US2895419A - Safety arming mechanism for fuses - Google Patents

Safety arming mechanism for fuses Download PDF

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Publication number
US2895419A
US2895419A US513836A US51383655A US2895419A US 2895419 A US2895419 A US 2895419A US 513836 A US513836 A US 513836A US 51383655 A US51383655 A US 51383655A US 2895419 A US2895419 A US 2895419A
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central spindle
striker
spindle
bolt
fuse
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US513836A
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Rosselet Jean
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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
    • F42C9/02—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by mechanical means
    • F42C9/04—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by mechanical means by spring motor
    • F42C9/041—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by mechanical means by spring motor the clockwork activating a security device, e.g. for unlocking the firing-pin
    • 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
    • F42C15/18—Arming-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
    • 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
    • F42C9/04—Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by mechanical means by spring motor
    • F42C9/048—Unlocking of clockwork mechanisms, e.g. by inertia or centrifugal forces; Means for disconnecting the clockwork mechanism from the setting mechanism

Definitions

  • the chief feature of my invention consists in that I provide a central spindle-arranged axially of the fuse and urged by a drivin'g spring which-is set when held in its inoperative position so as to produce the rotation of the central spindle whenreleased while a rocking weight subjected to the action'of a further spring is' adapted to execute permanentv oscillations round an-axis perpendicular to the axis of?
  • the fuse and an escape mechanism constituted by an escape wheelrigid with the central spindle and a cylinder rigidwith therocking weight is adapted to maintain the undampedoscillations of the rocking: weight and to adjust thus the speed of rotation of the central spindle.
  • the central spindle controls a striker bolt to hold the striker in its inoperative position and to release said strikerwhen the central spindle has executed a predetermined rotation corresponding to a predetermined number of oscillations of the rocking weight, the central spindle being provided with an axial bore for the passage of the: striker, therethrough.
  • Figs. 1 to 10 relate to a first embodiment and two detail. modifications and more specifically:
  • Fig. 1 is-an'axial cross-section of-a mechanism through line IIof-'Fig. 2.
  • Fig. 2 is a simplified horizontal cross-section of the mechanism through line IL-I'I of Fig. 3.
  • Fig. 3* is a sideview of the mechanism, partly sectional through line IIIIII of Fig. 2.
  • Fig. 5 illustrates a portion of the same mechanism in accordance with a modification.
  • Fig. 6 is an axial cross-section of said portion of the mechanism in another modification thereof.
  • Fig. 7 is a: transverse cross-section of the portion of mechanism shown in Fig. 6.
  • Figs. 8 and 9 illustrate an escape mechanism forming partof the safety arming mechanism.
  • Fig: 10' is a partial axial cross-section through a modified arming'mechanism.
  • Figs. 11 to 18 relate to a second embodiment, wherein the arms radially carried by the rocking weight carry auxiliary weights distributed in a balanced manner so that the action on said masses of centrifugal force arising under the action of the rotation of the missiles compensate each other. More specifically:
  • Figs. 11 and 12 illustrate the action of centrifugal force on a nonbalanced weight.
  • Fig. 13 illustrates the action of centrifugal force on a compound balanced rocking weight.
  • Figs. 14 to 18 illustrate different embodiments of the arms forming part of the rocking weight.
  • Figs. 19 and 20 relate to a thirdembodirnent and to a modification wherein.
  • the rocking weight adapted to exe cute undarnped oscillations round a diametrical axis perpendicular to the axis of the fuse includes a toothed wheel meshing with a further toothed wheel coaxial with the centralspindleon which it is mounted.
  • Fig. 19 is an axial cross-section of said third embodiment while Fig. 20 illustrates in plan view and perpendicularly to the central spindle a detail modification thereof.
  • Figs. 21 to 25 relate to a fourth embodiment and'to two modifications thereof, wherein the striker bolt located underneathv the tip of the-striker moves in a plane perpendicular to thecentral spindle. More specifically:
  • Fig. 21 is a partial axial cross-section of a mechanism incorporating'such a striker bolt.
  • Fig. 22 is a plan view of the mechanism illustrated in Fig. 21.
  • Fig. 23 is a plan view of/afirst modification.
  • Figs. 24' and 25 are respectively a partial axial. crosssection and a plan'view' of the same mechanismaccording to the second modification.
  • Fig. 26' illustrates partly and diagrammatically, in a plane perpendicular to the central spindle; amechanism for locking the striker.
  • Fig. 27 is a partial axial cross-section of said embodimerit of which Figs. 20 to 30 illustrate the cam system in various positions in aplane perpendicular to the central spindle.
  • Fig. 3-1 is asimplified view of amodification in a plane perpendicular to the central spindle;
  • the safety armingmechanism illustrated includes a central spindle lextendingalong the axis of the fuse which has not been illustrated; said spindle is guided in anupper bearing 2 centrally fitted inside an upper plate 3 and in a lower bearing 4 rigid with the lower plate 5-.
  • the central spindle- is provided with an axial bore 6 for the passage therethrough of a striker 7.
  • a rockingweight including two arms 8 and 9- located to either side of the central spindle 1 and rigidly interconnected bytwo transverse stays 10 and 11;
  • the arm 8' isrigidwith aspindle 12 pivotally carried inside a bearing 14;
  • the arm 9 is rigid with'a spindle 13 pivotally carried inside a bearing 15.
  • the common axis'of the two-spindles 12 and 13 extends diametrically across the axis of the central spindle 1 and perpendicularly thereto.
  • This system 813 forms arocking weight subjected to the action of a spring 16 constituted by a coil spring arranged coaxially with reference to the spindle 12 and inserted between the arm 8 and the bearing'14;
  • the rocking weight may execute angular oscillations round the axis of. the spindles 12- and 13 and occupy two extreme positions of a predetermined amplitude, illustrated in Fig. 1 by the locations 17 and 18 of the stay 10 to either side of the neutral position assumed by said stay 10.
  • An escape mechanism forming a mechanical connection between the central spindle and the rocking weight includes an escape wheel 19 rigid with-the central spindle 1 and a cylindrical member 20 or more accurately speaking' a cylindrical sector rigid with the spindle 13. This escape mechanism will be described hereinafter.
  • the central spindle 1 isurged into rotation by a. driving spring 21 constitutedby a coil spring coaxial with the central spindle 1 and one end of which. is: secured to the upper bearing 2 and the lower end of which is rigid with a ferrule 22 rigid with the central spindle 1.
  • the central spindle 1 is provided with a diametrical recess 23 extending perpendicularly to the axis of said shaft and in said recess is housed a striker bolt 24 held when the fuse is inoperative inside said recess 23 by a member 25 in the shape of a cylindrical sector coaxial with the central spindle 1 and rigid with the lower plate 5.
  • Said sector 25 is provided with a port 26 engageable by the bolt 24 when the central spindle has executed a predetermined angular shifting away from its striker-locking position illustrated in Fig. 4.
  • the bolt 24 is constituted by a bar provided with a longitudinal slot 27.
  • the collar 28 on the striker 7 engages the bolt 24 the slot in which provides a free passage for the tip 29 of the striker 7.
  • the rocking weight is held against rocking before the firing of the missile by two stops 30 and 31 constituted by two spring blades rigidly secured respectively to the upper plate 2 and to the lower plate 5.
  • an escape mechanism including an escape wheel 19 rigid with the central spindle 1 which is not illustrated in said figures, and which cooperates with a cylindrical sector 20 rigid with one end of the spindle 13 riveted or otherwise secured to the arm 9 of the rocking weight.
  • the escape wheel 19 is provided with six teeth of which one is illustrated as engaging the outer surface 72 of the cylindrical sector 20.
  • this escape mechanism is as follows: when the tooth 71 engages the outer surface 72 of the cylinder 20, the escape wheel 19 is stopped.
  • the oscillations of the rocking weight constrain the cylindrical sector to rock in the direction of the arrow 73 and thus to release said tooth 71 (Fig. 8); the escape wheel progresses through one half-pitch in the direction of the arrow 74 and the tooth 71 enters the position 76 shown in dotted lines in Fig. 9.
  • the tooth 71 imparts an impulse to the cylindrical sector 20, said impulse serving for the maintenance of the oscillations of the rocking weight.
  • the escape wheel 19 is again stopped as the tooth 71 which has entered the position illustrated at 76 in Figs.
  • the frequency of the oscillations is defined by the characteristic properties of the spring 16 and by the magnitude of the momentum of inertia of the rocking weight.
  • the operation of the safety arming means described hereinabove is as follows: I will first suppose that said mechanism is fitted in a gyratory fuse having its nose directed upwardly. When the fuse is inoperative, the rocking weight is held in its inoperative position 18 by the locking springs 30 and 31. The escape mechanism 19-40 also locks the central spindle in its inoperative position. The striker bolt 24 is held inside its recess 23 t by the cylindrical sector 25.
  • the striker bolt 24 registers with the opening 26 in the cylindrical sector 25. Said bolt is urged outwardly by centrifugal force and engages said opening 26: it passes thus out of its recess 23 and releases the striker 7 which is ready to execute its striking movement through a rearward axial movement; this means the fuse is now armed.
  • the release of the bolt is executed after a predetermined number of oscillations, starting from the firing of the shot and consequently the arming of the fuse is obtained after a predetermined period which forms the delay brought to the arming of the fuse on its path.
  • a delay of the magnitude of 0.1 second is readily obtainable and provides safety on a path the length of which is about meters for a missle with a muzzle velocity of 800 In. per second.
  • Fig. 5 a modification of the striker bolt constituted by a lever 41 rigid with an arm 42 pivotally secured at 43 and provided with a nose 44 cooperating with a cam 45 rigid with the central spindle 1, which latter revolves in the direction of the arrow 46.
  • the nose 44 is submitted to the action of a spring 48, said spring being illustrated diagrammatically as urging said nose against the cam 45.
  • the lever 41 which is supposed to be mounted over the rear end of the central spindle 1, closes the central perforation 6 in said central spindle 1 so as to lock the striker against movement.
  • the operation of last mentioned modification is as follows: when inoperative, the bolt 51 is held in its locking position by the cam 54. After a predetermined rotation of the cam 54 and a corresponding rotation of the central spindle 1, the bolt 51 is shifted radially by a cooperating spring and engages the receding section 61 of the cam 54 so as to release the striker 53.
  • the speed reducer constituted by the wheel 56 and pinion 57 inserted between the central spindle and the cam 54 allows the central spindle and the escape wheel to execute an angular shifting longer than one complete revolution and to increase the number of oscillations required before the release of the bolt whereby an increased safety on the path of the missile is obtained.
  • a section of a safety mechanism including a lower plate 5 and an upper plate 3 rigid with a cylindrical casing 81 serving as a guide for a bolt 82 adapted to move axially over the cylindrical casing 81 and held in its striker locking position by a coil spring 83 which urges it against a stop 84 rigid with said casing 31.
  • a plug 85' screwed into the casing 81 is provided with a tapping 86 inside which may be screwed a detonator and primer system.
  • the inertia-actuated bolt 82 is urged downwardly and uncovers the ports 89 and 90 whereby the springs 30 and 31 are released and open so as to allow the rocking weight to oscillate freely; the nose 88 of the spring 31 which moves then outwardly of the cylindrical casing 81 prevents the bolt 82 from returning into its inoperative position.
  • the mechanism for locking the rocking weight as just described is provided for missiles which assume in their flight no gyratory movement or only a small gyratory movement.
  • rocking weight adapted to executev oscillatory movements round the axis of the two spindles 12 and 13 extending in a direction perpendicular to the axis of the fuse 101.
  • the rocking weight includes again two arms 8' and 9 rigidly interconnected by two stays 10 and 11.
  • Fig. 11 is shown in dotted lines the location of the arm 8 in a rocked position of an irrelevant amplitude 102. In this position the stays 10 and 11 are subjected each to a centrifugal force 103 producing a torque which urges the arm 8 back into its neutral position of equilibrium shown in solid lines. Centrifugal force opposes thus the undamped oscillations of the rocking weight provided with the stays 10 and 11 round the common axis of the pivots 1-2 and 13.
  • a first compound rocking weight ineludes two stays 10 and 11 which are balanced by the two stays 1'04 and 105 of the second compound weight, which are pivotally secured at 112 to a diametrical axis perpendicular to the axis 101 of the fuse.
  • the two stays 104 and 105 of the second weight are positioned in a plane perpendicular to that of the stays 10 and 11 of the first weight.
  • a rocking weight including two discs 118 and 119 revolubly mounted at 112 and 113 and interconnected by two stays 10 and 11 which are balanced as far as centrifugal force is concerned by four masses 106, 107, 108, and 109 which are located in a diametrical plane of the discs perpendicular to the plane of the stays 10 and 11.
  • the stays 10 and 11 may also be balanced as illustrated in Fig. 16 by means of discs 128 provided with two 6 apertures and 111' arranged symmetrically with ref erence to a plane extending perpendicularly to the plane containing the stays 10 and 11 and symmetrically between said stays.
  • the weight of the stays 10and 11 may also be balanced by means of circular openings 122 provided in such discs 118 forming part of the compound rocking weight as illustrated in Fig. 17.
  • the shape of the arms of the rocking weight may also be that illustrated in Fig. 18, to wit, a cross-shaped member revolubly carried by a spindle 12 and associated with stays 10 and 11 and balancing weights 1'06 to 109 similar to those illustrated in Fig. 15.
  • safety means for a fuse arming mechanism including a central spindle 201 extending axially of the fuse and guided inside an upper bearing 202' centrally fitted in an upper plate 203 and inside a lower bearing 204formed in a lower plate 205.
  • the two plates 203 and 205 are held in position by two uprights 214 and 215.
  • the central spindle 201 carries a toothed escape Wheel 219 cooperating with a cylinder 220 adapted to reek to either side of a neutral position round a diametrical axis perpendicular to the axis of the fuse i.e. round the axis of the spindle 213 which bears against an attachment screw 229.
  • a pinion 221 rigid with said spindle 213 meshes with a toothed wheel 222 revolublymounted on the central spindle 201.
  • the operation of the mechanism just described is similar to that of the mechanism described with reference to Figs. 1 to 9.
  • the cylinder 220 executes undamped oscillations round the spindle 213 so as to carry along with it through the pinion 221 the toothed wheel 222 which executes in its turn oscillations round the central spindle 201.
  • the spring serving for the maintenance of the oscillations is constituted by a coil spring 223 coaxial with the central spindle 201 and secured through one end 224 to the pinion 222 and through its other end to the lower plate 205.
  • the weight oscillating with reference to the spindle 213 has its centre of gravity outside the axis of the fuse and centrifugal force urges said mass towards the bearing constituted by the attachment screw 229.
  • Fig. 20 a section of a mechanism similar to that of Fig. 19, wherein the rocking weight oscillating round a diametrically located spindle perpendicular to the axis of the fuse has its centre of gravity on said axis of the fuse.
  • Said mechanism includes again a lower plate 205 associated with two uprights 214 and 215 which serve as bearings for the two pivots, 2'12 and 213, of a rocking weight including two arms 208 and 209 rigid with two stays 210 and 211, while a cylinder 220 controls as precedingly a toothed wheel 222 similar to the wheel 222 illustrated in Fig. 19.
  • the elementary weights forming said compound rocking weight should be selected in a manner such that the centre of gravity of the oscillating mass lies on the axis of the fuse.
  • the two pivots or spindles 212 and 213 engage two small discs or the like members 226 and 227 serving as step bearings for them and fitted in the uprights 214 and 215.
  • the toothed pinion 221 meshing with the toothed wheel 222 and said toothed wheel 222 are both provided preferably with bevel teeth.
  • a mechanism including a lower plate 401, and an upper plate 402 serving as a bearing for a central spindle 403, provided with an axial bore for the passage of a striker 404 rigid when inoperative with the actual fuse which is not illustrated and which is located above the mechanism.
  • the central spindle 403 carries a cam 405 cooperating with alever 406 pivotally secured at 407 and including a terminal bolt-locking projection 408.
  • the lower plate 401 is provided with a diametrical recess 409 for'the striker bolt 410 extending underneath the tip of the striker 404 and held inside said recess by a perforated plate 411 fitted inside a primer carrier 412.
  • the nose 413 on the lever 406 engages the periphery of the cam 405 and the locking projection 408 rigid with the outer lever arm 406' holds the bolt 410 in its operative striker-locking position.
  • a bolt 421 for the striker pivotally secured at 422 and held in its locking position by the projection 408 for which it covers the central opening 417 in the plate 411, said perforation 417 being caused to register with the striker when the safety mechanism is released.
  • the bolt 421 is shifted through a rotation round an axis parallel with the central spindle. The remainder of the mechanism is the same as that illustrated in Figs. 21 and 22. l r
  • Figs. 24 and 25 a mechanism similar to that described with reference to Figs. 21 and 22 and including a lower plate 401, an upper plate 402, a central spindle 403 and a striker 404.
  • the central spindle 403 carries as precedingly a cam 405 cooperating with a lever 406 pivotally secured at 407 and includ ing a bolt-locking projection 408.
  • the lower plate 401 is provided with a diametrical housing for a striker-locking bolt 424 which held in said housing by a safety plate 425 underneath which is located a detonator carrier 426.
  • the bolt 424 is constituted by a recessed bar provided with a housing 427 for a primer, said housing communicating, before the arming of the fuse through the ports 428 and 429 with an annular housing 430 inside the detonator carrier 426.
  • the bolt holding the striker forms thus also a safety arrangement for the detonator.
  • the centre of gravity of the bolts is eccentric with reference to the axis of the striker so as to allow the movement of the bolt under the action of centrifugal force in the desired direction.
  • This movement may also be executed by means of a spring acting on the bolt.
  • the tubular central spindle 501 of the arming mechanism of the fuse carries a cam 502 (Figs. 26 to 31), said spindle being rcvolubly carried in a lower plate 503.
  • the lower plate 503 is provided as precedingly with a diametrical recess 409 for a bolt 510 located underneath the tip of a striker 404- shown cross-sectionally in Fig. 26.
  • Said striker extends inside the central tubular spindle 501.
  • the cam 502 is shown as provided with a receding section 504 for engagement with the nose 413 on the lever 406 pivotally secured at 407 (Figs. 28 and 29).
  • the cam 502 is provided with two shoulders 508 and 508 adapted to be engaged by a cam plug 509 guided between said shoulders on the inside of a stationary ring 510 rigid with the lower plate 503.
  • the cam plug 509 is axially guided inside the lower plate 503 and a spindle-holding plate 511 lying above the lower plate.
  • the cam plug is free inside its housing constituted by the receding section 504-508 of the cam and its outer surface is cylindrical.
  • the stationary ring 510 is provided with two ports or openings of which one 512 allows the pass-age therethrough of the nose 413 on the lever 406 while the second port 513 serves for the radial outward shifting of the cam plug 509.
  • the port 513 is formed beyond the port 512 in the direction of the arrow 414 illustrating the direction of rotation of the cam 502.
  • Fig. 28 illustrates the mechanism in its inoperative position for which the cam plug 509 is held in its cam engaging position by the stationary ring 510.
  • the cam plug 509 enters a position registering with the nose 413 of the lever 406 and prevents the latter from being shifted inwardly with reference to the cam.
  • said cam enters the position illustrated in Fig. 29.
  • the cam plug 509 registering now with the second port 513 in the ring 510 is urged centrifugally away from the shoulders 508 and 508' on the cam 502 and engages the cooperating surface 516 on the bearing block 515.
  • the cam 502 continues then rotating and when it has entered the position illustrated in Fig. 30, it has its receding section 504 registering with the first port 512 and with the nose 413 on the lever 406; consequently, the
  • lever 40 6 urged by a spring -R for instance pivots in the direction of the arrow 520 shown in Fig. 30 round the pin 407 and engages the receding section 504 in the earn 592. This pivotal movement of the lever 406'releases the striker bolt in the manner described with reference to Fig. 26.
  • the mechanism described hereinabove allows the earn 502 to execute a rotation through an angle longer than one revolution but less than two revolutions before it allows thelever 406 to rock. I obtain thus an arming mechanism with an increased safety on the path of the missile.
  • the stationary ring 520 is provided with a single port 521 both for the inward movement of the nose 413 on the lever 406-406 and for the outward movement of the plug 522 for the cam 523.
  • the receding section 524 in the cam 523 is not provided with any shoulder as in the case of the first example and it assumes the shapeof a cylindrical sector matching'the shape 'of the plug 52-2.
  • the bearing block 525 isengaged by the plug 522 when the cam is in the position for which'the outwardly shifted plug is shown in dot-and-dash lines in Fig. 31 i.e. when the cam 523 has executed a rotation by less than one complete revolution, starting from its inoperative position for which the receding section of the earn 524 lies on the right hand side of said cam, as illustrated in Fig. 31.
  • the safety arming mechanism is characterized by the fact that the central spindle is provided with a cam cooperating with a lever controlling the locking and the release of the striker bolt, said cam being provided with a depressed or receding section closed against the entrance of the lever into it before operation and during apart of the rotation of the central spindle by a camplug, while said cam is surrounded coaxially by a: stationary ring provided-with at least one port for the passage of the lever nose into the receding section ofthe cam and for the release of the cam plug.
  • This mechanism is designed in a manner such that the cam plug is held in its cam-closing position by the stationary ring and that during the rotation of the central spindle said plugprevents'first the nose on the lever from engaging said receding section of the cam, after which the plug moves'away from the cam'after it has passed underneath said nose through the passage afforded by the said port, whereby said cam is allowed to execute a rotation through an angle greater than one revolution before the lever is released and is allowed to pass through said port and to engage the receding section of the cam so as to release in'its turn the striker bolt.
  • a safety arming mechanism comprising a central axis of the central spindle to either side of a position of non-stable equilibrium, a regulating spring operatively connected with the rocking weight to urge it towards its position of non-stable equilibrium, an escape “mechanism operatively connecting the rocking weight with the central spindle to provide for constancy of the speed of rotation of the latter, a'bolt slidably mounted in the radially directed channel andengaging transversely in its.
  • a fuserfor a rotating-missile including afuse body and a striker slidable axiallyrthereof
  • a safety arming mechanism comprising a central spindle revolublyv carried axially of the fuse and provided with a central bore to slidingly house the striker and with.
  • a weight including two parallel arms, located symmetrically toeither, side of the central spindle and two parallel stays rigidly interconnecting said arms, a transverse spindle section rigid with each of said parallel arms and aligned along a common axis crossing perpendicularly the axis of, the central spindle, the center of gravity of said weight lying on the axis of the central spindle, said weight being adapted to rock with reference to the body ofthe fuse round said common spindle axis to either side of a position of non-stable equilibrium, a regulating spring operatively connected with the rocking weight to'urge it towards its position of non-stable equilibrium, an escape mechanism operatively connecting the rocking weight with the central spindle to provide for constancy of the speed of rotation of the latter, a bolt slidably mounted in the radial channel and engaging transversely in its original position the bore in the central spindle
  • a safety arming mechanism comprising a central spindle revolubly carried axially of the fuse and provided with a central bore carried axially of the fuse to slidingly house the striker and with a radially directed channel opening into said bore, a driving spring urging saidcentral spindle into rotation, a weight including two parallel arms, located symmetrically to either side of the central spindle and two parallel stays rigidly interconnecting said arms, a transverse spindle section rigid with each of said parallel arms and aligned along a@ common axis crossing perpendicularly the axis of the central spindle, the'center of gravity of said weight lying on the axis of the central spindle, said weight being adapted to rock with reference to the body of the fuse around said common spindle axis to either side of a position of non stable equilibrium, a coil springmounted, coaxially with reference to
  • a safety arming mechanism comprising a central spindle revolubly carried axially of the fuse and pro vided with a central bore to slidingly house the striker and with a radially directed channel opening into said bore, a coil spring arranged coaxially round the central spindle urging said central spindle into rotation, a weight adapted to rock with reference to the fuse body around an axis crossing perpendicularly the axis of the central spindle to either side of a position of non-stable equilibrium, a regulating spring operatively connected with the rocking weight to urge it towards its position of non-stable equilibrium, an escape mechanism operatively connecting the rocking weight with the central spindle to provide for constancy of the speed of rotation of the latter, a bolt slidably mounted in the radial channel and engaging transversely in its original position the bore in the central spindle to prevent the
  • a safety arming mechanism comprising a central spindle revolubly carried axially of the fuse and provided with a central bore to slidingly house the striker and with a radially directed channel opening into said bore, a driving spring urging said central spindle into rotation, 21 weight adapted to rock with reference to the fuse body around an axis crossing perpendicularly the axis of the central spindle to either side of a position of non-stable equilibrinm, a regulating spring operatively connected with the rocking weight to urge it towards its position of non-stable equilibrium, an escape mechanism operatively connecting the rocking weight with the central spindle to provide for constancy of the speed of rotation of the latter, a bolt slidably mounted in the radial channel, said bolt including a slotted section engaging transversely in its original position the bore in the central spindle to hold the
  • a safety arming mechanism comprising a central spindle revolubly carried axially of the fuse and provided with a central bore to slidingly house the striker and with a radially directed channel opening into said bore, a driving spring urging said central spindle into rotation, a Weight including two parallel arms, located symmetrically to either side of the central spindle and two parallel stays rigidly interconnecting said arms, a transverse spindle section rigid with each of said parallel arms and aligned along a common axis crossing perpendicularly the axis of the central spindle, the center of gravity of said weight lying on the axis of the central spindle, said weight being adapted to rock with reference to the body of the fuse around said common spindle axis to either side of a position of non-stable equilibrium, a regulating spring operatively connected with the rocking weight to urge it towards its
  • a safety arming mechanism comprising a central spindle revolubly carried axially of the fuse and provided with a central bore to slidingly house the striker and with a radially directed channel opening into said bore, two bearings in the fuse body for the opposite ends of said spindle respectively, a ferrule rigid with the central spindle, a driving spring urging said central spindle into rotation, one end of the spring being secured to the outer bearing and the other end to said ferrule, a weight adapted to rock with reference to the fuse body around an axis crossing perpendicularly the axis of the central spindle to either side of a position of non-stable equilibrium, a regulating spring operatively connected with the rocking weight to urge it towards its position of nonstable equilibrium, an escape mechanism operatively connecting the rocking weight with the central spindle to provide for constancy of the speed of rotation
  • a safety arming mechanism comprising a central spindle revolubly carried axially of the fuse and provided with a central bore to slidingly house the striker and with a radially directed channel opening into said bore, a driving spring urging said central spindle into rotation, a weight adapted to rock with reference to the fuse body around an axis crossing perpendicularly the axis of the central spindle to either side of a position of non-stable equilibrium, a regulating spring operatively connected with the rocking weight to urge it towards its position of non-stable equilibrium, an escape mechanism operatively connecting the rocking weight with the central spindle to proivde for constancy of the speed of rotation of the latter, a bolt slidably mounted in the radially directed channel and engaging transversely in its original position the bore in the central spindle to prevent the operative movement of the striker through said
  • a safety arming mechanism comprising a central spindle revolubly carried axially of the fuse and provided with a central bore to slidingly house the striker and with a radially directed channel opening into said bore, a driving spring urging said central spindle into rotation, a weight adapted to rock with reference to the fuse body around an axis crossing perpendicularly the axis of the central spindle to either side of a position of non-stable equilibrium, a regulating spring operatively connected with the rocking weight to urge it towards its position of non-stable equilibrium, an escape mechanism operatively connecting the rocking weight with the central spindle to provide for constancy of the speed of rotation of the later, a cam rigid with the central spindle, a bolt extending transversely of the central spindle through its radially directed channel and adapted to be shifted along said channel out of an original position
  • a safety arming mechanism comprising a central spindle revolubly carried axially of the fuse and provided with a central bore to slidingly house the striker and with a radially directed channel opening into said bore, a driving spring urging said central spindle into rotation, including two parallel arms located symmetrically to either side of the central spindle and two parallel stays rigidly interconnecting said arms, a transverse spindle section rigid with each of said parallel arms and aligned along a common axis crossing perpendicularly the axis of the central spindle, the center of gravity of said weight lying on the axis of the central spindle, said weight being adapted to rock with reference to the body of the fuse around said common spindle axis to either side of a position of non-stable equilibrium, a regulating spring operatively connected with the rocking weight to urge it towards its position of non-

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US513836A 1954-06-08 1955-06-07 Safety arming mechanism for fuses Expired - Lifetime US2895419A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH777779X 1954-06-08

Publications (1)

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US2895419A true US2895419A (en) 1959-07-21

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US513836A Expired - Lifetime US2895419A (en) 1954-06-08 1955-06-07 Safety arming mechanism for fuses

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US (1) US2895419A (pl)
BE (1) BE538731A (pl)
CH (1) CH319610A (pl)
FR (1) FR1132481A (pl)
GB (1) GB777779A (pl)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3017781A (en) * 1960-03-25 1962-01-23 John F Toomey Geared timing mechanism
US3073241A (en) * 1958-10-20 1963-01-15 Valerca Ets Safety device for the fuze of a gyrating missile during flight
US3120810A (en) * 1961-12-06 1964-02-11 Ralph G Eshleman Demolition firing device
US3124074A (en) * 1959-10-16 1964-03-10 Inertially armed fuze
US3162126A (en) * 1958-01-23 1964-12-22 Messrs Gebruder Junghans Ag Percussion fuze for projectiles without rifling
FR2428815A1 (fr) * 1978-06-12 1980-01-11 Mefina Sa Mecanisme de securite pour fusees de projectiles, de bombes, de mines ou d'engins explosifs

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT222546B (de) * 1958-09-24 1962-07-25 Karl Dipl Ing Leitner Geschoßzünder, insbesondere für Wurfgranaten
DE1118059B (de) * 1958-09-24 1961-11-23 Karl Leitner Dipl Ing Geschosszuender
DE1097325B (de) * 1959-01-30 1961-01-12 E H Helmut Junghans Dr Ing Mechanischer Aufschlagzuender fuer drallose Raketengeschosse
CN117339147B (zh) * 2023-12-04 2024-02-09 烟台优迈精密机械有限公司 多用途撞针式驱动器

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US289492A (en) * 1883-12-04 Time-shell
US1496271A (en) * 1923-06-22 1924-06-03 Junghans Oskar Percussion fuse
USRE16703E (en) * 1927-08-16 Andre vahatjd
US2083564A (en) * 1936-11-11 1937-06-15 Clarence F Hofstetter Fuse for bombs
US2149470A (en) * 1935-09-25 1939-03-07 Edgar Brandt Mechanical time fuse
US2183073A (en) * 1937-06-30 1939-12-12 Mifina S A Safety device for projectile fuses
US2369310A (en) * 1938-12-29 1945-02-13 Bendix Aviat Corp Mechanical time fuse
US2701527A (en) * 1948-07-06 1955-02-08 Louis P Granath Selective delayed-action fuze

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US289492A (en) * 1883-12-04 Time-shell
USRE16703E (en) * 1927-08-16 Andre vahatjd
US1496271A (en) * 1923-06-22 1924-06-03 Junghans Oskar Percussion fuse
US2149470A (en) * 1935-09-25 1939-03-07 Edgar Brandt Mechanical time fuse
US2083564A (en) * 1936-11-11 1937-06-15 Clarence F Hofstetter Fuse for bombs
US2183073A (en) * 1937-06-30 1939-12-12 Mifina S A Safety device for projectile fuses
US2369310A (en) * 1938-12-29 1945-02-13 Bendix Aviat Corp Mechanical time fuse
US2701527A (en) * 1948-07-06 1955-02-08 Louis P Granath Selective delayed-action fuze

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3162126A (en) * 1958-01-23 1964-12-22 Messrs Gebruder Junghans Ag Percussion fuze for projectiles without rifling
US3073241A (en) * 1958-10-20 1963-01-15 Valerca Ets Safety device for the fuze of a gyrating missile during flight
US3124074A (en) * 1959-10-16 1964-03-10 Inertially armed fuze
US3017781A (en) * 1960-03-25 1962-01-23 John F Toomey Geared timing mechanism
US3120810A (en) * 1961-12-06 1964-02-11 Ralph G Eshleman Demolition firing device
FR2428815A1 (fr) * 1978-06-12 1980-01-11 Mefina Sa Mecanisme de securite pour fusees de projectiles, de bombes, de mines ou d'engins explosifs

Also Published As

Publication number Publication date
FR1132481A (fr) 1957-03-12
GB777779A (en) 1957-06-26
CH319610A (fr) 1957-02-28
BE538731A (pl)

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