US1146484A - dunwoody - Google Patents
dunwoody Download PDFInfo
- Publication number
- US1146484A US1146484A US1146484DA US1146484A US 1146484 A US1146484 A US 1146484A US 1146484D A US1146484D A US 1146484DA US 1146484 A US1146484 A US 1146484A
- Authority
- US
- United States
- Prior art keywords
- cavity
- shell
- shoulder
- armor
- charge
- 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
- 230000000284 resting Effects 0.000 description 10
- 238000004880 explosion Methods 0.000 description 8
- 239000000203 mixture Substances 0.000 description 6
- 239000007787 solid Substances 0.000 description 6
- 229910000831 Steel Inorganic materials 0.000 description 4
- 238000007664 blowing Methods 0.000 description 4
- 239000002360 explosive Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 241001446467 Mama Species 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000000149 penetrating Effects 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
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
- F42B12/20—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
- F42B12/208—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 a plurality of charges within a single high explosive warhead
Definitions
- This invention relates toaln'ror piercing shells for ordnance and has for its'o'bject to provide a shell which will be comparatively inexpensive to produce and more effective in use than those heretofore proposed.
- Fig. 2 is a. View similar to Fig. 1 illustrating a slightly modified form of the invention.
- '1 indicates the body portion of any suitable shell, preferably provided with the chilled armor piercing point 2 and the soft steel cap 3.
- the cavity of the shell is made of two diameters as shown, substantial shoulder i between then'i.
- the larger or rear cavity 5 is filled with any suitable explos ve and the cavity 6 is preferably filled with a suitable high' explosive capable of being detonated after impact.
- Between the two cavities is the steel plug or block 7 firmly resting upon the shoulder 4 and provided with any suitable fuse 8', for exploding or detonating the compound in the cavity 6.
- a packing material 9 such as lead or other suitable material may be employed to insure that no gas leaks from the cavity 5 into the cavity ('3;
- a suitable basefuse 10 is employed to ignite the charge in the cavity 5 and it is preferred to 'use afuse 8' of the delay action type so that the explosion of the charge in the cavity (3 will come an instant later than the explosion of'the charge inf the cavity 5.
- the operation of the shell will be clear the said cavity (3 whereupon the plug 7 and filling the plug 7 may be screwed firmly into place and the cavity 5 loaded.
- the fuse-10 mavbe of such a character as to cause an explosion of the charge in cavity 5, which will have the effect of blowing off the rear of the shell and thereby adding an impulse to the penetration energy of the shell and causing the lat: ter to pierce more armor than-wouldotherwise be the case.
- An instant after impact the fuse 8" may be detonated or explode the charge (3 according to the character of the charge and the shell luwing had time to bury itself in the armor this second explosion will be largely utilized in further breaking up or shattering the armor.
- I may provide the cavity 5 with a weakened portion such as 12, but such weakened portion is not essential to the operation of the invention.
- Fig. 2- The modified form shown in Fig. 2- is substantially the same as that shown in Fig. 1 except that the wind shield 13 is omitted but the general contour of the forward portion let'of the shell cap 13. Also the soft metal cap 2 is given a more tapered Shape cap 3 in Fig. 1.
- the cavity 6 is readily is the same as that of the' resting on said shoulder and completely seption of a larger diameter and a forward 'portion of a'smaller diameter with an abrupt shoulder between said portions and a solid plug fitting gastight said larger portion,
- an armor piercing shell having an integral body portion provided with a rear and a forward cavity of dilferent diameters the combination of an abrupt shoulder integral with said body portion separating said cavities; a screw threaded member near the forward end of the rear cavity; and 2.
- a hardened armor piercing shell having an integral body portion provided with forward and rear cavities of difierent diameters, the combination of'an integral abrupt shoulder between said cavities; a hollow screw threaded member fitting the rear cavity and resting against said shoulder; a solid screw threadedplug fitting said hollow member and also resting against said shoulder; an explosive charge in each of said cavities; and means for igniting said charges, substantially as described.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Portable Nailing Machines And Staplers (AREA)
Description
atel-mainl 13, 1m.- l
H. H. C. DUNWOODY. ARMOR PIERCING SHELL. APPLICATION FILED MAR 22 1915 views, Figure snmon-r'mncmsisimtn To all-whom it mayconcern;
Be it known tl1al3.I HENRY-;H. ODD}?- u oonY,-;Bri'gadier. tirecl acitizen of the United at Washington, in the District oi Columb a, have invented certain new and: useful Improvements .in' Armor Piercing. Shells; and I lo hereb'ydeclare the following to be a full, clear, and exact description of the invention, such as will enable others skilled in the art to which it apperta'i-ns to make and use the same. p
.This invention relates toaln'ror piercing shells for ordnance and has for its'o'bject to provide a shell which will be comparatively inexpensive to produce and more effective in use than those heretofore proposed.
With these and other objects in view the invention consists in the novel details of con-' struction and combinations of parts, more fully hereinafter disclosed and particularly pointed out in the claims.
Referring to the accompanying drawings forming a part of this specification in which like numerals designate like parts in all the view of an armor piercingshell made in accordance with my invention;- and Fig. 2 is a. View similar to Fig. 1 illustrating a slightly modified form of the invention.
'1 indicates the body portion of any suitable shell, preferably provided with the chilled armor piercing point 2 and the soft steel cap 3. The cavity of the shell is made of two diameters as shown, substantial shoulder i between then'i. The larger or rear cavity 5 is filled with any suitable explos ve and the cavity 6 is preferably filled with a suitable high' explosive capable of being detonated after impact. Between the two cavities is the steel plug or block 7 firmly resting upon the shoulder 4 and provided with any suitable fuse 8', for exploding or detonating the compound in the cavity 6.
Since armor piercing shells of necessity.
must be put through a chilling or hardening process, more or less difficulty is experienced in getting a tight fit for the plug 7 in that if screw threads are formed on the interior of the cavity 5 before the hardening process they are apt to be distorted during the chilling operation and therefore. to not form as tight a joint as is desirable. in order to avoid the expense of. reshaping the. said screw threads after the hardening operation.
Sp'ccificaitmiibf Letter-s Iat'xit Application mamas,
I I l I I I mold' the-"cavities General, U. S. Army, 're-J States, residing 1 1s a diagrammatic sectional providing a forward or smaller as. w i.
im n when .nsos se y decreas s l e h' a aid i series-sine 1 ca e while the. shell is ube-. i ie into place, by means ofa llrydi aulie"jack; hen the said. tube 8 is may be readily screwed jammed tightly against the shoulderl. if desired a packing material 9 such as lead or other suitable material may be employed to insure that no gas leaks from the cavity 5 into the cavity ('3; A suitable basefuse 10 is employed to ignite the charge in the cavity 5 and it is preferred to 'use afuse 8' of the delay action type so that the explosion of the charge in the cavity (3 will come an instant later than the explosion of'the charge inf the cavity 5.
mice i ia iii-anagra 1.1
before, th liars-" ii -place the plug 7 into place .and
The operation of the shell will be clear the said cavity (3 whereupon the plug 7 and filling the plug 7 may be screwed firmly into place and the cavity 5 loaded. Upon impact the fuse-10 mavbe of such a character as to cause an explosion of the charge in cavity 5, which will have the effect of blowing off the rear of the shell and thereby adding an impulse to the penetration energy of the shell and causing the lat: ter to pierce more armor than-wouldotherwise be the case. An instant after impact the fuse 8" may be detonated or explode the charge (3 according to the character of the charge and the shell luwing had time to bury itself in the armor this second explosion will be largely utilized in further breaking up or shattering the armor. In order to facilitate the blowing off of the rear of the shell without destroying its penetrating qualities, I may provide the cavity 5 with a weakened portion such as 12, but such weakened portion is not essential to the operation of the invention.
The modified form shown in Fig. 2- is substantially the same as that shown in Fig. 1 except that the wind shield 13 is omitted but the general contour of the forward portion let'of the shell cap 13. Also the soft metal cap 2 is given a more tapered Shape cap 3 in Fig. 1.
15 in Fig. than is the The cavity 6 is readily is the same as that of the' resting on said shoulder and completely seption of a larger diameter and a forward 'portion of a'smaller diameter with an abrupt shoulder between said portions and a solid plug fitting gastight said larger portion,
aratinlg said POItlOIiSZ substantially as describe 3 a,
2. In an armor piercing shell having an integral body portion provided with a rear and a forward cavity of dilferent diameters the combination of an abrupt shoulder integral with said body portion separating said cavities; a screw threaded member near the forward end of the rear cavity; and 2.
solid closing plug engaging said screw threaded member and resting on said shoulder, substantially as described;
3. In a hardened armor piercing shell having an integral body portion provided with forward and rear cavities of difierent diameters, the combination of'an integral abrupt shoulder between said cavities; a hollow screw threaded member fitting the rear cavity and resting against said shoulder; a solid screw threadedplug fitting said hollow member and also resting against said shoulder; an explosive charge in each of said cavities; and means for igniting said charges, substantially as described.
In testimony whereof -I affix my signature.
HEJRY H. C. DUNWOODY.
Publications (1)
Publication Number | Publication Date |
---|---|
US1146484A true US1146484A (en) | 1915-07-13 |
Family
ID=3214569
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US1146484D Expired - Lifetime US1146484A (en) | dunwoody |
Country Status (1)
Country | Link |
---|---|
US (1) | US1146484A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2422559A (en) * | 1943-05-07 | 1947-06-17 | Harry J Nichols | Projectile |
US2422920A (en) * | 1942-08-18 | 1947-06-24 | Harry J Nichols | Armor-piercing drop bomb |
US2435095A (en) * | 1942-06-24 | 1948-01-27 | Harry J Nichols | Projectile |
US3234646A (en) * | 1959-08-12 | 1966-02-15 | American Mach & Foundry | Friction welding |
US3370535A (en) * | 1959-04-14 | 1968-02-27 | Aviation Uk | Armor piercing projectile |
US5698814A (en) * | 1995-03-10 | 1997-12-16 | The United States Of America As Represented By The Secretary Of The Air Force | Hard target penetrator with multi-segmenting casing cutter |
US5988071A (en) * | 1997-08-21 | 1999-11-23 | Lockheed Martin Corporation | Penetrator having multiple impact segments, including an explosive segment |
US6016753A (en) * | 1995-03-10 | 2000-01-25 | The United States Of America As Represented By The Secretary Of The Air Force | Explosive pipe cutting |
-
0
- US US1146484D patent/US1146484A/en not_active Expired - Lifetime
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2435095A (en) * | 1942-06-24 | 1948-01-27 | Harry J Nichols | Projectile |
US2422920A (en) * | 1942-08-18 | 1947-06-24 | Harry J Nichols | Armor-piercing drop bomb |
US2422559A (en) * | 1943-05-07 | 1947-06-17 | Harry J Nichols | Projectile |
US3370535A (en) * | 1959-04-14 | 1968-02-27 | Aviation Uk | Armor piercing projectile |
US3234646A (en) * | 1959-08-12 | 1966-02-15 | American Mach & Foundry | Friction welding |
US5698814A (en) * | 1995-03-10 | 1997-12-16 | The United States Of America As Represented By The Secretary Of The Air Force | Hard target penetrator with multi-segmenting casing cutter |
US6016753A (en) * | 1995-03-10 | 2000-01-25 | The United States Of America As Represented By The Secretary Of The Air Force | Explosive pipe cutting |
US5988071A (en) * | 1997-08-21 | 1999-11-23 | Lockheed Martin Corporation | Penetrator having multiple impact segments, including an explosive segment |
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