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
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.
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)
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)
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 |
-
1918
- 1918-06-12 GB GB967718A patent/GB125817A/en not_active Expired
- 1918-06-27 FR FR496758D patent/FR496758A/en not_active Expired
Cited By (1)
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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