US760338A - Projectile. - Google Patents

Projectile. Download PDF

Info

Publication number
US760338A
US760338A US16557003A US1903165570A US760338A US 760338 A US760338 A US 760338A US 16557003 A US16557003 A US 16557003A US 1903165570 A US1903165570 A US 1903165570A US 760338 A US760338 A US 760338A
Authority
US
United States
Prior art keywords
bullet
projectile
rotation
annulus
grooves
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
Application number
US16557003A
Inventor
Edward L Kwiatkowski
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US16557003A priority Critical patent/US760338A/en
Application granted granted Critical
Publication of US760338A publication Critical patent/US760338A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/02Stabilising arrangements
    • F42B10/26Stabilising arrangements using spin
    • F42B10/28Stabilising arrangements using spin induced by gas action
    • F42B10/30Stabilising arrangements using spin induced by gas action using rocket motor nozzles

Definitions

  • My invention relates'to projectiles; and it consists in increasing their initial velocity, their speed of rotation, and their penetration. Trajectory is flattened, impact augmented, and glancing minimized.
  • Figure 1 represents an elevation, partly sectional, of a cartridge provided with a bullet embodying my invention.
  • Figs. 2 and 3 represent, respectively, a rear elevation and a perspective view of the bullet or projectile detached.
  • A designates a cartridge-shell, which may be of the form required for any well-known or desired rifle or other arm.
  • B designates a bullet of the usual conical form, having a plane cylindric body C, at the rear of which is a butt D, in which are grooves E, which extend spirally in the direction of rotation from the body U to the rear face of the bullet.
  • said base In said base is a plurality of depressions G, the bottom wall of each of which is sector-shaped and theoretically sections of a screw of a desired pitch separated by crossbars G. In practice it may vary from this figure, with no material detraction from its value.
  • the outer curved sides of depression 6' do not extend to the edge of the bullet or communicate with grodve E, these being circumscribed by a plane annulus H, which acts to protect the gun-barrel from erosion, the bars G joining said annulus and serving to strengthen said annulus.
  • the point K of the bullet' is provided with a plurality of helical grooves L, forming cutting edges M.
  • My invention is applicable to projectiles made of any proper metal and of varying de.
  • a projectile comprising acylindric body adapted to fill the bore of a gun and a butt portion having grooves which extend spirally in the direction of rotation from said body to the rear face of the bullet.
  • a projectile comprising a cylindric body adapted to fill the bore of a gun, a butt poraplane annulus inclosing'depressions, the bot- 2i plane annulus inclosing a plurality of detoms of which are inclined in the direction of pressions separated by intersecting cross' 9 rotation. walls, the bottoms of said depressions being 3.
  • a projectile comprisinga cy'lindric body inclined in the direction of rotation.

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Description

No. 760,338; PATENTED MAY 17, 1904. B. L. KWIATKQWSKI. PROJBGTILE.
APPLIOATION FILED JULY 15, 1903.
K0 MODEL.
awwntoz wameam UNirnn STATES Patented May 1'7, 190%.
PATENT frricia.
PROJECTILE.
SPECIFICATION- forming part of Letters Patent NO. 760,338, dated May 17, 1904:. p
I Application filed July 15,1903. Serial No. 165,570. (No model.)
To (l/ZZ whom; it nuty concern:
Be it known that I, EDWARD L. KwrA'rnowsin, a subject of the King of Prussia, Emperor of Germany, (but having residedin the United States over one year last past and having declared my intention of becoming a citizen thereof,) residing in the city and county of Philadelphia, State of Pennsylvania, have invented new and useful Improvements in Pro. jectiles, of which the following is a specification.
My invention relates'to projectiles; and it consists in increasing their initial velocity, their speed of rotation, and their penetration. Trajectory is flattened, impact augmented, and glancing minimized.
It further consists of other-novel features of construction, all as will be hereinafter fully set forth.
Figure 1 represents an elevation, partly sectional, of a cartridge provided with a bullet embodying my invention. Figs. 2 and 3 represent, respectively, a rear elevation and a perspective view of the bullet or projectile detached.
Similar letters of reference indicate correponding parts in the figures. I
- Referring to the drawings, A designates a cartridge-shell, which may be of the form required for any well-known or desired rifle or other arm.
B designates a bullet of the usual conical form, having a plane cylindric body C, at the rear of which is a butt D, in which are grooves E, which extend spirally in the direction of rotation from the body U to the rear face of the bullet. In said base is a plurality of depressions G, the bottom wall of each of which is sector-shaped and theoretically sections of a screw of a desired pitch separated by crossbars G. In practice it may vary from this figure, with no material detraction from its value. It will be noted that'the outer curved sides of depression 6' do not extend to the edge of the bullet or communicate with grodve E, these being circumscribed by a plane annulus H, which acts to protect the gun-barrel from erosion, the bars G joining said annulus and serving to strengthen said annulus. The point K of the bullet'is provided with a plurality of helical grooves L, forming cutting edges M. I
The operation is as fol-lows: When the piece is fired, the cylindric body C of the bullet B fills the bore and prevents any escape of gas. At the same time the bullet is rotated in the direction of the arrow shown in Fig. 1 by the gas pressure 0n the sides of the grooves E and on the faces of the depressions Gr. It will be noted that the twist of the grooves E is insuch a direction as to rotate the bullet from left to right, as usual. This rotation is assisted by the pressure against the faces of the depressions G, escape ofsuch pressure directly against the sides of the gun-barrel being prevented by the circumscribing annulus H, which is strengthened by the intersect-' ing cross-bars G. In this Way erosion of the barrel is greatly reduced.
When the bullet strikes, the cutting edges-M of the depressionsL being faced in the direction of rotation enable the bullet to engage with and bore into an object. Because of this boring action the bullet will not glance even at a considerable incidental angle.
My invention is applicable to projectiles made of any proper metal and of varying de.
grees of hardness.
Various changes may be made in the details of construction shown withoutdeparting from the general spirit of my invention, and I do not, therefore, desire to be limited in each case to the same. i
Having thus described my invention, What I claim as new, and desire to secure by Letters Patent, is
l. A projectile comprising acylindric body adapted to fill the bore of a gun and a butt portion having grooves which extend spirally in the direction of rotation from said body to the rear face of the bullet.
2. A projectile comprising a cylindric body adapted to fill the bore of a gun, a butt poraplane annulus inclosing'depressions, the bot- 2i plane annulus inclosing a plurality of detoms of which are inclined in the direction of pressions separated by intersecting cross' 9 rotation. walls, the bottoms of said depressions being 3. A projectile comprisinga cy'lindric body inclined in the direction of rotation.
adapted to fill the bore of a gun, a butt por- EDVVARI) L. KVVlA'lhOlVSKI.
tion having grooves which extend spirally in Witnesses:
the direction of rotation from said body to the. J OiiN A. \NHGDERSHEIM,
rear of the bullet and a rear face consisting of GEO. L. (looruii.
US16557003A 1903-07-15 1903-07-15 Projectile. Expired - Lifetime US760338A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US16557003A US760338A (en) 1903-07-15 1903-07-15 Projectile.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US16557003A US760338A (en) 1903-07-15 1903-07-15 Projectile.

Publications (1)

Publication Number Publication Date
US760338A true US760338A (en) 1904-05-17

Family

ID=2828827

Family Applications (1)

Application Number Title Priority Date Filing Date
US16557003A Expired - Lifetime US760338A (en) 1903-07-15 1903-07-15 Projectile.

Country Status (1)

Country Link
US (1) US760338A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3217650A (en) * 1952-02-28 1965-11-16 Martin A Paul Offset liner for a cavity charge projectile
US4829906A (en) * 1987-09-08 1989-05-16 Kaswer Stanley W Cutting bullet
US4996924A (en) * 1987-08-11 1991-03-05 Mcclain Harry T Aerodynamic air foil surfaces for in-flight control for projectiles
US5164538A (en) * 1986-02-18 1992-11-17 Twenty-First Century Research Institute Projectile having plural rotatable sections with aerodynamic air foil surfaces
US6640722B2 (en) * 2001-09-19 2003-11-04 Armaturen-Gmbh Shell cap
US20130180424A1 (en) * 2010-08-30 2013-07-18 Duretek Inc. Bullet including an air-guiding recess
EP3137843A4 (en) * 2014-04-30 2018-01-03 G9 Holdings, LLC Projectile with enhanced ballistics
US20190186879A1 (en) * 2017-12-14 2019-06-20 Quantum Ammunition, Llc Projectiles for ammunition and methods of making and using the same
US20220364838A1 (en) * 2018-07-16 2022-11-17 Vista Outdoor Operations Llc Reduced stiffness barrel fired projectile

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3217650A (en) * 1952-02-28 1965-11-16 Martin A Paul Offset liner for a cavity charge projectile
US5164538A (en) * 1986-02-18 1992-11-17 Twenty-First Century Research Institute Projectile having plural rotatable sections with aerodynamic air foil surfaces
US4996924A (en) * 1987-08-11 1991-03-05 Mcclain Harry T Aerodynamic air foil surfaces for in-flight control for projectiles
US4829906A (en) * 1987-09-08 1989-05-16 Kaswer Stanley W Cutting bullet
US6640722B2 (en) * 2001-09-19 2003-11-04 Armaturen-Gmbh Shell cap
US20130180424A1 (en) * 2010-08-30 2013-07-18 Duretek Inc. Bullet including an air-guiding recess
US8973504B2 (en) * 2010-08-30 2015-03-10 Duretek Inc. Bullet including an air-guiding recess
USD868199S1 (en) 2014-04-30 2019-11-26 G9 Holdings, Llc Projectile
US11041703B2 (en) 2014-04-30 2021-06-22 G9 Holdings, Llc Projectile with enhanced ballistics
USD863492S1 (en) 2014-04-30 2019-10-15 G9 Holdings, Llc Projectile
EP3137843A4 (en) * 2014-04-30 2018-01-03 G9 Holdings, LLC Projectile with enhanced ballistics
US10502536B2 (en) 2014-04-30 2019-12-10 G9 Holdings, Llc Projectile with enhanced ballistics
US10578410B2 (en) 2014-04-30 2020-03-03 G9 Holdings, Llc Projectile with enhanced ballistics
US11808550B2 (en) 2014-04-30 2023-11-07 G9 Holdings, Llc Projectile with enhanced ballistics
USD980941S1 (en) 2014-04-30 2023-03-14 G9 Holdings, Llc Projectile
US11181351B2 (en) 2014-04-30 2021-11-23 G9 Holdings, Llc Projectile with enhanced ballistics
USD978277S1 (en) 2014-04-30 2023-02-14 G9 Holdings, Llc Projectile
US20190186879A1 (en) * 2017-12-14 2019-06-20 Quantum Ammunition, Llc Projectiles for ammunition and methods of making and using the same
US10823540B2 (en) * 2017-12-14 2020-11-03 Quantum Ammunition, Llc Projectiles for ammunition and methods of making and using the same
US20220364838A1 (en) * 2018-07-16 2022-11-17 Vista Outdoor Operations Llc Reduced stiffness barrel fired projectile
US11781843B2 (en) * 2018-07-16 2023-10-10 Federal Cartridge Company Reduced stiffness barrel fired projectile

Similar Documents

Publication Publication Date Title
US20220260351A1 (en) Projectile with Enhanced Ballistics
US7380505B1 (en) Muzzleloading firearm projectile
US760338A (en) Projectile.
US868938A (en) Barrel for portable firearms and cannon with deepened grooves.
US221249A (en) Improvement in projectiles for small-arms
US1275028A (en) Rifle-barrel.
US587801A (en) durnford
US326231A (en) Bullet
US315746A (en) Manuel costa de aeguibel
US1380171A (en) Ordnance
US592437A (en) Peter oberhammer
US300515A (en) Alois schheidbe
US835482A (en) Rifling.
US711209A (en) Projectile.
US840085A (en) Firearm.
US1122738A (en) Target-bullet.
US245994A (en) Howaed caee
US296958A (en) William hebleb
US39942A (en) Improvement in rifled projectiles
US1230712A (en) Rifle-barrel.
US14742A (en) Improvement in projectiles for fire-arms
US1012455A (en) Projectile.
US741738A (en) Projectile.
US1073349A (en) Mushroom-bullet.
US451088A (en) Projectile