US2373883A - Shell structure - Google Patents
Shell structure Download PDFInfo
- Publication number
- US2373883A US2373883A US463890A US46389042A US2373883A US 2373883 A US2373883 A US 2373883A US 463890 A US463890 A US 463890A US 46389042 A US46389042 A US 46389042A US 2373883 A US2373883 A US 2373883A
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- Prior art keywords
- shell
- charge
- detonating
- nose
- recess
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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
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/201—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
- F42B12/204—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking structures, e.g. specific buildings or fortifications, ships or vehicles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/02—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
- F42B33/0214—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges by casting
Definitions
- This invention relates to a shell structure and to a means of firing or detonating the same.
- the object of the present invention is generally to improve and simplify the construction and operation of explosive shells, bombs, and the like, and in particular to provide simple means of firing or detonating the same the instant a target fired upon is struck.
- Fig. l is a central, longitudinal section of the shell
- Fig. 2 is similar section showing the manner in which the shell is loaded.
- the purpose of this invention is to provide a means of detonating a shell or bomb which is so sensitive to impact that even the fabric, ply-wood or the thin sheet metal covering of an airplane wing or fuselage is more than sufiicient to insure instant detonation of the explosive charge of the shell.
- A indicates the body of the shell, 2 the rear end thereof, and 3 the pointed forward end or nose.
- a chamber at the inner end of which is placed a resilient cushioning pad 4 which is made of sponge rubber or the like, and placedwithin the chamber and extending through the open forward end of the shell (see Fig. 2) is a rubber bag 5 which is filled with T. N. 'I'.,'nitro-glyc erine jell, or any other suitable explosive substance.
- the outer open end of the bag has a bead l2 formed thereon. and the function thereof will hereinafter be described.
- a predetermined or measured amount of, for instance, nitro-glycerine jell is placed in the bag 5 either before or after it is placed in the chamber of the shell.
- the front end of the shell is opened at the time (see Fig. 2) and is then closed, as shown in Fig. 1, to confine the explosive and at the same time to divide the explosive into a main charge 1 and a primary or detonating charge 8, this division being accomplished by forming an annular raised surface within the chamber adjacent the front end at the point indicated at Ill, which at the same time forms a small outer chamber to receive the charge 8, this chamber being in turn closed by the outermost end of the shell or the lip indicated at H.
- the closing of the open end of the shell may be accomplished by forming dies, by spinning operation, or otherwise. After the front or open end of the shell is closed, the projecting end of the rubber bag is folded back over the point of the shell, as indicated at M, with the bead l2 rearmost.
- the shell is fired from the cannon in any suitable 'manner.
- the force or pressure of the air is great enough to exert a sufllcient pull on the rearwardly extending portion M and the bead 42 to pull the portion of the bag conof the nose where it is partially vaporized by the air to form a layer of gas which is so sensitive to impact that the moment a target is struck it is detonated, with the result that it opens the nose of the shell sufficiently to simultaneously detonate the main charge 1.
- the bead l2 is important as it ofiers more resistance to the air than the remaining portion. Thus by increasing or decreasing the thickness of the bead, practically any pull required may be obtained, and transfer of the nitro-glycerine from the charge 8 to the recess I5 during the flight of the shell is insured.
- Nitro-glycerine is sensitive to shock, and this is the reason why the pad 4 is employed; that is, it cushions the main charge 1 at the time the shell is discharged from the cannon.
- the cushioning effect must obviously be sufiicient to prevent detonation by shock.
- the charge I may also be replaced by T. N. T. or
- nitro-glycerine is essential as far as the charge 8 is concerned as it must be of a jell or liquid-like consistency in order to permit itto ooze out and collect in the recess l where it may be partially vaporized by the air to form a layer of gas which is highly sensitive to impact.
- a shell of the character described comprising, an elongated cylindrical body portion terminating in a pointed nose, said body having a chamber formed therein containing a main explosive charge and a detonating'charge, said detonating charge being placed in the nose forward of the main charge, and said detonating charge being composed of a semi-liquid substance, said nose having a recess formed on the exterior surface in front of the detonating charge, and means for transferring the liquid detonating substance during flight of the shell to the recess to vaporize and convert the liquid detonating substance into a gas which is readily detonated upon impact with the target.
- An explosive shell terminating in a pointed nose and having a recess formed in the exterior surface of the nose, a detonating charge positioned rearwardly of said recess and in communication therewith, said detonating charge being composed of a liquid-like substance, and means actuated by air drag during flight of the shell for transferring the liquid detonating substance into the recess to cause vaporization thereof with a formation of gas which is readily detonated upon impact with the target.
- An explosive shell terminating in a pointed nose and having a recess formed in the exterior surface of the nose, said shell having a chamber formed therein rearwardly of said recess, a rubber bag in said chamber and having its open end extending through the recess and folded back over the nose of the shell to form an air drag, a semi-liquid-like detonating substance filling the bag, means normally retaining said liquid substance against escape, but said means permitting transfer of the liquid substance from the chamber to the recess when the shell is in flight, and a bead on the folded back portion of the rubber bag whereby an air drag is produced to exert a sufiicient pull on the bag to contract it and force the liquid-like detonating substance into the recess to cause vaporization thereof with a formation of a gas which is readily detonated upon impact of the target.
- A-shell of the character described comprising, an elongated body portion tapered at the forward end to form a nose, said body having a chamber formed therein and opening through the nose, a rubber bag forming a lining for said chamber and having its open end extending beyond the nose and folded back over the nose to form an air drag, a main charge of explosive contained in the bag, a second charge consisting of a semi-liquid detonating substance also contained in the bag forward of the main charge, means normally separating the two charges, an annular compressible lip in the nose of the shell compressing the rubber forward of the detonating charge to normally retain it against escape, and a recess in the nose of the shell into which the detonating charge is transferred by air drag upon the folded back rubber when the shell is in flight.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Manufacturing & Machinery (AREA)
- Air Bags (AREA)
Description
- A ril 17, 1945. c. B. FERREL SHELL STRUCTURE Filed Oct. 30, 1942 IN VEN TOR. CLYDE B. FEP/PEL way? VFW A rro/P/m rs,
Patented Apr. 17, 1945 UNITED STATES PATENT OFFICE SHELL STRUCTURE Clyde B. Ferrel, San Francisco, Calif. Application October, 30, 1942, Serial No. 463,890
4 Claims.
This invention relates to a shell structure and to a means of firing or detonating the same.
The object of the present invention is generally to improve and simplify the construction and operation of explosive shells, bombs, and the like, and in particular to provide simple means of firing or detonating the same the instant a target fired upon is struck. 1
The shell structure is shown by way of illustration in the accompanying drawing, in which:
Fig. l is a central, longitudinal section of the shell, and
' Fig. 2 is similar section showing the manner in which the shell is loaded.
There are two general methods employed to control the time lag between the firing of a shell or bomb and the explosion thereof. One method requires the use of time fuses or clock-actuated timing devices or the like, while the other method employs a firing pin which is actuated by impact with the target. This latter type, while extensively used, depends upon a rather heavy impact in order to detonate the shell, and as such is not dependable when cannon are used on planes to shell enemy planes, as experience shows that the flimsy structure of the wings and fuselage of a plane does not give enough resistance or impact to detonate the explosive charge, with the result that the shell may pass through without exploding.
The purpose of this invention is to provide a means of detonating a shell or bomb which is so sensitive to impact that even the fabric, ply-wood or the thin sheet metal covering of an airplane wing or fuselage is more than sufiicient to insure instant detonation of the explosive charge of the shell.
The structure of the shell and the means whereby it is detonated will now be described.
In the drawing, A indicates the body of the shell, 2 the rear end thereof, and 3 the pointed forward end or nose. Formed within the shell is a chamber at the inner end of which is placed a resilient cushioning pad 4 which is made of sponge rubber or the like, and placedwithin the chamber and extending through the open forward end of the shell (see Fig. 2) is a rubber bag 5 which is filled with T. N. 'I'.,'nitro-glyc erine jell, or any other suitable explosive substance. The outer open end of the bag has a bead l2 formed thereon. and the function thereof will hereinafter be described.
A predetermined or measured amount of, for instance, nitro-glycerine jell is placed in the bag 5 either before or after it is placed in the chamber of the shell. The front end of the shell is opened at the time (see Fig. 2) and is then closed, as shown in Fig. 1, to confine the explosive and at the same time to divide the explosive into a main charge 1 and a primary or detonating charge 8, this division being accomplished by forming an annular raised surface within the chamber adjacent the front end at the point indicated at Ill, which at the same time forms a small outer chamber to receive the charge 8, this chamber being in turn closed by the outermost end of the shell or the lip indicated at H. The closing of the open end of the shell may be accomplished by forming dies, by spinning operation, or otherwise. After the front or open end of the shell is closed, the projecting end of the rubber bag is folded back over the point of the shell, as indicated at M, with the bead l2 rearmost.
In actual practice, the shell is fired from the cannon in any suitable 'manner. During its flight toward the target it travels at a comparatively high velocity. or at least at such a velocity that as it passes through the air the force or pressure of the air is great enough to exert a sufllcient pull on the rearwardly extending portion M and the bead 42 to pull the portion of the bag conof the nose where it is partially vaporized by the air to form a layer of gas which is so sensitive to impact that the moment a target is struck it is detonated, with the result that it opens the nose of the shell sufficiently to simultaneously detonate the main charge 1.
The bead l2 is important as it ofiers more resistance to the air than the remaining portion. Thus by increasing or decreasing the thickness of the bead, practically any pull required may be obtained, and transfer of the nitro-glycerine from the charge 8 to the recess I5 during the flight of the shell is insured.
Nitro-glycerine is sensitive to shock, and this is the reason why the pad 4 is employed; that is, it cushions the main charge 1 at the time the shell is discharged from the cannon. The cushioning effect must obviously be sufiicient to prevent detonation by shock.
It was previously stated that the front end of the shell was open during loading, as shown in Fig. 2, to permit insertion of the rubber bag and the filling thereof with a desired explosive, and that thereafter either by forming dies, by a spinning operation, or otherwise, the nose was forced inwardly or closed so as to assume the position shown in Fig. 1. In this operation the main charge of explosive, indicated at I, is sealed ofi at the point if! and the primary or detonating charge at the point lfla. This latter closure is such that the rubber is compressed sufficiently to seal and retain the charge 8, but when a pull is exerted on the rubber during flight, a sulficient quantity of the nitro-glycerine will ooze outwardly and collect in the recess I 5 to function as heretofore described. In other words, compression of the rubber when the lip II is forced inwardly is sufiicient to seal and retain the charge 8, but the pressure is insufiicient to prevent stretching r pulling outwardly of the rubber to decrease the area of the chamber 8 and thereby force the nitro-glycerine into the recess l5. Both the charges 1 and 8 may be nitro-glycerine, but
the charge I may also be replaced by T. N. T. or
any other detonating or burning explosive, though nitro-glycerine is essential as far as the charge 8 is concerned as it must be of a jell or liquid-like consistency in order to permit itto ooze out and collect in the recess l where it may be partially vaporized by the air to form a layer of gas which is highly sensitive to impact.
Having thus described and illustrated my invention, what I claim and desire to secure by Letters Patent is:
1. A shell of the character described comprising, an elongated cylindrical body portion terminating in a pointed nose, said body having a chamber formed therein containing a main explosive charge and a detonating'charge, said detonating charge being placed in the nose forward of the main charge, and said detonating charge being composed of a semi-liquid substance, said nose having a recess formed on the exterior surface in front of the detonating charge, and means for transferring the liquid detonating substance during flight of the shell to the recess to vaporize and convert the liquid detonating substance into a gas which is readily detonated upon impact with the target.
2. An explosive shell terminating in a pointed nose and having a recess formed in the exterior surface of the nose, a detonating charge positioned rearwardly of said recess and in communication therewith, said detonating charge being composed of a liquid-like substance, and means actuated by air drag during flight of the shell for transferring the liquid detonating substance into the recess to cause vaporization thereof with a formation of gas which is readily detonated upon impact with the target.
3, An explosive shell terminating in a pointed nose and having a recess formed in the exterior surface of the nose, said shell having a chamber formed therein rearwardly of said recess, a rubber bag in said chamber and having its open end extending through the recess and folded back over the nose of the shell to form an air drag, a semi-liquid-like detonating substance filling the bag, means normally retaining said liquid substance against escape, but said means permitting transfer of the liquid substance from the chamber to the recess when the shell is in flight, and a bead on the folded back portion of the rubber bag whereby an air drag is produced to exert a sufiicient pull on the bag to contract it and force the liquid-like detonating substance into the recess to cause vaporization thereof with a formation of a gas which is readily detonated upon impact of the target.
4. A-shell of the character described comprising, an elongated body portion tapered at the forward end to form a nose, said body having a chamber formed therein and opening through the nose, a rubber bag forming a lining for said chamber and having its open end extending beyond the nose and folded back over the nose to form an air drag, a main charge of explosive contained in the bag, a second charge consisting of a semi-liquid detonating substance also contained in the bag forward of the main charge, means normally separating the two charges, an annular compressible lip in the nose of the shell compressing the rubber forward of the detonating charge to normally retain it against escape, and a recess in the nose of the shell into which the detonating charge is transferred by air drag upon the folded back rubber when the shell is in flight.
CLYDE B. FERREL.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US463890A US2373883A (en) | 1942-10-30 | 1942-10-30 | Shell structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US463890A US2373883A (en) | 1942-10-30 | 1942-10-30 | Shell structure |
Publications (1)
Publication Number | Publication Date |
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US2373883A true US2373883A (en) | 1945-04-17 |
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US463890A Expired - Lifetime US2373883A (en) | 1942-10-30 | 1942-10-30 | Shell structure |
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Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2741178A (en) * | 1944-11-07 | 1956-04-10 | Francis R Russell | Tail ejection bomb loading |
US2903968A (en) * | 1954-07-13 | 1959-09-15 | Acf Ind Inc | Bomb casing for liquid and semi-liquid materials |
US3983820A (en) * | 1973-08-09 | 1976-10-05 | Thomson-Csf | Projectile having a lightened base |
US4147108A (en) * | 1955-03-17 | 1979-04-03 | Aai Corporation | Warhead |
US4152987A (en) * | 1977-02-18 | 1979-05-08 | The United States Of America As Represented By The Secretary Of The Navy | Impermeable polymer bomb liner for use with TNT containing explosives |
FR2494833A1 (en) * | 1980-11-25 | 1982-05-28 | Thomson Brandt | Friction welded seal caps for grenade casings - involving thin coatings pref. of polyvinylidene fluoride or chloride |
US4348958A (en) * | 1980-05-15 | 1982-09-14 | Systems, Science And Software | Projectile having impact responsive initiator means |
EP0123266A1 (en) * | 1983-04-23 | 1984-10-31 | Rheinmetall GmbH | Projectile with sabot |
US4876964A (en) * | 1986-05-29 | 1989-10-31 | Raufoss A/S | Projectile and method of making it |
EP1338860A2 (en) * | 2002-02-21 | 2003-08-27 | Rheinmetall W & M GmbH | Method for manufacturing a big calibre high explosive projectile and projectile manufactured by this method |
US20050183611A1 (en) * | 2002-03-11 | 2005-08-25 | Bae Systems Plc | Explosives liner |
WO2009103409A1 (en) | 2008-02-22 | 2009-08-27 | Rheinmetall Waffe Munition Gmbh | Explosive projectile and method for the production thereof |
WO2009103408A1 (en) | 2008-02-22 | 2009-08-27 | Rheinmetall Waffe Munition Gmbh | Explosive projectile |
US20100005996A1 (en) * | 2006-07-25 | 2010-01-14 | Rheinmetall Waffe Munition Gmbh | Liner |
US20120137918A1 (en) * | 2009-05-25 | 2012-06-07 | Rheinmetall Waffe Munition Gmbh | Method for producing a large-caliber explosive projectile, and an explosive projectile produced using this method |
US20120204751A1 (en) * | 2010-06-11 | 2012-08-16 | Severson Gregg J | Cartridge assembly having an integrated retention system |
-
1942
- 1942-10-30 US US463890A patent/US2373883A/en not_active Expired - Lifetime
Cited By (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2741178A (en) * | 1944-11-07 | 1956-04-10 | Francis R Russell | Tail ejection bomb loading |
US2903968A (en) * | 1954-07-13 | 1959-09-15 | Acf Ind Inc | Bomb casing for liquid and semi-liquid materials |
US4147108A (en) * | 1955-03-17 | 1979-04-03 | Aai Corporation | Warhead |
US3983820A (en) * | 1973-08-09 | 1976-10-05 | Thomson-Csf | Projectile having a lightened base |
US4152987A (en) * | 1977-02-18 | 1979-05-08 | The United States Of America As Represented By The Secretary Of The Navy | Impermeable polymer bomb liner for use with TNT containing explosives |
US4348958A (en) * | 1980-05-15 | 1982-09-14 | Systems, Science And Software | Projectile having impact responsive initiator means |
FR2494833A1 (en) * | 1980-11-25 | 1982-05-28 | Thomson Brandt | Friction welded seal caps for grenade casings - involving thin coatings pref. of polyvinylidene fluoride or chloride |
WO1984004380A1 (en) * | 1983-04-23 | 1984-11-08 | Rheinmetall Gmbh | Sabot projectile |
EP0123266A1 (en) * | 1983-04-23 | 1984-10-31 | Rheinmetall GmbH | Projectile with sabot |
US4876964A (en) * | 1986-05-29 | 1989-10-31 | Raufoss A/S | Projectile and method of making it |
US7114449B2 (en) | 2002-02-21 | 2006-10-03 | Rheinmetall W & M Gmbh | Method for producing a large-caliber, high-explosive projectile, and high-explosive projectile produced in accordance with the method |
EP1338860A2 (en) * | 2002-02-21 | 2003-08-27 | Rheinmetall W & M GmbH | Method for manufacturing a big calibre high explosive projectile and projectile manufactured by this method |
US20040031380A1 (en) * | 2002-02-21 | 2004-02-19 | Ernst-Wilhelm Altenau | Method for producing a large-caliber, high-explosive projectile, and high-explosive projectile produced in accordance with the method |
EP1338860A3 (en) * | 2002-02-21 | 2004-03-17 | Rheinmetall W & M GmbH | Method for manufacturing a big calibre high explosive projectile and projectile manufactured by this method |
US6860185B2 (en) * | 2002-02-21 | 2005-03-01 | Reinmetall W & M Gmbh | Method for producing a large-caliber, high-explosive projectile, and high-explosive projectile produced in accordance with the method |
US20060011053A1 (en) * | 2002-02-21 | 2006-01-19 | Rheinmetall W & M Gmbh | Method for producing a large-caliber, high-explosive projectile, and high-explosive projectile produced in accordance with the method |
US20050183611A1 (en) * | 2002-03-11 | 2005-08-25 | Bae Systems Plc | Explosives liner |
EP1485669B1 (en) * | 2002-03-11 | 2011-06-15 | BAE Systems PLC | Ordnance with explosives liner and method of manufacture of the ordnance |
AU2003215737B8 (en) * | 2002-03-11 | 2009-06-11 | Bae Systems Plc | Explosives liner |
US7370585B2 (en) | 2002-03-11 | 2008-05-13 | Bae Systems Plc | Explosives liner |
AU2009201798B2 (en) * | 2002-03-11 | 2011-10-27 | Bae Systems Plc | Method for filling an explosive ordnance |
US8408138B2 (en) * | 2006-07-25 | 2013-04-02 | Rheinmetall Waffe Munition Gmbh | Liner |
US20100005996A1 (en) * | 2006-07-25 | 2010-01-14 | Rheinmetall Waffe Munition Gmbh | Liner |
WO2009103408A1 (en) | 2008-02-22 | 2009-08-27 | Rheinmetall Waffe Munition Gmbh | Explosive projectile |
WO2009103409A1 (en) | 2008-02-22 | 2009-08-27 | Rheinmetall Waffe Munition Gmbh | Explosive projectile and method for the production thereof |
US20120137918A1 (en) * | 2009-05-25 | 2012-06-07 | Rheinmetall Waffe Munition Gmbh | Method for producing a large-caliber explosive projectile, and an explosive projectile produced using this method |
US8601950B2 (en) * | 2009-05-25 | 2013-12-10 | Rheinmetall Waffe Munition Gmbh | Method for producing a large-caliber explosive projectile, and an explosive projectile produced using this method |
US8739671B2 (en) | 2009-05-25 | 2014-06-03 | Rheinmetall Waffe Munition Gmbh | Method for producing a large-caliber explosive projectile |
US20120204751A1 (en) * | 2010-06-11 | 2012-08-16 | Severson Gregg J | Cartridge assembly having an integrated retention system |
US8627770B2 (en) * | 2010-06-11 | 2014-01-14 | Bae Systems Land & Armaments, L.P. | Cartridge assembly having an integrated retention system |
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