US2958285A - Fuze component design - Google Patents

Fuze component design Download PDF

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US2958285A
US2958285A US845295A US84529559A US2958285A US 2958285 A US2958285 A US 2958285A US 845295 A US845295 A US 845295A US 84529559 A US84529559 A US 84529559A US 2958285 A US2958285 A US 2958285A
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slider
fuze
bore
disc
movement
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US845295A
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Robert P Marshall
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C15/00Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges
    • F42C15/18Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved
    • F42C15/184Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a carrier for an element of the pyrotechnic or explosive train is moved using a slidable carrier

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Description

Nov. 1, 1960 R. P. MARSHALL FUZE COMPONENT DESIGN Filed Oct. 8, 1959 INVENTOR. 2429 Ember]: .Elwars'hall.
FUZE COMPONENT DESIGN Robert P. Marshall, 504 Vista Drive, Falls Church, Va.
Filed Oct. 8, 1959', Ser. No. 845,295
1 Claim. (Cl. 102-76) (Granted under Title'3'5,*U.S.' Code (1952), cc. 266) The invention describedherein may be manufactured and used by or for the Government for governmental; purposes without the payment to us of any royalty thereon.
This invention relates to a fuze component and more particularly relatesto a means to retard the movement of a spring actuated arming slider of a fuze in order to relieve the shock of the sliderseating at the end of its stroke and to provide a limited delay thereto.
The present invention is proposed as a solution of the premature functioning of non rotating 60 mm. and 81 mm. ammunition and its assembly to the M52 fuze. These premature functionings are believed to be caused by either the seating of the spring actuated arming slider, used in this typeof fuze, transmitting the shock of seating to an oversensitive detonator, or the result of the fuzes firing pin heing depressed once the slider has armed. It has been observed that the premature functionings have taken place from one to six feet from the muzzle of the weapon and it is desired to effect a delay arming of a short time duration to eliminate this hazard.
The present invention uses friction discs which are held without force within the slider, one disc having a square central opening so that it may rotate as it is being pulled along the length of a twisted actuating rod, also having a square cross section, as the slider is being moved into an armed position by a spring. The discs provide a time delay in the movement of the slider from unarmed to armed positions to allow the projectile to reach a safe distance from the muzzle of the weapon.
It is therefore a primary object of this invention to provide a time delay in the movement of an arming slider from its safe position in a fuze to an arming position therein.
It is another object of the invention to cushion the impact of a spring biased arming slider of a fuze upon reaching its armed position to prevent transmittal of the resultant shock to an over sensitive detonator in the fuze.
A further object of the invention is to provide a friction means to retard the movement of the spring biased slider in a fuze from a safety to an armed position.
A still further object is the provision of a plurality of friction discs within a spring biased arming slider, one disc having a square central opening adapted to be pulled along a helical rod, also having a square cross section whereby a short time delay is provided to the slider in its movement from a safety to an armed position.
A final object is to provide a fuze component that is simple in operation and reliable in functioning.
The invention will be best understood from a consideration of the following detailed description taken in connection with the accompanying drawing, it being understood however, that the invention is not limited to the specific illustration or description but that such illusnationor description constitutes a preferred embodiment of the invention.
In the drawing:
Fig. 1 is an axial section taken through the body of a fuze, the arming slider being in its safety position,
ie rates "atent Patented Nov. 1 1960 showing a delay mechanismnfq Ietardingi-them ovement of the slider constructed in accordance with the ,present invention;
Fig. 2 is a partial section view .of :.a,;modified fornnof time delay mechanism; I
Fig. 3 is a partial section view .of anothermodified form of time delay mechanism;
Fig. 4 is a perspective view of oneof .thefrict-ion discs having a square central opening;
Fig. 5 is a perspective view of ,a friction disc having a circular opening; and
Fig. 6 is a perspective view of another form of-disc comprising a split ring.
Referring to the drawing, '1 indicatesgenerally afuze and includes a body 2 provided with external threads 3 for attachment to a projectile (notshown) and ,rearward internal threads 4,for securing a booster cup (not shown). Forwardly disposed internal threads 5 areprovided for attachment of a fuze detonating element (not shown). Axial flash passageways 6 and -7 are provided. A transverse bore 8 is provided for receiving an arming slide indicated generally by 9. A bore riding pin 10 is slidable in a transverse bore 11in body 2.
Such pins are common in the art and are usually spring-pressed as shown in U.S. PatentNo. 1,992,928.
Arming slider 9 is provided with "a first central slot 12 in its inner portion to receive bore riding pin 10. A second slot 13 receives a detent 14 which normally prevents rotational movement of slide 9. This rotational movement is normally prevented due to the fact that slide 9 is provided with a flash pass-age 6:1 for receiving a detonating element or the like for completing the powder train when slide 9 is moved to its armed position.
Slide 9 has a reduced outer portion 15 which is axially bored as at 16. Bore 8 is closed at its outer end by screw cap 17 which is provided with a square axial bore 18. An actuating rod 19 having a square cross section and helical twist is secured in bore 18 by a pin 20. The outer portion 15 of slide 9 is counter-bored as at 21 and receives a friction disc 22 having a square central opening 23 (see Fig. 4) through which rod 19 passes. A second disc 24- (see Fig. 5) having a circular opening 25 of larger diameter than rod 19 is received in counterbore 21 and disposed below disc 22 as seen in Fig. 1. Both discs are retained in counter-bore 21 by crimping the outer edge of counter bore 21 as at 26.
Slide 9 is normally urged inwardly by coil spring 27.
In operation, the fuze body is attached to a projectile, not shown and to a detonating element, also not shown and completes a round of ammunition.
When fired from a weapon, bore riding pin 10 is ejected. Spring 27 tends to urge slider 9 towards its armed position in bore 8. Slider 9 is held against rotational movement by detent 1 4. In order that the projectile may not arm until a safe distance from the muzzle of the weapon, a limited delay is effected by the actuating rod 19 and friction discs 22 and 24 in the following manner: The actuating rod 19 is square in cross section and has a helical twist to give either one half revolution or one fourth revolution per inch for the purpose of causing friction disc 22, which has a square central opening, to rotate in counter-bore 21 as the rod 19 is pulled along its length as slider 9- moves in bore 8. In order for disc 22 to rotate, it must overcome the friction between its surface and the surface of friction disc 24 which has a round central opening 25 and is mounted below disc 22 also contained in counter-bore 21, and thus will retard the movement of slider 9.
A modified form of washer arrangement is illustrated in Fig. 2 and operates in the same manner as Fig. 1, however an additional member in the form of a split discs wherein an additional smooth disc 29 is used and in addition, a second spring 30 in an axial bore 31 in of a more sensitive loading of the friction discs.
In order that the device work as consistent as possible in extremes of hot and cold weather conditions, the friction discs in all these applications should be assembled in dry condition, without lubricants, and fabricated from materials such as stainless steel, brass or plastics with smooth hard surfacesof relative high strength and stiflness.
It is apparent from the foregoing that a highly eificient means has been devised to provide a time delay for retarding the movement of an arming slider in a fuze for preventing premature arming in the fuze until it has traveled a safe distance from the muzzle of a weapon. Its operation is reliable due to its simplicity of construction.
It is to be understood that the form of the invention herewith shown and described, is to be taken as a preferred example of the same, and that various changes in the shape, size and arrangement of parts may be resorted to without departing trom the spirit of the invention.
What is claimed is:
In combination, a fuze including a body having a transverse bore therein, a slider carrying a detonator slidably mounted in said bore for movement from an unarmed to an armed position, there being an axial bore slider 9 which biases against disc 29 and offers a means in the outer portion thereof, means urging said slider toward the armed position, a bore riding pin carried by said body engaging said slider and extending through said bore to normally restrain said slider in the unarmed position until firing occurs, said pin being disengaged from said slider upon firing and freeing said slider for movement towards the armed position, means carried by said body for preventing rotary movement of the slider in said transverse bore, and means for delaying movement of said slider toward the armed position comprising a helically twisted rod fixed in said body and extending into said axial bore, and at least two friction discs having central openings arranged in coaxial abutting relation in said slider and slidable on said rod, the central opening of one of said discs being of the same configuration as the cross sectional configuration of said rod, so that the last named disc will be frictionally rotated against the other upon movement of said slider toward the armed position.
References Cited in the file of this patent UNITED STATES PATENTS 1,992,926 Towner Feb. 26, 1935 2,779,287 Andrews Jan. 29, 1957 2,821,925 Var-aud Feb. 4, 1958 2,870,713 Saloranta Jan. 27, 1959 2,872,868 Donahue Feb. 10, 1959 FOREIGN PATENTS 186,248 Germany May 23, 1907
US845295A 1959-10-08 1959-10-08 Fuze component design Expired - Lifetime US2958285A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126828A (en) * 1964-03-31 tafel
US3319567A (en) * 1964-05-27 1967-05-16 Industrial Holding Ets Projectile fuse
US3726230A (en) * 1969-12-01 1973-04-10 Sampella Ab Oy Percussion fuse for projectiles
US3736876A (en) * 1970-06-26 1973-06-05 Us Navy Catalyst generator
US4449454A (en) * 1981-11-03 1984-05-22 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Safety mechanism for an explosive body

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE186248C (en) *
US1992926A (en) * 1932-11-01 1935-02-26 Harold G Towner Fuse for projectiles
US2779287A (en) * 1951-11-01 1957-01-29 Laurence M Andrews Contact fuze
US2821925A (en) * 1956-04-16 1958-02-04 Ufa Universal Finanzierungs Au Double-acting percussion fuze provided with a safety device for projectiles
US2870713A (en) * 1955-06-09 1959-01-27 Saloranta Arvo Ensio Fuse for shells
US2872868A (en) * 1955-07-11 1959-02-10 Jr William J Donahue Missile nose fuze

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE186248C (en) *
US1992926A (en) * 1932-11-01 1935-02-26 Harold G Towner Fuse for projectiles
US2779287A (en) * 1951-11-01 1957-01-29 Laurence M Andrews Contact fuze
US2870713A (en) * 1955-06-09 1959-01-27 Saloranta Arvo Ensio Fuse for shells
US2872868A (en) * 1955-07-11 1959-02-10 Jr William J Donahue Missile nose fuze
US2821925A (en) * 1956-04-16 1958-02-04 Ufa Universal Finanzierungs Au Double-acting percussion fuze provided with a safety device for projectiles

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126828A (en) * 1964-03-31 tafel
US3319567A (en) * 1964-05-27 1967-05-16 Industrial Holding Ets Projectile fuse
US3726230A (en) * 1969-12-01 1973-04-10 Sampella Ab Oy Percussion fuse for projectiles
US3736876A (en) * 1970-06-26 1973-06-05 Us Navy Catalyst generator
US4449454A (en) * 1981-11-03 1984-05-22 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Safety mechanism for an explosive body

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