US2369337A - Time shell - Google Patents

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US2369337A
US2369337A US384819A US38481941A US2369337A US 2369337 A US2369337 A US 2369337A US 384819 A US384819 A US 384819A US 38481941 A US38481941 A US 38481941A US 2369337 A US2369337 A US 2369337A
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shell
pin
firing
forwardly
spring
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US384819A
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Cahill Gerald
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C9/00Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
    • F42C9/02Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by mechanical means

Definitions

  • This invention relates to an explosive shell, and more particularly to mechanism whereby theexplosion of the shell is effected at a desired distance from the point of projection.
  • An object of the present; ⁇ invention is to provide an improved shell having mechanism for controlling the time of explosion which is more accurate and dependablethn prior devices like those above mentioned.
  • an object of the invention is to provide mechanism forcontrolling the explosion of shells which ⁇ issensitive to the velocity of the shellsin flight, and which will produce explosion when the velocity of the shell has decreased to some predetermined value below the muzzle velocity.
  • Another object is to provide such' mechanism which isreadily adjustable to produce'bursting of the shell at any desired distance from the gun which projects it. Further objects and advantages of the invention ⁇ will be apparent as the specification proceeds. ⁇
  • a pressure pin B Located axially within the shell casing is a pressure pin B. At its front end pin B extends beyond front casing part Il and is equipped with the knurled knob 22. The rearward end of the pin rests against the spring plate 23 which is urged forwardly against the pin by the compression spring 24.
  • the spring 24 is backed by the rear wall ⁇ I4 of the casing and is of such strength that when so ⁇ compressed it urges the pressure pin B forwardly with the same pressure as would be exerted by air against the front knob 22 when the shell leaves the muzzle of a gun after having pressure.
  • pin',. Figure 6 a broken longitudinal sec-A I tional View of a. second embodiment ofthe invention; Figure.
  • the shellA is carsince this forms no part of the present invention. ⁇
  • the shell A has the casing I2 which comprises been shot under conditions for which the shell is intended.
  • the front stem 25 of the pin B is slidably carried in the central axial channel 26 of the part Il. ⁇ Normally, ⁇ however, and until the shell is projected, pin B is held fixed in its rearward position as shown in Fig. 1 by the split collar C.
  • This, ⁇ collar is disposed within the cavity 21 rearward of part I1, and as more clearly illustrated by Figure 2, is formed of two parts. It has a central hole 28 ⁇ so as to lit about the stem 25, and has also a constriction 29 which iits into the neck 30 of the stem 25.
  • A. pair of shearable pins 3l extend through collar C and into the metal part I5 so as normally to hold the halves of the collar in place.
  • the lower part of pin B and. the spring 24 are ⁇ encased in the tubular member 32 which is mounted axially within the shell' between wall I4 and forward part I5.
  • a lock plate 33 is attached to the lower end portion of pin B and extends to the walls and into the slot 38 of tube 32. The setback incident to firing the shell will force the lock plate 33 over the pyramidal part B' of the stem B thus preventing the stem being rotated by the air pressure against it when the shell is in. flight.
  • the lower portion of pin B is provided with spiral groove or thread 35 and carries a nut
  • the firing mechanism D comprises the firing,
  • This pin 40 carried in the cylindrical cavity 4I in part I5. This pin is urged rearwardly by the spring 42 based against the front part l1.
  • the ilring pin 40 is normally retained in retracted position ⁇ against spring ⁇ 42 by trigger mechanism.
  • This l mechanism comprises the key 43 which is slidable transversely and extends inwardly through a slot in tube 32, this key being more clearly shown in Figure 4 of the drawings.
  • the outer end of key y43 extends to a position beneath the lower shoulder of the firing pin and so withholds this pin.
  • Centrally of the key 43 is a slot 44, and as will be more clearly seen from Figure 1, when the nut 36 moves forwardly the tip of the arm 3.9 will engage the slot 44 and serve to move the key inwardly so as to release the firing pin.
  • the release of the firing pin 40 punctures the percussion cap 45 and so serves to set off the powder.,
  • the key is held in its normal position by the iiat retaining spring 43.
  • the position of the nut member 36 can be adjusted by simply turning the knurled knob 22. This operates through the engagement; of .threads 35 and 31, on the pin and nut respectively to move the nut forwardly or rearwardly on the pin. This enables setting of the vshell to explode near or far from the point of projection simply by turning the pin at the nose of the shell.
  • FIG. 5 to 9 of the drawings Asecond construction is illustrated in the Figures 5 to 9 of the drawings.
  • the casing comprises the side wall 50, into which is screwed the forward portion 5 I, to which in turn is attached the front piece 52.
  • the pressure pin 53 has a front knob or nose piece 54 and has its stem 55 extending axially through the shell.
  • a cavity 56 in forward portion 5I contains the collar l51 formed in equal halves and which engages the neck portion 58 of the pressure pin.
  • the rearward portion of pin 53 carries the screw threads 59, and carried on and engaging these threads is the nut member 60 which has its side arms 6
  • Nut memberl has a forward extension 64 which is adapted, when the pin 53 moves forwardly, to about the rear end of the firing pin release bushing 65.
  • the forward part 5l contains a cylindrical cavity 61 the axis of which is inclined. ⁇ In this cavity is the U-shaped firing pin 68. The legs 68a and 68h of this pin extend about the release bushing and have at their top portion the groove v69 which will permit the flange 66 to slide therein.
  • a socket 80 is contained. in the crotch of the firing ⁇ pin into which the ange 66 may seat to hold the pin in retracted position until time for explosion. When the parts are assembled, a spring 8
  • a ash passage 10 extends in the tapped stopper 85 and connects withthe black powder booster 1I which is intended to incite, in turn, the detonator sticks 12 and the high explosive 13.
  • flash passage 10 is of tapered form,'and in orderv to have the percussion cap 14 at a right angle with this fuse passage, the percussion cap holder 15 is set at an angle 'with the shells axis. It isfor this reason that the firing pin 68 is, in this embodiment, set at such an angle to conform with this arrangement.
  • the knob structure disclosed enables setting of the shell to explode near or far from the point of projection, the knob being manipulated by simple mechanism not here shown but accessible for manipulation by the gunner.
  • mechanism for exploding said shell at a distance from the point of projection comprising a. ⁇ rotatable pin movable axially of said shell and having its front end exposed at the front of the shell, a locking member engaging said pin and holding it in rearward position, said member being movable through centrifugal action upon rotation of said shell to release said pin for axial movement, a coil spring urging said pin forward with a force balancing the air pressure against the-front end of said pin as Shell is in flight and being adapted to move said pin forwardly as said air pressure decreases upon movement of the shell from the gun, firing mechanism for setting oil?
  • trigger means controlling the operation of said ring mechanism
  • trigger release means carried by said pin for releasing said trigger means when said pin has moved forwardly to bring such release means into contact with said ⁇ trigger means, said release means being adjustable as to position along said pin by rotation of said pin.
  • an explosive shell mechanism for exploding said shell at a distance from the point of projection, comprising a rotatable pin mounted in said shell for axial movement with respect thereto and having its front end provided with a diaphragm exposed at the front of the shell, means carried by the shell holding said pin in a rearward position until after said shell has started its flight, a coil spring within the shell urging said pin forward with a force balancing the air pressure against said diaphragm as the shell starts its flight and being adapted to move said pin forwardly as said pressure diminishes, ring mechanism for setting off explosive material Within said shell, means for actuating said firing mechanism, and means carried by said rotatable pin for controlling said actuating mechanism, said control means being shiftable upon said pin upon rotation thereof to Vary the timing of the explosion.
  • means for exploding said shell at a distance from the point of projection comprising a member mounted in said shell for axial movement with respect thereto and having a diaphragm at the front end thereof extending beyond said shell, spring means in said shell engaging said member for urging the same forwardly with pressure balancing the air pressure against the front of the diaphragm when the shell is in night and effective to move said mem,-
  • an explosive shell mechanism for exploding said shell at a distance from the point of projection, comprising a member mounted within said shell for axial movement with respect thereto and having its front end exposed at the front of the shell, locking means engaging said member and holding it in rearward position until the shell is in flight, spring means urging said member forwardly with a force balancing the air pressure against the front end of the member as the shell is in flight and being adapted to move the member forwardly as the air pressure decreases upon the movement of the shell from the gun, firing mechanism for setting off the explosive within the shell, trigger means controlling the operation of said firing mechanism, and trigger release means carried by said member for releasing said trigger means when the member has moved forwardly to bring such release means into contact with said trigger means, said release means being adjustable as to position along said member.
  • an explosive shell mechanism for exploding said shell at a distance from the point oi projection, comprising a pin mounted within said shell for axial movement with respect thereto and having its front end exposed at the front of the shell, a locking member carried by the shell engaging said pin and holding it in rearward position, said member being movable through centrifugal action upon rotation of the shell to re- ⁇ lease said pin for axial movement, spring means supported within said shell in actuating relation with respect to said pin for urging said pin forwardly with a force balancing the air pressure against the front end of said pin as the shell is in flight and being adapted to move said pin forwardly as said air pressure decreases, 'a sleeve ex.- tending about said pin within the shell and longitudinally movable thereon, said sleeve being provided with an enlarged head, a ring hammer carried within said shell disposed adjacent said pin and provided with a recess for receiving the enlarged head of saidy sleeve in interlocking engagement, said

Description

- Feb. 13, 1945. G, CAHlLL I 2,369,337
TIME SHELL Filed March 24, 1941 2 Sheets-Sheet l l ik G. CAHILL Feb. 13, 1945.
TIME SHELL Filed March 24, 1941 2 Sheets-Sheet. 2
Patented Feb. 13, 1945 UNITED STATES PATENT OFFICE Y TIME SHELL Gerald Cahill, Michigan City, Ind.
` Application March 24, 1941,` serial No. 384,819
(c1. 1oz-sz) Claims.
This invention relates to an explosive shell, and more particularly to mechanism whereby theexplosion of the shell is effected at a desired distance from the point of projection. i
In the past, two general methods have been used for causing the explosion of shells after pro-` jection. `One method involves the use of a train of powder one end being ignited when the gun is fired, the other end of the train being` connected with the` body of the explosive, so ,that the time required for. this train of powder to burn representsithe time elapsing between projection and explosion of the shell. The other method which has been used involves a clock mechanism which begins to operate upon proiection `of the shell.
An object of the present;` invention is to provide an improved shell having mechanism for controlling the time of explosion which is more accurate and dependablethn prior devices like those above mentioned. z. v
More specica11y an object of the invention is to provide mechanism forcontrolling the explosion of shells which `issensitive to the velocity of the shellsin flight, and which will produce explosion when the velocity of the shell has decreased to some predetermined value below the muzzle velocity. .Another object is to provide such' mechanism which isreadily adjustable to produce'bursting of the shell at any desired distance from the gun which projects it. Further objects and advantages of the invention` will be apparent as the specification proceeds.`
verse sectional view taken as indicated at line`3 of Figure l; Figure 4, a broken transverse sectional view taken as indicated atline 4 of Figure 1; Figure 5, a detail View of the front end of the the function of setting off the detonator explosive 20, v
Located axially within the shell casing is a pressure pin B. At its front end pin B extends beyond front casing part Il and is equipped with the knurled knob 22. The rearward end of the pin rests against the spring plate 23 which is urged forwardly against the pin by the compression spring 24. The spring 24 is backed by the rear wall` I4 of the casing and is of such strength that when so `compressed it urges the pressure pin B forwardly with the same pressure as would be exerted by air against the front knob 22 when the shell leaves the muzzle of a gun after having pressure. pin',.Figure 6, a broken longitudinal sec-A I tional View of a. second embodiment ofthe invention; Figure. '1, a sectional view takenv asindicated at line ll of Figure 6; `Figure 8,` a perspec-` tive view of the firing pin shown in `Figure 6; and Figure 9, a detail viewof the firing pin release bushing also shown in Figure 6;
As illustrated in Figure 1', the shellA is carsince this forms no part of the present invention.`
The shell A has the casing I2 which comprises been shot under conditions for which the shell is intended.
The front stem 25 of the pin B is slidably carried in the central axial channel 26 of the part Il.` Normally,` however, and until the shell is projected, pin B is held fixed in its rearward position as shown in Fig. 1 by the split collar C. This,` collar is disposed within the cavity 21 rearward of part I1, and as more clearly illustrated by Figure 2, is formed of two parts. It has a central hole 28` so as to lit about the stem 25, and has also a constriction 29 which iits into the neck 30 of the stem 25. Thus when the halves of the collar C areV together about pin B, this pin is fixed and held against longitudinal movement. A. pair of shearable pins 3l extend through collar C and into the metal part I5 so as normally to hold the halves of the collar in place.
The lower part of pin B and. the spring 24 are `encased in the tubular member 32 which is mounted axially within the shell' between wall I4 and forward part I5. A lock plate 33 is attached to the lower end portion of pin B and extends to the walls and into the slot 38 of tube 32. The setback incident to firing the shell will force the lock plate 33 over the pyramidal part B' of the stem B thus preventing the stem being rotated by the air pressure against it when the shell is in. flight. The lower portion of pin B is provided with spiral groove or thread 35 and carries a nut The firing mechanism D comprises the firing,
pin 40 carried in the cylindrical cavity 4I in part I5. This pin is urged rearwardly by the spring 42 based against the front part l1. The ilring pin 40 is normally retained in retracted position` against spring `42 by trigger mechanism. This l mechanism comprises the key 43 which is slidable transversely and extends inwardly through a slot in tube 32, this key being more clearly shown in Figure 4 of the drawings. The outer end of key y43 extends to a position beneath the lower shoulder of the firing pin and so withholds this pin. Centrally of the key 43 is a slot 44, and as will be more clearly seen from Figure 1, when the nut 36 moves forwardly the tip of the arm 3.9 will engage the slot 44 and serve to move the key inwardly so as to release the firing pin. The release of the firing pin 40 punctures the percussion cap 45 and so serves to set off the powder., The key is held in its normal position by the iiat retaining spring 43.
In operation, when the improved shell is projected, the rifling of the gun imparts to it a whirling or rotating motion, and this serves to shear the pins 3l ofthe collar`C permitting the halves of this collar to separate and move outwardly. This action releases the pin B for longitudinal movement. However, as the pressure exerted against the pressure pin B by the spring 24 balances the air pressure against the knob 22 as the shell leaves the muzzle of the gun, there will be no forward movement of pin B at this time.
The speed of the shell, and consequently the air pressure at its front end, will be greatest at the time it leaves the muzzle of the gun, and from this instant its speed and the pressure against its front end decreases. As the air pressure against knob 22 decreases the pin B will be moved by the spring 24 to a forward position at which there is less pressure by spring 24 there being maintained a balance between the air pressure at the front and the spring pressure at the rear. lhus, as the shell moves in its flight the pressure pin B moves forwardly the distance traversed by the shell being measured by the forward movement of pin B.
When the pressure pin B has moved forwardly far enough to cause the arm 39 of nut 36 to engage the slot 44 of ,the slide member 43 and pull this member inwardly, the firing pin 40 will be released, will puncture the percussion cap 45 and thus set off the explosive materials.
It will be apparent that the position of the nut 36 on the pressure pin will determine how far forward this pin has to move in order to release the trigger mechanism comprising the slide member '43. Thus by adjusting the position of the nut 35 along the pin B the shell can be made to explode at different distances from the point of projection.
It is an important feature of the invention that the position of the nut member 36 can be adjusted by simply turning the knurled knob 22. This operates through the engagement; of .threads 35 and 31, on the pin and nut respectively to move the nut forwardly or rearwardly on the pin. This enables setting of the vshell to explode near or far from the point of projection simply by turning the pin at the nose of the shell.
Asecond construction is illustrated in the Figures 5 to 9 of the drawings. In this modification the casing comprises the side wall 50, into which is screwed the forward portion 5 I, to which in turn is attached the front piece 52.
The pressure pin 53 has a front knob or nose piece 54 and has its stem 55 extending axially through the shell. A cavity 56 in forward portion 5I contains the collar l51 formed in equal halves and which engages the neck portion 58 of the pressure pin. The rearward portion of pin 53 carries the screw threads 59, and carried on and engaging these threads is the nut member 60 which has its side arms 6| engaging the slots 62 in the central tube 63. Nut memberl) has a forward extension 64 which is adapted, when the pin 53 moves forwardly, to about the rear end of the firing pin release bushing 65. 'Ihis bushing, as shown more clearly in Figure 9, is tubular and has at its forward end an outwardly extending flange 66 and the lower or rearward edge vof this flange is slightly inclined. vThe reason for this will be more apparent after a description of the firing pin employed in this embodiment.
The forward part 5l contains a cylindrical cavity 61 the axis of which is inclined. `In this cavity is the U-shaped firing pin 68. The legs 68a and 68h of this pin extend about the release bushing and have at their top portion the groove v69 which will permit the flange 66 to slide therein. A socket 80 is contained. in the crotch of the firing `pin into which the ange 66 may seat to hold the pin in retracted position until time for explosion. When the parts are assembled, a spring 8| normally holds the flange 66 in position within socket 811.
A ash passage 10 extends in the tapped stopper 85 and connects withthe black powder booster 1I which is intended to incite, in turn, the detonator sticks 12 and the high explosive 13. The
flash passage 10 is of tapered form,'and in orderv to have the percussion cap 14 at a right angle with this fuse passage, the percussion cap holder 15 is set at an angle 'with the shells axis. It isfor this reason that the firing pin 68 is, in this embodiment, set at such an angle to conform with this arrangement.
In the operation of the shell shown in Figures 5 to 9, the shell, upon being projected is rotated and the centrifugal force thus produced operates to shear the pins 11 in the collar 51, thus to release the pressure pin 53. When the speed of the shell slackens, the pin moves forwardly as in the first embodiment described. The nut member 6!) advances to bring the extension 54 against the rear end of the firing pin release bushing 65 to move this bushing forwardly against springl 8l. 'I'his operates to release the ring pin 68 to the action of centrifugal force which then throws the pin outwardly, the flange 66 of the release bushing riding in the groove 69, bringing its point 18 against the percussion cap 14, with the consequent explosion of the shell.
As in the first embodiment described, the nose ily rotated by mechanism associated with the gun but not described herein for instantaneously adjusting the nut to the desired position. In other words, the knob structure disclosed enables setting of the shell to explode near or far from the point of projection, the knob being manipulated by simple mechanism not here shown but accessible for manipulation by the gunner.
Though in the foregoing detailed description I have described only two modifications of my invention, it will be apparent that the improved shell may be constructed in many other embodiments with widely differing structures, all within the spirit of the invention. The foregoing illustrations and specic descriptions are intended as explanatory only, and no unnecessary limitations should be understood therefrom.
I claim: v
1. In an explosive shell, mechanism for exploding said shell at a distance from the point of projection comprising a.` rotatable pin movable axially of said shell and having its front end exposed at the front of the shell, a locking member engaging said pin and holding it in rearward position, said member being movable through centrifugal action upon rotation of said shell to release said pin for axial movement, a coil spring urging said pin forward with a force balancing the air pressure against the-front end of said pin as Shell is in flight and being adapted to move said pin forwardly as said air pressure decreases upon movement of the shell from the gun, firing mechanism for setting oil? the explosives within said shell, trigger means controlling the operation of said ring mechanism, and trigger release means carried by said pin for releasing said trigger means when said pin has moved forwardly to bring such release means into contact with said `trigger means, said release means being adjustable as to position along said pin by rotation of said pin.
2. In an explosive shell, mechanism for exploding said shell at a distance from the point of projection, comprising a rotatable pin mounted in said shell for axial movement with respect thereto and having its front end provided with a diaphragm exposed at the front of the shell, means carried by the shell holding said pin in a rearward position until after said shell has started its flight, a coil spring within the shell urging said pin forward with a force balancing the air pressure against said diaphragm as the shell starts its flight and being adapted to move said pin forwardly as said pressure diminishes, ring mechanism for setting off explosive material Within said shell, means for actuating said firing mechanism, and means carried by said rotatable pin for controlling said actuating mechanism, said control means being shiftable upon said pin upon rotation thereof to Vary the timing of the explosion.
3. In an explosive shell, means for exploding said shell at a distance from the point of projection, comprising a member mounted in said shell for axial movement with respect thereto and having a diaphragm at the front end thereof extending beyond said shell, spring means in said shell engaging said member for urging the same forwardly with pressure balancing the air pressure against the front of the diaphragm when the shell is in night and effective to move said mem,-
ber forwardly as the air pressure against it de-` 4. In an explosive shell, mechanism for exploding said shell at a distance from the point of projection, comprising a member mounted within said shell for axial movement with respect thereto and having its front end exposed at the front of the shell, locking means engaging said member and holding it in rearward position until the shell is in flight, spring means urging said member forwardly with a force balancing the air pressure against the front end of the member as the shell is in flight and being adapted to move the member forwardly as the air pressure decreases upon the movement of the shell from the gun, firing mechanism for setting off the explosive within the shell, trigger means controlling the operation of said firing mechanism, and trigger release means carried by said member for releasing said trigger means when the member has moved forwardly to bring such release means into contact with said trigger means, said release means being adjustable as to position along said member.
5. In an explosive shell, mechanism for exploding said shell at a distance from the point oi projection, comprising a pin mounted within said shell for axial movement with respect thereto and having its front end exposed at the front of the shell, a locking member carried by the shell engaging said pin and holding it in rearward position, said member being movable through centrifugal action upon rotation of the shell to re-` lease said pin for axial movement, spring means supported within said shell in actuating relation with respect to said pin for urging said pin forwardly with a force balancing the air pressure against the front end of said pin as the shell is in flight and being adapted to move said pin forwardly as said air pressure decreases, 'a sleeve ex.- tending about said pin within the shell and longitudinally movable thereon, said sleeve being provided with an enlarged head, a ring hammer carried within said shell disposed adjacent said pin and provided with a recess for receiving the enlarged head of saidy sleeve in interlocking engagement, said hammer being movable to firing position by centrifugal force upon rotation of said shell when released from said interlocking engagement with the head of said sleeve, means carried by the pin for engaging said sleeve when the pin advances to move the head of the sleeve from interlocking engagement with the recess in said hammer, and releasing said hammer for movement to iiring position whereby said hammer moves to firing position to set offexplosive material within said shell.
` GERALD CAHILL.
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2479582A (en) * 1945-05-07 1949-08-23 James F Mccaslin Projectile fuse
US20080115686A1 (en) * 2006-11-17 2008-05-22 Crist Scott D Methods and apparatuses for projectile fuze setback generator power source and projectiles including same

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2479582A (en) * 1945-05-07 1949-08-23 James F Mccaslin Projectile fuse
US20080115686A1 (en) * 2006-11-17 2008-05-22 Crist Scott D Methods and apparatuses for projectile fuze setback generator power source and projectiles including same
US7669532B2 (en) * 2006-11-17 2010-03-02 Alliant Techsystems Inc. Methods and apparatuses for projectile fuze setback generator power source and projectiles including same

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