US730308A - Projectile for smooth and rifled bores. - Google Patents
Projectile for smooth and rifled bores. Download PDFInfo
- Publication number
- US730308A US730308A US11594902A US1902115949A US730308A US 730308 A US730308 A US 730308A US 11594902 A US11594902 A US 11594902A US 1902115949 A US1902115949 A US 1902115949A US 730308 A US730308 A US 730308A
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- United States
- Prior art keywords
- projectile
- smooth
- rifled
- bores
- bore
- 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
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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 for smooth and rifled bores of firearms, which'in consequence of its peculiar shape is selfguided-that is to say, keeps the direction given to it by the barrel and excludes the possibility of any deviation in the aim.
- a further advantage ofthe projectile is that the laws relating to stability or steadiness of flight of the projectile, according to which light projectiles in consequence of their slight inertia under high-gas pressures require a higher sectional load, and in consequence of this circumstance a stronger rifle pitch, do not apply.
- Figure 1 is a side view of the projectile; Fig. 2, a plan; Fig. 3, a longitudinal section; Fig. 4, a transverse section; Fig. 5, a side view of the projectile in combination with the known rotating device.
- Figs; 6 to 8 are different views of the same combination.
- the projectile Fig. 1, consists of a body a of a conical or tapering cylindrical form, the front part (the head of the projectile) being of the same caliber as the bore of the weapon,
- a flange b which is likewise of the same caliber and has inclined surfaces b' running to the body of the projectile.
- a flange b Between the head of the projectile and the flange b from four to six longitudinal Webs g are axially arranged, which, with the flange b, form fan-like divisions d on the body of the projectile.
- the projectile a is made hollow, andin the bore running through it a transverse piece 7.: is inserted and suitably shaped to-form winding screw-passages k, which when the projectile is in motion produce the actual rotation thereof.
- the firing operation is as follows: Directly the projectile leaves the weapon the resistant air acting on it is pressed sidewise at a right angle to the axis of the projectile by the head of the projectile and closes up behind the flange b.
- the longitudinal webs which in consequence of the rotation of the projectile act similarly to a centrifugal machine, the air surrounding the projectile is prevented from prematurely entering the divisions d and is first brought into contact with the'flangebon the body of the projectile.
- the result of this is that theair in the divisions dis powerfully rarefied during the flight of" self-guiding and the greatest possible stability or fixity of rotation of the projectile assured.
- a projectile comprising a tapered body portion, a head with beveled edges, a flange arranged at the bottom of the projectile, and longitudinal stays or webs which with the flange form fan-like compartments.
- a projectile comprising a tapered body portion with an axial bore, a head with beveled edges, a flange arranged at the bottom of the projectile, longitudinal stays or webs which with the flange form fan-like compartments, and a transverse piece in the bore forming one or more screw like passages, which cause the fired-01f projectile to rotate.
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- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Description
PATENTED JUNE 9, 1903.
0. F. P. STENDEBAGH.
PROJEGTILE FOR SMOOTH AND RIFLED BORES.
APPLICATION FILED JULY 17, 1902.
N0 MODEL.
UNITED STATES Patented June 9, 1903.
PATENT EFTCE.
CARL FRIEDRICH PIIILIPP STENDEBACH, or MooKERN, NEAR LEIPZIG,
GERMANY.
PROJECTILE FOR SMOOTH AND RIFLED BORES.
SPECIFICATION formingpart of Letters Patent No; 730,308, dated June 9, 1903.
Application filed July 17,1902. Serial No. 116.949. (No model-'3 in Projectiles for Smooth and Rifled Bores;
and I do hereby declare 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 appertains to make and-use the same.
This invention relates to a projectile for smooth and rifled bores of firearms, which'in consequence of its peculiar shape is selfguided-that is to say, keeps the direction given to it by the barrel and excludes the possibility of any deviation in the aim.
A further advantage ofthe projectile is that the laws relating to stability or steadiness of flight of the projectile, according to which light projectiles in consequence of their slight inertia under high-gas pressures require a higher sectional load, and in consequence of this circumstance a stronger rifle pitch, do not apply.
-By means of this invention a considerably greater steadiness of flight is assured with rifled tubes than has been possible hitherto, this being due tolthe peculiar external form of the projectile and the eflect of the resistance offered by the air, while a combination of this external arrangement with the known device in the interior of the projectile, whereby the projectile is likewise rotated through the resistance presented by the air, renders the projectile also suitable for smooth bores, so that the superiority of the rifled bore of the same caliber over the smooth bore disappears.
In the drawings, Figure 1 is a side view of the projectile; Fig. 2, a plan; Fig. 3, a longitudinal section; Fig. 4, a transverse section; Fig. 5, a side view of the projectile in combination with the known rotating device. Figs; 6 to 8 are different views of the same combination.
\Vith the assistance of the drawings the invention will be made clear, asfollows:
The projectile, Fig. 1, consists of a body a of a conical or tapering cylindrical form, the front part (the head of the projectile) being of the same caliber as the bore of the weapon,
made with a beveled edge and having only a.
thin face or facet for the purpose of more easily inserting it in the bore. At the back of the projectile is a flange b, which is likewise of the same caliber and has inclined surfaces b' running to the body of the projectile. Between the head of the projectile and the flange b from four to six longitudinal Webs g are axially arranged, which, with the flange b, form fan-like divisions d on the body of the projectile.
In the combination. for smooth bores illustrated in Figs. 5 to 8 the longitudinal webs g project somewhat and serve, with the ring b, as a guide for the projectile in the bore.
The projectile ais made hollow, andin the bore running through it a transverse piece 7.: is inserted and suitably shaped to-form winding screw-passages k, which when the projectile is in motion produce the actual rotation thereof.
The firing operation is as follows: Directly the projectile leaves the weapon the resistant air acting on it is pressed sidewise at a right angle to the axis of the projectile by the head of the projectile and closes up behind the flange b. By means of the longitudinal webs, which in consequence of the rotation of the projectile act similarly to a centrifugal machine, the air surrounding the projectile is prevented from prematurely entering the divisions d and is first brought into contact with the'flangebon the body of the projectile. The result of this is that theair in the divisions dis powerfully rarefied during the flight of" self-guiding and the greatest possible stability or fixity of rotation of the projectile assured.
What I claim, and desire to secure by Letters Patent, is-
l. A projectile, comprising a tapered body portion, a head with beveled edges, a flange arranged at the bottom of the projectile, and longitudinal stays or webs which with the flange form fan-like compartments.
2. A projectile, comprising a tapered body portion with an axial bore, a head with beveled edges, a flange arranged at the bottom of the projectile, longitudinal stays or webs which with the flange form fan-like compartments, and a transverse piece in the bore forming one or more screw like passages, which cause the fired-01f projectile to rotate.
In testimony whereof I have affixed my signature in presence of two witnesses.
CARL FRlEDRICli IllILlPP S'lIlNDEBAOII. \Vitnesses:
RUDOLPH FRICKE, I-I. SACK, Jun.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11594902A US730308A (en) | 1902-07-17 | 1902-07-17 | Projectile for smooth and rifled bores. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11594902A US730308A (en) | 1902-07-17 | 1902-07-17 | Projectile for smooth and rifled bores. |
Publications (1)
Publication Number | Publication Date |
---|---|
US730308A true US730308A (en) | 1903-06-09 |
Family
ID=2798815
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11594902A Expired - Lifetime US730308A (en) | 1902-07-17 | 1902-07-17 | Projectile for smooth and rifled bores. |
Country Status (1)
Country | Link |
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US (1) | US730308A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2471074A (en) * | 1943-05-06 | 1949-05-24 | Cone Automatic Mach Co Inc | Multiple spindle lathe |
US2559955A (en) * | 1946-11-26 | 1951-07-10 | Harlow H Hartwell | Projectile |
US4553479A (en) * | 1983-04-11 | 1985-11-19 | Tolcon Steel Corporation | Plastic bullet |
US4627357A (en) * | 1984-09-27 | 1986-12-09 | Pranas Gobis | Ammunition projectile |
-
1902
- 1902-07-17 US US11594902A patent/US730308A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2471074A (en) * | 1943-05-06 | 1949-05-24 | Cone Automatic Mach Co Inc | Multiple spindle lathe |
US2559955A (en) * | 1946-11-26 | 1951-07-10 | Harlow H Hartwell | Projectile |
US4553479A (en) * | 1983-04-11 | 1985-11-19 | Tolcon Steel Corporation | Plastic bullet |
US4627357A (en) * | 1984-09-27 | 1986-12-09 | Pranas Gobis | Ammunition projectile |
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