US3726230A - Percussion fuse for projectiles - Google Patents

Percussion fuse for projectiles Download PDF

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Publication number
US3726230A
US3726230A US00093533A US3726230DA US3726230A US 3726230 A US3726230 A US 3726230A US 00093533 A US00093533 A US 00093533A US 3726230D A US3726230D A US 3726230DA US 3726230 A US3726230 A US 3726230A
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United States
Prior art keywords
bore
carrier
carrier means
fusing
towards
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
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US00093533A
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English (en)
Inventor
N Asikainen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SAMPELLA Oy AB
SAMPELLA SF Oy AB
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SAMPELLA Oy AB
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Filing date
Publication date
Priority claimed from DE19691960184 external-priority patent/DE1960184C/de
Application filed by SAMPELLA Oy AB filed Critical SAMPELLA Oy AB
Application granted granted Critical
Publication of US3726230A publication Critical patent/US3726230A/en
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Expired - Lifetime legal-status Critical Current

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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
    • F42C15/18—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
    • F42C15/184—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 using a slidable carrier
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00—Details of fuzes

Definitions

  • a percussion fuse for use in projectiles includes a cylindrical bore in a housing and a carrier in the bore for supporting at least one primer and which is moved to a fusing position where it may be detonated following firing of the projectile.
  • a resilient deformable seal ring is attached to the carrier and is deformed by the walls of the bore during movement therethrough to retard movement of the carrier and delay fusing.
  • a multiple position stop device may be used to stop a selected one of a plurality of different primers at the fusing position.
  • SHEET 3 [1F 3 IN VE N TOR o /69L ERA/0 As/K/I/mw PERCUSSION FUSE FOR PROJECTILES
  • This invention relates to improvements in percussion fuses for use in projectiles and more particularly to a construction for a percussion fuse which retards movement of a primer carrier and moves any one of a plurality of primers to fusing position.
  • a commonly known form of percussion fuse includes a carrier for supporting a primer which is movable from a releasably locked position to a fusing position where it may be detonated by a needle-bolt. Movement of the carrier to the fusing position is accomplished by spring means.
  • the primer carrier is released from its locked position by a safety device only after the projectile has left the gun barrel.
  • the spring means then acts to press on the primer carrier moving the primer carrier and causing the primer to be positioned within the range of action of the needle-bolt.
  • a delay device is required.
  • a common form of delay device is a gear and escapement mechanism which is coupled to the primer carrier.
  • Such a mechanism includes a greater number of separate mechanical parts requiring a substantial amount of space in the fuse casing and also is expensive since the mechanical parts must be manufactured with high percision.
  • Such a mechanism has the further disadvantage that it is sensitive to shock and blows, thus requiring a special mounting arrangement in the fuse casing. Assembly of a fuse requiring such a mechanism is costly.
  • a bore is provided in a housing for containing a slidably mounted carrier means for supporting at least one primer.
  • the carrier is movable between a position where it is retained by a releasable locking device and where the primer itself is outside of the range of action of a primer detonation device and a position where the primer may be detonated by the detonation device.
  • Spring biasing means is provided to move the carrier between the locked position and the fusing position, but this movement is retarded by a resilient deformable means such as an encircling seal ring mounted on the carrier which cooperates with the cylindrical bore of the housing and is deformed during movement of the carrier.
  • a delay time which is much longer than has been obtainable with previously known mechanisms is possible with the delay mechanism of the present invention.
  • the construction of the delay mechanism is greatly simplified and all mechanically moving parts of previously known delay mechanisms are eliminated.
  • the delay in movement of the primer carrier is effected solely by the deformation of the seal ring as the spring means pushes the carrier towards the fusing position. No additional space is required for the delay mechanism.
  • Other advantages of the improved delay mechanism include its reliability even under conditions of extreme cold, e.g., 40C which is not possible with previously known delay mechanisms.
  • Delay is not only caused by the deformation of the seal ring but also by the fact that air pressure builds up in the bore in which the primer carrier is located in advance of the seal ring as it is being pushed towards the fusing position.
  • the carrier and the spring means must overcome a back pressure as it moves forward.
  • the seal ring causes a vacuum to be generated behind it as it moves towards the fusing position whereby a cumulative double delay effect is obtained. It will be appreciated that the safety of the fuse is considerably increased in view of the lenthened duration of travel of the primer carrier. Furthermore, since the overall assembly is simplified the fuse housing itself can be shortened.
  • the cylinder bore in the fuse housing may be conically shaped whereby deformation of the seal ring producing the time delay is more efficiently initiated.
  • the deformation progresses gradually as the carrier moves along the bore and there is less chance that the carrier movement might be stopped prematurely by the resistance caused by the seal ring in contact with the cylinder bore wall.
  • the seal ring itself comprises at least one seal washer of elastic material such as a rubber or elastic plastic.
  • Polytetrafluorethylene known commercially as Teflon is a preferred material.
  • the seal washer may be retained between the carrier itself and a bush mounted on the carrier.
  • several seal discs having different diameters may be used. In such instances the washer in the forward position with respect to the direction of movement of the carrier is larger in diameterthan the cylinder bore. If there are two further washers, the one contiguous to and behind the first washer is smaller than the diameter of the carrier while the next adjacent washer has a larger diameter than the carrier.
  • the deformed projecting part of the largest seal washer is supported by the deformation of the other seal washers aspressure is applied against the inner wall of the bore.
  • the carrier may be designed to support more than one primer, the primers being spaced apart longitudinally along the carrier. This is desirable where a selection of primers is desired which when detonated will act at different speeds.
  • the carrier is provided with a step-shaped groove which may be engaged by a set screw mounted in the housing.
  • the set screw movement of the primer carrier can be limited to one of a number of positions whereby the selected primer may be located at the fusing position when the carrier stops.
  • FIG. 1 is a longitudinal section of a percussion fuse according to the invention
  • FIG. 2 is a side view of the fuse of FIG. 1 partially in section to show the central part in the transverse medial plane;
  • FIG. 3 is a cross-section along the line IIIIII of FIG.
  • FIG. 4 is a further embodiment of a percussion fuse according to the invention shown in longitudinal section;
  • FIGS. 5, 6 and 7 show the delay mechanism in detail at various stages during movement of the primer carrier.
  • FIGS. 8 and 9 show the movable primer carrier of FIG. 3 in two further positions.
  • the fuse shown generally at 1 includes a casing 2 having a cap portion 3 which conveniently is screwed into place on the casing.
  • the cap portion 3 includes a bore 4 in which a needle-bolt 6 is slidably mounted.
  • the needle-bolt 6 includes a head and is held in the percussion position by the helical and compressible spring 7.
  • An inertia shell 8 surrounds the needle-bolt 6 and is retained in a normal position by helical and compressible spring 9 which is presses against the head portion of the inertia shell 8 at the one end and against the casing 2 at the opposite end.
  • the head portion of the inertia shell presses against and retains retaining balls 10 in position.
  • a transverse bore 11 in casing 2 contains a transversely movable primer carrier 13 which itself includes a bore 14 having a closed end.
  • the bore 14 is designed to receive one end of the inertia shell 8 which is normally positioned only a short distance into the bore 14.
  • a plurality of primers 15 and 16 are arranged longitudinally in carrier 13, each of the primers having a different rate of action when detonated.
  • Carrier 13 is biased towards the right as seen in FIG. 1 by helical spring 17 which engages at its one end a screw cap 18 and the carrier 13 at the opposite end.
  • a preliminary percussion cap 19 is located adjacent the transverse bore 11 and a main percussion cap 20 is located on the opposite side of the preliminary percussion cap 19.
  • the primer carrier 13a is provided with an extension 13b which extends out of the casing 2 to indicate externally the position of the carrier 13a.
  • the primer carrier 13, 13a is secured against movement within the bore 11 by the engagement of the inertia shell 8 in bore 14.
  • the primer carrier may be additionally secured by a wire clip 21 which is inserted from the outside. When the gun barrel is loaded with the projectile, the wire clip 21 is removed.
  • the inertia shell 8 Upon firing the projectile the inertia shell 8 will be driven downwardly as seen in FIG. 1 compressing spring 9 and the end of the inertia shell 8 will extend more deeply into bore 14 in the carrier 13. The movement downwardly of the head of the inertia shell 8 releases the retaining balls 10 which drop aside into the space surrounding the spring 9. As acceleration of the projectile decreases the spring 9 overcomes the inertia of shell 8 and moves the shell upwardly beyond its original position since the head of the shell is no longer blocked by the retaining balls 10. The opposite end of the shell 8 moves out of the closed bore 14 in the carrier 13 thereby releasing the carrier. Spring 17 then pushes the primer carrier 13 towards the right as seen in FIG. 1.
  • the delay mechanism 22 begins to take effect. It consists of a sealing device having at least one seal washer.
  • the washers 23, 24 and 25 are secured between the primer carrier 13 and a bush 26 pressed onto the end of the carrier.
  • the washer 23 which is contiguous to the carrier body 13 has the largest diameter which is greater than the diameter of bore 11 in which the primer carrier 13 is movably positioned.
  • the seal washer 25 adjacent to bush 26 is greater in diameter than that of primer carrier 13 while the intermediate washer 24 is smaller in diameter than the diameter of carrier 13.
  • the entry to bore 1 1 is conical at 11a, the purpose being to facilitate the entry of the elastic seal washer 23 as it is deformed during movement of the carrier 13.
  • the projecting part of the seal washer 23 begins to deform and is bent down adopting an arcuate shape against the conical surface 11a.
  • the deformation increases as the carrier moves further along past the conical part 11a and then the deformation is stabilized as the carrier moves beyond the conical portion 11a. Since all three washers 23, 24 and 25 project over the flange section of bush 26, washers 25 and 24 are also elastically deformed when the primer carrier 13 is pushed further into bore 11.
  • the diameter of washer 25 is preferably such that this washer 25 comes to bear on the bent-down washer 23 thus reinforcing the pressure of the bent part of washer 23 against the walls of cylindrical bore 11.
  • the same reinforcement is obtained from the bending of the thicker intermediate washer 24.
  • a substantially air-tight seal is maintained between the primer carrier 13 and bore 11 so that the air in bore 11 in advance of the washers is compressed causing a counter-pressure to the action of spring 17.
  • a vacuum is generated in the space on the opposite side of the washers. This also contributes to the delay in the movement of primer carrier 13.
  • the delay mechanism 22 is actuated as the result of the elastic deformation of the washers.
  • the action of spring 17 becomes only slowly effective, and in this way the safety of the fuse is considerably increased and extended in time.
  • a set screw 27 is provided which may be regulated to adjust its extension into groove 28 in the carrier 13 or 13a.
  • the bottom of the groove 28 is stepped to provide stop surfaces 29 and 30.
  • the length of movement of the carrier 13 can be controlled depending upon which stop surface 29 or 30 the end of the set screw 27 contacts.
  • the set screw 27 is adjusted to project far enough that the primer carrier 13 is stopped when stop 29 reaches the end of the set screw 27 (FIG. 9). With the set screw 27 in a less extended position, stop surface 30 will come into contact with the end of the set screw so that the faster acting primer 15 is stopped at the fusing position below needle-bolt 6.
  • the fuse can be set to the fast or slow primer at any time before firing.
  • the set screw 27 can be designed as an additional safety device if it is adjusted to contact the surface of the carrier 13 while the carrier is in its retracted position. Thus, before the projectile is loaded in a gun, the set screw must be adjusted to one of the predetermined positions depending upon the primer desired.
  • a percussion fuse for use in projectiles comprising a. a housing,
  • primer detonation means movable along a first path in said housing
  • carrier means for supporting at least one primer and movable along said bore between a retained position adjacent said one end of said bore and at least one fusing position
  • said carrier means including sealing means engaging the surface of said bore to cause a vacuum to be created in said bore between one end thereof and said sealing means and increasing pneumatic pressure to be created in said bore between the opposite end of said bore and said sealing means as said carrier means, upon release of said locking means, moves from said retained position towards said fusing position,
  • a percussion fuse as claimed in claim 1 wherein said carrier means includes a plurality of stepped abutment means and means to support a plurality of primers arranged longitudinally thereon, said housing comprising adjustable stop means for engaging one of said stepped abutment means whereby any one of said primers can be preselected to automatically move to said fusing position by regulation of said stop means.
  • a percussion fuse for use in projectiles comprising a. a housing,
  • primer detonation means movable along a first path in said housing
  • a cylindrical bore in said housing defining a second path intersecting said first path, said bore being closed at at least one end, ssssssssssss d.
  • carrier means for supporting at least one primer and movable along said bore between a retained position adjacent said one end of said bore and at least one fusing position,
  • said carrier means including sealing means engaging the surface of said bore to cause a vacuum to be created in said bore between said one end thereof and said sealing means as said carrier means, upon release of said locking means, moves from said retained position towards said fusing position,
  • said sealing means comprising at least one deformable seal element mounted on said carrier means and having a greater peripheral diameter than said bore for engaging the surface of said bore, and
  • a percussion fuse for use in projectiles comprising a. a housing,
  • primer detonation means movable along a first path in said housing
  • carrier means for supporting at least one primer and movable along said bore between a retained position adjacent said one end of said bore and at least one fusing position
  • inertia actuated releasable locking means for retaining said carrier means in said retained position and against movement by said biasing means towards said fusing position
  • said carrier means including sealing means engaging the surface of said bore to cause a vacuum to be created in said bore between said one end thereof and said sealing means as said carrier means, upon release of said locking means, moves from said retained position towards said fusing position,
  • said sealing means comprising a pair of deformable seal elements mounted on said carrier means a spaced distance from each other, one of said seal elements having a peripheral diameter greater than that of said bore and the other of said seal elements having a peripheral diameter greater than that of said carrier means and an intermediate element mounted on said carrier means positioned between said one and other seal elements and having a peripheral diameter less than that of said carrier means whereby said other and intermediate elements reinforce the pressure of said one seal element against the surface of said bore to maintain a substantially airtight seal,

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Toys (AREA)
  • Fuses (AREA)
US00093533A 1969-12-01 1970-11-30 Percussion fuse for projectiles Expired - Lifetime US3726230A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691960184 DE1960184C (de) 1969-12-01 Aufschlagzünder, vornehmlich für Wurfgeschosse, mit querbeweglichem Zündpilleträger

Publications (1)

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US3726230A true US3726230A (en) 1973-04-10

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US00093533A Expired - Lifetime US3726230A (en) 1969-12-01 1970-11-30 Percussion fuse for projectiles

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US (1) US3726230A (da)
CA (1) CA942581A (da)
DK (1) DK132914C (da)
FI (1) FI52003C (da)
FR (1) FR2072723A5 (da)
GB (1) GB1303464A (da)
IL (1) IL35686A (da)
NO (1) NO126592B (da)
SE (1) SE361213B (da)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR342099A (da) *
US1689470A (en) * 1925-02-20 1928-10-30 Adelman Arthur Bore safety device for fuses
US1848355A (en) * 1930-11-12 1932-03-08 John M King Combination fuse
US2705921A (en) * 1949-12-15 1955-04-12 Jr John W Moseman Fuze for non-rotating shaped charge projectiles
US2870713A (en) * 1955-06-09 1959-01-27 Saloranta Arvo Ensio Fuse for shells
US2958285A (en) * 1959-10-08 1960-11-01 Robert P Marshall Fuze component design

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR342099A (da) *
US1689470A (en) * 1925-02-20 1928-10-30 Adelman Arthur Bore safety device for fuses
US1848355A (en) * 1930-11-12 1932-03-08 John M King Combination fuse
US2705921A (en) * 1949-12-15 1955-04-12 Jr John W Moseman Fuze for non-rotating shaped charge projectiles
US2870713A (en) * 1955-06-09 1959-01-27 Saloranta Arvo Ensio Fuse for shells
US2958285A (en) * 1959-10-08 1960-11-01 Robert P Marshall Fuze component design

Also Published As

Publication number Publication date
DK132914C (da) 1976-07-19
FI52003C (fi) 1977-05-10
DE1960184A1 (da) 1971-08-26
GB1303464A (da) 1973-01-17
CA942581A (en) 1974-02-26
FR2072723A5 (da) 1971-09-24
IL35686A0 (en) 1971-04-28
DK132914B (da) 1976-02-23
SE361213B (da) 1973-10-22
FI52003B (da) 1977-01-31
IL35686A (en) 1974-12-31
NO126592B (da) 1973-02-26

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