WO1996001974A1 - Training projectile - Google Patents

Training projectile Download PDF

Info

Publication number
WO1996001974A1
WO1996001974A1 PCT/US1995/006472 US9506472W WO9601974A1 WO 1996001974 A1 WO1996001974 A1 WO 1996001974A1 US 9506472 W US9506472 W US 9506472W WO 9601974 A1 WO9601974 A1 WO 9601974A1
Authority
WO
WIPO (PCT)
Prior art keywords
projectile
nose
main body
tail
rear end
Prior art date
Application number
PCT/US1995/006472
Other languages
French (fr)
Inventor
Anthony Farina
Mark Young
Original Assignee
United States Of America Secretary Of The Army
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 United States Of America Secretary Of The Army filed Critical United States Of America Secretary Of The Army
Priority to JP8504284A priority Critical patent/JPH09512897A/en
Priority to AU26452/95A priority patent/AU2645295A/en
Priority to CA002194549A priority patent/CA2194549C/en
Priority to KR1019970700061A priority patent/KR100223259B1/en
Priority to EP95921348A priority patent/EP0769127A4/en
Publication of WO1996001974A1 publication Critical patent/WO1996001974A1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A33/00—Adaptations for training; Gun simulators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B8/00—Practice or training ammunition
    • F42B8/12—Projectiles or missiles
    • 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
    • F42B10/04—Stabilising arrangements using fixed fins
    • F42B10/06—Tail fins

Definitions

  • a training projectile embodying the invention has its center of gravity far forward in the body of the projectile and carries, at its rear end, a slotted flared tail piece which provides the desired stability and drag in flight.
  • Fig. 1 is a perspective view of the invention and Fig. 2 is a plan view of a portion of the device of Fig. 1.
  • a training projectile 10 embodying the invention includes a main body portion 20 which is generally cylindrical in form and has a generally conical nose portion 30 and a tail portion 40 including a downwardly tapering portion 50, a short cylindrical portion 60 and a flared tail piece 70.
  • the flared tail piece 70 tapers outwardly from a small diameter to a larger diameter and the large diameter end has a plurality of generally rectangular slots 80 disposed about its surface. As illustrated in Fig. 2, the slots 80 are preferably disposed at a small angle to the longitudinal line (shown dashed) which runs through each along the wall of the flared tail piece. This angle, in one embodiment of the invention, is one degree.
  • the center of gravity of the projectile 10 is as close to the nose cone 30 as possible and this is achieved by having the nose and perhaps one fourth or one third of the body made of steel or another relatively heavy weight material and the remainder of the projectile made of aluminum, or another relatively lightweight material about 3/4" thick.
  • the projectile had a length of about 660mm, the main body 20 had a diameter of about 80mm, and the center of gravity was about 200 to 250 mm from the tip of the nose.
  • the flare tail piece 70 In operation of a projectile 10 embodying the invention, with the center of gravity near the front of the projectile, the flare tail piece 70 provides great stability and a favorable drag which limits the operating range of the projectile, as desired.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

This invention is a training projectile (10) having a main body (20), a nose (30), and a tail (40) including a flared tail member (70). The center of gravity of the projectile is located close to the nose.

Description

TRAINING PROJECTILE
The invention described herein may be manufactured, and used by or for the Government of the United States for governmental purposes.
BACKGROUND OF THE INVENTION The military have many different types of projectiles of tank and artillery rounds and new ones are being developed constantly. For each operating projectile, an identically shaped training projectile is required for use in training personnel who will use the real or armed projectile. Usually, the design of a training projectile is relatively straightforward, particularly when the projectile is of small diameter. However, a newly developed projectile has a relatively large diameter and the design of a training version thereof which is stable in flight, light in weight and traverses a suitable distance is not straightforward.
SUMMARY OF THE INVENTION A training projectile embodying the invention has its center of gravity far forward in the body of the projectile and carries, at its rear end, a slotted flared tail piece which provides the desired stability and drag in flight.
DESCRIPTION OF THE DRAWINGS Fig. 1 is a perspective view of the invention and Fig. 2 is a plan view of a portion of the device of Fig. 1.
DESCRIPTION OF THE INVENTION A training projectile 10 embodying the invention includes a main body portion 20 which is generally cylindrical in form and has a generally conical nose portion 30 and a tail portion 40 including a downwardly tapering portion 50, a short cylindrical portion 60 and a flared tail piece 70.
According to the invention the flared tail piece 70 tapers outwardly from a small diameter to a larger diameter and the large diameter end has a plurality of generally rectangular slots 80 disposed about its surface. As illustrated in Fig. 2, the slots 80 are preferably disposed at a small angle to the longitudinal line (shown dashed) which runs through each along the wall of the flared tail piece. This angle, in one embodiment of the invention, is one degree.
According to the invention, the center of gravity of the projectile 10 is as close to the nose cone 30 as possible and this is achieved by having the nose and perhaps one fourth or one third of the body made of steel or another relatively heavy weight material and the remainder of the projectile made of aluminum, or another relatively lightweight material about 3/4" thick.
In one embodiment of the invention, the projectile had a length of about 660mm, the main body 20 had a diameter of about 80mm, and the center of gravity was about 200 to 250 mm from the tip of the nose.
In operation of a projectile 10 embodying the invention, with the center of gravity near the front of the projectile, the flare tail piece 70 provides great stability and a favorable drag which limits the operating range of the projectile, as desired.

Claims

What is claimed is:
1. A training projectile comprising a main cylindrical body, a generally conical nose cone at the front end of said main body and a tail portion at the rear end of said main body, said tail portion including an outwardly flared member having slots in its end, said projectile having its center of gravity close to said nose.
2. the projectile defined in claim 1 wherein said nose is made of a heavy weight material and the greater portion of said main body and said tail are made of a lightweight material whereby the center of gravity of said projectile is close to the nose thereof.
3. The projectile defined in claim 1 wherein said nose and a portion of the main body secured thereto being of steel and the remainder of said main body and said tail being of aluminum.
4. The projectile defined in Claim 1 wherein said tail includes at its rear end an outwardly flared flare having a rear end, and a plurality of slots in said rear end of said flare.
5. The projectile defined in claim 4 wherein said slots are disposed at a small angle to the longitudinal axis thereof.
6. The projectile defined in claim 5 wherein said angle is about one degree.
PCT/US1995/006472 1994-07-07 1995-05-15 Training projectile WO1996001974A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP8504284A JPH09512897A (en) 1994-07-07 1995-05-15 Training projectile
AU26452/95A AU2645295A (en) 1994-07-07 1995-05-15 Training projectile
CA002194549A CA2194549C (en) 1994-07-07 1995-05-15 Training projectile
KR1019970700061A KR100223259B1 (en) 1994-07-07 1995-05-15 Training projectile
EP95921348A EP0769127A4 (en) 1994-07-07 1995-05-15 Training projectile

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/273,032 US5498160A (en) 1994-07-07 1994-07-07 Training projectile
US08/273,032 1994-07-07

Publications (1)

Publication Number Publication Date
WO1996001974A1 true WO1996001974A1 (en) 1996-01-25

Family

ID=23042266

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1995/006472 WO1996001974A1 (en) 1994-07-07 1995-05-15 Training projectile

Country Status (7)

Country Link
US (1) US5498160A (en)
EP (1) EP0769127A4 (en)
JP (1) JPH09512897A (en)
KR (1) KR100223259B1 (en)
AU (1) AU2645295A (en)
CA (1) CA2194549C (en)
WO (1) WO1996001974A1 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5725179A (en) * 1996-11-04 1998-03-10 The United States Of America As Represented By The Secretary Of The Army Expansion wave spin inducing generator
US6123289A (en) * 1997-06-23 2000-09-26 The United States Of America As Represented By The Secretary Of The Army Training projectile
US6699091B1 (en) 1999-11-04 2004-03-02 Jon A. Warner Hand-launchable underwater projectile toy
US7624683B2 (en) * 2001-08-23 2009-12-01 Raytheon Company Kinetic energy rod warhead with projectile spacing
US20060283348A1 (en) * 2001-08-23 2006-12-21 Lloyd Richard M Kinetic energy rod warhead with self-aligning penetrators
US7150234B2 (en) * 2004-09-30 2006-12-19 The United States Of America As Represented By The Secretary Of The Army Finless training projectile with improved flight stability over an extended range
US8033890B2 (en) * 2005-05-18 2011-10-11 Warner Jon A Self-propelled hydrodynamic underwater toy
DE102005036574A1 (en) 2005-08-01 2007-02-08 Rheinmetall Waffe Munition Gmbh Projectile with a conical structure
US7568433B1 (en) * 2006-02-22 2009-08-04 The United States Of America As Represented By The Secretary Of The Army Aerodynamically stable finless projectile
US7829829B2 (en) * 2007-06-27 2010-11-09 Kazak Composites, Incorporated Grid fin control system for a fluid-borne object
US8418623B2 (en) 2010-04-02 2013-04-16 Raytheon Company Multi-point time spacing kinetic energy rod warhead and system
US8640625B1 (en) * 2011-08-17 2014-02-04 The United States Of America As Represented By The Secretary Of The Army Kinetic energy training projectile
KR102133740B1 (en) * 2020-02-13 2020-07-14 국방과학연구소 Earth penetrating projectile having enhanced penetration movement stability

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3955509A (en) * 1969-03-21 1976-05-11 The United States Of America As Represented By The United States Energy Research And Development Administration Fuel-air munition and device
US4251079A (en) * 1978-07-03 1981-02-17 Earl Hugh E Pellet for an air, gas or spring gun
US4779535A (en) * 1987-10-16 1988-10-25 Nagatoshi Maki Slug assembly for shotgun shotshell
US4909152A (en) * 1987-08-08 1990-03-20 Mauser-Werke Oberndorf Gmbh Cartridge for the expulsion of liquids under pressure
US5148750A (en) * 1981-12-24 1992-09-22 Rheinmetall Gmbh Unitary projectile

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1067754A (en) * 1976-08-16 1979-12-11 Maurice A. Laviolette Modular practice bomb
DE2747313C2 (en) * 1977-10-21 1983-01-20 Rheinmetall GmbH, 4000 Düsseldorf Sub-caliber arrow projectile with a resistance-stabilizing conical tail section
DE3205612A1 (en) * 1982-02-17 1983-09-08 Mauser-Werke Oberndorf Gmbh, 7238 Oberndorf SHELL FOR TRAINING AMMUNITION
US4428294A (en) * 1982-08-16 1984-01-31 The United States Of America As Represented By The Secretary Of The Army Finless gun-fired practice round
DE3615585C1 (en) * 1986-05-09 1991-02-28 Rheinmetall Gmbh Projectile for firing from an electromagnetic projectile acceleration device
DE3933534C2 (en) * 1989-10-07 1995-01-19 Diehl Gmbh & Co Practice bullet for target shooting without explosives with large-caliber weapons
US5070791A (en) * 1990-11-30 1991-12-10 The United States Of America As Represented By The Secretary Of The Army Projectile tail cone
US5228855A (en) * 1992-03-31 1993-07-20 Ffe International Mortar training ammunition device having independently rotatable vent closure rings

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3955509A (en) * 1969-03-21 1976-05-11 The United States Of America As Represented By The United States Energy Research And Development Administration Fuel-air munition and device
US4251079A (en) * 1978-07-03 1981-02-17 Earl Hugh E Pellet for an air, gas or spring gun
US5148750A (en) * 1981-12-24 1992-09-22 Rheinmetall Gmbh Unitary projectile
US4909152A (en) * 1987-08-08 1990-03-20 Mauser-Werke Oberndorf Gmbh Cartridge for the expulsion of liquids under pressure
US4779535A (en) * 1987-10-16 1988-10-25 Nagatoshi Maki Slug assembly for shotgun shotshell

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP0769127A4 *

Also Published As

Publication number Publication date
KR970705000A (en) 1997-09-06
AU2645295A (en) 1996-02-09
JPH09512897A (en) 1997-12-22
EP0769127A1 (en) 1997-04-23
CA2194549C (en) 2001-12-11
US5498160A (en) 1996-03-12
KR100223259B1 (en) 1999-10-15
CA2194549A1 (en) 1996-01-25
EP0769127A4 (en) 1997-07-02

Similar Documents

Publication Publication Date Title
US5498160A (en) Training projectile
US4612860A (en) Projectile
GB2033556A (en) Dummy projectile
KR970705003A (en) Aerodynamically stabilized launch system for use in underwater objects
ATE235038T1 (en) BULLET WITH IMPROVED FLYING PROPERTIES
US4334657A (en) Device for fin-stabilized shell or the like
US4075946A (en) Armor piercing projectile
US5725179A (en) Expansion wave spin inducing generator
KR20040011552A (en) Artillery projectile comprising an interchangeable payload
WO2006091232B1 (en) A finless training projectile with improved flight stability over an extended range
US8123637B1 (en) Stun projectile for a blow gun
US5125344A (en) Limited range training projectile
US4337911A (en) Non-spinning projectile
US5476045A (en) Limited range projectile
US11118879B2 (en) Projectile for firearms
SE8200194L (en) CHARGE
US4961384A (en) Hypervelocity penetrator for an electromagnetic accelerator
DE4022462C2 (en)
GB2032070A (en) Cartridges
US4022103A (en) Gas dynamic sabot stripper
US11236976B2 (en) Arrowhead
US5501155A (en) Hollow training round
US5798479A (en) Undersized kinetic-energy practice projectile of the dart type
US20190234719A1 (en) Multi-segmented shaft
EP0270527B1 (en) Armour piercing projectile

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AT AU CA CH CN DE DK ES FI GB JP KR LU MX NO PT SE SG US

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FR GB GR IE IT LU MC NL PT SE

121 Ep: the epo has been informed by wipo that ep was designated in this application
DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
WWE Wipo information: entry into national phase

Ref document number: 1995921348

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2194549

Country of ref document: CA

Ref document number: 1019970700061

Country of ref document: KR

WWP Wipo information: published in national office

Ref document number: 1995921348

Country of ref document: EP

REG Reference to national code

Ref country code: DE

Ref legal event code: 8642

WWP Wipo information: published in national office

Ref document number: 1019970700061

Country of ref document: KR

WWR Wipo information: refused in national office

Ref document number: 1995921348

Country of ref document: EP

WWW Wipo information: withdrawn in national office

Ref document number: 1995921348

Country of ref document: EP

WWG Wipo information: grant in national office

Ref document number: 1019970700061

Country of ref document: KR