US35503A - beowke - Google Patents
beowke Download PDFInfo
- Publication number
- US35503A US35503A US35503DA US35503A US 35503 A US35503 A US 35503A US 35503D A US35503D A US 35503DA US 35503 A US35503 A US 35503A
- Authority
- US
- United States
- Prior art keywords
- projectile
- wings
- gun
- percussion
- recesses
- 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
- 210000002445 Nipples Anatomy 0.000 description 10
- 238000009527 percussion Methods 0.000 description 10
- 241000220010 Rhode Species 0.000 description 4
- 230000000875 corresponding Effects 0.000 description 4
- 238000004880 explosion Methods 0.000 description 4
- 239000002360 explosive Substances 0.000 description 4
- 238000004642 transportation engineering Methods 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000003721 gunpowder Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000003405 preventing Effects 0.000 description 2
- 230000000284 resting Effects 0.000 description 2
- 230000000717 retained 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
- 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
- F42B10/02—Stabilising arrangements
- F42B10/26—Stabilising arrangements using spin
- F42B10/28—Stabilising arrangements using spin induced by gas action
- F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles
Definitions
- This invention consists, first, in a certain arrangement of obliquely-expanding wings for the purpose of obtaining a rotary motion of a projectile about its axis by the resistance of the atmosphere to its flight when tired from a smooth-bored gun.
- A is the body of the projectile, made with an opening at its point, as shown, or at its base, for the introduction of the charge, and fitted with a screw-plug, B, to close it after being charged.
- 11 b are recesses formed at equal distances apart all around the exterior of the body A, for the reception of the expanding wings D D, said recesses having their sides parallel with the axis of the projectile, as shown, or oblique thereto.
- the said wings D D' are attached at their rear ends to the bodyA by means of pins 0 0, inserted through them and through the portions of the body at the sides of their respective recesses b b, at an angle of about forty- I five degrees to planes passing longitudinally through the axis of the projectile, and the rear ends of thesaid wings are made parallel with the said pins, to enable them to swing outward bya movementupon the said pins in the manner shown in Fig. 2.
- the rear ends of the recesses b b are also made parallel with the said pins.
- the exterior surfaces of the wings are so formed that when closed up into the recesses Z) 1) their exterior surfaces are flush with the exterior surface of the body A.
- a a nipple, d with a vent, n, to the central cavity, 0, which contains the charge of gunpowder to effect the disruption of the body A of the projectile, and a percussion-cap, f, or other percussion priming is applied to each nipple,and under the front portion of each wing there is placed a stop, composed of a piece of wire, which is arranged across the cavity b,with its ends resting in notches h 7L, provided in the body A, on each side of the recess 1), for its reception, such stops being for the purpose of keeping the wings out of contact with the caps or other priming during the transportation of the projectile.
- E is a packing-band of soft metal, applied bythe gases developed in the explosion of the charge of the gun, for the purpose of prevent ing windage.
- the projectile, charged and capped, and with the stops 9 g and band j j applied, may
- the band j is slipped off. and the stops 9 9 may be allowed to drop out of their places and from the pro jectile, which is inserted into the gun in the same manner as any other projectile.
- the wings D are caused by their inertia to fly out fromthe body Ain the manner shown in Fig. 2, in which condition they are retained bythe pressure of the air in front of them during the flight of the projectile, and in which condition, owing to the spiral or nearly spiral arrangement of their faces or inner sides relatively to the axis of the wings DD and confining the said wings round the base of the projectile to be expanded be transp orted and handled with perfect safety.
- the proj ecti1e the resistance of the atmosphere, acting against the said faces or sides, causes the rotation of the projectile on its axis.
- the wings On the striking of the projectile against any body having sufficient resisting-power to stop or considerably retard the body A,the wings, continuing to move forward by the momentum they have acquired, are causedto strike like hammers upon the percussion caps ff, which are thereby exploded and caused to fire the charge in the cavity 0 and produce the disruption of the body A.
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Description
W. E. BROWNE.
Shell.
Patented June 10, 1862.
lnve ntor NFETERS. PHOTO-LITHQGRAPHER, WASHeNTON, D C.
theirs STATES Parana @rrrce.
\V. E. BROVVNE, OF VALLEY FALLS, RHODE ISLAND.
IMPROVEMENT IN-EXPLQSEVE eeoanorsres Foe ORDNANCE.
Specification forming part of Letters Patent No. 35,5493. dated June 10, 186
539 all whom it may concern:
Be it known that 1, WILLIAM E. BROWNE, of Valley Falls, in the county of Providence and State of Rhode Island, have invented certain new and useful Improvements in Elongated Projectiles for Ordnance; and I do hereby declare that the following is a full,. clear, and exact description of the same, reference being had to the accompanying drawings, forming part of this specification, in which- Figure l is a side view of an elongated explosive projectile with myimprovement, showing it in condition for transportation. Fig. 2 is a similar View of the same, showing the pro j ectile in the condition it assumes on its discharge from the gun. Fig. 3 is a central 1ongitudinal section of the same, corresponding with Fig. 1.
Similar letters of reference indicate corresponding parts in the several figures.
This invention consists, first, in a certain arrangement of obliquely-expanding wings for the purpose of obtaining a rotary motion of a projectile about its axis by the resistance of the atmosphere to its flight when tired from a smooth-bored gun. I
It consists, secondly, in a certain mode of combining one or more expanding wings and a nipple or nipples, or their equivalents, for the reception of percussion-caps or other percussion priming in an explosive projectile, for the purpose of making-such wing or wings constitute a hammer or hammers by which the said priming is exploded on the projectile striking.
To enable others to make and use my invention, I will proceed to describe its construction and operation.
A is the body of the projectile, made with an opening at its point, as shown, or at its base, for the introduction of the charge, and fitted with a screw-plug, B, to close it after being charged.
11 b are recesses formed at equal distances apart all around the exterior of the body A, for the reception of the expanding wings D D, said recesses having their sides parallel with the axis of the projectile, as shown, or oblique thereto. The said wings D D'are attached at their rear ends to the bodyA by means of pins 0 0, inserted through them and through the portions of the body at the sides of their respective recesses b b, at an angle of about forty- I five degrees to planes passing longitudinally through the axis of the projectile, and the rear ends of thesaid wings are made parallel with the said pins, to enable them to swing outward bya movementupon the said pins in the manner shown in Fig. 2. The rear ends of the recesses b b are also made parallel with the said pins. The exterior surfaces of the wingsare so formed that when closed up into the recesses Z) 1) their exterior surfaces are flush with the exterior surface of the body A. In one or more of the recesses b b or in each one there is provided a a nipple, d, with a vent, n, to the central cavity, 0, which contains the charge of gunpowder to effect the disruption of the body A of the projectile, and a percussion-cap, f, or other percussion priming is applied to each nipple,and under the front portion of each wing there is placed a stop, composed of a piece of wire, which is arranged across the cavity b,with its ends resting in notches h 7L, provided in the body A, on each side of the recess 1), for its reception, such stops being for the purpose of keeping the wings out of contact with the caps or other priming during the transportation of the projectile. These pins are kept in place until the projectile is placed in the gun, by means of a band, j, of wire or other material, encircling the body of the projectile around within their recesses b b.
E is a packing-band of soft metal, applied bythe gases developed in the explosion of the charge of the gun, for the purpose of prevent ing windage.
The projectile, charged and capped, and with the stops 9 g and band j j applied, may
\Vhen it is to be inserted in the gun,the band j is slipped off. and the stops 9 9 may be allowed to drop out of their places and from the pro jectile, which is inserted into the gun in the same manner as any other projectile. "When the discharge of the gun takes place on the projectile leaving the gun, the wings D are caused by their inertia to fly out fromthe body Ain the manner shown in Fig. 2, in which condition they are retained bythe pressure of the air in front of them during the flight of the projectile, and in which condition, owing to the spiral or nearly spiral arrangement of their faces or inner sides relatively to the axis of the wings DD and confining the said wings round the base of the projectile to be expanded be transp orted and handled with perfect safety.
the proj ecti1e,the resistance of the atmosphere, acting against the said faces or sides, causes the rotation of the projectile on its axis. On the striking of the projectile against any body having sufficient resisting-power to stop or considerably retard the body A,the wings, continuing to move forward by the momentum they have acquired, are causedto strike like hammers upon the percussion caps ff, which are thereby exploded and caused to fire the charge in the cavity 0 and produce the disruption of the body A.
I do not claim, broadly, furnishing a pr0- jectile with Wings which fly out from the body and assume a spiral relation thereto in the flight of the projectile; but
What I claim as my invention, and desire to secure by Letters Patent, is-
1. The arrangement of the expanding wings D D to swing from recesses in the sides of the body of the projectile upon pins 00, arranged obliquely to planes passing through the axis of the projectile, substantially as and for the purpose herein set forth.
2. The combination of one or more expanding wings, D D, attached to the body of the projectile, and one or more nipples or their equivalents provided on the said body for the reception of percussion-caps or other percussion prin1ing,whereby the said wings are made to constitute hammers for the explosion of the percussion priming, substantially as herein specified. W. E. BR-OTWNE.
\Vitnesses:
VINCENT BROWN, WILLIAM SPINK.
Publications (1)
Publication Number | Publication Date |
---|---|
US35503A true US35503A (en) | 1862-06-10 |
Family
ID=2105080
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US35503D Expired - Lifetime US35503A (en) | beowke |
Country Status (1)
Country | Link |
---|---|
US (1) | US35503A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3115831A (en) * | 1961-09-26 | 1963-12-31 | Suter Henry | Flexible rotochute |
US3834311A (en) * | 1971-06-01 | 1974-09-10 | Mb Ass | Cartridge |
US4030421A (en) * | 1975-06-26 | 1977-06-21 | Smith & Wesson Chemical Company, Inc. | Dual purpose projectile and weapon combination |
US4040331A (en) * | 1974-07-03 | 1977-08-09 | Smith & Wesson Chemical Company, Inc. | Dual purpose projectile and weapon combination |
US20040250712A1 (en) * | 2002-12-31 | 2004-12-16 | Tippey Darold D. | Process of packaging a compressible article |
-
0
- US US35503D patent/US35503A/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3115831A (en) * | 1961-09-26 | 1963-12-31 | Suter Henry | Flexible rotochute |
US3834311A (en) * | 1971-06-01 | 1974-09-10 | Mb Ass | Cartridge |
US4040331A (en) * | 1974-07-03 | 1977-08-09 | Smith & Wesson Chemical Company, Inc. | Dual purpose projectile and weapon combination |
US4030421A (en) * | 1975-06-26 | 1977-06-21 | Smith & Wesson Chemical Company, Inc. | Dual purpose projectile and weapon combination |
US20040250712A1 (en) * | 2002-12-31 | 2004-12-16 | Tippey Darold D. | Process of packaging a compressible article |
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