GB572791A - Improvements in or relating to delaying mechanisms for use on projectiles - Google Patents
Improvements in or relating to delaying mechanisms for use on projectilesInfo
- Publication number
- GB572791A GB572791A GB1635741A GB1635741A GB572791A GB 572791 A GB572791 A GB 572791A GB 1635741 A GB1635741 A GB 1635741A GB 1635741 A GB1635741 A GB 1635741A GB 572791 A GB572791 A GB 572791A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lever
- mass
- tail
- disc
- clockwise
- 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
- F42C11/00—Electric fuzes
-
- 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
- F42C15/24—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by inertia means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C9/00—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
- F42C9/02—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by mechanical means
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Abstract
572,791. Projectile fuzes. WEST & CO., Ltd., A., and BREEZE, V. L. Dec. 18, 1941, No. 16357. [Class 9 (i)] Fuzes for projectiles which accelerate for a considerable period, e.g. self-propelled rockettype projectiles, comprise means for delaying arming of the fuze until the acceleration has fallen to a given value. In the construction shown, the arming of the fuze is accomplished with two pairs of fixed contacts 9 which are bridged by two contacts 10. Prior to discharge of the projectile, the parts are in the position shown. Each contact 10 is mounted on a lever 11 which is pivoted at 11a and pulled clockwise by a spring 5 anchored to the vertical arm of a bell-crank lever 3. The horizontal arm of the lever 3 abuts the lever 11 and holds the contact 10 away from the contacts 9. The lever 3 is and fixed on the shaft, between the plates, is a mass 6. It is to be assumed in the drawings that the projectile travels upwardly. When the projectile is discharged and accelerates, the mass 6 moves downwards by inertia and thus rotates the shaft 7 and disc 8 anti-clockwise. When the disc 8 has moved through 90 degrees, an opening 12 in the disc is opposite the tail 3a, so that the tail may drop into the opening and the lever 3 may rock clockwise to allow the contact 9, 10 to be made ; but the tail does not immediately drop into the opening, for the horizontal arm of the lever 3 also is held back by inertia. When the acceleration drops to a certain value, the spring 5 rocks the lever 3 clockwise and the contact 9, 10 is made. A safety device which ensures that the mass 6 will not move downwardly when the device is dropped, comprises a fly-wheel 13 so geared to the shaft 7 that as the shaft rotates slowly the fly-wheel moves rapidly. This device may be replaced by an air dashpot. The mass 6 is biassed to the normal position by a light spring 14. When the mass 6 reaches its permissive (opening-opposite-tail) position, it is latched there by a spring 15 which engages a recess 16 in the mass. The members 3 also may be latched-in after they have moved clockwise. In modified arrangements, (a) a circuit normally established may be interrupted by movement of the tail away from the disc 8 ; (b) the radius of that part of the surface of the disc 8 extending between the tail 3a and the opening 12 may increase, thus providing a delay additional to that caused by the fly-wheel 13. The elements 3, 8, 9, 10, 11 are duplicated on each side of the mass 11. The device is mounted on a base 1.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1635741A GB572791A (en) | 1941-12-18 | 1941-12-18 | Improvements in or relating to delaying mechanisms for use on projectiles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1635741A GB572791A (en) | 1941-12-18 | 1941-12-18 | Improvements in or relating to delaying mechanisms for use on projectiles |
Publications (1)
Publication Number | Publication Date |
---|---|
GB572791A true GB572791A (en) | 1945-10-24 |
Family
ID=10075837
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1635741A Expired GB572791A (en) | 1941-12-18 | 1941-12-18 | Improvements in or relating to delaying mechanisms for use on projectiles |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB572791A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1172994B (en) * | 1961-11-30 | 1964-06-25 | Jean Rochat | Electric ignition device for projectiles |
-
1941
- 1941-12-18 GB GB1635741A patent/GB572791A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1172994B (en) * | 1961-11-30 | 1964-06-25 | Jean Rochat | Electric ignition device for projectiles |
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