US2323561A - Means for destroying aircraft - Google Patents
Means for destroying aircraft Download PDFInfo
- Publication number
- US2323561A US2323561A US376213A US37621341A US2323561A US 2323561 A US2323561 A US 2323561A US 376213 A US376213 A US 376213A US 37621341 A US37621341 A US 37621341A US 2323561 A US2323561 A US 2323561A
- Authority
- US
- United States
- Prior art keywords
- sections
- projectile
- container
- compartments
- destroying
- 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
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Classifications
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- 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
- F42B12/56—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 discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
- F41H11/04—Aerial barrages
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
Definitions
- Another object of my invention is to provide a device of the above described character equipped with means operable for maintaining a mine or mine field in the air over appreciable length of time as compared with mines equipped with parachutes and the like.
- a further object of my invention is to provide a device of the above described character so constructed and arranged wherein the mine or mines may be released or planted in the air at a predetermined height.
- An important object of my invention is to provide a device of the character described which is simple in construction, durable in use, efiicient in operation and economical in manufacture.
- Figure 1 is a side elevation of my invention.
- Figure 2 is a sectional view taken on the line 2-42 of Figure 1.
- Figure 3 is a side elevation of the projectile and illustrating the same in open position with a plurality of mines released therefrom.
- Figure 4 is a sectional view taken on the line t-il of Figure 1.
- Figure 5 is a vertical sectional view, partly in elevation of one of the mines.
- Figure 6 is a detail sectional view illustrating the arrangement of the valve stem and projectile wall whereby the inner compartment or tube of the mine is inflated previous to the projectile being fired into the air and the mine releasedtherefrom.
- My invention is directed to producing novel and efiective means for destroying hostile aircraft and constitutes means for an attack upon a plane, or fleet of planes, and also as a defensive means for discouraging or excluding hostile planes from flying over a city, fort, ship, fleet or other area or locality to be protected.
- I provide a shell 5 having fitted in the open end thereof the lower or base end portion of a projectile 6, it being understood that the shell 5 is provided with a suitable ex-- plosive charge (not shown) whereby the projectile is fired into the air, a suitable gun or similar device being employed for receiving the shell and projectile and for detonating the aforementioned explosive charge.
- the projectile 6 comprises an elongated substantially cylindriform casing 1 formed with a pair of lengthwise disposed separable sections 8 and with said sect-ions being hinged together at their lower ends as at 9.
- Each section is fashioned with upper, interjacent and lower partitions H), II and I2 respectively and with the partition i2 constituting the bottom wall of the projectile.
- Each section 8 is also fashioned with a longitudinal partition l3 extending between the partitions lll and I2 and coacting with the partitions II], II and l2'and the peripheral wall [4 of the projectile to define a quaternary of mine compartments or chambers I5 with the compartments of one section separated from the compartments of the other sections by a releasable partition l6 inserted therebetween.
- each section superjacent the partition I0, is fashioned with a substantially semicylindriform housing coacting. with the housing of the other section to form a substantially cylindriform bowl l'l having its upper and lower ends ldisposed an appreciable distance without and within the upper end of the projectile respectively.
- the upper end of the bowl is fashioned with a circumferential flange I8 and closed bymeans of a cap I9 having its margin formed with an arcuate lip 20 embracing and surrounding the flange l8" whereby the upper ends of the sections 8 are secured together in connected relation.
- for instance, gun powder or thelike, maintained in substantially compressed condition therein by means of a disk 22 overlying. said powder and subjacent the cap IS.
- the bottom wall of the bowl I! is provided with an opening 23 through which extends one end of a fuse 24, the latter being coiled or otherwise disposed within the top of the projectile between the bowl and the partitions 8.
- the opposite end of the fuse 24 extends through an opening 25 formed in the wall M of the projectile and terminates in proximity to the bowl l'l. Obviously, igniting of the outward disposed end of the fuse 24 will explode the powder 2
- effects rupture of the lip 20 and pivotable separation or opening of the sections .ments ii of their respective sections.
- the balloon comprises inner and outer tubes 3
- which is of relatively stiff material, is disposed substantially centrally within the outer tube 32 and is provided with a plurality of outlet flapper valves 33 and an intake valve stem 34 whereby a suitable fluid may be introduced therein for inflating the outer tube.
- the outer tube 32, adjacent the stem 34, is provided with an opening 35 for receiving the outer end of the stem 34 and with a flapper valve 36 for closing said opening 35 when the outer tube 32 is inflated and the stem withdrawn from said opening.
- the peripheral wall l4 of the projectile is provided with a plurality of openigns 31 through which the outer ends of the valve stems 34 extend.
- the balloons 30 are deflated and disposed within the respective compartments I5 when the sections 8 are secured together in closed relation.
- the valve stems extend through the openings 3'! and inflating fluid is introduced into the inner tube 3
- the projectile is fired in a desired direction in the air with the outer end of the fuse 24 ignited to effect explosion of the powder 2
- the balloons 30 will be released from the sections, it being understood that the release of the partition IE permits inflation of the outer tubes 32 to cause a subsequent floating of the balloons in the air.
- Each ballon may carry an explosive and a detonating means therefor set off by impact. This forms no part of the present invention.
- an elongated substantially cylindrical container having one end reduced and rounded and including companion sections extending longitudinally thereof, means hinging the sections together to permit the container to swing fully open from end to end thereof, walls integral with the sections and extending inwardly and outwardly of the container at the rounded end thereof and coacting to form an explosive chamber fully open at one end and out wardly of the container, a destructible cap clinched to the walls outwardly of the container for closing the chamber to retain an explosive therein and for securing the sections together against separation and hinging movement relative movement to each other in an end to end manner relative to the container, a fuse connected with the chamber and extending through a wall of one of the sections of the container, partitions in each section to form balloon compartments, and a solid panel loosely mounted in said container to separate the balloon compartments of one section from like compartments of the other section.
- an elongated substantially cylindrical container having one end reduced and rounded and including companion sections extending longitudinally thereof, means hinging the sections together to permit the container to swing fully open from end to end thereof, walls integral with the sections and extending inwardly and outwardly of the container at the rounded end thereof and coacting to form an explosive chamber fully open at one end and outwardly of the container, a destructible cap clinched to the Walls outwardly of the container for closing the chamber to retain an explosive therein and for securing the sections together against separation and hinging movement rela-' tive to each other in an end to end manner relative to the container, a fuse connected with the chamber and extending through a wall of one of the sections of the container, partitions in each section to form balloon compartments, a solid panel loosely mounted in said container to separate the balloon compartments of one section from like compartments of the other section, and a collapsible balloon arranged in each compartment and including a collapsible outer airtight shell and a rigid
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
July 6, 1943 P. F. NEWMAN MEANS FOR DESTROYING AIRCRAFT Filed Jan. 27, 1941 2 Sheets-Sheet l RENewmeam,
July 6, 1943. P. F. NEWMAN 2323 561 MEANS FOR DESTROYING AIRCRAF'I' Filed Jan. 27, 1941 2 Sheets-Sheet 2 July 6, 1943 STATES PATENT OFFICE My invention is directed to means for destroying aircraft and has as one of the principal objects thereof the provision of a device so constructed and arranged whereby a mine or mine field may be projected and suspended in the air for destroying hostile aircraft during warfare.
Another object of my invention is to provide a device of the above described character equipped with means operable for maintaining a mine or mine field in the air over appreciable length of time as compared with mines equipped with parachutes and the like.
A further object of my invention is to provide a device of the above described character so constructed and arranged wherein the mine or mines may be released or planted in the air at a predetermined height.
An important object of my invention is to provide a device of the character described which is simple in construction, durable in use, efiicient in operation and economical in manufacture.
Other objects and advantages will be apparent from the following description, appended claims and annexed drawings.
Referring to the drawings wherein like reference characters designate like parts throughout the several views:
Figure 1 is a side elevation of my invention.
Figure 2 is a sectional view taken on the line 2-42 of Figure 1.
Figure 3 is a side elevation of the projectile and illustrating the same in open position with a plurality of mines released therefrom.
Figure 4 is a sectional view taken on the line t-il of Figure 1.
Figure 5 is a vertical sectional view, partly in elevation of one of the mines.
Figure 6 is a detail sectional view illustrating the arrangement of the valve stem and projectile wall whereby the inner compartment or tube of the mine is inflated previous to the projectile being fired into the air and the mine releasedtherefrom.
My invention is directed to producing novel and efiective means for destroying hostile aircraft and constitutes means for an attack upon a plane, or fleet of planes, and also as a defensive means for discouraging or excluding hostile planes from flying over a city, fort, ship, fleet or other area or locality to be protected.
In practising my invention, as illustrated in the drawings, I provide a shell 5 having fitted in the open end thereof the lower or base end portion of a projectile 6, it being understood that the shell 5 is provided with a suitable ex-- plosive charge (not shown) whereby the projectile is fired into the air, a suitable gun or similar device being employed for receiving the shell and projectile and for detonating the aforementioned explosive charge.
The projectile 6 comprises an elongated substantially cylindriform casing 1 formed with a pair of lengthwise disposed separable sections 8 and with said sect-ions being hinged together at their lower ends as at 9. Each section is fashioned with upper, interjacent and lower partitions H), II and I2 respectively and with the partition i2 constituting the bottom wall of the projectile. Each section 8 is also fashioned with a longitudinal partition l3 extending between the partitions lll and I2 and coacting with the partitions II], II and l2'and the peripheral wall [4 of the projectile to define a quaternary of mine compartments or chambers I5 with the compartments of one section separated from the compartments of the other sections by a releasable partition l6 inserted therebetween.
The upper end of each section, superjacent the partition I0, is fashioned with a substantially semicylindriform housing coacting. with the housing of the other section to form a substantially cylindriform bowl l'l having its upper and lower ends ldisposed an appreciable distance without and within the upper end of the projectile respectively. The upper end of the bowl is fashioned with a circumferential flange I8 and closed bymeans of a cap I9 having its margin formed with an arcuate lip 20 embracing and surrounding the flange l8" whereby the upper ends of the sections 8 are secured together in connected relation. I I
Disposed within the bowl I! is an explosive 2|, for instance, gun powder or thelike, maintained in substantially compressed condition therein by means of a disk 22 overlying. said powder and subjacent the cap IS. The bottom wall of the bowl I! is provided with an opening 23 through which extends one end of a fuse 24, the latter being coiled or otherwise disposed within the top of the projectile between the bowl and the partitions 8. The opposite end of the fuse 24 extends through an opening 25 formed in the wall M of the projectile and terminates in proximity to the bowl l'l. Obviously, igniting of the outward disposed end of the fuse 24 will explode the powder 2| within the bowl I! when the fuse is consumed. The explosion of the powder 2| effects rupture of the lip 20 and pivotable separation or opening of the sections .ments ii of their respective sections.
8 with respect to each other as clearly illustrated in Figure 3 of the drawings. Opening of the sections I serve to release the partition Ii thereby opening the chambers or compart- From the foregoing, it will be apparent that by varying the length of the fuse 24, the exploding of the powder 2| may be obtained at a desired and predetermined time.
Disposed in each of the compartments I5 is a mine30, the latter constituting a balloon. The balloon comprises inner and outer tubes 3| and 32 respectively and which are constructed of rubber or other suitable material. The inner tube 3|, which is of relatively stiff material, is disposed substantially centrally within the outer tube 32 and is provided with a plurality of outlet flapper valves 33 and an intake valve stem 34 whereby a suitable fluid may be introduced therein for inflating the outer tube. The outer tube 32, adjacent the stem 34, is provided with an opening 35 for receiving the outer end of the stem 34 and with a flapper valve 36 for closing said opening 35 when the outer tube 32 is inflated and the stem withdrawn from said opening. The peripheral wall l4 of the projectile is provided with a plurality of openigns 31 through which the outer ends of the valve stems 34 extend.
The balloons 30 are deflated and disposed within the respective compartments I5 when the sections 8 are secured together in closed relation. When the balloons are thus positioned, the valve stems extend through the openings 3'! and inflating fluid is introduced into the inner tube 3| through said stem 31, it being understood that the fluid is contained within the inner tube 3| under pressure and that the outer tube 32 is enwrapped about said inner tube.
In operation, the projectile is fired in a desired direction in the air with the outer end of the fuse 24 ignited to effect explosion of the powder 2| at a predetermined height. When the sections 8 are exploded to open position by the powder 2|, as heretofore described, the balloons 30 will be released from the sections, it being understood that the release of the partition IE permits inflation of the outer tubes 32 to cause a subsequent floating of the balloons in the air. Each ballon may carry an explosive and a detonating means therefor set off by impact. This forms no part of the present invention.
From the foregoing, it will be apparent that I have provided novel means for destroying aircraft and that said means is so constructed and arranged whereby the same is maintained in the air over a materially greater period of time as compared to parachutes suspended mines or the like.
Without further elaboration the foregoing will so fully explain the invention that others may, by applying current knowledge, readily adapt the same for use under various conditions of service. Moreover, it is not indispensable that all the features of the invention be used conjointly since they may be employed advantageously in various combinations and sub-combinations.
It is obvious that the invention is not confined to the herein described use therefor as it may be utilized for any purpose to which it is adaptable. It is therefore to be understood that the invention is not limited to the specific construction as illustrated and described as the same is only illustrative of the principles of operation, which are capable of extended application in various forms, and that the invention comprehends all construction within the scope of the appended claims.
What I claim is:
1. In a projectile, an elongated substantially cylindrical container having one end reduced and rounded and including companion sections extending longitudinally thereof, means hinging the sections together to permit the container to swing fully open from end to end thereof, walls integral with the sections and extending inwardly and outwardly of the container at the rounded end thereof and coacting to form an explosive chamber fully open at one end and out wardly of the container, a destructible cap clinched to the walls outwardly of the container for closing the chamber to retain an explosive therein and for securing the sections together against separation and hinging movement relative movement to each other in an end to end manner relative to the container, a fuse connected with the chamber and extending through a wall of one of the sections of the container, partitions in each section to form balloon compartments, and a solid panel loosely mounted in said container to separate the balloon compartments of one section from like compartments of the other section.
2. In a projectile, an elongated substantially cylindrical container having one end reduced and rounded and including companion sections extending longitudinally thereof, means hinging the sections together to permit the container to swing fully open from end to end thereof, walls integral with the sections and extending inwardly and outwardly of the container at the rounded end thereof and coacting to form an explosive chamber fully open at one end and outwardly of the container, a destructible cap clinched to the Walls outwardly of the container for closing the chamber to retain an explosive therein and for securing the sections together against separation and hinging movement rela-' tive to each other in an end to end manner relative to the container, a fuse connected with the chamber and extending through a wall of one of the sections of the container, partitions in each section to form balloon compartments, a solid panel loosely mounted in said container to separate the balloon compartments of one section from like compartments of the other section, and a collapsible balloon arranged in each compartment and including a collapsible outer airtight shell and a rigid tube arranged in the outer shell and in communication therewith, and means to permit the introduction of fluid pressure in said tubes while the balloons are collapsed within the compartments for inflating the outer shells of the balloons on the release of the latter from the compartments.
PHIL F. NEWMAN.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US376213A US2323561A (en) | 1941-01-27 | 1941-01-27 | Means for destroying aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US376213A US2323561A (en) | 1941-01-27 | 1941-01-27 | Means for destroying aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
US2323561A true US2323561A (en) | 1943-07-06 |
Family
ID=23484121
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US376213A Expired - Lifetime US2323561A (en) | 1941-01-27 | 1941-01-27 | Means for destroying aircraft |
Country Status (1)
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US (1) | US2323561A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2447941A (en) * | 1943-05-31 | 1948-08-24 | Imber Jack | Aerial bomb, pyrotechnic device, and the like |
US2809583A (en) * | 1952-12-04 | 1957-10-15 | Roman L Ortynsky | Cluster bomb |
US4112848A (en) * | 1969-11-06 | 1978-09-12 | Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung | Warhead construction |
FR2547912A1 (en) * | 1983-06-27 | 1984-12-28 | Lacroix E Tous Artifices | MULTI-LOADED MUNITION, IN PARTICULAR DISPERSABLE MIXED ANTICHAR AND ANTIPERSONNEL MINE |
-
1941
- 1941-01-27 US US376213A patent/US2323561A/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2447941A (en) * | 1943-05-31 | 1948-08-24 | Imber Jack | Aerial bomb, pyrotechnic device, and the like |
US2809583A (en) * | 1952-12-04 | 1957-10-15 | Roman L Ortynsky | Cluster bomb |
US4112848A (en) * | 1969-11-06 | 1978-09-12 | Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung | Warhead construction |
FR2547912A1 (en) * | 1983-06-27 | 1984-12-28 | Lacroix E Tous Artifices | MULTI-LOADED MUNITION, IN PARTICULAR DISPERSABLE MIXED ANTICHAR AND ANTIPERSONNEL MINE |
EP0130125A1 (en) * | 1983-06-27 | 1985-01-02 | Etienne Lacroix - Tous Artifices Sa | Deployable mine having subcharges, in particular a combined anti-tank and anti-personnel mine |
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