US2438438A - Bomb detonating mechanism - Google Patents
Bomb detonating mechanism Download PDFInfo
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- US2438438A US2438438A US514439A US51443943A US2438438A US 2438438 A US2438438 A US 2438438A US 514439 A US514439 A US 514439A US 51443943 A US51443943 A US 51443943A US 2438438 A US2438438 A US 2438438A
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- bomb
- release
- firing
- responsive
- detonating
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C5/00—Fuzes actuated by exposure to a predetermined ambient fluid pressure
- F42C5/02—Fuzes actuated by exposure to a predetermined ambient fluid pressure barometric pressure
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- 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
- F42C9/14—Double fuzes; Multiple fuzes
- F42C9/141—Impact fuze in combination with a clockwork time fuze
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Emergency Lowering Means (AREA)
Description
23, 1948. J. H. HAMMOND, JR 7 2,438,433
BOMB DETONATING MECHANISM Filed Dec. 16, 1943 INVENTOR JOHN HAY5 HAMMOND, JR.
Patented Mar. 23,, 1948 UNITED STATES ATENT OFFICE BOMB DETONATING MECHANISM John Hays Hammond, Jr., Gloucester, Mass. Application December 16, 1943, Serial No. 514,439
7 Claims. 1
This invention relates-to projectiles and more particularly to bombs provided with concussion detonating devices.
An object of this invention is to provide a bomb with a device which will cause the bomb to explode by the concussion produced by the explosion of another bomb.
A further object of the invention is to provide a bomb with a delay action device which will make the concussion operated mechanism inactive for a predetermined time after the bomb has struck its target.
Another object of the invention is to provide means for exploding the bomb a predetermined time after it has struck the target irrespective of the operation of the concussion operated mechanism.
The invention also consists in certain new and original features of constructions and combinations of parts hereinafter set forth and claimed.
Although the novel features which are believed to be characteristic of this invention will be particularly pointed out in the claims appended hereto, the invention itself, as to its objects and advantages, the mode of its operation and the manner of its organization may be better understood by referring to the following description taken in connection with the accompanying drawings forming a part thereof, in which The single figure is a side elevation, partl in section, of a bomb constructed in accordancewith the invention.
In the following description parts will be identified by specific terms for convenience, but they are intended to be as generic in their application to similar parts as the art will permit.
Referring to the accompanying drawing a bomb H is provided with a rotatable cap l2 having a slot I3 and a mark M which registers with a scale 15 graduated in seconds. Secured to the rotatable cap 12 is a shaft I6 to which is attached an arm I! made of material which will be permanently deformed when bent. Fastened to the arm I! is a weight I 8 and apin I9, the latter engaging a slot in an arm 2| which is secured to a disc 22. The disc 22 is rotatably mounted on a shaft 23 which has a bearing in a cross member 24. A friction cap 25 is mounted on the shaft 23 and tends to hold the disc 22 in any desired position.
Also secured to the shaft 23 are a gear 29 and a cam 26, having a notch 21, a coiled spring 28 is attached between the shaft 23 and a projection 3! on the cross member 24.
The disc 22 is provided with a notch 32 which at suitable times is engaged by a pin 33 mounted on an arm 34. The arm 34 is secured to one end of a shaft 35, which has a bearing in the cross member 24 and carries on its lower end a detent 36. A tension spring 31 is attached to the detent 36 and tends to rotate it, together with the arm 34, in a clockwise direction as seen from above. 1
The detent 36 engages a collar 38 attached to a rod 39 which is slidably mounted in a bracket 4! on the cross member 24. A compression spring 42 is provided which tends to move the rod 39 to the left. The rod 39 engages a pawl 43 which is rotatably mounted on a bracket 44. A spring 45 presses against the pawl 43 and tends to hold it in engagement with th rod 39 and with a stud 43 which is mounted on a diaphragm 41. The diaphragm 41 is mounted in an opening 48 provided in the side of the bomb l l.
(Io-operating with the cam 25 is a pin 5| secured to an arm 52 which is mounted on the end of ashaft 53. The shaft 53 is rotatably mounted in the cross member 24 and carries a detent 54 which engages a collar 55 secured to a rod 56 which is slidably mounted in cross members 22 and 51. A tension spring 58 tends to rotate the arm 52 and detent 54 in a counterclockwise direction as seen from above. A second .collar 59 is secured to the rod 56 the lower end of which forms a firing pin 6|, which when released fires the primer 62 which in turn detonates the explosive charge 63. A compression spring 65 mounted between the collar 59 and the cross member 24 tends to move the rod 56 downward.
Meshing with the gear 29 is a pinion 55 secured to a shaft 66 which is rotatably mounted in brackets 51 and 68. Secured to the shaft 65 is a second gear 69 which meshes with a, second pinion 1! mounted on a shaft 12 which is journaled in the bracket 68. Attached to the shaft 12 is an escapement ratchet 13 which co-operates with an escapement pawl 14 mounted on a shaft 15 which is journaled in the cross member 5?, Attached to the shaft 15 is one end of an escapement spring 16 the other end of which is secured to a lug Tl on the cross member 51. Weights 18 are screwed on to threaded extensions 19 of the escapement pawl 14.
In the operation of the bomb shown in the accompanying figure the cap I2 is rotated in a counterclockwise direction by inserting a tool in the slot 13 until the mark l4 registers with the designation on the scale l5 of the number of seconds time delay that it is desired to have. The rotation of the cap l2 causes the arm I! to be rotated which in turn causes the arm 2| and disc 22 to be rotated a like amount. The disc 22 is allowed to rotate with respect to the shaft 23 due to the action of the friction cap 25.
When the bomb is dropped and strikes its target the weight [8 will bend the arm which will remain bent, thus releasing the pin I9 from the arm 2|. The shaft 23 is then free to turn in a clockwise direction, as seen from above under the action of the spring 28, carrying with it the discs 22 and 26 and the gear 29. The gear 29, by means of the gear train 65, 69, 1| drives the escapement 1314 in a well-known manner; so that the shaft 23 rotates at a predetermined speed dependent on the position of the weights [8 on the threaded arms 19.
After the cam 26 has rotated thru a small angle the pin will drop into the notch 21 which will allow the detent 54 to be rotated in a counterclockwise direction under the action of the spring 58. This will release the collar 55 but the shaft 56 will not move as it is prevented from so doing by the pawl 43 engaging the collar 59.
If an adjacent bomb explodes the concussion transmitted thru the air will force the diaphragm 41 inward which by means of the stud 46 will cause the pawl 43 to be rotated in a counterclockwise direction thus releasing the collar 59. The rod 56 will then be forced downward under the action of the spring 64 which will cause the firing pin 6| to strike the detonator 62 thus exploding the explosive charge 63.
If no adjacent bomb explodes the shaft 23 will continue to slowly turn until the pin 33 drops into the notch 32 of the disc 22. This will allow the detent 36 to be rotated in a clockwise direction under the action of the spring 31, thus releasing the collar 36. This will allow the rod 39 to be moved to the left under the action of the spring 42 which will push the pawl 43 outof engagement with the collar 59. This as previously described causes the detonation of the explosive charge 63.
It is thus seen that this invention provides a bomb which will be held inactive for a predetermined time after it strikes the target after which it will be exploded by the concussion produced by the exploding of adjacent bombs. If no adjacent bombs explode the bomb itself will explode after a second predetermined interval of time.
It has been found in bombing that the greatest effect is produced when a salvo of bombs explode simultaneously. This effect is produced by the present invention for when a salvo of bombs is dropped the time mechanism of the first bomb to strike the target is started and as the successive bombs strike their time mechanisms are successively started. Each of the bombs then becomes alive in succession and lies on the target until the time mechanism of the first bomb causes it to explode, as already described. The concussion of the explosion of the first bomb will, therefore, cause the explosion of all the bombs in the salvo simultaneously thus'producing the maximum destructive effect.
Although only a specific embodiment of this invention has been shown herein, it is to be understood that the invention is not limited thereto but may be embodied in various forms without departing from the spirit of the invention as defined by the appended claims.
I claim:
1. A bomb firing mechanism comprising detonating mechanism, restraining means to prevent actuation thereof, mechanism responsive to external compressional waves, means actuated by said last mechanism to release said restraining means for firing said bomb, holding means rendering said detonating mechanism inoperative, timed means to release said holding means for rendering said bomb responsive to said compression responsive mechanism, and means responsive to impact connected to start said timed means in operation.
2. A bomb firing mechanism comprising detonating mechanism, locking means for said detonating mechanism, timed means to release said locking means, additional holding means to hold said detonating mechanism against operation, a diaphragm responsive to external compressional waves, and means actuated by said diaphragm to release said holding means for firing said bomb, and means responsive to impact connected to start said timed means in operation.
3. A bomb firing mechanism comprising detonating mechanism, restraining means to prevent actuation thereof, mechanism responsive to external compressional waves, release means actuated by said last mechanism to release said restraining means for firing said bomb, timed means to actuate said release means independently of said last mechanism, and means responsive to impact connected to start said timed means in operation.
4. A bomb firing mechanism comprising detonating mechanism, restraining means to prevent actuation thereof, mechanism responsive to external compressional waves, means actuated by said last mechanism to release said restrainin means for firing said bomb, additional holding means rendering said detonating mechanism inoperative, timed means to release said holding means for rendering said bomb responsive to said compression responsive mechanism, timed means to release said restraining means for firing said bomb after a predetermined time, and means responsive to impact connected to start both of said timed means in operation.
5.-A bomb firing mechanism comprising detonating mechanism, restraining means to prevent actuation thereof, mechanism responsive to external compressional waves, means actuated by said last mechanism to release said restraining means for firing said bomb, additional holding means rendering said detonating mechanism inoperative, timed means to release said holding means for rendering said bomb responsive to said compression responsive mechanism, timed means to release said restraining means for firing said bomb after a predetermined time, means setting said last timed means for controlling the extent of time delay produced thereby, and means responsive to impact connected to start both of said timed means in operation.
6. A bomb firing mechanism comprising detonating mechanism, locking means for said detonating mechanism, timed means to release said locking means, additional holding means to hold said detonating mechanism against operation, a diaphragm responsive to external compressional Waves, means actuated by said diaphragm to release said holding means for firing said bomb, means actuated by said timed means to release said holding means for firing said bomb after a predetermined time, and means responsive to impact connected to start both of said timed means in operation.
7. A bomb firing mechanism comprising detonating mechanism, locking mean for said detonating mechanism, timed means to release said 5 locking means, additional holding means to hold said detonating mechanism against operation, a diaphragm responsive to external compressional Waves, means actuated by said diaphragm to release said holding means for firing said bomb, means actuated by said timed means to release said holding means for firing said bomb after a predetermined time, means setting said last means to control the time delay introduced Number thereby, and means responsive to impact con- 10 Number nected to start said timed means in operation.
JOHN HAYS HAMMOND, JR.
REFERENCES CITED UNITED STATES PATENTS Name Date Leon Apr. 27, 1915 Dunlop Aug. 15, 1916 Bold Aug. 16, 1927 Barkley Feb. 8, 1944 FOREIGN PATENTS Country Date Italy Dec. 4, 1939 Great Britain Aug. 3, 1933 Great Britain July 18, 1941 file of this patent:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US514439A US2438438A (en) | 1943-12-16 | 1943-12-16 | Bomb detonating mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US514439A US2438438A (en) | 1943-12-16 | 1943-12-16 | Bomb detonating mechanism |
Publications (1)
Publication Number | Publication Date |
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US2438438A true US2438438A (en) | 1948-03-23 |
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Application Number | Title | Priority Date | Filing Date |
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US514439A Expired - Lifetime US2438438A (en) | 1943-12-16 | 1943-12-16 | Bomb detonating mechanism |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2514499A (en) * | 1946-03-22 | 1950-07-11 | Us Sec War | Delay action fuse |
US2669929A (en) * | 1947-03-13 | 1954-02-23 | George O Shull | Safety device |
US2913984A (en) * | 1957-11-20 | 1959-11-24 | James M Meek | Safety and arming device having remotely located rotor actuating means |
US2958282A (en) * | 1956-11-14 | 1960-11-01 | Czajkowski Norman | Programming device for a projectile |
US3286632A (en) * | 1964-06-30 | 1966-11-22 | Jr James H Potts | Dual time option mechanical fuze |
US3329091A (en) * | 1965-08-17 | 1967-07-04 | Mitchell G Angelos | Pressure responsive mechanical firing device |
US4207626A (en) * | 1954-06-07 | 1980-06-10 | The United States Of America As Represented By The Secretary Of The Navy | Acoustic decoy and jammer |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1137222A (en) * | 1908-02-11 | 1915-04-27 | Leon Steering Device Company | Torpedo and other submarine apparatus. |
US1194726A (en) * | 1916-08-15 | Submarine bomb | ||
US1639075A (en) * | 1923-12-03 | 1927-08-16 | Charles H Pearson | Aerial-bomb fuse |
GB396171A (en) * | 1932-04-11 | 1933-08-03 | Helmut Junghans | Fuse for anti-aircraft shells |
GB538049A (en) * | 1939-01-18 | 1941-07-18 | Eric George Fisher | Improvements in or relating to fuzes for projectiles |
US2341351A (en) * | 1941-05-15 | 1944-02-08 | Barkley Joseph Amos | Aerial mine |
-
1943
- 1943-12-16 US US514439A patent/US2438438A/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1194726A (en) * | 1916-08-15 | Submarine bomb | ||
US1137222A (en) * | 1908-02-11 | 1915-04-27 | Leon Steering Device Company | Torpedo and other submarine apparatus. |
US1639075A (en) * | 1923-12-03 | 1927-08-16 | Charles H Pearson | Aerial-bomb fuse |
GB396171A (en) * | 1932-04-11 | 1933-08-03 | Helmut Junghans | Fuse for anti-aircraft shells |
GB538049A (en) * | 1939-01-18 | 1941-07-18 | Eric George Fisher | Improvements in or relating to fuzes for projectiles |
US2341351A (en) * | 1941-05-15 | 1944-02-08 | Barkley Joseph Amos | Aerial mine |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2514499A (en) * | 1946-03-22 | 1950-07-11 | Us Sec War | Delay action fuse |
US2669929A (en) * | 1947-03-13 | 1954-02-23 | George O Shull | Safety device |
US4207626A (en) * | 1954-06-07 | 1980-06-10 | The United States Of America As Represented By The Secretary Of The Navy | Acoustic decoy and jammer |
US2958282A (en) * | 1956-11-14 | 1960-11-01 | Czajkowski Norman | Programming device for a projectile |
US2913984A (en) * | 1957-11-20 | 1959-11-24 | James M Meek | Safety and arming device having remotely located rotor actuating means |
US3286632A (en) * | 1964-06-30 | 1966-11-22 | Jr James H Potts | Dual time option mechanical fuze |
US3329091A (en) * | 1965-08-17 | 1967-07-04 | Mitchell G Angelos | Pressure responsive mechanical firing device |
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