GB125817A - Improvements in and relating to Projectiles. - Google Patents

Improvements in and relating to Projectiles.

Info

Publication number
GB125817A
GB125817A GB967718A GB967718A GB125817A GB 125817 A GB125817 A GB 125817A GB 967718 A GB967718 A GB 967718A GB 967718 A GB967718 A GB 967718A GB 125817 A GB125817 A GB 125817A
Authority
GB
United Kingdom
Prior art keywords
projectiles
fin
shell
relating
groove
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
Application number
GB967718A
Inventor
John Mathius Kaylor
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 GB967718A priority Critical patent/GB125817A/en
Priority to FR496758D priority patent/FR496758A/en
Publication of GB125817A publication Critical patent/GB125817A/en
Expired legal-status Critical Current

Links

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
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Orthopedics, Nursing, And Contraception (AREA)

Abstract

125,817. Kaylor, J. M. June 12, 1918. Ordnance design.-Relates to guns for use with winged projectiles. According to the invention, the gun, shown in section in Fig. 5, has along the bottom of its bore 2 a longitudinal groove 31 to receive a stabilizing-fin on the projectile. The purpose of the groove is to ensure that when the shell is discharged the fin is in a vertical position and a pair of sustaining-wings, projected through the shell-body by springs, are horizontal.
GB967718A 1918-06-12 1918-06-12 Improvements in and relating to Projectiles. Expired GB125817A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB967718A GB125817A (en) 1918-06-12 1918-06-12 Improvements in and relating to Projectiles.
FR496758D FR496758A (en) 1918-06-12 1918-06-27 Projectile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB967718A GB125817A (en) 1918-06-12 1918-06-12 Improvements in and relating to Projectiles.

Publications (1)

Publication Number Publication Date
GB125817A true GB125817A (en) 1919-05-01

Family

ID=32343855

Family Applications (1)

Application Number Title Priority Date Filing Date
GB967718A Expired GB125817A (en) 1918-06-12 1918-06-12 Improvements in and relating to Projectiles.

Country Status (2)

Country Link
FR (1) FR496758A (en)
GB (1) GB125817A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1199664B (en) * 1962-09-11 1965-08-26 Dynamit Nobel Ag Folding tail, especially for rocket projectiles

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1428717C2 (en) * 1964-09-28 1974-05-30 Dynamit Nobel Ag Tail fairing for rockets with central nozzle and folding tail
DE2457503C2 (en) * 1974-12-05 1984-11-29 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Infantry bullet
US5150861A (en) * 1990-01-26 1992-09-29 The Boeing Company Variable sweep side force generator and roll control device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1199664B (en) * 1962-09-11 1965-08-26 Dynamit Nobel Ag Folding tail, especially for rocket projectiles

Also Published As

Publication number Publication date
FR496758A (en) 1919-11-15

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