US517560A - Projectile - Google Patents
Projectile Download PDFInfo
- Publication number
- US517560A US517560A US517560DA US517560A US 517560 A US517560 A US 517560A US 517560D A US517560D A US 517560DA US 517560 A US517560 A US 517560A
- Authority
- US
- United States
- Prior art keywords
- projectile
- passage
- air
- axial passage
- ashley
- 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
- 210000000614 Ribs Anatomy 0.000 description 4
- 238000004880 explosion Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 101710033606 PSMA5 Proteins 0.000 description 2
- 235000002912 Salvia officinalis Nutrition 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 235000017423 hawthorn Nutrition 0.000 description 2
- 235000002020 sage Nutrition 0.000 description 2
- 239000001296 salvia officinalis l. Substances 0.000 description 2
- 239000007779 soft material Substances 0.000 description 2
- 239000000126 substance Substances 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 relates to a projectile constructed with an axial passage extending en'- tirely through it and closed at its rear end by a cap looselyitted thereto, so as to be thrown off by the force of -the air vpassing through the projectile, after'the latter is discharged, whereby the projectile will travel with less -re- ⁇ sistance, greater speed and distance, and in a straight course.
- the invention has for its-object to provide an improved projectile of this character, as hereinafter described andclaimed.
- the invention consists of the construction hereinafter described and claimed.
- v Figure 1 is a longitudinal section of the projectile comprehending my invention.
- Fig. 2 is an exterior view of the same projectile, and
- Fig. 3 is a detail.
- the .projectile is providedY with an axial passage extending entirely througn it.
- the object of this passage is to enable me to make the heaviest possible' projectile of a given length which will meet with the smallest resistance of the air.
- a further object of the passage is to direct the flight of the projectile. Vhen the projectile is inserted into the gun for tiring the rear end which receives the force of the explosion is covered with a cap,
- a represents the body of the projectile
- b represents the axial passage through it
- c represents the cap over the rear end of the projectile.
- Fig. l the passage b is shown lined with 6o a tube d which has acutting edge and iiange projecting from the forward end to strenghten the projectile when the body'is made of softer material, such -as lead, and also to enable the projectile to pierce refractory substances against which it is directed.
- This lining may be provided with the ribs or grooves as shown in Fig. 3, to impart the rotary movement to the projectile.
- a cylindrical projectile having an 'axial passage extending entirely through it, au open ended tube" fitting said passage and havinga bell-shaped rifled mouth at its forward end.
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Earth Drilling (AREA)
Description
'I (-o Model.)
F. M. ASHLEY.
PROJBGTILB.
l No. 517,560. Patented Apr,.-3,-1894.
/ /1//0/1/1//1//0/,1 IIIIIIII//II/IIIIIIIIIIIIIIIIIII/IA,
figli INVENTOH i530. ArrH/VEY. I
FRANK M. ASHLEY, OF HAWTHORNE,'ASSIGNOR OF ONE-FORTH TO WOOD MCKEE, OF PATERSON, NEW JERSEY. 'Y
PROJ Ecrit-7E.
SPECIFICATION forming part of Letters Patent N0. 517,560, dated April 3,1894.
Application iiled February 29,1892. Serial No. 423,109. (No model.)
To all whom t may concern.-
Be it known that I, FRANK M. ASHLEY, citizen vof the'United States, residing in Hawthorne, in the county of Passaic and State of New Jersey, have invented certain new and useful Improvements in Projectiles, of which the following is a specification.
This invention relates to a projectile constructed with an axial passage extending en'- tirely through it and closed at its rear end by a cap looselyitted thereto, so as to be thrown off by the force of -the air vpassing through the projectile, after'the latter is discharged, whereby the projectile will travel with less -re- `sistance, greater speed and distance, and in a straight course.
The invention has for its-object to provide an improved projectile of this character, as hereinafter described andclaimed.
The invention consists of the construction hereinafter described and claimed.
In the accompanying drawings: vFigure 1 is a longitudinal section of the projectile comprehending my invention. Fig. 2 is an exterior view of the same projectile, and Fig. 3 is a detail.
The .projectile is providedY with an axial passage extending entirely througn it. The object of this passage is to enable me to make the heaviest possible' projectile of a given length which will meet with the smallest resistance of the air. A further object of the passage is to direct the flight of the projectile. Vhen the projectile is inserted into the gun for tiring the rear end which receives the force of the explosion is covered with a cap,
which is loosely applied to the projectile and is sufficiently strong to withstand the force of the explosion. When'the projectile leaves the gunthe pressure of the air through ',the axial passage forces the cap olf from the end of the projectile and thus provides an uninterrupted passage for the air, which materially reduces the vresistance thereof.
Referring to the drawings by letter, a represents the body of the projectile, b represents the axial passage through it and c represents the cap over the rear end of the projectile. Y
In ordento secure additional accuracy in 5e the flight ofa projectile and to dispense with the rifling of the gun barrel, I propose to make the forward end of the passage bellshaped and to form spiral ribs b thereon. Whenthe air rushing through the axial pas- 5 5 sage during the flight of the projectile, strikes these spiral formations it will cause the projectile to rotate on its axis and thereby iny sure a straight course.
In Fig. l the passage b is shown lined with 6o a tube d which has acutting edge and iiange projecting from the forward end to strenghten the projectile when the body'is made of softer material, such -as lead, and also to enable the projectile to pierce refractory substances against which it is directed. This lining may be provided with the ribs or grooves as shown in Fig. 3, to impart the rotary movement to the projectile.
Having thus described my invention, I 7o clairnl. A cylindrical projectile having an 'axial passage extending entirely through it, au open ended tube" fitting said passage and havinga bell-shaped rifled mouth at its forward end.
2. A cylindrical projectile'having an axial passage extending entirely through it and made of soft material, such as lead,anda1in ing tube of harder material than the body of the projectile and having its forward end re- 8c inforced for the purpose described. In witness whereof I have hereunto signed my name in the presence of `tw'o subscribing witnesses. v FRANK M. ASHLEY.A
Witnesses:
I JAMES F. KAVANAGH, WM. A. RosENBAUM.
Publications (1)
Publication Number | Publication Date |
---|---|
US517560A true US517560A (en) | 1894-04-03 |
Family
ID=2586363
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US517560D Expired - Lifetime US517560A (en) | Projectile |
Country Status (1)
Country | Link |
---|---|
US (1) | US517560A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2433334A (en) * | 1944-01-11 | 1947-12-30 | Birkeland Leigh Forstner | Ammunition |
US3063376A (en) * | 1959-11-12 | 1962-11-13 | Powell Edward Baden | Slug for shotgun |
US4627357A (en) * | 1984-09-27 | 1986-12-09 | Pranas Gobis | Ammunition projectile |
US5471719A (en) * | 1993-05-10 | 1995-12-05 | Sawyers; William L. | Air gun pellet forming method |
US20070074637A1 (en) * | 2005-04-01 | 2007-04-05 | Pontieri James M | Aerodynamic air gun projectile |
USD980376S1 (en) * | 2018-12-13 | 2023-03-07 | Jennifer R. Hossack | Pellet |
-
0
- US US517560D patent/US517560A/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2433334A (en) * | 1944-01-11 | 1947-12-30 | Birkeland Leigh Forstner | Ammunition |
US3063376A (en) * | 1959-11-12 | 1962-11-13 | Powell Edward Baden | Slug for shotgun |
US4627357A (en) * | 1984-09-27 | 1986-12-09 | Pranas Gobis | Ammunition projectile |
US5471719A (en) * | 1993-05-10 | 1995-12-05 | Sawyers; William L. | Air gun pellet forming method |
US20070074637A1 (en) * | 2005-04-01 | 2007-04-05 | Pontieri James M | Aerodynamic air gun projectile |
US7222573B2 (en) | 2005-04-01 | 2007-05-29 | Pontieri James M | Aerodynamic air gun projectile |
USD980376S1 (en) * | 2018-12-13 | 2023-03-07 | Jennifer R. Hossack | Pellet |
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