GB112718A - Improvements in Projectiles. - Google Patents
Improvements in Projectiles.Info
- Publication number
- GB112718A GB112718A GB712717A GB712717A GB112718A GB 112718 A GB112718 A GB 112718A GB 712717 A GB712717 A GB 712717A GB 712717 A GB712717 A GB 712717A GB 112718 A GB112718 A GB 112718A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wings
- projectile
- hinge
- rings
- flight
- 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
- F42B10/16—Wrap-around fins
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
112,718. Haines, G. B., and Duffield, G. B. May 17, 1917. Projectiles.-Consists in providing a projectile with two or more pivoted wings, so arranged as to be automatically extensible during flight to support the projectile in the air. Figs. 1 and 4 show a projectile adapted to be fired from a smooth-bore gun, wings D, D<1> being hinged longitudinally so that normally they fold around the body A, as shown. In flight, the wings are extended by airpressure under them, and this action may be assisted by springs L. To effect a further spreading of the wings, each one may be made in two sections, hinged together. The wings may be geared together. In a further modification, the axis of the hinge of the wings may be slightly inclined to the longitudinal axis of the projectile by adjusting the forward end of the hinge in a radial direction, the object being to attain a greater lifting-power. Fig. 7 shows the invention applied to a projectile for a rifled gun. The wings D are carried by rings H, I mounted on ball bearings. A collapsible vane K is secured to the ring H, to prevent rotation of the rings due to friction.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB712717A GB112718A (en) | 1917-05-17 | 1917-05-17 | Improvements in Projectiles. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB712717A GB112718A (en) | 1917-05-17 | 1917-05-17 | Improvements in Projectiles. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB112718A true GB112718A (en) | 1918-01-24 |
Family
ID=32246360
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB712717A Expired GB112718A (en) | 1917-05-17 | 1917-05-17 | Improvements in Projectiles. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB112718A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3724373A (en) * | 1970-12-15 | 1973-04-03 | Atomic Energy Commission | Retarded glide bomb |
US4165847A (en) * | 1976-06-25 | 1979-08-28 | Societe Europeenne De Propulsion | Tail unit for a missile |
US5816531A (en) * | 1997-02-04 | 1998-10-06 | The United States Of America As Represented By The Secretary Of The Army | Range correction module for a spin stabilized projectile |
US5826821A (en) * | 1997-08-04 | 1998-10-27 | The United States Of America As Represented By The Secretary Of The Army | Drag control module for range correction of a spin stabil |
EP2539666A4 (en) * | 2010-02-25 | 2015-05-06 | Bae Systems Bofors Ab | Shell arranged with extensible wings and guiding device |
-
1917
- 1917-05-17 GB GB712717A patent/GB112718A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3724373A (en) * | 1970-12-15 | 1973-04-03 | Atomic Energy Commission | Retarded glide bomb |
US4165847A (en) * | 1976-06-25 | 1979-08-28 | Societe Europeenne De Propulsion | Tail unit for a missile |
US5816531A (en) * | 1997-02-04 | 1998-10-06 | The United States Of America As Represented By The Secretary Of The Army | Range correction module for a spin stabilized projectile |
US5826821A (en) * | 1997-08-04 | 1998-10-27 | The United States Of America As Represented By The Secretary Of The Army | Drag control module for range correction of a spin stabil |
EP2539666A4 (en) * | 2010-02-25 | 2015-05-06 | Bae Systems Bofors Ab | Shell arranged with extensible wings and guiding device |
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