US2653541A - Container for inflammable liquids - Google Patents
Container for inflammable liquids Download PDFInfo
- Publication number
- US2653541A US2653541A US120027A US12002749A US2653541A US 2653541 A US2653541 A US 2653541A US 120027 A US120027 A US 120027A US 12002749 A US12002749 A US 12002749A US 2653541 A US2653541 A US 2653541A
- Authority
- US
- United States
- Prior art keywords
- bomb
- sections
- container
- tie rod
- section
- 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
- 239000007788 liquid Substances 0.000 title description 5
- 238000010276 construction Methods 0.000 description 5
- 230000003014 reinforcing effect Effects 0.000 description 4
- 238000007789 sealing Methods 0.000 description 4
- 150000001875 compounds Chemical class 0.000 description 3
- 239000012530 fluid Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000013011 mating Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229920003023 plastic Polymers 0.000 description 2
- 102000012152 Securin Human genes 0.000 description 1
- 108010061477 Securin Proteins 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
- 238000003466 welding 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
- F42B12/44—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 of incendiary type
Definitions
- This invention relates to fire bombs and more particularly to the features of construction of such bombs for use on high performance fighter airplanes.
- a conventional fire bomb with its conventional features of construction would be totally unsatisfactory with respect to weight if it were designed to be externally mounted and used in the manner described above. It may be further pointed out that excessive wei ht is not the only disadvantage of this type of construction.
- the spasmodic and erratic detonation of the conventional bomb is in a large part due to its design features concerning ignitor location and operation.
- storage and shipping of this type fire bomb is made difficult because the shape of its component parts prevents compact packaging. It is a laborious job to assemble a fire bomb featuring the conventional design, thus requiring too much time, and even then the parts are very apt to be bent out of hape or otherwise made useless by distortion of the tapped holes, etc.
- Another object of this invention is to facilitate storage and crating by designing the component parts so that they may be telescoped into a compact package.
- Another object of this invention is to provide a bomb capable of withstanding high speed flight when exteriorly mounted.
- Another object of this invention is to provide a fire bomb which may be readily formed without requiring special fabricating machinery.
- a further object of this invention is to provide a bomb which may be used with existing installations and conform in other respects to conventional bombing equipment, and techniques.
- Figure 1 is a View of the assembled bomb.
- Figure 2 is an exploded view of the bomb.
- Figure 3 is a fragmentary sectional View of the end assembly through the tip portion of the bomb.
- Figure 4 is a fragmentary sectional View showing the arrangement for making a fluid-tight joint between sections.
- Figure 5 shows two complete bombs, unassembled and crated.
- the fire bomb pictured in Figure 1 can best be described by referring to Figures 2, 3 and l.
- the cylindrical center section l and the two conical end sections designated as nose section 2 and tail section 3, are secured together by a tie rod l.
- Removable reinforcing panels 5 are secured to center section I.
- Supporting lugs 5 are mounted on center section I.
- Filler caps 7 cover openings in nose section 2 and tail section 3.
- an ignitor 8 shown in Figure 1 is secured to the bomb by tie rod 4, through ignitor base Hi.
- Transparent plastic fairing caps 9 are attached to ignitor base it) covering ignitors 8.
- Conical end section 2 or 3 is built up from two identically formed sheets making up the top and bottom halves; their shapes being developed from 50% of the leading edge of the symmetrical airfoil, N. A. C. A. 663-.020.
- a pressed bulkhead i3 is seam-welded to the two sheets at the small end of the cone section.
- a large ring is which holds annular ring gasket 52 also is seam-welded to the opposite or base end of the two sheets.
- Ring I6 is formed with a bevel facing generally inwardly of the section for seating gasket 42. The lapped edges of the upper and lower sheets are seam-welded.
- Center section I is a cylinder consisting of one rolled sheet with a lapped edge.
- Identical rings I! are resistance seam-welded to the ends of the cylindrically formed sheet with an extension provided thereon to allow reinforcing panels 5 to be mounted.
- Rings ii are provided with an L-shaped seat facing generally outwardly of said section for seating gasket l2.
- the lapped edges of the sheet are seam-we1ded and a sway brace reinforcing sheet 18 is added to the inside surface of the cylinder by spot Welding. Supporting lugs 6 are then seamed to the reinforced surface providing means by which the bomb is mounted.
- Tie rod 4 extends beyond nut i 5 to proyide a mount for ignitor B.
- the transparent plastic fair- 4 concave inwardly thereof, said sections being provided with annular seating rings circumferentially attached to the open ends thereof, and annular ring gaskets placed therebetween for providing a fluid-tight seal between said sections, a tie rod erg tending axially through said sections and said.
- annular sealing ring gaskets and washers having compound bevels formed thereon fitting around said tie rod outwardly of said bulkheads, saidcompound bevels mating the surfaces of said bulkheads and said sealing ring gaskets, nuts threadedly engaging said tie rod for sectiring said sections and said seals in fluidtisht relationship, said container being provided with supporting. lugs attached thereon, openings fprmed in said container for filling, closure means for said openings when filled, and removable caps ing cap 9 shown in Figure 2 is fastened to the ignitor base H! to protect ignitor 8 from external forces.
- Permanently attached arming wire housings 23 are welded to the inside wall of end sections 2 and 3 extending therethrough to ring l6. Arming wires 24 and 25 extending through housings 23 provide a means for detaching cap 9 and for arming the bomb when the bomb is released. Cap 9 is held on one end by arming wire clip l9 and on the other end by a supporting stud with a spring release 28. When arming wire clip i9 is detached by pulling arming wire 24 therefrom, cap 9 is ejected by spring release 2
- the advantages of this fire bomb are eyidenced in the cylindrical and conical sections by virtue of their features of construction and assembly.
- the end sections are identical and are interchangeable.
- the cylindrical center section makes it possible to use a longer center section in the event more volume is desired.
- Filler caps in both end sections allow filling if'desired, or a choice of the more convenient position for single filling.
- the bomb may be suspended from either end forward using existing installations and conforming in other respects to conventional bombing equipment and techniques. Unass'eme bled, these bombs may be crated in pairs in a suitable crate 26, shown in dash lines in Figure.
- a fire bomb structure comprising a nose section, a center section and a tail section, said center section being substantially cylindrical, said nose and tail sections being substantially circular in cross-section with substantially conical exterior surfaces, bulkheads formed at the small ends of said end sections being concave inwardly thereof, annular rings forming the open ends of said sections, said annular rings on said end sections having beveled surfaces facing generally inwardly of said sections, and said annular rings on said center section having l .-shaped seats facing generally outwardly of said sections, annular ring gaskets interposed between said annular rings being held tightly therebetween, a tie rod extending axially through said sections and said bulkheads, annular sealing ring baskets and washers having compound bevels formed thereon fitting around said tie rod outwardly of said bulkheads, said compound bevels mating the surfaces of said bulkheads and said sealing ring gaskets, nuts threadedly engaging said tie rod for securing said sections and said seals in fluid.- tight relationship, reinforcing panels fastened
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
- Sept. 29, 1953 A. E. KANODE ETAL 5 35 CONTAINER FOR INFLAMMABLB LIQUIDS F iled Oct. 7, 1949 2 Sheets-Sheet 1 INVENTORS Sept. 29, 1953 KANODE r 2,653,541
CONTAINER FOR INFLAMMABLE LIQUIDS Filed Oct. 7, 1949 2 Sheets-Sheet 2 I N VEN TORS Patented Sept. 29, 1953 @NETE STATES PATENT GFFHE CONTAINER FOR INFLAMMABLE LIQUIDS ration of Maryland Application October 7, 1949, Serial N 0. 120,027
2 Claims.
This invention relates to fire bombs and more particularly to the features of construction of such bombs for use on high performance fighter airplanes.
The externally mounted containers for inflammable liquids that may be used as fire bombs on an aircraft of the type mentioned above, must have certain qualifications alien to the ordinary design. It is necessary to mount the bomb exteriorly, usually under the main wing structure, because of the limited space available in the fuselage; thus, the exposed bomb must be capable of withstanding the forces to which it is subjected by the conditions of high speed iiight. Monocoque construction of conventional fire bombs will not permit those desirable qualities, mentioned herebelow, to be incorporated into the design, whereas the fire bomb of this invention offers a novel solution to the problem, representing the ultimate in simplicity of design and strength.
A conventional fire bomb with its conventional features of construction would be totally unsatisfactory with respect to weight if it were designed to be externally mounted and used in the manner described above. it may be further pointed out that excessive wei ht is not the only disadvantage of this type of construction. The spasmodic and erratic detonation of the conventional bomb is in a large part due to its design features concerning ignitor location and operation. Also, storage and shipping of this type fire bomb is made difficult because the shape of its component parts prevents compact packaging. It is a laborious job to assemble a fire bomb featuring the conventional design, thus requiring too much time, and even then the parts are very apt to be bent out of hape or otherwise made useless by distortion of the tapped holes, etc.
It is an object of this invention to provide a lightweight, low cost, dependable fire bomb which may be assembled with a minimum of time and effort.
Another object of this invention is to facilitate storage and crating by designing the component parts so that they may be telescoped into a compact package.
Another object of this invention is to provide a bomb capable of withstanding high speed flight when exteriorly mounted.
Another object of this invention is to provide a fire bomb which may be readily formed without requiring special fabricating machinery.
A further object of this invention is to provide a bomb which may be used with existing installations and conform in other respects to conventional bombing equipment, and techniques.
Further and other objects will become apparent from the accompanying description and drawings which form a part of this disclosure and in which like numerals refer to like parts.
Figure 1 is a View of the assembled bomb.
Figure 2 is an exploded view of the bomb.
Figure 3 is a fragmentary sectional View of the end assembly through the tip portion of the bomb.
Figure 4 is a fragmentary sectional View showing the arrangement for making a fluid-tight joint between sections.
Figure 5 shows two complete bombs, unassembled and crated.
The fire bomb pictured in Figure 1 can best be described by referring to Figures 2, 3 and l. The cylindrical center section l and the two conical end sections designated as nose section 2 and tail section 3, are secured together by a tie rod l. Removable reinforcing panels 5 are secured to center section I. Supporting lugs 5 are mounted on center section I. Filler caps 7 cover openings in nose section 2 and tail section 3. At the outer end of the end sections 2 and 3, an ignitor 8, shown in Figure 1, is secured to the bomb by tie rod 4, through ignitor base Hi. Transparent plastic fairing caps 9 are attached to ignitor base it) covering ignitors 8.
Center section I is a cylinder consisting of one rolled sheet with a lapped edge. Identical rings I! are resistance seam-welded to the ends of the cylindrically formed sheet with an extension provided thereon to allow reinforcing panels 5 to be mounted. Rings ii are provided with an L-shaped seat facing generally outwardly of said section for seating gasket l2. The lapped edges of the sheet are seam-we1ded and a sway brace reinforcing sheet 18 is added to the inside surface of the cylinder by spot Welding. Supporting lugs 6 are then seamed to the reinforced surface providing means by which the bomb is mounted.
This bomb or container must be fluid tight and to accomplish this, resilient annular or O-ring gaskets II and I2 are employed as shown in Figures 2 and 3. After arranging sections l, 2, and 3 in an assembling position and seating annular ring gaskets I l and [2 between rings I! and I6, which are welded to said sections as described previously, and-between-bulkheads l3 and beveled lit/21811611514, the sections are ready ;to be drawn tightly together. Tie rod 4 extends through a beveled washer [4, through annular ring gasket ll, through an opening bulkhead l3 and continues on until it emerges at the opposite end of the bomb through an identical seal:- ing arrangement. An ordinarynut vI 5 then screws over the threaded ends of tie rod 4; securin sec,- tions I, 2, and 3 and effecting a seal at all joints. Tie rod 4 extends beyond nut i 5 to proyide a mount for ignitor B. The transparent plastic fair- 4 concave inwardly thereof, said sections being provided with annular seating rings circumferentially attached to the open ends thereof, and annular ring gaskets placed therebetween for providing a fluid-tight seal between said sections, a tie rod erg tending axially through said sections and said. bulk-heads, annular sealing ring gaskets and washers having compound bevels formed thereon fitting around said tie rod outwardly of said bulkheads, saidcompound bevels mating the surfaces of said bulkheads and said sealing ring gaskets, nuts threadedly engaging said tie rod for sectiring said sections and said seals in fluidtisht relationship, said container being provided with supporting. lugs attached thereon, openings fprmed in said container for filling, closure means for said openings when filled, and removable caps ing cap 9 shown in Figure 2 is fastened to the ignitor base H! to protect ignitor 8 from external forces. Permanently attached arming wire housings 23 are welded to the inside wall of end sections 2 and 3 extending therethrough to ring l6. Arming wires 24 and 25 extending through housings 23 provide a means for detaching cap 9 and for arming the bomb when the bomb is released. Cap 9 is held on one end by arming wire clip l9 and on the other end by a supporting stud with a spring release 28. When arming wire clip i9 is detached by pulling arming wire 24 therefrom, cap 9 is ejected by spring release 2| allowing air to contact the small blades 22 on ignitor 8. Simultaneously with the release of cap 9, arming wire is pulled loose from ignitor 8 permitting blades 22 to rotate.
The advantages of this fire bomb are eyidenced in the cylindrical and conical sections by virtue of their features of construction and assembly. The end sections are identical and are interchangeable. The cylindrical center section makes it possible to use a longer center section in the event more volume is desired. ,Filler caps in both end sections allow filling if'desired, or a choice of the more convenient position for single filling. There are no raw. edges of sheet metal to injure personnel or become bent out of shape before assembly. There are no- 'tapped holes to become clogged or burred to causeldelay and scrappage. The bomb may be suspended from either end forward using existing installations and conforming in other respects to conventional bombing equipment and techniques. Unass'eme bled, these bombs may be crated in pairs in a suitable crate 26, shown in dash lines in Figure.
5, for storage or shipping in a minimum of space,
attached adjacent the end sections for reducing drag.
2.A fire bomb structure comprising a nose section, a center section and a tail section, said center section being substantially cylindrical, said nose and tail sections being substantially circular in cross-section with substantially conical exterior surfaces, bulkheads formed at the small ends of said end sections being concave inwardly thereof, annular rings forming the open ends of said sections, said annular rings on said end sections having beveled surfaces facing generally inwardly of said sections, and said annular rings on said center section having l .-shaped seats facing generally outwardly of said sections, annular ring gaskets interposed between said annular rings being held tightly therebetween, a tie rod extending axially through said sections and said bulkheads, annular sealing ring baskets and washers having compound bevels formed thereon fitting around said tie rod outwardly of said bulkheads, said compound bevels mating the surfaces of said bulkheads and said sealing ring gaskets, nuts threadedly engaging said tie rod for securing said sections and said seals in fluid.- tight relationship, reinforcing panels fastened to said annular rings within said center section, said container having supporting lugs attached thereon, openings formed in said container for charging, closure means for said openings when charged, means for detonating said charge attached to said tie rod adjacent the end thereof, a removable cap protecting said detonating means.
ALBERT E". KANODE. CARROLL I-I. MATSON.
References Cited in the file of this patent UNITED STATES PATENTS g ea Br ta n F b- 2i. 1.9 0
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US120027A US2653541A (en) | 1949-10-07 | 1949-10-07 | Container for inflammable liquids |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US120027A US2653541A (en) | 1949-10-07 | 1949-10-07 | Container for inflammable liquids |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2653541A true US2653541A (en) | 1953-09-29 |
Family
ID=22387853
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US120027A Expired - Lifetime US2653541A (en) | 1949-10-07 | 1949-10-07 | Container for inflammable liquids |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2653541A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2832503A (en) * | 1954-08-16 | 1958-04-29 | Royal Jet Inc | Method and apparatus for sealingly joining fuel tank sections, and fuel tanks formed thereby |
| US2895635A (en) * | 1954-09-23 | 1959-07-21 | Bristol Aircraft Ltd | Containers for attachment to the exterior of aircraft |
| US3005406A (en) * | 1955-05-16 | 1961-10-24 | Howard W Ronfeldt | Fire bomb |
| US3160373A (en) * | 1963-09-25 | 1964-12-08 | Republic Aviat Corp | External store for aircraft |
| US3437035A (en) * | 1965-10-05 | 1969-04-08 | Us Navy | Method and apparatus for disseminating fluid from vehicle in flight |
| US3469730A (en) * | 1966-11-18 | 1969-09-30 | Mc Donnell Douglas Corp | Nestable shaped cargo carrier construction |
| US3498218A (en) * | 1968-03-06 | 1970-03-03 | Us Navy | Bomblet |
| US4113130A (en) * | 1977-08-01 | 1978-09-12 | Mcdonnell Douglas Corporation | Joint for a nestable cargo carrier |
| US20200313209A1 (en) * | 2019-04-01 | 2020-10-01 | Bell Helicopter Textron Inc. | Structural gaseous material storage tank |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE85362C (en) * | ||||
| FR498458A (en) * | 1915-10-11 | 1920-01-13 | Demetrio Maggiora | Bomb |
| GB518259A (en) * | 1939-07-13 | 1940-02-21 | F E Proprietary Company Ltd | Improvements in or relating to fire extinguishing bombs or grenades |
| US2366374A (en) * | 1941-06-18 | 1945-01-02 | Budd Edward G Mfg Co | Bomb casing |
| US2385502A (en) * | 1941-06-11 | 1945-09-25 | Thomas M Finley | Incendiary bomb |
| US2401788A (en) * | 1942-08-13 | 1946-06-11 | Mccollum Thelma | Incendiary bomb |
-
1949
- 1949-10-07 US US120027A patent/US2653541A/en not_active Expired - Lifetime
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE85362C (en) * | ||||
| FR498458A (en) * | 1915-10-11 | 1920-01-13 | Demetrio Maggiora | Bomb |
| GB518259A (en) * | 1939-07-13 | 1940-02-21 | F E Proprietary Company Ltd | Improvements in or relating to fire extinguishing bombs or grenades |
| US2385502A (en) * | 1941-06-11 | 1945-09-25 | Thomas M Finley | Incendiary bomb |
| US2366374A (en) * | 1941-06-18 | 1945-01-02 | Budd Edward G Mfg Co | Bomb casing |
| US2401788A (en) * | 1942-08-13 | 1946-06-11 | Mccollum Thelma | Incendiary bomb |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2832503A (en) * | 1954-08-16 | 1958-04-29 | Royal Jet Inc | Method and apparatus for sealingly joining fuel tank sections, and fuel tanks formed thereby |
| US2895635A (en) * | 1954-09-23 | 1959-07-21 | Bristol Aircraft Ltd | Containers for attachment to the exterior of aircraft |
| US3005406A (en) * | 1955-05-16 | 1961-10-24 | Howard W Ronfeldt | Fire bomb |
| US3160373A (en) * | 1963-09-25 | 1964-12-08 | Republic Aviat Corp | External store for aircraft |
| US3437035A (en) * | 1965-10-05 | 1969-04-08 | Us Navy | Method and apparatus for disseminating fluid from vehicle in flight |
| US3469730A (en) * | 1966-11-18 | 1969-09-30 | Mc Donnell Douglas Corp | Nestable shaped cargo carrier construction |
| US3498218A (en) * | 1968-03-06 | 1970-03-03 | Us Navy | Bomblet |
| US4113130A (en) * | 1977-08-01 | 1978-09-12 | Mcdonnell Douglas Corporation | Joint for a nestable cargo carrier |
| US20200313209A1 (en) * | 2019-04-01 | 2020-10-01 | Bell Helicopter Textron Inc. | Structural gaseous material storage tank |
| US11742500B2 (en) * | 2019-04-01 | 2023-08-29 | Textron Innovations Inc. | Structural gaseous material storage tank |
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