US1755023A - Electric fuse for projectiles - Google Patents

Electric fuse for projectiles Download PDF

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Publication number
US1755023A
US1755023A US200683A US20068327A US1755023A US 1755023 A US1755023 A US 1755023A US 200683 A US200683 A US 200683A US 20068327 A US20068327 A US 20068327A US 1755023 A US1755023 A US 1755023A
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United States
Prior art keywords
condenser
current
coil
wire
projectile
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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
US200683A
Inventor
Ruhlemann Herbert
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.)
Rheinische Metallwaaren and Maschinenfabrik AG
Original Assignee
Rheinische Metallwaaren and Maschinenfabrik AG
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
Priority to BE350641D priority Critical patent/BE350641A/xx
Priority to BE350642D priority patent/BE350642A/xx
Priority to NL27541D priority patent/NL27541C/xx
Priority to NL27722D priority patent/NL27722C/xx
Priority to BE343130D priority patent/BE343130A/xx
Priority claimed from DER67999D external-priority patent/DE476379C/en
Priority to DER69907D priority patent/DE486942C/en
Priority claimed from DER71029D external-priority patent/DE486944C/en
Priority to DER71029D priority patent/DE486944C/en
Priority to CH127058D priority patent/CH127058A/en
Application filed by Rheinische Metallwaaren and Maschinenfabrik AG filed Critical Rheinische Metallwaaren and Maschinenfabrik AG
Priority to FR638284D priority patent/FR638284A/en
Priority to GB17105/27A priority patent/GB273338A/en
Priority to CH132353D priority patent/CH132353A/en
Priority to FR35264D priority patent/FR35264E/en
Priority to FR35409D priority patent/FR35409E/en
Priority to US270465A priority patent/US1791606A/en
Priority to GB1188828A priority patent/GB289436A/en
Priority to GB12252/28A priority patent/GB289473A/en
Priority to DER75975D priority patent/DE491466C/en
Priority to DER78400D priority patent/DE502303C/en
Priority to US432865A priority patent/US1858969A/en
Priority claimed from US432865A external-priority patent/US1858969A/en
Publication of US1755023A publication Critical patent/US1755023A/en
Application granted granted Critical
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C11/00Electric fuzes
    • F42C11/04Electric fuzes with current induction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C11/00Electric fuzes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C11/00Electric fuzes
    • F42C11/06Electric fuzes with time delay by electric circuitry
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C17/00Fuze-setting apparatus
    • F42C17/04Fuze-setting apparatus for electric fuzes

Definitions

  • the ignition of the priming-composition for the explosive mlxture is, as is well known, effected by a heating wire which is automatically switched into the circuit of a source of current.
  • accumulators dry cells or wet cells, or generators actuated by the rotating movement of the projectile.
  • the current operates a" switch gear which after a certain adjustable period of time closes the circuit of the current source across the heating Wire and 'in this manner effects the ignition of the priming-composition.
  • the ignition is e ected at an exactly determined point of time after firing of the projectile by proportioning the strength of current flowing from the current source to the ignition wire which current according to the adjusted strength heats the wire after a shorter or longer action to the degree necessary for the ignition of the priming-composition.
  • the adjustment of the current to the strength necessary for obtaining the desired ignition time point may for instance preferably be effected by a regulating resistance connected in series with the heating wire.
  • This manner of regulation is suitablefor any current source used and permits an exact determination of the time point of ignition.
  • the strength of the current may, however, be regulated in another manner by a regulating device particularly suitable for the special source of current used.
  • a permanent magnet is used as sourceof current for electrical time-fuses which magnet in the moment of firing of the projectile makes a movement relative to or in a coil and generates an induction current in this coil which serves for heatmg the heating wire of the priming-composition.
  • This current source used hitherto for impact-fuses only has, compared with the cells, accumulators or generators used with the known time-fuses, the advantage of being sim 1e, insensible and capable of being stored or an indefinite period of time.
  • the current generated is, fort e purpose 'of obtaining more advanced oints of time of ignition, also, not passed irectly through the regulating resistance to the ignition wire, but this current is used first for loading a condenser which discharges over the reslstance adjusted to a certain height and over the ignition wire.
  • Fig. 1 shows a longitudinal section of a fuse according to the invention
  • 2 is a cross section on the line A-B
  • Fig. 3 shows diagrammatically the electrical connections
  • Fig. 4 is a detail of the modification shown in Fig. 3.
  • a permanent magnet a is arranged shiftable in the longitudinal direction.
  • the magnet the lock spring b.
  • a coil body a wound with several turns d of insulated copper-wire is fixed in the head of the projectile.
  • the two ends of the turns (l are connected to a condenser f which, for instance, may be formed as a aper condenser with two tinfoils isolated y insulating paper.
  • the one end of the turns d is connected across the contact to the one tin-foil of the condenser 7, while the other endof the turns cl is led over contact (1 to a metal strip 2' which is stretched across the path of the magnet a and over contact A: to the other tin-foil of the condenser
  • the conductors e, g, i and k are insulated from the body of the projectile.
  • the tin-foil of the condenser 7 connected to the'contact e is also connected to the insulated conductor Z.
  • Connected to this conductor at m is the one end of a thin resistance Wire 0 embedded in the priming-composition n and serving as heating or ignition wire.
  • This wire may, in the manner of the filament of an incandescent lamp, be wound or bent in a spiral or coil or in zigzag.
  • a wire of Silit or of a similar material may be used.
  • the other end of the resistance wire is connected at p to the contact 9 which in turn slides upon the surface of a resistance r arranged in a circle.
  • the resistance 1' is insulated and unmovably arranged in a ring 8 which is rotatably and adjustably mounted in the head of the projectile.
  • the rin s has in this construction the function 0 the usual composition ring in burning-fuses.
  • the one end of the resistance r which in the example illustrated forms an angularly bent, helically woundwire is free, whereas its other end -'is electrically connected to the head of the projectile by means of a screw't.
  • the magnet a When firing the projectile the magnet a by the inertia of its mass comes free from the locking springs?) and moves to the rear in the head of the projectile. During this move ment the lines of force of the magnet intersect the turns of the coil 12 and generate in the latter an induction current by which the condenser is loaded, as this coil d, as stated above, is connected to both coatings of the condenser f. Shortly before reaching its rear end position the magnet a impacts upon the metal strip 71 and bends same in the middle. Hereby the one end of the metal strip is withdrawn from the contact The circuit of the coil d across the condenser f is opened and the loaded condenser f is disconnected from the coil d.
  • the circuit of the condenser across the heating wire 0 of the priming-composition n is closed by the metal strip 11 bent in its m'iddle by the magnet to such an extent as to make contact with the rear closing nut of the head of the projectile.
  • the current flows from the one tinfoil of the condenser [through the conductor Z and the screw m to the heating wire 0 from which the current passes through the screw 12 and the contact 9 to the resistance r.
  • the current flows there through a greater or smaller number of wire turns, i. e. a greater or smaller length of the resistance wire itself until it passes at the end at t into the body of the projectile and returns throu h the latter to the metal strip P Q 0,2 1.] .r.tg-cal.
  • T e ring 8 is for this purpose, as the priming-composition of burning-fuses, provided with a scale indicating the ignition tim'e points after firin which together with a mark at the head o the projectile permits to read oil the ignition time'adjusted.
  • the magnet a on firing of the projectile moves through the coil (1 and generates in the latter an induction current which loads the condenser f.
  • the current in this case flows from the one end Z of the coil (1 through the points 2, 3, 4, to the other end 6 of the coil d.
  • a part of the induction current ows in a second circuit 1, 2, 7, 8, 9, 10, 11, 12, 6 through the primingecomposition n and an exactly adjusted constant resistance w.
  • This second circuit causes a preheating of the ignition Wire 0. If, for instance, the detonation point is at 400 C. the ignition wire is preheated by this circuit to a temperature of about 350 C. At the end-of the movement of the magnet a with regard to the coil d, the latter is disconnected from the condenser f and moreover the circuit for preheating the ignition wire is opened. The metal stri i then comes into the position shown in dotted lines and hereby closes the condenser f over the ignition wire 0 and the strength after a longer period of action only, A
  • resistance 1' adjustable by. the moving contact u.
  • the discharge of the condenser 1 then takes place from the one tinfoil 4 through the points 3, 13, 14, 15, 10, 11, 12, 6 to its second coating 5.
  • This current furnished by the condenser f during the flight of the projectile is proportioned by the resistance 1' in.
  • an automatically actin contact device may be used by means of whic when the projectile impacts upon an aim, the electric energy generated by the movement at the magnet a in the induction coil is passed through the ignition wire 0, so that the ignition of the priming-composition is caused.
  • said condenser and to close the circuit through said regulating resistance and said heating wire, for the purpose of permitting the condenser to discharge, and a contact device for automatically shortcircuiting the regulating resistance in the circuit from said condenser to said heating Wire, said contact device acting when the projectile impacts upon an aim earlier than the time- :fuse has come to action.
  • a heating wire for igniting the priming-composition in combination anexplosive mixture, :1 priming-composition, a heating wire for igniting the priming-composition,-a source of current in a circuit containing the said heating. wire, means for regulating the stren th of the current fiowin to the heating wire for the purpose o heating said wire to the degree requiredcfor igniting the priming-com )osition after a shorter or lon er duration ot the action of the current, an a contact device for automatically short-circuiting the regulating resistance in the circuit from said condenser to said heating wire, said contact device acting when the projectile impacts upon an aim earlier than the timefuse has come to action.
  • an electric time-fuse for projectiles in combination an explosive mixture, a priming composition, a heating Wire for igniting said priming composition, an induction coil, a permanent magnet movably mounted in said coil, said magnet being shifted in said coil and generates electric energy when the projectile is fired, a circuit connecting said energy generator with the heating wire, a condenser in said circuit loaded by said energy generator, a regulating resistance in the circuit of the heating Wire, and a movable contact in said circuit in the ath of said movable magnet, said contact eing, at the end of the movement of said magnet, shifted by said magnet to cut the said coil from said condenser and to close the circuit through said-regulating resistance and said heating wire, for the purpose of permitting the condenser to discharge.
  • condenser in said circuit loaded by said: energy generator, a regulating resistance n the circuit of the heating wire, a movable contact in said circuit in the path of said movable magnet, said contact being, at the end of the movement of said magnet, shift-ed'by said magnet to cut the said coil from said condenser and to close the circuit through said regulating resistance and said heating wire, for the urpose of permitting the condenser to disc arg'e,and means for preheatsignature.

Description

April 15, 1930. H. RUHLEMANN ELECTRIC FUSE FOR PROJECTILES Filed June 22, 1927 INVENTD R HE/"Lerf FJI LZeman-n BY J 4' ATI'EI FKNEY.
Patented Apr, 15, 1930 cairn HERBERT nimrmemr, or .SOMMERDA, GERMANY, ASSIGNOR T anmmsonn ME- TALLWAAREN- UNID mescnmnnrena, on nussELDoRr-nnnmoar, GERMANY,
A CORPOTION" 0F GERMANY ELECTRIC m en non rnomorrnns Applipation filed. .Tune 22, 1927, Serial No. 200,683, and in Germany June 28, 1926.
In electric fuses for projectiles, whether timeor impact-fuses, the ignition of the priming-composition for the explosive mlxture is, as is well known, effected by a heating wire which is automatically switched into the circuit of a source of current. As current sources in time-fuses are used accumulators dry cells or wet cells, or generators actuated by the rotating movement of the projectile. The current operates a" switch gear which after a certain adjustable period of time closes the circuit of the current source across the heating Wire and 'in this manner effects the ignition of the priming-composition.
These complicate andsensitive intermediate switch gears are dispensed with in fuses according to the invention. As roposed by the invention, the ignition is e ected at an exactly determined point of time after firing of the projectile by proportioning the strength of current flowing from the current source to the ignition wire which current according to the adjusted strength heats the wire after a shorter or longer action to the degree necessary for the ignition of the priming-composition.
The adjustment of the current to the strength necessary for obtaining the desired ignition time point may for instance preferably be effected by a regulating resistance connected in series with the heating wire. This manner of regulation is suitablefor any current source used and permits an exact determination of the time point of ignition. The strength of the current may, however, be regulated in another manner by a regulating device particularly suitable for the special source of current used.
According-to the present invention a permanent magnet is used as sourceof current for electrical time-fuses which magnet in the moment of firing of the projectile makes a movement relative to or in a coil and generates an induction current in this coil which serves for heatmg the heating wire of the priming-composition. This current source used hitherto for impact-fuses only has, compared with the cells, accumulators or generators used with the known time-fuses, the advantage of being sim 1e, insensible and capable of being stored or an indefinite period of time. c
As the current generation by the permanent magnet is efiected and continued durin a short eriod of time, the current generated is, fort e purpose 'of obtaining more advanced oints of time of ignition, also, not passed irectly through the regulating resistance to the ignition wire, but this current is used first for loading a condenser which discharges over the reslstance adjusted to a certain height and over the ignition wire.
By the use of the invention 1n combination with a permanent magnet which in well known manner for the current generation makes a relative movement when the projectile impacts upon an aim only, a simple and efiective electric impact-fuse with adjustable retardation also is provided and by a suitable arrangement and construction of the internal electric device a pure electric double-fuse is provided. 7
In the accompanying'drawings some modifications of electric fuses according to the invention are shown by way of example in connection with a time-fuse. v
Fig. 1 shows a longitudinal section of a fuse according to the invention, 2 is a cross section on the line A-B Fig. 3 shows diagrammatically the electrical connections and Fig. 4 is a detail of the modification shown in Fig. 3.
In the longitudinal axis of the projectile a permanent magnet a is arranged shiftable in the longitudinal direction. The magnet the lock spring b. Around the magnet a is arranged a coil body a wound with several turns d of insulated copper-wire. The coil body a is fixed in the head of the projectile. The two ends of the turns (l are connected to a condenser f which, for instance, may be formed as a aper condenser with two tinfoils isolated y insulating paper. The one end of the turns d is connected across the contact to the one tin-foil of the condenser 7, while the other endof the turns cl is led over contact (1 to a metal strip 2' which is stretched across the path of the magnet a and over contact A: to the other tin-foil of the condenser The conductors e, g, i and k are insulated from the body of the projectile.
-The tin-foil of the condenser 7 connected to the'contact e is also connected to the insulated conductor Z. Connected to this conductor at m is the one end of a thin resistance Wire 0 embedded in the priming-composition n and serving as heating or ignition wire. This wire may, in the manner of the filament of an incandescent lamp, be wound or bent in a spiral or coil or in zigzag. Instead of an ordinary resistance wire a wire of Silit or of a similar material may be used. The other end of the resistance wire is connected at p to the contact 9 which in turn slides upon the surface of a resistance r arranged in a circle. -The resistance 1' is insulated and unmovably arranged in a ring 8 which is rotatably and adjustably mounted in the head of the projectile. The rin s has in this construction the function 0 the usual composition ring in burning-fuses. The one end of the resistance r which in the example illustrated forms an angularly bent, helically woundwire is free, whereas its other end -'is electrically connected to the head of the projectile by means of a screw't.
When firing the projectile the magnet a by the inertia of its mass comes free from the locking springs?) and moves to the rear in the head of the projectile. During this move ment the lines of force of the magnet intersect the turns of the coil 12 and generate in the latter an induction current by which the condenser is loaded, as this coil d, as stated above, is connected to both coatings of the condenser f. Shortly before reaching its rear end position the magnet a impacts upon the metal strip 71 and bends same in the middle. Hereby the one end of the metal strip is withdrawn from the contact The circuit of the coil d across the condenser f is opened and the loaded condenser f is disconnected from the coil d.
At the same time the circuit of the condenser across the heating wire 0 of the priming-composition n is closed by the metal strip 11 bent in its m'iddle by the magnet to such an extent as to make contact with the rear closing nut of the head of the projectile. Thereby the current flows from the one tinfoil of the condenser [through the conductor Z and the screw m to the heating wire 0 from which the current passes through the screw 12 and the contact 9 to the resistance r. According to the angular position of the ring a inthe head of the projectile, the current flows there through a greater or smaller number of wire turns, i. e. a greater or smaller length of the resistance wire itself until it passes at the end at t into the body of the projectile and returns throu h the latter to the metal strip P Q 0,2 1.] .r.tg-cal.
that is to say the amount of'heat generated depends upon the strength of the current.
As a quite definite degree of heat is re uired for igniting the riming-composition, t e ignition will beeflected with a current of low whereas with a high strength of current ignltion takes place aftera short period of t me already. By 'means of the regulating resistance r the strengthof the current and thereby the desired time necessar for causing ignition may be adjusted. T e ring 8 is for this purpose, as the priming-composition of burning-fuses, provided with a scale indicating the ignition tim'e points after firin which together with a mark at the head o the projectile permits to read oil the ignition time'adjusted. y In the modification shown in Fig. 3 the magnet a, as in the construction above described, on firing of the projectile moves through the coil (1 and generates in the latter an induction current which loads the condenser f. The current in this case flows from the one end Z of the coil (1 through the points 2, 3, 4, to the other end 6 of the coil d. During loading of the condenser f however, a part of the induction current ows in a second circuit 1, 2, 7, 8, 9, 10, 11, 12, 6 through the primingecomposition n and an exactly adjusted constant resistance w.
This second circuit causes a preheating of the ignition Wire 0. If, for instance, the detonation point is at 400 C. the ignition wire is preheated by this circuit to a temperature of about 350 C. At the end-of the movement of the magnet a with regard to the coil d, the latter is disconnected from the condenser f and moreover the circuit for preheating the ignition wire is opened. The metal stri i then comes into the position shown in dotted lines and hereby closes the condenser f over the ignition wire 0 and the strength after a longer period of action only, A
resistance 1' adjustable by. the moving contact u. The discharge of the condenser 1 then takes place from the one tinfoil 4 through the points 3, 13, 14, 15, 10, 11, 12, 6 to its second coating 5. This current furnished by the condenser f during the flight of the projectile is proportioned by the resistance 1' in.
such a manner that it effects the remaining heating ofthe ignition wire from 350 C. to the temperature of 450 C. which corresponds to the detonation oint of the priming-composition and there ore the ignition of the latter after the" lapse of the time adjusted at the indicating device of the resistance r.
Fig. 4 illustrates a device which makes the electric time-fuse described above also suitable as an impact-fuse. If during the flight of the projectile the priming-composition will not be caused to ignite at the adjusted ignition time point, the resiliently mounted contact piece 4) will, when the projectile impacts upon an aim, be thrown forward by the inertia of its mass. Hereby the contact piece 12 is pressed against a fixed contact a and shortcircuits resistance 1'. The rest of the con-= denser load may hereby at once discharge Without resistance through the priming-composition which efiects the ignition of the lat ter. According to another arrangement not shown an automatically actin contact device may be used by means of whic when the projectile impacts upon an aim, the electric energy generated by the movement at the magnet a in the induction coil is passed through the ignition wire 0, so that the ignition of the priming-composition is caused.
What I claim is: I 1. In an electric time-fuse for projectiles, in combination an explosive mixture, a priming-composition, a heating wire for igniting said priming-composition, an induction coil, a permanent magnet loosely mounted in said 0011, said magnet being shifted in said coil and generating electric energy when the projectile is fired, a circuit connecting said energy generator to said heating wire, a condenser in said circuit loaded by said energy generator, a regulating resistance in the circuit of the heating Wire, a movable contact in said circuit in the path of said movable magnet, said contact being at the end of the movement of said magnet shifted by the latter to cut the said coil of? said condenser and to close the circuit through said regulating resistance and said heating wire, for the purpose of permitting the condenser to discharge, and a contact device for automatically shortcircuiting the regulating resistance in the circuit from said condenser to said heating Wire, said contact device acting when the projectile impacts upon an aim earlier than the time- :fuse has come to action.
I. In an electric time-fuse ior projectiles, in combination anexplosive mixture, :1 priming-composition, a heating wire for igniting the priming-composition,-a source of current in a circuit containing the said heating. wire, means for regulating the stren th of the current fiowin to the heating wire for the purpose o heating said wire to the degree requiredcfor igniting the priming-com )osition after a shorter or lon er duration ot the action of the current, an a contact device for automatically short-circuiting the regulating resistance in the circuit from said condenser to said heating wire, said contact device acting when the projectile impacts upon an aim earlier than the timefuse has come to action. I
3. In an electric time-fuse for projectiles, in combination an explosive mixture, a priming composition, a heating wire for igniting said priming composition an inductioncoil, a permanent magnet movablymountedin said coil, said magnet being shifted in said coil and generates electric energy when the projectile is fired, a circuit connecting said energy generator with the heating wire, a condenser in said circuit loaded by said ener y generator, and a regulating resistance in t e circuit of the heating Wire.
t. In an electric time-fuse for projectiles, in combination an explosive mixture, a priming composition, a heating Wire for igniting said priming composition, an induction coil, a permanent magnet movably mounted in said coil, said magnet being shifted in said coil and generates electric energy when the projectile is fired, a circuit connecting said energy generator with the heating wire, a condenser in said circuit loaded by said energy generator,a regulating resistance in the circuit of the heating Wire, and a movable contact in said circuit in the ath of said movable magnet, said contact eing, at the end of the movement of said magnet, shifted by said magnet to cut the said coil from said condenser and to close the circuit through said-regulating resistance and said heating wire, for the purpose of permitting the condenser to discharge.
5. In an electric time-fuse for projectiles, in combination an explosive mixture, a priming composition, a heating wire for igniting said priming composition, an induction coil, a permanent magnet movably mounted in said coil, said magnet being shifted in said coil and generates electric energy when the projectile is fired, a circuit connecting said energy. generator With the heating wire, a
condenser in said circuit loaded by said: energy generator, a regulating resistance n the circuit of the heating wire, a movable contact in said circuit in the path of said movable magnet, said contact being, at the end of the movement of said magnet, shift-ed'by said magnet to cut the said coil from said condenser and to close the circuit through said regulating resistance and said heating wire, for the urpose of permitting the condenser to disc arg'e,and means for preheatsignature.
ing the heatin wire hi the current enerated in said coil uring t e loading 0 the condenser.
6; An electric igniter for projectiles com HERBERT RflHLEMA iI,
US200683A 1926-06-26 1927-06-22 Electric fuse for projectiles Expired - Lifetime US1755023A (en)

Priority Applications (19)

Application Number Priority Date Filing Date Title
BE350642D BE350642A (en) 1926-06-26
NL27541D NL27541C (en) 1926-06-26
NL27722D NL27722C (en) 1926-06-26
BE343130D BE343130A (en) 1926-06-26
BE350641D BE350641A (en) 1926-06-26
DER69907D DE486942C (en) 1926-06-26 1927-01-14 Electric igniter
DER71029D DE486944C (en) 1926-06-26 1927-04-28 Method and device for tempering electrical projectile fuses
CH127058D CH127058A (en) 1926-06-26 1927-06-22 Electric detonator.
FR638284D FR638284A (en) 1926-06-26 1927-06-25 Electric rocket
GB17105/27A GB273338A (en) 1926-06-26 1927-06-27 Electric fuses for explosive shells
CH132353D CH132353A (en) 1926-06-26 1928-04-13 Electric time fuse.
FR35264D FR35264E (en) 1926-06-26 1928-04-16 Electric rocket
US270465A US1791606A (en) 1926-06-26 1928-04-16 Setting electric projectile fuses
FR35409D FR35409E (en) 1926-06-26 1928-04-16 Electric rocket
GB1188828A GB289436A (en) 1926-06-26 1928-04-23 Electric impact fuses for projectiles
GB12252/28A GB289473A (en) 1926-06-26 1928-04-26 Process and apparatus for timing the ignition of electric projectile fuses
DER75975D DE491466C (en) 1926-06-26 1928-10-13 Electric igniter
DER78400D DE502303C (en) 1926-06-26 1929-06-14 Electric bullet fuse
US432865A US1858969A (en) 1926-06-26 1930-03-03 Electric fuse for projectiles

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DER67999D DE476379C (en) 1926-06-26 1926-06-26 Electric igniter
DER71029D DE486944C (en) 1926-06-26 1927-04-28 Method and device for tempering electrical projectile fuses
US432865A US1858969A (en) 1926-06-26 1930-03-03 Electric fuse for projectiles

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US1755023A true US1755023A (en) 1930-04-15

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US200683A Expired - Lifetime US1755023A (en) 1926-06-26 1927-06-22 Electric fuse for projectiles

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Cited By (14)

* Cited by examiner, † Cited by third party
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US2509910A (en) * 1943-04-16 1950-05-30 Us Navy Time-delay circuit
US2514297A (en) * 1943-03-03 1950-07-04 Us Navy Apparatus for observing the conduct of a projectile in a gun
US2848948A (en) * 1944-05-16 1958-08-26 Harold J Plumley Magnetic inertia controlled fuze
US2869364A (en) * 1953-01-27 1959-01-20 Kabik Irving Apparatus and method for nondestructive testing of initiators
US2925776A (en) * 1944-05-15 1960-02-23 Robert G Ferris Combination amplifier and oscillator unit
US2942549A (en) * 1943-03-19 1960-06-28 Henry F Dunlap Delay condenser safety device
US2950400A (en) * 1942-03-30 1960-08-23 Itt Protective circuit for radio repeater
US2962967A (en) * 1943-12-21 1960-12-06 Harold W Bixby Fuze
US3035520A (en) * 1955-01-24 1962-05-22 Robert E Koeppen Inertia actuated electric unit
US3073994A (en) * 1958-11-22 1963-01-15 Bolkow Entwicklungen Kg Ignition means for reaction motors used in connection with missiles
US3353486A (en) * 1966-03-03 1967-11-21 Robert M Haiken Self-destructing fuze system for rotating projectiles
US4221168A (en) * 1948-01-15 1980-09-09 Neddermeyer Seth H Condenser powered fuze
US20060180223A1 (en) * 2003-06-16 2006-08-17 Biomerieux Electrically opended micro fluid-valve
US10578413B1 (en) * 2017-06-23 2020-03-03 Douglas Burke Bullet projectile with internal electro-mechanical action producing combustion for warfare

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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US2514297A (en) * 1943-03-03 1950-07-04 Us Navy Apparatus for observing the conduct of a projectile in a gun
US2942549A (en) * 1943-03-19 1960-06-28 Henry F Dunlap Delay condenser safety device
US2509910A (en) * 1943-04-16 1950-05-30 Us Navy Time-delay circuit
US2962967A (en) * 1943-12-21 1960-12-06 Harold W Bixby Fuze
US2925776A (en) * 1944-05-15 1960-02-23 Robert G Ferris Combination amplifier and oscillator unit
US2848948A (en) * 1944-05-16 1958-08-26 Harold J Plumley Magnetic inertia controlled fuze
US4221168A (en) * 1948-01-15 1980-09-09 Neddermeyer Seth H Condenser powered fuze
US2869364A (en) * 1953-01-27 1959-01-20 Kabik Irving Apparatus and method for nondestructive testing of initiators
US3035520A (en) * 1955-01-24 1962-05-22 Robert E Koeppen Inertia actuated electric unit
US3073994A (en) * 1958-11-22 1963-01-15 Bolkow Entwicklungen Kg Ignition means for reaction motors used in connection with missiles
US3353486A (en) * 1966-03-03 1967-11-21 Robert M Haiken Self-destructing fuze system for rotating projectiles
US20060180223A1 (en) * 2003-06-16 2006-08-17 Biomerieux Electrically opended micro fluid-valve
US7159618B2 (en) 2003-06-16 2007-01-09 Bio{acute over (m)}erieux Electrically opened micro fluid valve
US10578413B1 (en) * 2017-06-23 2020-03-03 Douglas Burke Bullet projectile with internal electro-mechanical action producing combustion for warfare

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