US2397781A - Fuse - Google Patents

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Publication number
US2397781A
US2397781A US555310A US55531031A US2397781A US 2397781 A US2397781 A US 2397781A US 555310 A US555310 A US 555310A US 55531031 A US55531031 A US 55531031A US 2397781 A US2397781 A US 2397781A
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Prior art keywords
cylindrical member
striker
fuse
holder
impact
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Expired - Lifetime
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US555310A
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Max W Fischer
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C9/00Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
    • F42C9/10Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition the timing being caused by combustion
    • 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
    • F42C15/18Arming-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
    • F42C15/184Arming-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
    • 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
    • F42C15/28Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids
    • F42C15/295Arming-means in fuzes; Safety means for preventing premature detonation of fuzes or charges operated by flow of fluent material, e.g. shot, fluids operated by a turbine or a propeller; Mounting means therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C9/00Time fuzes; Combined time and percussion or pressure-actuated fuzes; Fuzes for timed self-destruction of ammunition
    • F42C9/14Double fuzes; Multiple fuzes
    • F42C9/142Double fuzes; Multiple fuzes combined time and percussion fuzes in which the timing is caused by combustion

Description

April 1946. M. w. FISCHER 2,397,781
FUSE
Filed Aug. 5 19351 3 Sheets-Sheet 1 jwenib'r. J71. 0212607222:
Apria 2, 1946 M. w. FISCHER 2,397,781
FUSE
Filed Aug. 5, 1931 s Sheets-Sheet 2 HHHHHH liwezw J]. Z0. 1 2807062? diiorrzgq pril 2, 1946. M. w. FISCHER 2,397,731
FUSE
Filed Aug. 5, 1931 3 Sheets-Sheet 3 fiweim J17; Zflfiseker.
Patented Apr. 2, 1946 with 'E'ATES PATENT fiFliifiE Claims.
The invention relates broadly to aerial bombs and more particularly to a fuse therefor.
An object of the invention is to provide a fuse tor use in a highly explosive aerial bomb.
Another object of the invention is to provide a fuse for aerial bombs that may be set to be fired at one of several desired intervals of time after contact with a target.
A further object of this invention is to provide a fuse for aerial bombs that can be readily rendered safe after it has been armed for firing.
A still further object of the invention is to provide a fuse for an aerial bomb that is cheap to manufacture, simple and efficient in operation, and that is assembled and disassembled without injury to the operator.
With the above and other objects in view, the invention consistsin the construction, combination and arrangement of parts as will be described more fully hereinafter.
Reference is to be had to the accompanying drawings forming a part of this specification, and in which:
Fig. 1 is a longitudinal sectional view of the invention showing the fuse set in an unarmed position, time adjusting nut 25 adjusted to setting C;
Fig. 2 is a similar view showing the fuse set in an armed position for instantaneous firing, resulting from setting C;
Fig. 3 is a sectional view of the fuse firing mechanism set in position for delayed firing, resulting from setting A;
Fig. 4 is a sectional view of the fuse set for instantaneous firing resulting from setting C and at the moment of contact with a target;
Fig. 5 is a detail of the detonator holder, and
Fig. 6 is a detail of the detonator holder guide.
The fuse to be described hereinafter is .composed of a body member, a time element, a time adjusting mechanism, an arming mechanism and a detonating mechanism.
The body member I is provided with .a threaded portion 2 which is threaded into the shell 3 of an aerial bomb so that it extends partly within the bomb. The body member is divided into suitable compartments for the reception of the time element, detonating mechanism, and fulminate, all to be later described. The compartment holding the time element is open ended and is interiorly threaded at its open end to receive a threaded adapter ring 4 that is itself interiorly threaded.
The time element consists of a substantially cylindrical member 5 having a screw threaded extension 6 engageable in the adapterring 4. Cylindrical member 5 is rotatable in the body member 1 and is maintained in its proper alignment with respect to the body member by projections or shoulders 1. One of these projections receives an adjustable 'key 8 through which the cylindrical member 5 receives its rotation, as will be described later. Cushion washer 22 protects the time elements when member 5 is in the unarmed position and gasket '2! reduces the shock when the forward shoulder of member 5 comes in contact with adapter 4. Time element holders 9 and ID are mounted in the bore of the member 5, they being provided with firing pins H and i2, iulminate booster charges [3 and 14, time charges I 5 and I6, and primer caps I1 and I8. Firing pins II and I2 are held in time element holders 9 and I0 respectively by a crimp in the metal of the holder. The firing pins are easily forced out on impact under the action of striker 26. Time charges 15 and 15 are compressed black powder.
Vent holes '42 are to prevent building up a pressure which would change the time of burning of these charges. The time element holders are separated by a disk "I9 which is made of a material that, under ordinary circumstances, will sustain the pressure of the firing pin H, but if the setting of time adjustingnut 25 permits sufficient movement of striker 26 disk [.9 will beruptured as explained later when the bomb contacts with a target, permitting the firing. pin H to make contact with primer cap 18. This disk abuts against a shoulder 20 formed by increasing the diameter of the bore of the member 5. Shoulders 20 and 21 respectively prevent forward movement of time element holders ID and 9. Striker spring 24 prevents striker '26, when nut 29 allows su'flicient movement, irom striking primer cap 1'! until overcome by the force of striking a target. Time elements 9 and 10 are held against the respective shoulders 2'! and 28 by shear ring 2.8. When the time adjusting nut 25 is .set to permit suflicient movement of striker 26., this ring will be sheared on impact with a target as will be explained later.
On impact, the movement that striker 26 will have relative to member 5 is fixed by the setting of time adjusting nut 25 which is secured at any particular setting by pin 30.
The fuse is armed by the motion of propeller 29 as the bomb drops through the air. Propeller and nut 2.9 advance until they strike time adjusting nut 25. The energy created by the momentum of propeller and nut 29 is then transmitted through key 8 to member 5 causing it to rotate, which rotation is continued under the driving 26 and the permitted movement of the striker 7 relative to member 5.
Setting time adjusting nut 25 with mark aligned with the forward edge of nut 29 secures instantaneous action on heavy im act only. This setting leaves no space such as 39 in Fig.- 1. In arming, propeller and nut 29niove' member 5 forward as previously described, but'the arm-.
ing is slower as member 5 must be turned with the first movement of propeller and nut 29; and furthermore this setting allows no movement of striker '26 relative to member 5 upon impact with the target. The fuse can be detonated only by the shearing of the threads between extension 6 of member 5 and ring 4. These threads are made of such material that they will shear only on heavy impact and not on impact withli ht construction or water. The shearing permits firing pin l2 to detonate main detonator 31 which in turn detonates the tetryl booster. and bomb charge 40 Which in turn detonates the bomb itself. This setting is designed for assuring the bomb to pass through light decks or roofs and to burst on impact with'armor or concrete.
Setting time adjusting nut with mark A aligned with the forward edge of nut .29. secures a long delay in firing when the bomb is to be used against penetrable targets such as light decks, roofs, etc. This setting leaves a small space 39 which on arming leaves space M. Fig. 3, which, on impact with a light constructed tar et, allows sufficient movement of striker 26 relative to member 5 to strike and fire primer cap H but 7 not to move time element holder 9. The primer flame ignites time train I5 and in turn fulminate charge l3, the explosion of which forces firing pin El through shear disk 19 and fires primer cap 18. Primer cap IBignites time train l6 and in turn fulminate charge Mwhich drives firing pin l2 into the main fulminate detonator 31 which detonates the bomb aspreviously described. This long delayed action is designed to be used for impact on water from any altig This settude to give a depth charge effect. ting also gives instantaneous action on impenetrable targets such as heavy armor or concrete by shearing the threads between extension 6 and ring 4 as previously described.
Setting time adjusting nut 25 with mark B aligned with the forward edge ofnut 29 secures long delay on water impact from low altitudes. short delay on water impact from high altitudes and on penetrable targets and instantaneous action on impenetrable targets. This setting provides for a longer space 39 than. for setting A which on arming leaves a correspondingly longer space M, Fig. 2, and this on impact with a target allows sufficient movement of striker 2E relh ative to member 5 to shear disk I 9, fire primer cap 18 and ignite time charge It. This cuts the delay to one-half or less if desired. The difference between the actions on water impact from high altitudes and from low altitudes is governed by the strength of shear disk l9. At
low altitudes when the force of the impact is not suflicient to shear disk It the action will be as described under setting A for long delay. Upon heavy impact, the instantaneous action is as described under setting 0.
Setting time adjusting nut 25 with mark C aligned with the forward edge of nut 29, secures instantaneous action on all solid targets, long delay action on water impact from low altitudes and short delay action on water impact from high altitudes. This setting leaves a longer space 39 than for setting B which on arming leaves a correspondingly longerspace ll, Fig. 2, and this on impact with a target allows suflicient movement of striker 26 relative to member 5 to move time element holders 9 and Hi to shear the ring 28 allowing firing pin I2 to strike the main fulminate detonator 3?, giving instantaneous explosive action. Shear ring 28 is strong enough to withstand water impact. This setting therefore will give long delay on water impact from low altitudes and short delay on water impact from high altitudes as explained for setting B. However, it will shear on impact with a heavy deck whereas the threads between threaded extension 6 and ring 4 will shear only on heavy armor or concrete.
Fig. 3 shows how time adjusting nut 25 can be secured by lock pin 30 and slot 43 at each half turn. This is sufiiciently accurate for the required. x
The arming propeller-and-nut 29 are secured from rotation until just before the bomb is used. This is accomplished by propeller locking pin 33 and propeller locking pin holder 3!. The locking pin is secured in place between the propeller blades of which there are usually more than thetwo, shown in accompanying drawings. The lock ing pin holder is movable around the end of the fuse and is secured at any position by propeller holder lock screw 32 which also puts sufiicient pressure on pin 33 to hold it in place. V
In case the fuse has been armed unintentionally" or accidentally, itcan very conveniently be rendered safe for shipment; examination or readjustment, by removing it from the bomb, if already attached, and unscrewing the detonator holder guide one-fourth turn until its slot is parallel to the axis of the fuse, since the flat guide will act upon the coacting fiat portion of detonator holder 34 and rotate the holder so that the detonator 3'! is at right angles to the axis of the fuse. The fuse may then be disassembled and reassembled without danger to the operator. The detonator holder may be removed by unscrewing detonator holder closing plug 35.
It will be noted that the design has eliminated all complicated machine operations, thus lending itself to ready and cheap manufacture on automatic machines, punch presses or die casting machinery.
While in the foregoing there has been illustrated and described such combinations and arrangements of elements as constitute the preferred embodiment of this invention, it is nevertheless desired 'to emphasiz the fact that the interpretation of the invention should be conclusive only when made in the light of subjoined claims.
I claim:
1. An aero bomb fuse comprising a head formed with a cavity, a cylindrical member within said cavity, a firing pin at the rear end of said cylindrical member, a detonator holder held in-an unarmed position by said firing pin, a threaded ring at the mouth of said cavity, a threaded extension settings 7 tosaid cylindrical member passing through and engaging the threads of said ring, said engaged threads being of such material that they will shear only upon heavy impact, and a propeller fixedto the forward end of said extension Whereby said cylindrical member and firing pin are moved forward allowing said detonator holder to move to the armed position.
2. An aero bomb fuse comprising a head formed with a cavity with threads at its mouth, a cylindrical member having radial projections at each end for maintaining alignment within said cavity, two time element holders in tandem within cylindrical member each containing a primer cap, a time charge and a fulminate booster charge, said cylindrical member having two shoulders within to prevent respectively the forward move ment of said time element holders relative to said cylindrical member, a shear disk controlling the commencement of rearward movement of said forward time element holder relative to said cylindrical member, a shear ring controlling the commencement of rearward movement of said rear time element holder relative to said cylindrical member, a detonator holder held in an unarmed position by the firing pin of said rear time element holder, an inside and outside threaded ring engaging the threads at the mouth of said cavity, a cylindrical threaded extension to said cylindrical member passing through and engaging the inside threads of said ring, said engaged threads of said ring and extension being of such material that they will shear only on heavy hm pact, a striker passing through said threaded extension, a head on th rear end of said striker limiting its forward movement, a spring for controlling the commencement of the rearward movement of said striker relative to said cylindrical member, a key providing for rotation of said cylindrical member with said striker, a propeller-and-nut engaging the threads on the forward end of said striker whereby said cylindrical member and its contained elements are moved forward allowing said detonator holder to move to the armed position, a time adjusting nut limiting the forward movement of said propeller and-nut relative to said striker Which propellerand-nut in turn upon impact limits the rearward movement of said striker relative to said cylindrical member, a propeller locking pin and holder, and a detonator holder guide by which said detonator holder can be rotated and the fuse rendered safe after arming.
3. An aero bomb fuse comprising a head formed with a cavity with threads at its mouth, a cylindrical member having radial projections at each end for maintaining alignment within said cavity, two time element holders in tandem within said cylindrical member each containing a primer cap, a time charge and a fulminate booster charge, said cylindrical member having two shoulders within to prevent respectively the forward move ment of said time element holders relative to said cylindrical member, a shear disk controlling the commencement of rearward movement of said forward time element holder relative to said cylindrical member, a shear ring controlling the commencement of rearward movement of said rear time element holder relative to said cylindrical member, a detonator holder held in an unarmed position by the firing pin of said rear time element holder, an inside and outside threaded ring engaging the threads at the mouth of said cavity, a cylindrical threaded extension to said cylindrical member passing through and engaging the inside threads of said ring, said engaged threads of said ring and extension being of such material that they will shear only on heavy impact, a striker passing through said threaded extension, 2, head on the rear end of said striker limiting its forward movement, a spring for controlling the commencement of the rearward movement of said striker relative to said cylindrical member, a key providing for rotation of said cylindrical member with said striker, a propellerand-nut engaging the threads on the forward end of said striker whereby said cylindrical mem her and its contained elements are moved forward allowing said detonator holder to move to the armed position, and a time adjusting nut limiting the forward movement of said propeller-and-nut relative to said striker which propeller-and-nut in turn upon impact limits the rearward movement of said striker relative to said cylindrical member.
4. An aero bomb fuse comprising a head formed with a cavity with threads at its mouth, a cylindrical member having radial projections at each end for maintaining alignment within said cavity, two time element holders in tandem within said cylindrical member each containing a primer cap, a time charge and a fulminate booster charge, said cylindrical member having two shoulders within to prevent respectively the forward movement of said time element holders relative to said cylindrical member, a shear disk controlling the commencement of rearward movement of said forward time element holder relative to said cylindrical member, a shear ring controlling the commencement of rearward movement of said rear time element holder relative to said cylindrical member, a detonator holder held in an unarmed position by the firing pin of said rear time element holder, an inside and outside threaded ring engaging the threads at the mouth of said cavity, a cylindrical threaded extension to said cylindrical member passing through and engaging the inside threads of said ring, said engaged threads of said ring and extension being of such material that they will shear only on heavy impact, a striker passing through said threaded extension, a head on the rear end of said striker limiting its forward movement, a spring for controlling the commencement of the rearward movement of said striker relative to said cylindrical member, a key providing for rotation of said cylindrical member with said striker, a propeller-and-nut engaging the threads on the forward end of said striker whereby said cylindrical member and its contained elements are moved forward allowing said detonator holder to move to the armed position, a time adjusting not limiting the forward movement of said propeller-and-nut relative to said striker which propeller-and-nut in turn upon impact limits the rearward movement of said striker relative to said cylindrical member, and a detonator holder guide by which said detonator holder can be rotated and the fuse rendered safe after arming.
5. An aero bomb fuse comprising a head formed with a cavity with threads at its mouth, a cylindrical member having radial projections at each end for maintaining alignment within said cavity, two time element holders in tandem within said cylindrical member each containing a primer can, a time charge and a fulminate booster charge, said cylindrical member having two shoulders within to prevent respectively the forward movement of said time element holders relative to said cylindrical member, a, shear disk controlling the commencement of rearward movement of said forward time element holder relative to said cylindrical member, a shear ring controlling the commencement of rearward movement of said rear time element holder relative to said cylindrical member, a detonator holder held in an unarmed position by the firing pm of said rear time element holder, an inside and outside threaded ring engaging the threads at the mouth of said cavity, a cylindrical threaded extension to said cylindrical member passing through and engaging the inside threads of said ring, said engaged threads of said ring and extension being of such material that they Will shear only on heavy impact, a striker passing through said threaded extension,
7 a head on the rear end of saidflstrikerilimiting its forward movement, a spring for controlling the commencement of the rearward movement of said striker relative to said cylindrical member, a key providing for rotation of said cylindrical member with said striker, a, propeller-and-nut engaging the threads on the forward end of said striker whereby said cylindrical member and its contained elements are moved forward allowing said detonator holder to move to the armed position, a time adjusting nut limiting the forward movement of said propeller-and-nut relative to said striker which propeller-and-nut in turn upon impact limits the rearward movement of said striker relative to said cylindrical member, and a propeller locking pin and holder.
, MAX W. FISCHER.
US555310A 1931-08-05 1931-08-05 Fuse Expired - Lifetime US2397781A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2524060A (en) * 1945-05-22 1950-10-03 Lyle K Liljegren Projectile fuse
US2652777A (en) * 1941-07-15 1953-09-22 Raymond L Graumann Hydrostatic tail fuse
US2719458A (en) * 1950-05-31 1955-10-04 Albert M Stott Electrically fired percussion primer
US2742859A (en) * 1946-12-20 1956-04-24 Charles F Bowersett Nose fuze for a bomb
US2750888A (en) * 1946-11-13 1956-06-19 Robert O Wynn Long delay bomb tail fuze
US2754759A (en) * 1947-08-29 1956-07-17 Kenneth L Baker Time delay fuze for a rocket
US2883910A (en) * 1956-06-18 1959-04-28 Thomas G Nessler Airborne store ejector bolt
US2900907A (en) * 1952-05-07 1959-08-25 Marvin L Kempton Retardation device for the recovery of projectile components
US3103172A (en) * 1960-09-21 1963-09-10 Frank C Hutchison Fuze
US3112703A (en) * 1954-12-13 1963-12-03 Urdapilleta Jose Luis Amilibin Universal hand grenades and projectiles
EP2144033A2 (en) * 2008-07-11 2010-01-13 JUNGHANS Microtec GmbH Fuse for a projectile

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2652777A (en) * 1941-07-15 1953-09-22 Raymond L Graumann Hydrostatic tail fuse
US2524060A (en) * 1945-05-22 1950-10-03 Lyle K Liljegren Projectile fuse
US2750888A (en) * 1946-11-13 1956-06-19 Robert O Wynn Long delay bomb tail fuze
US2742859A (en) * 1946-12-20 1956-04-24 Charles F Bowersett Nose fuze for a bomb
US2754759A (en) * 1947-08-29 1956-07-17 Kenneth L Baker Time delay fuze for a rocket
US2719458A (en) * 1950-05-31 1955-10-04 Albert M Stott Electrically fired percussion primer
US2900907A (en) * 1952-05-07 1959-08-25 Marvin L Kempton Retardation device for the recovery of projectile components
US3112703A (en) * 1954-12-13 1963-12-03 Urdapilleta Jose Luis Amilibin Universal hand grenades and projectiles
US2883910A (en) * 1956-06-18 1959-04-28 Thomas G Nessler Airborne store ejector bolt
US3103172A (en) * 1960-09-21 1963-09-10 Frank C Hutchison Fuze
EP2144033A2 (en) * 2008-07-11 2010-01-13 JUNGHANS Microtec GmbH Fuse for a projectile
EP2144033A3 (en) * 2008-07-11 2013-06-19 JUNGHANS Microtec GmbH Fuse for a projectile

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