US3667395A - Dummy shell - Google Patents
Dummy shell Download PDFInfo
- Publication number
- US3667395A US3667395A US827727A US3667395DA US3667395A US 3667395 A US3667395 A US 3667395A US 827727 A US827727 A US 827727A US 3667395D A US3667395D A US 3667395DA US 3667395 A US3667395 A US 3667395A
- Authority
- US
- United States
- Prior art keywords
- shell
- ignition
- impact
- decomposition
- jacket
- 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
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B8/00—Practice or training ammunition
- F42B8/12—Projectiles or missiles
- F42B8/14—Projectiles or missiles disintegrating in flight or upon impact
Definitions
- the present invention relates to a dummy shell having a screwed-in impact-ignition device and a decomposition device.
- Shells of this type are known in many structures. They consist substantially of an ignition housing and a shell head, respectively, which is screwed into the shell jacket, which ignition housing and shell head, respectively, receives again an impact-ignition device and decomposition device.
- the decomposition device serves, among others, the purpose of bringing about the shell to detonate nevertheless, in case of an inclined impact of the shell, that means, when the impact-ignition device does not become efiective, or if it fails for any other reasons. In such firings, it happens that the complete ignition device, namely the impact-ignition device and the decomposition device are thrown out of the shell jacket and the shell is not brought to detonation by the failing decomposition device.
- This set breaking point is prepared such, that the cross-section of the ignition housing and of the shell heads, respectively, as well as of the impact-ignition device is reduced by a recess of annular groove-like shape.
- FIG. 1 is a section through the shell head of a dummy shell
- An ignition comprising an impact ignition cross-section of the im act ignition device Q is brought about by the annular groove as well as of the ignition housing 2 by the annular groove 5.
- the end face limitation 7 of the shell jacket 1 is formed as a truncated cone. lf now the shell performs an impact in the manner shown in FIG. 2, the ignition housing 2 and the impact ignition device 3, respectively, break off at the set breaking points 10 and 11, whereby it is brought about, that the decomposition device 4 by a set breaking off of the impact-ignition device and of the ignition housing is not torn out of the shell sleeve 12, rather remains for the start of the detonation of the shell in the shell jacket 12.
- the truncated cone-like formed end face limit 7 of the shell jacket 1 rejects slide-like the soil 13 which is prevented from penetration between the shell jacket 1 and the decomposition device 4 and prying open of the shell jacket 1. Thereby the possibility is removed that the decomposition device 4 gets lost by the prying open the shell jacket 1 of the shell sleeve 12.
- annular groove turned in from the inside into the ignition housing, which retains a thin jacket wall as a set breaking point.
- This annular groove can be again advantageously conically formed.
- a dummy shell comprising,
- an ignition housing forming a shell tip secured to said shell jacket
- a one-piece ignition device contained in said ignition housing and comprising an impact-ignition means and a decomposition ignition means,
- said decomposition ignition means being screwed into said ignition housing
- said ignition housing being provided with a first annular recess formed set breaking point
- said ignition device being provided with a second annular recess formed set breaking point between said impact-ignition means and said decomposition ignition means, and
- said first and second annular recesses forming set breaking points being disposed adjacent one another at the same longitudinal distance of said shell, such that by an inclined striking of said dummy shell on a target, said igni tion housing with said impact-ignition means breaks off in said set breaking points and said decomposition ignition means remains in said shell jacket.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Working Measures On Existing Buildindgs (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
- Toys (AREA)
Abstract
A dummy shell with a screwed-in impact-ignition-anddecomposition device which comprises means for weakening the cross-section of the head of the shell at a set breaking point within the range of the connecting plane between the impactignition device and the decomposition device. By this arrangement it is brought about that upon inclined or flat impact of the shell, the impact-ignition-device separates itself from the decomposition device, and the latter remains in the jacket of the shell.
Description
D Umted States Patent [151 3,667,395
Romer et al. 51 June 6, 1972 54 DUMMY SHELL 2,447,033 8/1948 Shapiro ..l02/92.7 3,019,733 2/1962 Braid... ..102/92.7 Inventors Rudolf Romer; Heinz p, both of u 3,048,110 8/1962 West.... ..102 53 dorf, Germany 3,1 10,262 11/1963 West ..l02/54 [73] Assignee: Rheinmetall GmbH, Dusseldorf, Germany Prim), EXammer Roben R stab] [22] Filed; May 25 9 9 Attorney-Emest G. Montague [21] Appl. No.: 827,727 57 ABSTRACT A dummy shell with a screwed-in impact-ignition-and-decom- [30] Foreign Application Priority Data position device which comprises means for weakening the cross-section of the head of the shell at a set breaking point June 1, 1968 Germany ..P 17 03 518.6 within the range of the connecting plane'between the impacp ignition device and the decomposition device. By this arrange- [52] US. Cl ..102/92.7, 102/53 mem it i brought about that upon i li or fl t impact f [5]] Int. Cl ..F42b 5/22 the shell, the impact-ignition-device separates itself from the [58] Field of Search... l02/92.7, 56, 41, 52, 53, 54 decomposition device, and the latter remains in the jacket of the shell.
[56] References Cited 3 Claims 2 Drawing Figures UNITED STATES PATENTS 1,875,985 9/1932 Brandt ..102/92.7 X
IN VE N 70/? 62m Jay PATENTEDJUH 61972 The present invention relates to a dummy shell having a screwed-in impact-ignition device and a decomposition device.
Shells of this type are known in many structures. They consist substantially of an ignition housing and a shell head, respectively, which is screwed into the shell jacket, which ignition housing and shell head, respectively, receives again an impact-ignition device and decomposition device. The decomposition device serves, among others, the purpose of bringing about the shell to detonate nevertheless, in case of an inclined impact of the shell, that means, when the impact-ignition device does not become efiective, or if it fails for any other reasons. In such firings, it happens that the complete ignition device, namely the impact-ignition device and the decomposition device are thrown out of the shell jacket and the shell is not brought to detonation by the failing decomposition device. Aside from the fact that the shell does not fulfill its task to bring about detonation upon impact or after a predetermined time period, a serious danger is created by the shell jackets filled with explosives remaining unimpaired, since upon using of short practice places, a shell separated from the ignition device could fly beyond a maximum permitted path and thus could create appreciable damage.
It is one object of the present invention to provide a dummy shell in which upon flat or inclined impact a loosening of the decomposition device is prevented and thus a decomposition of the shell is assured in every case.
It is another object of the present invention to provide a dummy shell, wherein within the range of the connecting plane between the impact-ignition device and the decomposition device, the shell head cross-section is reduced to a set braking point such that upon inclined or flat impact of the shell the impact ignition device separates from the decomposition device at the set braking point and the decomposition device remains. This set breaking point is prepared such, that the cross-section of the ignition housing and of the shell heads, respectively, as well as of the impact-ignition device is reduced by a recess of annular groove-like shape.
It is a further advantageous development of the present in-.
vention to raise and to form as a truncated cone the end face limit of the shell jacket up to the range of the set breaking point such, that during sliding of the shell jacket separated from the impact-ignition device, over the ground, the shell jacket is effective to within the truncated cone-like end face limit disposed within the range of the breaking point, against prying open of the shell jacket and throwing out the decomposition device by rejection of the penetrating soil. Several other possibilities are also available for the production of the set breaking point. Without this conical end face limit the drawback would be present, that the straight end face created during breaking up upon sliding over the ground would create a shovel effect, which would make possible the penetration of the soil between the shell jacket and the decomposition device. A prying open of the shell jacket and throw out of the decomposition device would then occur.
With these and other objects in view which will become apparent in the following detailed description, the present invention, which is shown by example only, will be clearly understood in connection with the accompanying drawing, in which:
FIG. 1 is a section through the shell head of a dummy shell;
' and the threaded pin 9. An ignition comprising an impact ignition cross-section of the im act ignition device Q is brought about by the annular groove as well as of the ignition housing 2 by the annular groove 5. The end face limitation 7 of the shell jacket 1 is formed as a truncated cone. lf now the shell performs an impact in the manner shown in FIG. 2, the ignition housing 2 and the impact ignition device 3, respectively, break off at the set breaking points 10 and 11, whereby it is brought about, that the decomposition device 4 by a set breaking off of the impact-ignition device and of the ignition housing is not torn out of the shell sleeve 12, rather remains for the start of the detonation of the shell in the shell jacket 12. During further sliding of the shell' jacket 12 on the ground, the truncated cone-like formed end face limit 7 of the shell jacket 1 rejects slide-like the soil 13 which is prevented from penetration between the shell jacket 1 and the decomposition device 4 and prying open of the shell jacket 1. Thereby the possibility is removed that the decomposition device 4 gets lost by the prying open the shell jacket 1 of the shell sleeve 12.
Within the framework of the present invention for production of the set breaking point, several possibilities are available, as for instance, an annular groove turned in from the inside into the ignition housing, which retains a thin jacket wall as a set breaking point. This annular groove can be again advantageously conically formed.
While we have disclosed one embodiment of the present invention, it is to be understood that this embodiment is given by example only and not in a limiting sense.
We claim:
1. A dummy shell, comprising,
a shell jacket,
an ignition housing forming a shell tip secured to said shell jacket,
a one-piece ignition device contained in said ignition housing and comprising an impact-ignition means and a decomposition ignition means,
said decomposition ignition means being screwed into said ignition housing,
said ignition housing being provided with a first annular recess formed set breaking point,
said ignition device being provided with a second annular recess formed set breaking point between said impact-ignition means and said decomposition ignition means, and
said first and second annular recesses forming set breaking points being disposed adjacent one another at the same longitudinal distance of said shell, such that by an inclined striking of said dummy shell on a target, said igni tion housing with said impact-ignition means breaks off in said set breaking points and said decomposition ignition means remains in said shell jacket.
2. The dummy shell, as set forth in claim 1, wherein said shell jacket extends substantially to the level of said annular recess in said ignition housing, whereby the reduction of the cross-section obtained thereby, serves as said first set breaking point.
3. The dummy shell, as set forth in claim 3, wherein said shell jacket has an end fonnation disposed within the range of said first set breaking point and having the shape of a truncated cone, such that upon sliding of a said shell jacket after being separated from said impact ignition
Claims (3)
1. A dummy shell, comprising, a shell jacket, an ignition housing forming a shell tip secured to said shell jacket, a one-piece ignition device contained in said ignition housing and comprising an impact-ignition means and a decomposition ignition means, said decomposition ignition means being screwed into said ignition housing, said ignition housing being provided with a first annular recess formed set breaking point, said ignition device being provided with a second annular recess formed set breaking point between said impact-ignition means and said decomposition ignition means, and said first and second annular recesses forming set breaking points being disposed adjacent one another at the same longitudinal distance of said shell, such that by an inclined striking of said dummy shell on a target, said ignition housing with said impact-ignition means breaks off in said set breaking points and said decomposition ignition means remains in said shell jacket.
2. The dummy shell, as set forth in claim 1, wherein said shell jacket extends substantially to the level of said annular recess in said ignition housing, whereby the reduction of the cross-section obtained thereby, seRves as said first set breaking point.
3. The dummy shell, as set forth in claim 3, wherein said shell jacket has an end formation disposed within the range of said first set breaking point and having the shape of a truncated cone, such that upon sliding of a said shell jacket after being separated from said impact ignition means, over the ground, said end formation is effective against prying open of said shell jacket and spattering of said decomposition device by rejection of penetrating soil material.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19681703518 DE1703518C3 (en) | 1968-06-01 | Exercise floor |
Publications (1)
Publication Number | Publication Date |
---|---|
US3667395A true US3667395A (en) | 1972-06-06 |
Family
ID=5688455
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US827727A Expired - Lifetime US3667395A (en) | 1968-06-01 | 1969-05-26 | Dummy shell |
Country Status (7)
Country | Link |
---|---|
US (1) | US3667395A (en) |
BE (1) | BE731616A (en) |
CH (1) | CH478397A (en) |
FR (1) | FR2010014A1 (en) |
GB (1) | GB1253402A (en) |
NL (1) | NL157714B (en) |
SE (1) | SE356585B (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4362107A (en) * | 1978-10-14 | 1982-12-07 | Rheinmetall Gmbh | Practice projectile |
US20110000392A1 (en) * | 2007-05-08 | 2011-01-06 | Kapeles John A | Reloadable training ammunition |
US20220026186A1 (en) * | 2018-11-26 | 2022-01-27 | Rheinmetall Waffe Munition Gmbh | Test and/or practice ammunition |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3017380A1 (en) * | 1980-05-07 | 1981-11-12 | Rheinmetall GmbH, 4000 Düsseldorf | Shell or projectile with explosive head - which is connected to guide vanes by shaft with construction allowing breakage at specified point |
DE3031722A1 (en) * | 1980-08-23 | 1986-10-09 | Rheinmetall GmbH, 4000 Düsseldorf | BALANCE SHOOTING ARRANGEMENT WITH TOP-SIDED DRIVE CAGE |
FR2606868B1 (en) * | 1980-09-23 | 1989-06-23 | France Etat Armement | PERFORATING PROJECTILE WITH FRAGILIZED PERFORATING HEAD |
EP0597142B1 (en) * | 1992-11-10 | 1998-06-17 | Raufoss A/S | A practice projectile |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1875985A (en) * | 1930-05-16 | 1932-09-06 | Brandt Edgar William | Projectile |
US2447033A (en) * | 1945-04-27 | 1948-08-17 | Shapiro Michael | Dummy projectile |
US3019733A (en) * | 1957-05-21 | 1962-02-06 | Harvey Machine Co Inc | Projectile construction |
US3048110A (en) * | 1959-09-15 | 1962-08-07 | Stanley E West | Frangible nose cone |
US3110262A (en) * | 1962-02-02 | 1963-11-12 | Stanley E West | Shock mitigating nose |
-
1969
- 1969-03-13 CH CH380269A patent/CH478397A/en not_active IP Right Cessation
- 1969-03-20 NL NL6904302.A patent/NL157714B/en not_active IP Right Cessation
- 1969-04-16 BE BE731616D patent/BE731616A/xx unknown
- 1969-04-21 GB GB20230/69A patent/GB1253402A/en not_active Expired
- 1969-05-09 SE SE06575/69A patent/SE356585B/xx unknown
- 1969-05-26 US US827727A patent/US3667395A/en not_active Expired - Lifetime
- 1969-05-29 FR FR6917595A patent/FR2010014A1/fr not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1875985A (en) * | 1930-05-16 | 1932-09-06 | Brandt Edgar William | Projectile |
US2447033A (en) * | 1945-04-27 | 1948-08-17 | Shapiro Michael | Dummy projectile |
US3019733A (en) * | 1957-05-21 | 1962-02-06 | Harvey Machine Co Inc | Projectile construction |
US3048110A (en) * | 1959-09-15 | 1962-08-07 | Stanley E West | Frangible nose cone |
US3110262A (en) * | 1962-02-02 | 1963-11-12 | Stanley E West | Shock mitigating nose |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4362107A (en) * | 1978-10-14 | 1982-12-07 | Rheinmetall Gmbh | Practice projectile |
US20110000392A1 (en) * | 2007-05-08 | 2011-01-06 | Kapeles John A | Reloadable training ammunition |
US8312812B2 (en) * | 2007-05-08 | 2012-11-20 | Safariland, Llc | Reloadable training ammunition |
US20220026186A1 (en) * | 2018-11-26 | 2022-01-27 | Rheinmetall Waffe Munition Gmbh | Test and/or practice ammunition |
Also Published As
Publication number | Publication date |
---|---|
SE356585B (en) | 1973-05-28 |
DE1703518B2 (en) | 1976-02-26 |
DE1703518A1 (en) | 1971-12-30 |
BE731616A (en) | 1969-10-01 |
NL6904302A (en) | 1969-12-03 |
FR2010014A1 (en) | 1970-02-13 |
GB1253402A (en) | 1971-11-10 |
NL157714B (en) | 1978-08-15 |
CH478397A (en) | 1969-09-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5988071A (en) | Penetrator having multiple impact segments, including an explosive segment | |
US3667395A (en) | Dummy shell | |
US3731630A (en) | High-explosive armor-piercing shell | |
US3208385A (en) | Incendiary shell | |
NO145702B (en) | Projectile. | |
US2564870A (en) | Armor-piercing and incendiary shell | |
DK160021B (en) | Armor-Burning Grenade | |
DE19917144A1 (en) | Combination warhead for e.g. guided missile or sub-munition with penetrative and explosive effects satisfying logistic and economic requirements | |
KR101349932B1 (en) | Insensitive penetrator warhead with side-vent-hole | |
EP1001244B1 (en) | Artillery projectile | |
US4212245A (en) | Bottom fuse | |
DE3933442C2 (en) | ||
US4567830A (en) | Impact fuze | |
GB241941A (en) | Fuses for projectiles | |
FI92761B (en) | Armored explosive shell | |
DE2651692A1 (en) | BULB FLOOR | |
US2371510A (en) | Projectile | |
RU2346230C2 (en) | "tverich" fragmenting-bundle shell | |
US1042830A (en) | Pressure-fuse for projectiles, mines, torpedoes, &c. | |
US1490464A (en) | Armor-piercing projectile | |
US2453151A (en) | Projectile | |
US1250410A (en) | Shell-fuse. | |
DE360959C (en) | Impact fuse with plunger | |
US2425769A (en) | Self-destruction fuze | |
US2639669A (en) | Sheathed fuse |