US2778310A - Safety device for projectiles - Google Patents

Safety device for projectiles Download PDF

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Publication number
US2778310A
US2778310A US283600A US28360052A US2778310A US 2778310 A US2778310 A US 2778310A US 283600 A US283600 A US 283600A US 28360052 A US28360052 A US 28360052A US 2778310 A US2778310 A US 2778310A
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United States
Prior art keywords
safety device
spring
obturator
projectiles
safety
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Expired - Lifetime
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US283600A
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Brandt Edgar William
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Anstalt Fuer die Entwicklung von Erfindungen und Gewerblichen Anwendungen ENERGA
Original Assignee
Anstalt Fuer die Entwicklung von Erfindungen und Gewerblichen Anwendungen ENERGA
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Publication of US2778310A publication Critical patent/US2778310A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C1/00Impact fuzes, i.e. fuzes actuated only by ammunition impact
    • F42C1/02Impact fuzes, i.e. fuzes actuated only by ammunition impact with firing-pin structurally combined with fuze
    • 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
    • F42C15/24Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by inertia means
    • 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
    • F42C15/34Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein the safety or arming action is effected by a blocking-member in the pyrotechnic or explosive train between primer and main charge

Definitions

  • This invention relates to projectiles of the type comprising a head fuze and a detonator disposed towardsl kind comprising two parts which are movable relatively to loneanother, one ofwhich parts has ⁇ at* least one groovein which is engaged a sliding memberintegral with the other part, forming an obturator, and which is operated by a resiliently constrained member, for
  • the moving part of the device serves as a screen in the safety position, and must be dislodged passage for the transmission of fire from the head fuze to the detonator.
  • the safety device according to the present invention is characterised in that the resiliently constrainedthrust member is secured by itsfront end to the obturator and is provided: at its rear end with a valve which, under the v action of the thrust member, keeps the internal passage of the safety device closed until the principal obturator is completely released.
  • the muzzle safety device still functions by virtue of the fact that the valve hereinbefore referred to is forced under the action of the gases liable to pass between the two parts of the device, tightly against its seat.
  • the obturatoi in order to supplement the action of the safety device, has on its outer face a group of sealing grooves which, similarly to piston rings, oppose the passage of the gases between the two parts of the device, as long as the latter has not operated.
  • Fig. 1 illustrates the projectile in partial axial section
  • Fig. 2 is an enlarged axial section of the safety device denoted by the reference numeral 1 in Fig. 1;
  • FIG. 3 shows the functioning of the safety device shown in Fig. 2.
  • the safety device 1 of the present invention is interposed, in a hollow-charge kgrenade 2, between a head fuze 3 and a detonator 4, the latter havice ing the function of communicating the fire to a relay charge 5, which explodes the high explosive charge 6, the metal cap 7 of which lines the cavity 8.
  • Figures 2 and 3 show details ofthe construction of the safety device having, in a casing 1a a hollow inertia device or obturator 9, which carries two slides 10 each of which engages in a zig-zag groove 11 provided in the support 12.
  • An ejection spring 13 holds the inertia member 9 bearing against the slide 10 at the bottom of the blind part 11b of the groove 11 ( Figure 3). In this position, the obturator 9 prevents transmission of fire from the primer 14 to the detonator 4.
  • the spring 13 is secured at its yfront end to a nipple 15 firmly fitted in the solid head of the obturator 9, and a small seal 16 is fixed to the rear end of the spring 13, s0 that in the safety position, the seal 16 bears against a circular seating 17 formed in the base of the support 12 and thus reinforces the obturation provided by the inertia member 9.
  • the inertia member 9 is provided on its outer face with a series of grooves 18 which imposes a fauxd path on any accidental transmission of fire.
  • the inertia member 9 On firing the shot, the inertia member 9 under the influence' of the propulsive action, while following the movement imposed on it by the blind part 11b of the groove, compresses the thrust member or spring 13 by inertia and then, on the cessation of the positive acceleration, the spring 13 pushes the inertia member 9 towards the front and its slides ⁇ 10 follow respectively the branches .11a ofeach of the zig-zag grooves. As long as the spring 13 has not been completely slackened, the seal 16 remains in position and continues to close the passage provided in the base of the support 12.
  • a safety and delay device for a projectile fuse comprising a support with a longitudinally extending passage References Cited in the file of this patent UNITED STATES PATENTS Prato oct. 1o, 1944 Brandt May 6, 1952 FOREIGN VPATENTS Switzerland 1 Aug. 1, 1950

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Air Bags (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Automotive Seat Belt Assembly (AREA)
  • Emergency Lowering Means (AREA)

Description

Jan. 22, 1957 E. w. BRANDT SAFETY DEVICE FOR PRoJEcT'ILEs Filed April 22, 1952 ATTORNEY:
United States Patient O SAFETY DEVICE Fon rRoJEC'rILEs Edgar William Brandt, Geneva, Switzerland, assignor to Anstalt fur die Entwicklung von Erfindungen und Gewerblichen Anwendungen Energaj Vaduz, Liechtenstein, a corporation of Liechtenstein l Application April 22, 1952, Serial No. 253,618@
1 Claim. (Cl. 1112-73) This invention relates to projectiles of the type comprising a head fuze and a detonator disposed towardsl kind comprising two parts which are movable relatively to loneanother, one ofwhich parts has `at* least one groovein which is engaged a sliding memberintegral with the other part, forming an obturator, and which is operated by a resiliently constrained member, for
example, a spring. The moving part of the device serves as a screen in the safety position, and must be dislodged passage for the transmission of fire from the head fuze to the detonator.
The safety device according to the present invention is characterised in that the resiliently constrainedthrust member is secured by itsfront end to the obturator and is provided: at its rear end with a valve which, under the v action of the thrust member, keeps the internal passage of the safety device closed until the principal obturator is completely released.
The result produced by the aforedescribed arrangement is that until the end of the operation of the safety mechanism, the valve ensures perfect obturation, and
that, in the event of accidental percussion of the head'` fuze immediately after firing the shot, the muzzle safety device still functions by virtue of the fact that the valve hereinbefore referred to is forced under the action of the gases liable to pass between the two parts of the device, tightly against its seat.
According to one embodiment of the invention, in order to supplement the action of the safety device, the obturatoi has on its outer face a group of sealing grooves which, similarly to piston rings, oppose the passage of the gases between the two parts of the device, as long as the latter has not operated.
In order to enable the invention to be more readily understood, reference `is made to the accompanying drawings, Which" illustrate diagrammatically and by way of example, one embodiment thereof and in which:
Fig. 1 illustrates the projectile in partial axial section;
Fig. 2 is an enlarged axial section of the safety device denoted by the reference numeral 1 in Fig. 1; and
after the shot has been fred,`thereby freeing the useful Fig. 3 shows the functioning of the safety device shown in Fig. 2. Y
As shown in Fig. 1, the safety device 1 of the present invention is interposed, in a hollow-charge kgrenade 2, between a head fuze 3 and a detonator 4, the latter havice ing the function of communicating the fire to a relay charge 5, which explodes the high explosive charge 6, the metal cap 7 of which lines the cavity 8.
Figures 2 and 3 show details ofthe construction of the safety device having, in a casing 1a a hollow inertia device or obturator 9, which carries two slides 10 each of which engages in a zig-zag groove 11 provided in the support 12.
An ejection spring 13 holds the inertia member 9 bearing against the slide 10 at the bottom of the blind part 11b of the groove 11 (Figure 3). In this position, the obturator 9 prevents transmission of fire from the primer 14 to the detonator 4.
The spring 13 is secured at its yfront end to a nipple 15 firmly fitted in the solid head of the obturator 9, and a small seal 16 is fixed to the rear end of the spring 13, s0 that in the safety position, the seal 16 bears against a circular seating 17 formed in the base of the support 12 and thus reinforces the obturation provided by the inertia member 9.
In'order to ensure perfect tightness of the safety device, the inertia member 9 is provided on its outer face with a series of grooves 18 which imposes a baied path on any accidental transmission of fire.
On firing the shot, the inertia member 9 under the influence' of the propulsive action, while following the movement imposed on it by the blind part 11b of the groove, compresses the thrust member or spring 13 by inertia and then, on the cessation of the positive acceleration, the spring 13 pushes the inertia member 9 towards the front and its slides `10 follow respectively the branches .11a ofeach of the zig-zag grooves. As long as the spring 13 has not been completely slackened, the seal 16 remains in position and continues to close the passage provided in the base of the support 12. The inertia member or obturator 9, when ejected by the spring 13, frees the `firing orifice and by falling into the cavity 8 of the projectile, takes up position, together with the attached spring 13 and seal 16, near the primer 14, at 9a (Figure l). Since the spring 13 is secured to the obturator 9, it accompanies the latter whenit is displaced from the cap 8, so that lwhen the explosion occurs the spring is no longer in the field of action of the perforating jet. Experience shows that `the penetrating power of the hollow explosive charge is thereby improved.
It is obvious that the invention has only been described by way of example and that various modifications and alterations can be made thereto without departing from the scope thereof as defined by the appended claim.V
What I claim is:
A safety and delay device for a projectile fuse, comprising a support with a longitudinally extending passage References Cited in the file of this patent UNITED STATES PATENTS Prato oct. 1o, 1944 Brandt May 6, 1952 FOREIGN VPATENTS Switzerland 1 Aug. 1, 1950
US283600A 1946-11-02 1952-04-22 Safety device for projectiles Expired - Lifetime US2778310A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH620875X 1946-11-02
CH711928X 1951-04-24

Publications (1)

Publication Number Publication Date
US2778310A true US2778310A (en) 1957-01-22

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ID=31189211

Family Applications (2)

Application Number Title Priority Date Filing Date
US760425A Expired - Lifetime US2595757A (en) 1946-11-02 1947-07-11 Fuse
US283600A Expired - Lifetime US2778310A (en) 1946-11-02 1952-04-22 Safety device for projectiles

Family Applications Before (1)

Application Number Title Priority Date Filing Date
US760425A Expired - Lifetime US2595757A (en) 1946-11-02 1947-07-11 Fuse

Country Status (8)

Country Link
US (2) US2595757A (en)
BE (2) BE475670A (en)
CH (3) CH268198A (en)
DE (3) DE850418C (en)
FR (1) FR954538A (en)
GB (2) GB620875A (en)
LU (1) LU31364A1 (en)
NL (2) NL82408C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4815381A (en) * 1988-05-20 1989-03-28 Morton Thiokol, Inc. Multiple pulse inertial arm/disarm switch
WO2002073119A1 (en) * 2001-03-12 2002-09-19 Nico-Pyrotechnik Hanns-Jürgen Diederichs GmbH & Co. KG Igniter with a safety device for a projectile which is shot from a pipe with angular momentum

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE510153A (en) * 1946-11-02 Energa
US2712284A (en) * 1951-06-19 1955-07-05 Haroid E Thomas Delayed arming safety fuse
NL97798C (en) * 1953-12-24 Brandt Soc Nouv Ets
US3289588A (en) * 1954-03-16 1966-12-06 Aaron L Hitchens Caliber 50 spotting bullets
US2850979A (en) * 1954-04-19 1958-09-09 Magnavox Co Time delay control means
US2872868A (en) * 1955-07-11 1959-02-10 Jr William J Donahue Missile nose fuze
US2856855A (en) * 1955-10-13 1958-10-21 Samuel D Horowitz Retainer assembly for a fuze
US3018734A (en) * 1955-11-30 1962-01-30 Maguavox Company Delay firing mechanism
US2934019A (en) * 1956-02-02 1960-04-26 Charles R Olsen Fuze assembly
US2925778A (en) * 1957-03-15 1960-02-23 Stewart Warner Corp Helix type delay detent
DE1206977B (en) * 1958-05-21 1965-12-16 Gen Electric High voltage electrical conductor
US2926609A (en) * 1958-05-28 1960-03-01 Henry R Van Goey Gas operated safety and arming mechanism
BE629210A (en) * 1962-03-08
CH456403A (en) * 1966-07-28 1968-07-31 Tamerlan Ets Percussion fuze for projectile
US3760734A (en) * 1972-04-28 1973-09-25 Us Army Delayed arming device
US3960087A (en) * 1974-10-04 1976-06-01 The United States Of America As Represented By The Secretary Of The Navy Smoke and illumination signal
US4047485A (en) * 1975-12-24 1977-09-13 Motorola, Inc. Compact electrical fuze
CH617262A5 (en) * 1977-12-02 1980-05-14 Sarmac Sa
BE879302A (en) * 1978-12-22 1980-04-10 Sarmac Sa PERCUTANT HEAD ROCKET FOR EXPLOSIVE PROJECTILE
DE3373938D1 (en) * 1982-03-04 1987-11-05 Royal Ordnance Plc Improvements in or relating to safety devices for carrier shells
DE3426847C1 (en) * 1984-07-21 1992-04-09 Diehl Gmbh & Co Projectile-forming explosive charge insert
US4716830A (en) * 1985-07-29 1988-01-05 Morton Thiokol, Inc. Inertia safety and arming device
DE3827785A1 (en) * 1988-08-16 1990-02-22 Nico Pyrotechnik DISTANCE IGNITION WITH PRE-PIPE SAFETY
US7258068B2 (en) * 2003-06-30 2007-08-21 Kdi Precision Products, Inc. Safety and arming apparatus and method for a munition
DE102007016488B3 (en) * 2007-04-05 2009-01-22 Diehl Bgt Defence Gmbh & Co. Kg Penetallable projectile
US9689649B1 (en) * 2014-08-20 2017-06-27 The United States Of America As Represented By The Secretary Of The Army Obturator for 105MM projectile

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2360043A (en) * 1939-08-05 1944-10-10 Prato Cesare Del Percussion cap safety device for percussion fuses
CH268198A (en) * 1946-11-02 1950-05-15 Energa Safety device for detonator.

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DE304246C (en) *
DE299199C (en) *
GB190518185A (en) * 1905-09-08 1906-05-03 King S Norton Metal Company Lt Improvements in Fuzes for Lyddite Shells and other Explosive Projectiles.
US1053857A (en) * 1912-04-09 1913-02-18 Boforsgullspang Ab Shell-fuse with safety device.
US1208105A (en) * 1916-07-18 1916-12-12 William Dalton Projectile-fuse.
GB126684A (en) * 1917-02-10 1919-05-22 Rudge Whitworth Ltd Improvements in or relating to Percussion Fuzes for Projectiles.
FR513998A (en) * 1919-10-08 1921-02-28 Schneider & Cie Double-primer firing device for large caliber projectiles
DE359102C (en) * 1920-11-12 1922-09-19 Hermann Schirrmacher Fuse for the firing pin
FR611707A (en) * 1926-02-25 1926-10-09 Rocket safety
US1792631A (en) * 1929-01-09 1931-02-17 Stephen D Deevy Fuse for projectiles
FR695190A (en) * 1929-08-21 1930-12-12 Percussion fuze with delayed arming
BE417407A (en) * 1936-09-11
FR830370A (en) * 1936-12-04 1938-07-28 Highly sensitive rocket with delayed arming and adjustable operation
BE439558A (en) * 1939-08-05

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2360043A (en) * 1939-08-05 1944-10-10 Prato Cesare Del Percussion cap safety device for percussion fuses
CH268198A (en) * 1946-11-02 1950-05-15 Energa Safety device for detonator.
US2595757A (en) * 1946-11-02 1952-05-06 Energa Fuse

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4815381A (en) * 1988-05-20 1989-03-28 Morton Thiokol, Inc. Multiple pulse inertial arm/disarm switch
WO2002073119A1 (en) * 2001-03-12 2002-09-19 Nico-Pyrotechnik Hanns-Jürgen Diederichs GmbH & Co. KG Igniter with a safety device for a projectile which is shot from a pipe with angular momentum

Also Published As

Publication number Publication date
DE892871C (en) 1953-10-12
GB620875A (en) 1949-03-31
CH268198A (en) 1950-05-15
DE850418C (en) 1952-09-25
BE475670A (en)
CH289732A (en) 1953-03-31
NL69639C (en)
US2595757A (en) 1952-05-06
GB711928A (en) 1954-07-14
NL82408C (en)
LU31364A1 (en)
FR954538A (en) 1950-01-03
CH264011A (en) 1949-09-30
DE877573C (en) 1953-04-09
BE510153A (en)

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