US3557656A - Charging explosive projectiles, especially hollow charge projectiles - Google Patents

Charging explosive projectiles, especially hollow charge projectiles Download PDF

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US3557656A
US3557656A US437636A US43763665A US3557656A US 3557656 A US3557656 A US 3557656A US 437636 A US437636 A US 437636A US 43763665 A US43763665 A US 43763665A US 3557656 A US3557656 A US 3557656A
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explosive
projectile
nonmolten
plug
charge
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Michel Precoul
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SOC TECHNIQUE DE RECHERCHES INDUSTIELLES ET MECHANIQUES
TECH DE RECH INDUSTIELLES ET M
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TECH DE RECH INDUSTIELLES ET M
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B1/00Explosive charges characterised by form or shape but not dependent on shape of container
    • F42B1/02Shaped or hollow charges
    • F42B1/036Manufacturing processes therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B1/00Explosive charges characterised by form or shape but not dependent on shape of container
    • F42B1/02Shaped or hollow charges
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B33/00Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
    • F42B33/02Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B33/00Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
    • F42B33/02Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
    • F42B33/0214Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges by casting
    • F42B33/0221Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges by casting by centrifugal casting

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Drilling And Exploitation, And Mining Machines And Methods (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

Explosive projectiles are charged with the aid of a mixture comprising a molten liquid explosive and a granular solid explosive more brisant and powerful than the molten liquid explosive. During charging the projectile is set in motion by a rotation about its longitudinal axis, that is to say, the projectile, being vertically positioned, the rotation about the longitudinal axis of the projectile is carried out during cooling of the projectile filled with explosive mixture. During centrifuging and cooling the projectile is furnished with a plug sealing the bottom of the projectile, said plug having an inner shape in contact with the explosive mixture of such form that the centrifuging throws out toward the periphery the particles of the heavy, brisant, powerful, nonmolten explosive.

Description

United States Patent [31 965,880 and 991,222
[54] CHARGING EXPLOSIVE PROJECTILES,
ESPECIALLY HOLLOW CHARGE PROJECTILES 11 Claims, 8 Drawing Figs.
[52] US. Cl 86/31 F42b 1/02 [50] Field ofSearch 86/20, 20 3,
[56] References Cited UNITED STATES PATENTS 3,192,289 6/1965 Jagiello 86/20X 1,844,701 2/1932 Tama 86/20(.5) 2,897,714 8/1959 Precoul 82/20 Primary Examiner-Benjamin A. Borchelt Assistant ExaminerStephen C. Bentley Attorney-Davis, Hoxie, Faithful] & Hapgood ABSTRACT: Explosive projectiles are charged with the aid of a mixture comprising a molten liquid explosive and a granular solid explosive more brisant and powerful than the molten liquid explosive. During charging the projectile is set in motion by a rotation about its longitudinal axis, that is to say, the projectile, being vertically positioned, the rotation about the longitudinal axis of the projectile is carried out during cooling of the projectile filled with explosive mixture. During centrifuging and cooling the projectile is furnished with a plug sealing the bottom of the projectile, said plug having an inner shape in contact with the explosive mixture of such form that the centrifuging throws out toward the periphery the particles of the heavy, brisant, powerful, nonmolten explosive.
PATENIED JAN 26 Ian sum 0F 4 CHARGING EXPLOSIVE PRQJECTILE E PECIALLY HOLLOW CHARGE PROJECTILES This invention is concerned with charging projectiles with the aid of a mixture containing a molten liquid explosive (tolite or TNT for example) and a granular solid explosive,
powerful and brisant (Hexogen (RDX) of octogen, for example).
It is well known to effect charging when the charge is still liquid by centrifuging around an axis perpendicular to the longitudinal axis of the projectile, with a suitable position before the axis of rotation or to the rear of the casing, depending on the direction in which one desires the density and the content of the heavy explosive in the interior of the principal charge to progress or increase. A position sufficiently remote from the axis of rotation with relation to the cavity receiving the explosive and the use of a sufficient mass of the explosive employed, permits, moreover, one to obtain a homogenous charge.
Nevertheless, such a process leads,'by its very nature, to embodiments which are costly and complex, given the necessity of making a tightly closed container turn about an axis perpendicular to its own axis, and of reheating.
Further, this principle of charging results in the sections or planes perpendicular to the axis of charging having constant characteristics.
The present'invention has for an object a process of charg ing which also involves rotation and centrifuging, but having for its purpose to effect nonuniform concentrations of nonmolten, heavy, powerful, brisant explosive particles, such as RDX of'octogen, for example, mixed with a liquid explosive, such as TNT, for example, and in particular to effect a concentration of heavy nonmolten explosive, toward the periphery of the projectile, along the casing; and also toward the base of the casing or internal sheath of a hollow charge, when a device. of that nature is concerned. 1
This peripheral concentration of brisant, heavy, powerful, nonmolten explosive, because of its very high speed of detonation, permits onetoobtainthe effects of priming through a toroidal shock wave, even if the priming is an axial-priming; and permits one also to reinforce and amplify the speed of propagation of the peripheral w.ave,,that is to say of the'transformedtoroidalwave, evenif the priming is already of sucha composition as to develop atoroidal wave.
For the realization ofa process according'to the invention, one submits theprojectile at ,chargingand during the pouring of the explosive mixture, to a rotationiabout its longitudinal axis, which results, throughcentrifuging, in a concentration of theheavy, brisant, powerful, nonmoltenexplosive toward the periphery of the charging.
The combination of the effect of gravity with the effect of centrifuging, about the: longitudinal axis of the projectile, and
the action of the profile of the conical=internal sheath (in the caseof a hollow charge), procuresat thesame time, according to the invention, a concentrationqof heavy, brisant, powerful, nonmolten explosive toward the base of the sheath..To this effeet, the projectile to becharged.according'tothe invention is placed vertically, the sheath ,beingdownward.
The various other characteristics and advantages of the invention will become obvious from the description which follows, lt isemphasized; moreover-that .thedescription is merely exemplaryandais-notintended to ,be lirnitingrand that many othermodesof construction, shapes, proportionsanddispositions may equally .well. housed without departing: from the limits'of the invention.
'lxheiexample describedibelow isconcerned witha projectile having a hollow charge. lt'is,pointed.out,,however; that theinvention may, be'appliedwithout departing from its principles to all other types-of explosive projectile not provided with a hollowcharge,
lnthe descriptionwhichfollowsreference is-.rnade,to,theattacheddrawingsin.which:
FIG. 1 is aviewin longitudinal.sectiomofa hollow charge projectile, charged, in accordance with the invention, with centrifuging about itslongitudinal axis during pouring;
FIG. 2 is a view in elevation and in section of an apparatus suitable for carrying out a charging, in accordance with the invention;
FIG. 3 is a partial view in longitudinal sections of a projectile charged according to the invention;
FIG. 4 is a diagram, relating to FIG. 3, representing the content of granular, heavy, brisant, nonmolten explosive, in different charging zones of the projectile of FIG. 3;
FIG. 5 is a view analogous to FIG. 3, of a projectile furnished during centrifuging and chilling with a seal at the base, illustrating a preferred construction of said seal;
FIG. ,6 is a diagram analogous to the diagram of FIG. 4, but relating to FIG. 5;
FIG 7 is a View analogous to that of FIG. 5, of a projectile, furnished during centrifuging and chilling, with a seal for the base, illustrating another form of said seal;
FIG. 8 is a diagram analogous to the'diagram of FIG. 4, but concerned with FIG. 7.
A projectile in accordance with the invention comprises an envelope or casing 10 on the after part of which is fixed, for charging, a funnel-support 12, the inner sheath 13 of the hollow charge closing the cavity to be charged with explosive.
tions of the two types of explosive may vary considerably but in general there will be from 40 to 60 parts by weight of the liquid explosive (e.g. TNT) per parts of granular explosive.
The assembly, brought to the fusion temperature of the molten explosive is placed in a mechanical device, which functions according to the invention, to rotate the assembly about the longitudinal axis X-X of the projectile. For the mechanical device one may use that shown in FIG. 2.
Referring to FIG. 2 a suitable device comprises a plate 17, carried on a shaft 18 turning in a support-bearing 19 formed. integrally with a frame 20. The shaft 18 is rotated by a rnotor 21, the shaft 21a of which is connected to the shaft 18 of the plate 17 by a conventional power train having a belt 22 and pulleys 23, 23a. Variation of the speed of rotation of the shaft 18 may be obtained by any conventional means, as by varying electrically the speed of the motor 21. Preferably, however, the control mechanism shown in FIG. 2 is used. This permits one to vary the spacing of the flanges of the pulley fixed on the driving shaft 21a; the system containing a rod 24, operated by a handwheel 24a which functions through the gearing 25, 25a to displace the flange 23 of the pulley in question.
On the plate l=7 is disposed a cylindrical casing 26 into which is introduced the body 10 with the sheath of the hollow charge 13. The funnel+support 12 is fixed to this body. .The supports 27, 27a maintain the assembly in place in the casing 26. At its upper part the casing 26 is closed by aseal 28,introduced between the internal ,wall of the casing and the upper part of the funnel-support 12. The seal 28 carries an axle or spindle 29 above which is applied, through rolls 30, a centerlngpiece 31, screwed on afixed cover 32, carried by the posts 33 formed integrally with the frame 20.
The rotation ,to which the body of the projectile is subjected iscontinued for theduration of the chillingof the projectile. In the case of pouring or decantation-by gravity, the axis X-X is vertical. Reheating in-the course of the operation maybe provided if necessary. Naturally, by varying the parameters such as the speed of rotation, the duration of decantation and chilling, the temperature of decantation, the characteristics andproportions of theexplosive mixture, the quantity of ex- .plosive employed, and the proportionsand the form of the funnel-support 12,.one may determine the characteristics of the charge which one desires toobtain.
However, in general, there is enrichment and increase of the content of heavy, powerful, brisant explosive having a high speed ofdetonation when one moves away from the axis X-X of the projectile and, similarly, an increase, in the same direction, of the density. There is therefore a maximum concentration of heavy, brisant, powerful explosive having a high speed of detonation near the periphery 15 of the charge and equally toward the base 16 of the charge, surrounding the base of the internal sheath in the case of a hollow charge. The arrows f-f' show the amplification of the effect of the toroidal priming shock wave as a result of the increase in speed of detonation in the zone 15 having a higher density and a higher content of heavy, brisant, powerful explosive of higher speed of detonation.
One will note, moreover, the advantage, by no means negligible, which is prescribed by the great simplicity of a system of rotation about the axis of the projectile during the pouring and chilling of a projectile filled with a mixed liquid explosive and carrying a charging funnel, without it being necessary to have recourse to the heavy complex and sealed apparatus which is required with rotation about an axis perpendicular to the longitudinal axis of the projectile.
FIGS. 3 and 4 show schematically the results which one obtains by centrifuging about the axis X-X' of the projectile 10, the latter having been topped by the supported reservoir 12 containing the mixed liquid explosive 14.
In FIG. 4 the ordinate represents the content in percent of heavy granular nonmolten explosive (RDX, for example). The solid lines represent the content of RDX obtained after centrifuging in the charging zones 4 to l of FIG. 3 on both sides of the axis XX' of the projectile.
The pouring and chilling having been conducted during centrifuging, one obtains according to FIG. 4, an increasing content of RDX from the zone 4 to the zone 1 at the base of the internal sheath 13. The centrifuging system according to the invention permits therefore, one to obtain in the zone 1 more than 75 percent RDX, a remarkable result for pouring at atmospheric pressure.
However, in the different zones the content of RDX is substantially constant from the axis X-X' to the periphery of the projectile.
According to another feature of the invention there may also be obtained an improved charge by obtaining an enrichment of the heavy, brisant, solid, particulate explosive in the charge, at the periphery of the axial zone included between the apex ofthe internal sheath and the primer.
For this effect, according to the invention, the projectile is provided, during centrifuging and chilling with a base plug a such as 34 or 35 (FIGS. 5 and 7 respectively) whose profile in contact with the liquid explosive, is formed as an hydrodynamic deflector effective to throw toward the periphery of the charge (region g) the granular nonmolten particles of heavy, powerful, brisant explosive such as RDX or octogen, thus enriching the periphery of the charge.
According to the invention, the profile of the base sealing plug in contact with the liquid explosive has a cusp 34 or 35' lying on the longitudinal axis XX' of the projectile and a hollow section, for example like a half torus 36 (FIG. 7) or a quarter torus 36' (FIG. 5) which functions to throw the particles of heavy explosive in a centrifugal direction.
FIG. 6, analogous to FIG. 4, shows the content of RDX in zones 1 to 4, which may be obtained with the plug 34 in the form of a quarter torus of FIG. 5.
FIG, 8 shows the content of RDX in zones 1 to 4 which may be obtained with the plug 35 in the shape of the half torus of FIG. 7, analogous to FIG. 5.
Naturally, the percentages of RDX indicated in FIGS. 6 and 8 are only illustrative and all other proportions may be obtained, without departing from the principles ofthe invention.
The same is true ofthe sealing sections of FIGS. 5 and 7.
It is apparent, therefore, from FIGS. 6 and 8 that the use during centrifuging and chilling of a plug having a section according to the invention keeps a fundamental advantage of the invention, the sensible enrichment in heavy nonmolten explosive at the base of the internal sheath. At the same time as one goes toward the rear of the projectile ( zones 3 and 4 particu larly), i.e. toward the priming, the RDX content increases transversely from the axis X-X of the projectile, with very appreciable enrichment at the periphery. For example, in the rear zone 4 there is 75 percent RDX at the periphery compared to 45 to 50 percent at the axis, while in zone 3 there is 75 percent at the periphery against 68 percent at the axis.
One obtains, therefore, thanks to the base plug according to the invention, a transfer of nonmolten particles of heavy, powerful explosive from the axis toward the periphery with a corresponding impoverishment in the RDX content in the axial zone of the charge between the apex of the internal sheath and the priming.
This distribution of powerful brisant explosive resulting from these arrangements, produces again a more toroidal form of wave of detonation, initiated by the primer, in its propagation through the charge.
There follow all the advantages of efficacy and perforating power of a hollow charge, as already described in prior patents.
It is emphasized, however, that the invention is equally applicable, without departing from its principles to all explosive projectiles, as well as to projectiles having a hollow charge.
Similarly, the invention is not applicable only to charging with decantation during centrifuging. It is applicable also without departing from its principles to charging in two phases:
a. preliminary pouring with a reserve ofliquid explosive.
b. centrifuging with chilling of a projectile having a plug with a section according to the invention.
Iclaim:
1. In a process for charging an explosive projectile having a base plug with a fluid mixture comprising a molten liquid explosive and a heavy, brisant and powerful explosive in granular, nonmolten form, the improvement which comprises rotating the projectile about its longitudinal axis during charging and deflecting the nonmolten explosive particles toward the periphery of the projectile by the action of a surface provided on said base plug.
2. The process claimed in claim 1 wherein the nonmolten explosive is decanted by gravity.
3. The process claimed in claim 1 wherein the nonmolten explosive is decanted by gravity in a separate prior operation.
4. The process claimed in claim 1 wherein the plug has an interior cusp directed toward the projectile along the axis of the projectile.
5. The process claimed in claim 1 in which the plug has a section in the form ofa quarter hollow torus.
6. The process claimed in claim 1 in which the plug has a section in the form ofa half hollow torus.
7. In a process for charging hollow charge explosive projectiles with a fluid mixture comprising a molten liquid explosive and a heavy, brisant and powerful explosive in granular nonmolten form, said projectile having a forward end and a primer end and including an inner sheath for the hollow charge, the improvement which comprises rotating the projectile, disposed vertically, about its longitudinal axis during charging and transferring the particles of nonmolten explosive from the axis to the periphery of the charge to cause an impoverishment in the concentration of nonmolten explosive particles in the axial part of the zone lying between the apex of the conical inner sheath and the primer end of the charge, with a corresponding enrichment at the periphery of that zone.
8. The process claimed in claim 7 wherein the projectile filled with the fluid explosive mixture is cooled and the rotation is carried out during cooling.
9. The process claimed in claim 8 wherein the molten explosive is poured with the aid of gravity into the po projectile to fill it.
10. The process I claimed in claim 7 wherein the projectile is heated during rotation.
11. The process claimed in claim 7 wherein during rotation the projectile is provided with a support-funnel filled with explosive mixture.

Claims (11)

1. In a process for charging an explosive projectile having a base plug with a fluid mixture comprising a molten liquid explosive and a heavy, brisant and powerful explosive in granular, nonmolten form, the imprOvement which comprises rotating the projectile about its longitudinal axis during charging and deflecting the nonmolten explosive particles toward the periphery of the projectile by the action of a surface provided on said base plug.
2. The process claimed in claim 1 wherein the nonmolten explosive is decanted by gravity.
3. The process claimed in claim 1 wherein the nonmolten explosive is decanted by gravity in a separate prior operation.
4. The process claimed in claim 1 wherein the plug has an interior cusp directed toward the projectile along the axis of the projectile.
5. The process claimed in claim 1 in which the plug has a section in the form of a quarter hollow torus.
6. The process claimed in claim 1 in which the plug has a section in the form of a half hollow torus.
7. In a process for charging hollow charge explosive projectiles with a fluid mixture comprising a molten liquid explosive and a heavy, brisant and powerful explosive in granular nonmolten form, said projectile having a forward end and a primer end and including an inner sheath for the hollow charge, the improvement which comprises rotating the projectile, disposed vertically, about its longitudinal axis during charging and transferring the particles of nonmolten explosive from the axis to the periphery of the charge to cause an impoverishment in the concentration of nonmolten explosive particles in the axial part of the zone lying between the apex of the conical inner sheath and the primer end of the charge, with a corresponding enrichment at the periphery of that zone.
8. The process claimed in claim 7 wherein the projectile filled with the fluid explosive mixture is cooled and the rotation is carried out during cooling.
9. The process claimed in claim 8 wherein the molten explosive is poured with the aid of gravity into the po projectile to fill it.
10. The process l claimed in claim 7 wherein the projectile is heated during rotation.
11. The process claimed in claim 7 wherein during rotation the projectile is provided with a support-funnel filled with explosive mixture.
US437636A 1964-03-03 1965-03-02 Charging explosive projectiles, especially hollow charge projectiles Expired - Lifetime US3557656A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2338374A1 (en) * 1976-01-15 1977-08-12 Alsetex Explosive charge for making holes in ground - has gas generator formed as rear cone shaped portion to assist penetration
US4170940A (en) * 1976-09-27 1979-10-16 Societe D'etudes, De Realisations Et D'applications Techniques Projectile charges
US4331078A (en) * 1978-06-12 1982-05-25 Dynamit Nobel Aktiengesellschaft Instantaneous detonator with insert member within fuze casing
FR2643979A1 (en) * 1983-08-19 1990-09-07 Fraunhofer Ges Forschung DEVICE FOR PRODUCING EXPLOSIVE-CONFORMED PROJECTILES
US6244186B1 (en) 1999-07-26 2001-06-12 Joseph F. L. John Pichard Air gun pellet
US20070074637A1 (en) * 2005-04-01 2007-04-05 Pontieri James M Aerodynamic air gun projectile
US8573107B1 (en) * 2011-08-02 2013-11-05 The United States Of America As Represented By The Secretary Of The Army Burster tube loading apparatus and method
US20150219427A1 (en) * 2014-01-31 2015-08-06 Alford Research Limited Linear shaped charges

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10112253C1 (en) * 2001-03-14 2002-11-28 Josef Schmeiler Cartridge, used as ammunition, has propellants with different ignition behavior, hardening behavior and ignition delay in concentric layers within cartridge shell

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1844701A (en) * 1929-12-19 1932-02-09 Tama Cyrano Method and apparatus for centrifugal casting
US2897714A (en) * 1954-12-17 1959-08-04 Soc Tech De Rech Ind Method of and device for charging explosive projectiles
US3192289A (en) * 1963-08-30 1965-06-29 Leonard T Jagiello Method of casting solid propellant rocket motors

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1844701A (en) * 1929-12-19 1932-02-09 Tama Cyrano Method and apparatus for centrifugal casting
US2897714A (en) * 1954-12-17 1959-08-04 Soc Tech De Rech Ind Method of and device for charging explosive projectiles
US3192289A (en) * 1963-08-30 1965-06-29 Leonard T Jagiello Method of casting solid propellant rocket motors

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2338374A1 (en) * 1976-01-15 1977-08-12 Alsetex Explosive charge for making holes in ground - has gas generator formed as rear cone shaped portion to assist penetration
US4170940A (en) * 1976-09-27 1979-10-16 Societe D'etudes, De Realisations Et D'applications Techniques Projectile charges
US4305324A (en) * 1976-09-27 1981-12-15 Societe D'etudes, De Realisations Et D'applications Techniques Projectile charges
US4331078A (en) * 1978-06-12 1982-05-25 Dynamit Nobel Aktiengesellschaft Instantaneous detonator with insert member within fuze casing
FR2643979A1 (en) * 1983-08-19 1990-09-07 Fraunhofer Ges Forschung DEVICE FOR PRODUCING EXPLOSIVE-CONFORMED PROJECTILES
US6244186B1 (en) 1999-07-26 2001-06-12 Joseph F. L. John Pichard Air gun pellet
US20070074637A1 (en) * 2005-04-01 2007-04-05 Pontieri James M Aerodynamic air gun projectile
US7222573B2 (en) 2005-04-01 2007-05-29 Pontieri James M Aerodynamic air gun projectile
US8573107B1 (en) * 2011-08-02 2013-11-05 The United States Of America As Represented By The Secretary Of The Army Burster tube loading apparatus and method
US20150219427A1 (en) * 2014-01-31 2015-08-06 Alford Research Limited Linear shaped charges
US9534874B2 (en) * 2014-01-31 2017-01-03 Alford Research Limited Linear shaped charges

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DE1453864B2 (en) 1975-11-27

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