention is to provide a bomb which employs gasoline or some other highly volatile fluid which when it reaches its objective releases a heavy cloud of gas which is then ignited, the bomb serving to be destructive both from an explosive standpoint and that of incendiarism.
Other objects and advantages of the invention will become apparent to the reader of the following description. 2
In the drawings:
Figure 1 represents a side elevational view of the bomb.
Figure 2 is a top plan view.
Figure 3 is a bottom lan view.
Figure 4 is a longitudinal section.
Figure 5 is an enlarged cross-sectional view taken substantially on the line 5-5 of Figure 4.
Figure 6 is an enlarged sectional viewtaken substantially on the line 6-6 of Figure 4.
Referring to the drawings wherein like numerals designate like parts, it can be seen that the bomb is made up of a jacket 5 having a closed upper end 6 and a conical-shaped lower end I. This end terminates in a rather snub thick end portion 8 having a threaded bore therethrough for high explosive l3. This partition |2 has a packing gland l4 through which the rod is slidable.
The lower end of the rod I has a pointed head l5 which will assist in piercing an objective or sticking in the ground to hold the bomb in upright position. Interposed between the head l5 and the time fuse unit 9 is acoiled compression spring l6, which serves to hold the upper end of the rod I normally from .the glass vial H which is held by suitable securing means l8 to the underside of a partition l9 situated a slight distance upwardly in the jacket 5 from the partition l2. This glass or fragile vial or container I! contains a load of carbide 20, the container being liquidproof depending into a volume 2| of water. The partition I9 has openings therein normally closed by plugs 22 which will yield only at a certain pressure, such as will be built up by contact of the carbide with the water 2|.
Adjacent the top 6 is another partition 23 downwardly through which depends a stack 24,
spouts 25 radiating therefrom and terminating at the side of the jacket 5 where openings 26 a e located. These openings are normally closed by small plugs 21 which are dislodged when a certain predetermined pressure is imposed thereon.
The chamber 28 defined by the partitions l8 and 23 contains gasoline or some'other highly volatile liquid.
The upper end of the jacket 5 is provided ,with fins 29.
t It' can now be seen that when the bomb is released from an aircraft, it drives down with its lower end pointing earthward and guided by the fins 29. The head l5 strikes first resulting in the fragile container riding against the upper end of the pin breaking and discharging its load of carbide into the water 2|. A pressure is thus developed in the chamber containing the water 2|, which results in the dislodging of the plugs 22. This pressure builds up against the gasoline in the chamber 28 resulting in the gasoline spraying from the bomb, for instance, as the bomb passes downwardly through several floors of a building. The gasoline under pressure dislodges the plugs 21 and the gasoline in both liquid and gaseous form will escape and leave a highly the upper end of which, that is, the portion beinflammable path which will be set off when the time fuse 9 goes off igniting the dynamite gelatin or other explosive l3.
While the foregoing specification sets forth the invention in specific terms, it is to be understood that numerous changes in the shape, size and materials may be resorted to without departing from the spirit and scope of the invention as claimed hereinafter. v
Having described the invention, what as new is:
A bomb comprising a jacket having .a leading end, a plurality of transverse partitions in said jacket dividing the same into a front chamber and a rear chamber, one of the partitions separating said chambers, the front chamber being loaded with water, andthe rear chamber with volatile liquid, a rupturable container projecting from said one partition into said front chamber and being loaded with carbide for mixing with the water to form a gas for expelling the volatile liquid out of the rear chamber, a plunger in said leading end for rupturing said container under impact of the plunger against the target, plugs in said one partition displaceable by the pressure of gas formed in the front chamber to admit such gas to the rear chamber for expelling said volatile liquid, and a volatile liquid manifold leading from said rear chamber to the outside is claimed or the jacket and provided with pressure blowout plugs therein.
STEPHEN W. FIRTH.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US429541A US2372264A (en) | 1942-02-04 | 1942-02-04 | Bomb |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US429541A US2372264A (en) | 1942-02-04 | 1942-02-04 | Bomb |
Publications (1)
Publication Number | Publication Date |
---|---|
US2372264A true US2372264A (en) | 1945-03-27 |
Family
ID=23703701
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US429541A Expired - Lifetime US2372264A (en) | 1942-02-04 | 1942-02-04 | Bomb |
Country Status (1)
Country | Link |
---|---|
US (1) | US2372264A (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2630066A (en) * | 1945-02-08 | 1953-03-03 | Speers G Ponder | Incendiary bomb |
US3472165A (en) * | 1963-03-28 | 1969-10-14 | Us Air Force | Warhead |
US3492944A (en) * | 1968-04-04 | 1970-02-03 | Us Army | Two compartment thermal generator sphere |
US3496867A (en) * | 1965-10-13 | 1970-02-24 | Gilmour C Macdonald | Thermal radiation weapon |
US3570401A (en) * | 1967-08-24 | 1971-03-16 | North American Rockwell | Explosive apparatus |
US3596603A (en) * | 1966-09-12 | 1971-08-03 | Us Navy | Method of dispersing bw/cw or other materials |
US3596602A (en) * | 1966-09-12 | 1971-08-03 | William A Gey | Distributed explosives agent dispersal system |
US3724319A (en) * | 1967-03-08 | 1973-04-03 | Us Navy | Fax minefield clearing device |
US3786756A (en) * | 1972-11-15 | 1974-01-22 | L Looger | Gaseous grenade |
US3955509A (en) * | 1969-03-21 | 1976-05-11 | The United States Of America As Represented By The United States Energy Research And Development Administration | Fuel-air munition and device |
US4132169A (en) * | 1970-11-06 | 1979-01-02 | Beech Aircraft Corporation | Fuel-air type bomb |
US4132170A (en) * | 1971-02-12 | 1979-01-02 | Beech Aircraft Corporation | Fuel-air type bomb |
US20160238360A1 (en) * | 2015-02-13 | 2016-08-18 | Dmd Systems Llc | Fuel/air concussion apparatus |
-
1942
- 1942-02-04 US US429541A patent/US2372264A/en not_active Expired - Lifetime
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2630066A (en) * | 1945-02-08 | 1953-03-03 | Speers G Ponder | Incendiary bomb |
US3472165A (en) * | 1963-03-28 | 1969-10-14 | Us Air Force | Warhead |
US3496867A (en) * | 1965-10-13 | 1970-02-24 | Gilmour C Macdonald | Thermal radiation weapon |
US3596603A (en) * | 1966-09-12 | 1971-08-03 | Us Navy | Method of dispersing bw/cw or other materials |
US3596602A (en) * | 1966-09-12 | 1971-08-03 | William A Gey | Distributed explosives agent dispersal system |
US3724319A (en) * | 1967-03-08 | 1973-04-03 | Us Navy | Fax minefield clearing device |
US3570401A (en) * | 1967-08-24 | 1971-03-16 | North American Rockwell | Explosive apparatus |
US3492944A (en) * | 1968-04-04 | 1970-02-03 | Us Army | Two compartment thermal generator sphere |
US3955509A (en) * | 1969-03-21 | 1976-05-11 | The United States Of America As Represented By The United States Energy Research And Development Administration | Fuel-air munition and device |
US4132169A (en) * | 1970-11-06 | 1979-01-02 | Beech Aircraft Corporation | Fuel-air type bomb |
US4132170A (en) * | 1971-02-12 | 1979-01-02 | Beech Aircraft Corporation | Fuel-air type bomb |
US3786756A (en) * | 1972-11-15 | 1974-01-22 | L Looger | Gaseous grenade |
US20160238360A1 (en) * | 2015-02-13 | 2016-08-18 | Dmd Systems Llc | Fuel/air concussion apparatus |
US9726466B2 (en) * | 2015-02-13 | 2017-08-08 | Dmd Systems, Llc | Fuel/air concussion apparatus |
US20170292819A1 (en) * | 2015-02-13 | 2017-10-12 | Dmd Systems, Llc | Fuel/air concussion apparatus and method |
US10139204B2 (en) * | 2015-02-13 | 2018-11-27 | Dmd Systems Llc | Fuel/air concussion apparatus and method |
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