US2014393A - Fuse for projectiles - Google Patents

Fuse for projectiles Download PDF

Info

Publication number
US2014393A
US2014393A US728916A US72891634A US2014393A US 2014393 A US2014393 A US 2014393A US 728916 A US728916 A US 728916A US 72891634 A US72891634 A US 72891634A US 2014393 A US2014393 A US 2014393A
Authority
US
United States
Prior art keywords
striker
fuse
pin
casing
rotor
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
Application number
US728916A
Inventor
Marvin L Mathsen
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.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US728916A priority Critical patent/US2014393A/en
Application granted granted Critical
Publication of US2014393A publication Critical patent/US2014393A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F42C15/20Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin
    • F42C15/22Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges wherein a securing-pin or latch is removed to arm the fuze, e.g. removed from the firing-pin using centrifugal force

Definitions

  • This invention relates to a fuse for projectiles.
  • 'Ihe principal object of the invention is to provide a. bore-safe fuse in which a pair of relatively movable members are connected by linkage which function during ight to move one of the members to unarmed position and to hold it in such position until impact.
  • a further object is to associate one of said members with a mask whereby the mask cannot be removed until the fuse is in flight.
  • Another object is to provide astriker and ring pin with a bore-safe device.
  • FIG. 1 is a longitudinal sectional view of a fuse constructed in accordance with the invention and showing the parts in normal position.
  • Fig. 2 is a fragmentary sectional view showing the parts in position during flight.
  • Fig. 3 is a similar view of a modification.
  • Fig. 4 is a longitudinal sectional view of a further modication.
  • the fuse comprises a casing formed by a body 5 threadedly connected to a base 6 and a nose 1.
  • the base carries the usual booster charge 8, detonator 9 and houses a conventional rotor I0 mounted on a pivot pin II.
  • a primer I2 carried thereby is positioned axially of the fuse and in line with the detonator.
  • a ring pin I6 and a striker I'I are positioned axially of the fuse casing and are arranged with their adjoining ends intertted.
  • the lower end I8 of the striker is provided with a the spirit of the inven-l socket I9 for receiving the reduced upper end 20 of the firing pin.
  • a spring 2I in the socket normally urges the ring pin and striker apart and maintains the point I4 of the ring pin'in the blind cavity I5 of the rotor. 5
  • the ring pin and striker are connected by a plurality of sets of linkages, each consisting of a pair of links 22 and 23, respectively attached to the firing pin and striker by pivot pins 24 and 25 and linked to one another by a pivot pin 26.
  • the l0 adjoining end portions of the links carry weights 21.
  • the lower end 28 for convenienceA in manufacture bling the striker I1 includes a front part IIa which protrudes from the nose 1 of the casing. 20
  • a pin 32 in the nose I enters a longitudinally extending groove 33 in the part I'la and restrains the striker, against rotational displacement.
  • a sleeve 36 surrounding the spring 34 holds it against excessive lateral displacement.
  • a fuse a casing, an explosive unit in the casing, a member masking the explosive unit and mounted for movement to unmasking position, a striker ⁇ having its front end passing through the nose of the casing and having a socket-in its rear end, a spring normally holding the striker in for-- ward position with its front end protruding from the casing, a flring'pin having its front end disposed in the socket of the striker, a spring conned between the striker and firing pin and northe firing pin rearwardly into the path of movement of the masking member and linkages connecting the striker and firing pin and operable by centrifugal force to withdraw the ring pin from the path of movement of the masking member.
  • a fuse In a fuse, a casing, an explosive unit in the casing, a member masking the explosive unit and mounted for movement to unmasking position, a striker having its front end passing through the nose of the casing, a spring normally holding the striker in forward position with its front end protruding from the casing, aring pin in line with the striker,.a. spring confined between the striker and firing pin and normally urging the firing pin striker and ring pin and operable by .centrifugal force to withdraw the ring pin from of movement of the masking member.
  • a striker In a fuse, a striker, a firing pin coaxial with the striker, a spring normally urging the striker and firing pin apart, and linkages connecting the striker and firing pin and operable by centrifugal force during night of the fuse to relatively move the striker and ring pin towards one another.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Bags (AREA)
  • Automotive Seat Belt Assembly (AREA)

Description

Sept. 17, 1935. M. L. MATHsEN V r A2,014,393
FUSE FOR PRoJEcTILEs Filed June 4. 1954 fig-1- Fefeffi5-4f Marvin L- Mathsen Patented Sept. 17, 1935 UNITED STATES FUSE FOR PROJECTILES Marvin L. Matlisen, Rockaway, N. J.
Application June 4,
1934, serial Nanveasie l 3 Claims. (Cl. 102,-39) (Granted under the act of March 3, 1883, as
amended April The invention described herein may be manufactured and used by or for the Government for governmental purposes, without the lpayment to me of any royalty thereon.
This invention relates to a fuse for projectiles. j
'Ihe principal object of the invention is to provide a. bore-safe fuse in which a pair of relatively movable members are connected by linkage which function during ight to move one of the members to unarmed position and to hold it in such position until impact.
A further object is to associate one of said members with a mask whereby the mask cannot be removed until the fuse is in flight.
Another object is to provide astriker and ring pin with a bore-safe device.
With the foregoing and other objects in view,
may be made within the scope of what is claimed Without departing from tion.
A practical embodiment of the invention is illustrated in the accompanying drawing, wherein: Fig. 1 is a longitudinal sectional view of a fuse constructed in accordance with the invention and showing the parts in normal position.
Fig. 2 is a fragmentary sectional view showing the parts in position during flight.
Fig. 3 is a similar view of a modification.
Fig. 4 is a longitudinal sectional view of a further modication.
Referring to Figs. 1 and42 the fuse comprises a casing formed by a body 5 threadedly connected to a base 6 and a nose 1.
The base carries the usual booster charge 8, detonator 9 and houses a conventional rotor I0 mounted on a pivot pin II. When the rotor is in armed positionya primer I2 carried thereby is positioned axially of the fuse and in line with the detonator.
'I'he rotor is normally held in the unarmed position, masking the detonator by means of a transversely disposed bolt I3 adapted to be withdrawn from engagement with the rotor due to the action of centrifugal force and it is also held against rotation by the point I4 of a ring pin which is disposed in a blind cavity I5 in the rotor.
A ring pin I6 and a striker I'I are positioned axially of the fuse casing and are arranged with their adjoining ends intertted. the lower end I8 of the striker is provided with a the spirit of the inven-l socket I9 for receiving the reduced upper end 20 of the firing pin. A spring 2I in the socket normally urges the ring pin and striker apart and maintains the point I4 of the ring pin'in the blind cavity I5 of the rotor. 5
The ring pin and striker are connected by a plurality of sets of linkages, each consisting of a pair of links 22 and 23, respectively attached to the firing pin and striker by pivot pins 24 and 25 and linked to one another by a pivot pin 26. The l0 adjoining end portions of the links carry weights 21.
The lower end 28 For convenienceA in manufacture bling the striker I1 includes a front part IIa which protrudes from the nose 1 of the casing. 20 A pin 32 in the nose I enters a longitudinally extending groove 33 in the part I'la and restrains the striker, against rotational displacement. A
A sleeve 36 surrounding the spring 34 holds it against excessive lateral displacement.
In the modication shown in Fig. 3 the ring and need not be provided with a primer.
In the modification shown in Fig.' 4 the striker 39 -is in one piece and the firing pin 40 enters an aperture 4I in the base 42 of the fuse casing. It 35 directly engages a transversely movable slide 43. which masks the primer-detonator 44.
The operation of the fuse shown in Figs. 1 and the parts assume the positions shown in Fig. 2. The bolt I3 is moved by 'centrifugal force out of engagement with the rotor and the adjoining ends of the links 22 and 23, moving outward under the influence of centrifugal force, withdraw the firing pin from the rotor. The rotor, being now free, turns under the action of centrifugal force andv positions theprimer I2 in line with the detonator 9 and the point I4 of the ring pin.
On impact the striker and the iring pinv are driven rearwardly to actuate the primer. In ythe mally urging I claim. i 1. In a fuse. a casing, an explosive unit in the casing, a member masking the explosive unit and mounted for movement to unmasking position, a striker `having its front end passing through the nose of the casing and having a socket-in its rear end, a spring normally holding the striker in for-- ward position with its front end protruding from the casing, a flring'pin having its front end disposed in the socket of the striker, a spring conned between the striker and firing pin and northe firing pin rearwardly into the path of movement of the masking member and linkages connecting the striker and firing pin and operable by centrifugal force to withdraw the ring pin from the path of movement of the masking member.
2. In a fuse, a casing, an explosive unit in the casing, a member masking the explosive unit and mounted for movement to unmasking position, a striker having its front end passing through the nose of the casing, a spring normally holding the striker in forward position with its front end protruding from the casing, aring pin in line with the striker,.a. spring confined between the striker and firing pin and normally urging the firing pin striker and ring pin and operable by .centrifugal force to withdraw the ring pin from of movement of the masking member.
3. In a fuse, a striker, a firing pin coaxial with the striker, a spring normally urging the striker and firing pin apart, and linkages connecting the striker and firing pin and operable by centrifugal force during night of the fuse to relatively move the striker and ring pin towards one another. MARVIN L. MATHSEN.
the path of movement of the
US728916A 1934-06-04 1934-06-04 Fuse for projectiles Expired - Lifetime US2014393A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US728916A US2014393A (en) 1934-06-04 1934-06-04 Fuse for projectiles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US728916A US2014393A (en) 1934-06-04 1934-06-04 Fuse for projectiles

Publications (1)

Publication Number Publication Date
US2014393A true US2014393A (en) 1935-09-17

Family

ID=24928790

Family Applications (1)

Application Number Title Priority Date Filing Date
US728916A Expired - Lifetime US2014393A (en) 1934-06-04 1934-06-04 Fuse for projectiles

Country Status (1)

Country Link
US (1) US2014393A (en)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2441939A (en) * 1939-11-14 1948-05-18 Harry J Nichols Fuse
US2513185A (en) * 1945-02-03 1950-06-27 Us Navy Pressure armed fuse
US2537855A (en) * 1944-06-09 1951-01-09 Henry H Porter Point contact fuse
US2586437A (en) * 1943-11-13 1952-02-19 Us Navy Powder train interrupter
US2593775A (en) * 1944-08-14 1952-04-22 Gen Time Corp Fuse
US2700934A (en) * 1945-08-29 1955-02-01 Marion L J Lambert Centrifugal fuze unlatched by setback
US2818812A (en) * 1952-10-14 1958-01-07 Donald H Shenk Fuse
US2838999A (en) * 1954-04-27 1958-06-17 Bombrini Parodi Delfino Sensitive fuses
US2850980A (en) * 1955-07-08 1958-09-09 Albert E Stevenson Point detonating fuze for high velocity round
US2924176A (en) * 1955-09-21 1960-02-09 Jr Alois G Neuwirth Centrifugally armed and self-destroying impact fuze
US2934018A (en) * 1958-08-27 1960-04-26 Olin Mathieson Fuze
US2962968A (en) * 1955-09-21 1960-12-06 Jr Alois G Neuwirth Centrifugally armed and selfdestroying impact fuze
US2963974A (en) * 1958-05-09 1960-12-13 Bendix Corp Impact detonating fuze with arming delay
US2978984A (en) * 1958-04-10 1961-04-11 Czajkowski Norman Inertia time delay mechanism
US3022733A (en) * 1958-04-25 1962-02-27 Junghans Helmut Rotary shell fuze
US3090311A (en) * 1959-09-26 1963-05-21 Rheinmetall Gmbh Mechanical fuze for projectiles
US3102479A (en) * 1955-03-18 1963-09-03 Magnavox Co Fuze mechanism
US3374709A (en) * 1967-03-23 1968-03-26 Thiokol Chemical Corp Force-responsive actuator

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2441939A (en) * 1939-11-14 1948-05-18 Harry J Nichols Fuse
US2586437A (en) * 1943-11-13 1952-02-19 Us Navy Powder train interrupter
US2537855A (en) * 1944-06-09 1951-01-09 Henry H Porter Point contact fuse
US2593775A (en) * 1944-08-14 1952-04-22 Gen Time Corp Fuse
US2513185A (en) * 1945-02-03 1950-06-27 Us Navy Pressure armed fuse
US2700934A (en) * 1945-08-29 1955-02-01 Marion L J Lambert Centrifugal fuze unlatched by setback
US2818812A (en) * 1952-10-14 1958-01-07 Donald H Shenk Fuse
US2838999A (en) * 1954-04-27 1958-06-17 Bombrini Parodi Delfino Sensitive fuses
US3102479A (en) * 1955-03-18 1963-09-03 Magnavox Co Fuze mechanism
US2850980A (en) * 1955-07-08 1958-09-09 Albert E Stevenson Point detonating fuze for high velocity round
US2962968A (en) * 1955-09-21 1960-12-06 Jr Alois G Neuwirth Centrifugally armed and selfdestroying impact fuze
US2924176A (en) * 1955-09-21 1960-02-09 Jr Alois G Neuwirth Centrifugally armed and self-destroying impact fuze
US2978984A (en) * 1958-04-10 1961-04-11 Czajkowski Norman Inertia time delay mechanism
US3022733A (en) * 1958-04-25 1962-02-27 Junghans Helmut Rotary shell fuze
US2963974A (en) * 1958-05-09 1960-12-13 Bendix Corp Impact detonating fuze with arming delay
US2934018A (en) * 1958-08-27 1960-04-26 Olin Mathieson Fuze
US3090311A (en) * 1959-09-26 1963-05-21 Rheinmetall Gmbh Mechanical fuze for projectiles
US3374709A (en) * 1967-03-23 1968-03-26 Thiokol Chemical Corp Force-responsive actuator

Similar Documents

Publication Publication Date Title
US2014393A (en) Fuse for projectiles
US2129692A (en) Fuse
US2076602A (en) Fuse for projectiles
US1975809A (en) Fuse for projectiles
US1933608A (en) Combination fuse for projectiles
US2068708A (en) Fuse for projectiles
US2845866A (en) Fuse for a projectile and applications thereof
US2436837A (en) Fuse for antitank mines
US2043266A (en) Fuse for projectiles
GB987453A (en) Improvements in or relating to projectile fuzes
US1992926A (en) Fuse for projectiles
US1916244A (en) Fuse for projectiles
GB398052A (en) Improvements in or relating to percussion fuses for projectiles
US2513536A (en) All angle of impact inertia fuse
US1690331A (en) Supersensitive fuse for drop bombs
US1842467A (en) Point detonating fuse
US1563418A (en) Fuse
GB440338A (en) Improvements in or relating to percussion fuzes for projectiles
US1814059A (en) Fuse
US1518247A (en) Tracer fuse
US1775660A (en) Combination fuse for projectiles
US1955779A (en) Fuse for projectiles
US2495717A (en) Fuse
US1545866A (en) Instantaneous impact fuse for high-explosive shells
US1567232A (en) Percussion element for time fuses