US2485817A - Detonator safety device - Google Patents
Detonator safety device Download PDFInfo
- Publication number
- US2485817A US2485817A US483303A US48330343A US2485817A US 2485817 A US2485817 A US 2485817A US 483303 A US483303 A US 483303A US 48330343 A US48330343 A US 48330343A US 2485817 A US2485817 A US 2485817A
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- United States
- Prior art keywords
- arm
- safety
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- housing
- 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 - Lifetime
Links
- 238000004880 explosion Methods 0.000 description 11
- 239000004020 conductors Substances 0.000 description 9
- 238000010438 heat treatment Methods 0.000 description 8
- 230000000903 blocking Effects 0.000 description 6
- 281000152478 Thermo Fisher Scientific companies 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical compound 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[C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 238000007906 compression Methods 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006011 modification reactions Methods 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 231100000817 safety factors Toxicity 0.000 description 1
- 229910000679 solders Inorganic materials 0.000 description 1
Images
Classifications
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- 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
- F42C15/34—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by a blocking-member in the pyrotechnic or explosive train between primer and main charge
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- 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
- F42C15/36—Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein arming is effected by combustion or fusion of an element; Arming methods using temperature gradients
Description
Ot. 25, 1949. s. H. DIKE: 2,485,817
DETONATOR SAFETY DEVICE Filed April 16, 1943 43 NNNNNN 0R SHE'LDON H. D/KE Patented Oct. 25, 1949 UNITED STATES PATENT GFFICE DETONATOR SAFETY DEVICE Sheldon H. Dike, Ventnor, N. J., assigner to the United States of America as represented by the Secretary of the Navy Application April 16, 1943, Serial No. 483,303
(C1. IGZ-70.2)
4 Claims.
This invention relates to safety devices for use with the detonator in an explosive projectile of the type which rotates during its ight. More particularly, the invention has reference -to a novel safety device for this purpose including a control member movable between safe and armed positions by centrifugal force and which is normally secured in its safe position by means operable electrically with a time delay to release the member. The new safety device is simple and compact in construction and provides a high safety factor.
One object of the invention resides in the provision o f a novel safety device including a control member whch is normally held in a safe position by fusible means operable electrically to release the member after the projectile is red from a gun. The control member may be arranged to control a suitable safety element, such as a gate in the explosion discharge passage of the detonator or a switch in a detonating circuit, or lboth. A safety device made in accordance with the invention comprises a housing containing a control member in the form of a pivoted arm movable between safe and armed positions by centrifugal force, and means including a conductor connected to the arm and latching the arm in its safe position, the latchng means being operable electrically to release the arm. A current source is connected at one side to the latching means and is grounded at the other side to the housing, whereby the current source is in circuit with the arm and the latching means. The circuit is normally open and is designed to be closed by a switch responsive to iring the projectile from the gun, so that the latching means is operated to release the arm. Preferably, the control arm when released operates a switch inthe detonating circuit to explode the detonator and also retracts a latch for permitting a safety gate to move from the explosion discharge passage of the detonator.
Another object of the invention is to provide a novel safety detonator for rotary projectiles which is positive and reliable in operation and provides a time delay in arming the detonator.
These and other objects of the invention may be understood by reference to the accompanying drawing, in which Fig. 1 is a front view of one form of the new safety device, the housing and the insulating block being in section, to show the channels therein clearly;
Figs, 2 and 3 are longitudinal sectional views on the lines 2-2 and 3-3, respectively, in Fig.
2 1, the insulating block being omitted in Fig. 3;
Fig. 4 is a transverse sectional view on the line 4 4 in Fig. 2;
Fig. 5 is a perspective view of the safety gate shown in Figs. 2, 3 and 4, and
Fig. 6 is a schematic view of the device showing the electrical connections.
The new safety device is illustrated in a form suitable for use in a radio-controlled proximity fuze of the type disclosed in a copending application of M. A. Tuve et al., Serial No. 471,388, led January 6, 1943, although it will be understood that the device may take other forms. Referring to the drawing, the device there shown comprises a cylindrical housing I0 having an externally threaded course II on its front end portion so that the housing may be screwed into the usual can (not shown) for containing the parts of the proximity fuze in the projectile casing. At its rear end, the housing has an external flange I2 designed to engage the end of the can when the housing is screwed tightly therein. A threaded chamber I3 is formed in the rear end of the housing to receive the usual booster (not shown) for detonating the main charge in the main charge in the projectile casing. Intermediate its ends, the housing has a transverse bore, forming a cylinder I4 closed at its outer end by a threaded plug I5, the cylinder communicating with the booster chamber I3 through an explosion discharge passage I6 disposed axially of said chamber. A second cylinder I8 extends transversely of the housing at right angles to the cylinder I4 and contains an electrically operable squib I9. The inner end of the squib cylinder I8 terminates adjacent one side of the cylinder I4 and is separated therefrom by a thin, frangible Wall 20.
A safety gate 22 is slidable in the cylinder I4 and is urged against the inner end thereof by a. compression spring 23 seated on the plug I5, the inner end of the spring being coiled around a projection 22a on the gate for locating the spring in the cylinder I4. Near its inner end, the gate has a transverse notch 24 which normally receives a segment 25 on the rear end of a rotatable shaft 26 extending longitudinally through the housing. In the normal position of the shaft, as shown in Figs. 2 and 4, part of the segment 25 is disposed in the notch 24 so as to lock the gate in its innermost position where it blocks the explosion discharge passage I6. Accordingly, if the squib i9 should accidentally explode, the explosion is prevented from iiring the booster through passage I6. When the shaft 26 is rotated substantially 90, the segment 2,5 is moved completely out of notch 24 and releases the gate.
The shaft 26 terminates in an insulating block 21 secured in a recess 28 in the front of the housing. In its front face, the block 21 is provided With a recess 29 in the form of a sector of a circle, the apex of the recess being offset from the axis of the housing, which corresponds to the axis of rotation of the projectile. The front end of shaft 26 is located in the apex of the recess and has a control arm 3l! secured thereto, the arm being normally held at one end of the recess by a pin 3i which is slidable longitudinally in the insulating block under a force of setback to release the arm. On the free end of the arm 3B is an insulated switch contact 32, and when the arm is released it is movable on the shaft by centrifugal force to the opposite end of the recess where the contact 32 engages a pair of xed contacts 33 and 33a in the block 21.
'Ihe contact 33 is connected through a Wire 34 to a terminal plug 35 in the insulating block which is formed with a suitable groove 36 for receiving the wiring. The plug 35 is designed to t in a suitable socket (not shown) in the adjacent part of the fuze, the socket being connected to the positive side of a battery 31, preferably through a normally open switch 38 which is closed by a force of setback when the projectile is red. The Y other contact 33a is connected to one side of the squib I9 by a wire 4D which extends along the groove 3E, an intersecting groove 4i and an opening 42 in the block 21 and the housing. The other side of the squib is connected to a wire 43 which leads through the opening 42 and a groove 44 in the insulating block to a terminal plug 45 designed to nt in a suitable socket (not shown) connected to the negative side of the battery which is grounded to the housing I0, as shown at 46. Preferably, the squib IS is normally short-circuited by a setback switch 41 connected between the wires 4t and 43 and disposed in a recess 48 which intersects the wiring grooves in the insulating block. The switch 41 may be of any conventional type which is normally closed and opens when subjected to a force of setback incident to firing the projectile.
A recess 50 is formed in the front face of the insulating block and contains a heating element 5 5I here shown as a carbon cylinder. On one end of the cylinder is a fusible head 52 made of eutectic solder, or the like, in which the looped end of a flexible conductor 53 is embedded. The conductor 53 extends from the head 52 along a. groove 54 in the insulating block and is connected to the free end of the control arm 3D. The opposite end of the heating element 5I has a head 55 connected through a conductor 55 to a terminal plug 51 in the insulating block, the plug 51 being designed to fit in a socket (not shown) connected through setback switch 38 to the positive side of the battery.
Normally, the control arm 30 is held in a safe position by the setback-operated detent 3I and conductor 53, and in this position of the arm the gate 22 is locked in its safe position by shaft 25. Also, the detonating circuit is held open because the switch contact 32 is maintained out of engagement with the contacts 33, 33a. It will be understood that if the detent 3I should be operated accidentally, the control arm 3D is still locked in its safe position by the conductor 53, and if the latter should be broken accidentally, the control arm still remains in its safe position for the reason that it can move to its armed position only by the action of centrifugal force. The short-circuiting switch 41 and the setback switch 38 provide additional safety means for preventing premature detonation of the squib I9. The squib is preferably under control of a normally open switch 6D operable by a radio apparatus (not shown) in response to proximity of the projectile to a target, as disclosed in the above-identified application of M. A. Tuve et al.
When the projectile is fired from a gun, the switch 38 closes under the resulting force of setback, and the switch 41 is opened by the force of setback to remove the shortcircuit from squib I9. In addition, the force of setback renders the detent 3I inoperative so that it can no longer prevent movement of control arm 30. Upon closing of switch 38, the heating element 5I is energized by a circuit traceable from the positive side of battery 31 through switch 38, terminal plug 51, the heating element, conductor 53, arm 30, shaft 26, and the housing I Il to the negative side of the battery through the ground connection 46. The carbon cylinder 5I then commences to heat the fusible head 52 which, after a predetermined time interval, becomes suiciently soft to release the looped end of conductor 53. As a result, the arm 3Q is released and swings to the opposite end of recess 29 under the action of centrifugal force incident to rotation of the projectile in its flight. The swinging movement of the arm 33 rotates shaft 23 through substantially 90 so as to release the gate 22 which then moves outwardly under centrifugal force against the spring 23 to clear the explosion discharge passage I6. When the arm 30 approaches its armed position, shown in dotted lines in Fig. 1, it also engages contact 32 with the switch contacts 33, 33a and thereby prepares the detonating circuit traceable from the negative side of battery 31 through plug 45, normally open switch B0, wire 43, squib I9, wire 40, switch 32--33-33a, wire 34, plug 35 and switch 38 to the positive side of the battery. Accordingly, when the switch is closed in response to proximity of the projectile to a target, the squib I9 is exploded and fractures the thin wall 20, the explosion being communicated through discharge passage I6 to the booster in recess I3.
It will be evident that the new safety device may be made in a compact form and is of a relatively simple construction which affords a high factor of safety. The heating element 5I provides a time-delay of a predetermined amount in the arming of the squib I9, and by locking the control arm 30 the heating element serves the dual function of retaining the safety gate 22 in its safe position and maintaining the detonating circuit open at the switch contacts 33, 33a;
Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
What is claimed is:
l. A safety device comprising a safety member movable between operative and inoperative positions, means including a thermo-responsive element for holding said member in its operative position, means for heating the thermo-responsive element t'o release the safety member, said device having an explosion discharge passage therein, a detonating element disposed in said explosiondischarge passage, a gate normally blocking said passage and movable to a position for clearing said passage, and means under control of the safety member for locking the gate in the passage and operable to release the gate on movement of said member to its inoperative position.
2. A safety device comprising a safety member movable between operative and inoperative positions, means including a thermo-responsive element for holding said member in its operative position, means for heating the thermo-responsive element to release the safety member, an electrical detonating element disposed in an explosion discharge passage, a gate normally blocking the passage and movable to a position for clearing the passage, means under control of the safety member for locking the gate in the passage and operable to release the gate on movement of said member to its inoperative position, and a circuit for energizing the detonating element including a switch operable by the safety member.
3. A detonator for rotary projectiles, which comprises a housing, an electrical squib in the housing operable through an explosion discharge passage, a gate normally blocking the passage and movable by centrifugal force to a position for unblocking the passage, a shaft in the housing for locking the gate in its blocking position and rotatable to release the gate, an arm on the shaft operable by centrifugal force to rotate the shaft, means including a conductor connected to the arm for securing the arm against movement to hold the shaft in its locking position, said means being operable electrically to release the arm, a current source connected at one side to said means and grounded at the other side to the housing, whereby the current source is in circuit with the shaft, the arm and said means, a switch responsive to firing of the projectile for closing said circuit to cause said means to release the arm, and a detonating circuit for the squib including a safety switch operable by said arm.
4. A detonator for rotary projectiles, which comprises a housing, having an explosion discharge passage therein, an electrical squib in the housing operable through said passage, a gate normally blocking the passage and movable by centrifugal force to a position for unblocking the passage, a shaft in the housing for locking the gate in its blocking position and movable to release the gate, an arm on the shaft operable by centrifugal force to so move the shaft, means for securing the arm against movement, to hold the shaft in its locking position, said means being operable electrically to release the arm, a source of electricity connected in circuit with the shaft, the arm and said last-named means, a switch responsive to ring of the projectile for closing said circuit to cause said means to release the arm, and a detonating circuit for the squib including a safety switch operable by said arm.
SHELDON H. DIKE.
REFERENCES CITED The following references are of record in the le of this patent:
FOREIGN PATENTS Number Country Date 241,941 Great Britain Nov. 26, 1925 265,797 Italy July 6, 1929 376,987 Italy Dec. 4, 1939
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US483303A US2485817A (en) | 1943-04-16 | 1943-04-16 | Detonator safety device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US483303A US2485817A (en) | 1943-04-16 | 1943-04-16 | Detonator safety device |
Publications (1)
Publication Number | Publication Date |
---|---|
US2485817A true US2485817A (en) | 1949-10-25 |
Family
ID=23919536
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US483303A Expired - Lifetime US2485817A (en) | 1943-04-16 | 1943-04-16 | Detonator safety device |
Country Status (1)
Country | Link |
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US (1) | US2485817A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2920570A (en) * | 1956-12-17 | 1960-01-12 | Albert E Martin | Safety and delay arming device |
US2934016A (en) * | 1957-01-31 | 1960-04-26 | Mountjoy Garrard | Nylon timer |
US2982213A (en) * | 1958-03-28 | 1961-05-02 | William G Meschino | Arming switch |
US3075465A (en) * | 1957-07-23 | 1963-01-29 | Magnavox Co | Centrifugal fuze |
US3167018A (en) * | 1962-03-19 | 1965-01-26 | Aeronca Mfg Corp | Missile safety and arming circuit |
US3517618A (en) * | 1960-04-19 | 1970-06-30 | Us Navy | Electric "point blank" bomb fuze |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB241941A (en) * | 1923-05-26 | 1925-11-26 | Bohdan Pantoflicek | Fuses for projectiles |
-
1943
- 1943-04-16 US US483303A patent/US2485817A/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB241941A (en) * | 1923-05-26 | 1925-11-26 | Bohdan Pantoflicek | Fuses for projectiles |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2920570A (en) * | 1956-12-17 | 1960-01-12 | Albert E Martin | Safety and delay arming device |
US2934016A (en) * | 1957-01-31 | 1960-04-26 | Mountjoy Garrard | Nylon timer |
US3075465A (en) * | 1957-07-23 | 1963-01-29 | Magnavox Co | Centrifugal fuze |
US2982213A (en) * | 1958-03-28 | 1961-05-02 | William G Meschino | Arming switch |
US3517618A (en) * | 1960-04-19 | 1970-06-30 | Us Navy | Electric "point blank" bomb fuze |
US3167018A (en) * | 1962-03-19 | 1965-01-26 | Aeronca Mfg Corp | Missile safety and arming circuit |
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