GB535579A - Improvements in or relating to percussion fuzes for projectiles - Google Patents
Improvements in or relating to percussion fuzes for projectilesInfo
- Publication number
- GB535579A GB535579A GB27548/39A GB2754839A GB535579A GB 535579 A GB535579 A GB 535579A GB 27548/39 A GB27548/39 A GB 27548/39A GB 2754839 A GB2754839 A GB 2754839A GB 535579 A GB535579 A GB 535579A
- Authority
- GB
- United Kingdom
- Prior art keywords
- projectile
- gyroscopic
- axis
- striker
- washer
- 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
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/16—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the firing pin is displaced out of the action line for safety
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C15/00—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
- F42C15/20—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin
- F42C15/22—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin using centrifugal force
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
535,579. Ammunition projectiles. PATCHETT, G. W. Oct. 9, 1939, No. 27548. [Class 9 (i)] Relates to percussion fuzes of the kind in which a striker is moved into alignment with an ignition cap by the action of a gyroscopic element rotated by frictional engagement with the projectile and serving to arm the fuze during flight. According to the invention, the gyroscopic element is so mounted in the projectile that in addition to the usual three degrees of freedom of movement it has a further movement in a direction along the axis of the projectile. In the form shown in Fig. 1, the gyroscopic element 16 carrying the striker 18 is assembled with its axis inclined, the lower end resting on a washer 19 having a central aperture leading to the percussion cap of the detonator 15. The element has concentric spherical surfaces 20, 21 engaging a spherical abutment face 23 on a hollow impact member 24 the forward movement of which is restrained by centrifugal spring members 29. On firing, the rotation of the projectile causes release of the members 29 and during acceleration the member 24 presses on the element 16 and imparts spin so that during deceleration, when the member 24 moves forward, this element can move to bring its axis into line with the axis of the projectile. On impact, the member 24 is forced inwards to move the striker into engagement with the percussion cap. In the modification shown in Fig. 2, the gyroscopic element is set with the striker pin 40 at right angles to the axis of the projectile and is retained by a washer 42 which sets back on discharge. The impact member 24 also moves rearwardly during acceleration to retain the gyroscopic element in frictional engagement with the washer. When deceleration occurs, the member 24 moves forwardly and the gyroscopic member precesses until the pin 40 is in line with the axial percussion cap. The gyroscopic member is in the form of two interfitting discs 39 enclosing a central gapped loading disc 43.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB27548/39A GB535579A (en) | 1939-10-09 | 1939-10-09 | Improvements in or relating to percussion fuzes for projectiles |
US360321A US2322543A (en) | 1939-10-09 | 1940-10-08 | Percussion fuse for projectiles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB27548/39A GB535579A (en) | 1939-10-09 | 1939-10-09 | Improvements in or relating to percussion fuzes for projectiles |
Publications (1)
Publication Number | Publication Date |
---|---|
GB535579A true GB535579A (en) | 1941-04-15 |
Family
ID=10261384
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB27548/39A Expired GB535579A (en) | 1939-10-09 | 1939-10-09 | Improvements in or relating to percussion fuzes for projectiles |
Country Status (2)
Country | Link |
---|---|
US (1) | US2322543A (en) |
GB (1) | GB535579A (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2682835A (en) * | 1951-11-28 | 1954-07-06 | Us Army | Delay arming device |
US3264995A (en) * | 1964-05-11 | 1966-08-09 | Avco Corp | Mechanical fuze operable on grazing impact |
-
1939
- 1939-10-09 GB GB27548/39A patent/GB535579A/en not_active Expired
-
1940
- 1940-10-08 US US360321A patent/US2322543A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US2322543A (en) | 1943-06-22 |
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