序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
1 穿甲弹及其制造方法 CN99816689.8 1999-05-06 CN1352740A 2002-06-05 阿卡第·G·希布诺夫; 瓦希里·P·格里阿捷夫; 维克托·K·捷林卡; 弗拉基米尔·M·高罗里夫
发明涉及一种穿甲弹,它在射击武器中使用以杀伤配备个人防弹设备的敌人的有生量。本发明还涉及制造穿甲弹的方法。本发明的目的是提高上述子弹的穿透作用。本发明的穿甲弹具有弹壳(1),它带有头部(A)、引导部分(B)和尾部(C)。弹壳(1)还具有穿甲弹芯(3),它安装在头部(A)内,使由其凸出,以及它连接至上述弹壳(1)的尾部(C)的内表面,而且上述弹壳还具有衬套(2)。弹芯一子弹的中部截面的面积比的范围为0.3至0.4,而它们的重量比至少为0.45以及在尾部(C)的弹壳(1)的厚度和弹芯(3)的直径比的范围为0.1至0.2。本发明还涉及制造穿甲弹的方法,穿甲弹具有穿甲弹芯(3)由弹壳(1)凸出,而且上述方法包括将带有衬套(2)的弹芯(3)压配进入弹壳(1)以及压缩弹壳(1)的头部(A)。在压缩弹壳(1)的头部(A)时,本方法还包括同时沿弹芯(3)压缩上述弹壳(1)的尾部(C)。
2 穿甲弹及其制造方法 CN99816689.8 1999-05-06 CN1144022C 2004-03-31 阿卡第·G·希布诺夫; 瓦希里·P·格里阿捷夫; 维克托·K·捷林卡; 弗拉基米尔·M·高罗里夫
发明涉及一种穿甲弹,它具有弹壳(1),弹壳(1)带有头部(A)、引导部分(B)和尾部(C),弹壳(1)还具有穿甲弹芯(3),它安装在头部(A)内,使由其凸出,以及它连接至上述弹壳(1)的尾部(C)的内表面,而且上述弹壳还具有衬套(2),在尾部(C)的弹壳(1)的厚度和弹芯(3)的直径的比的范围为0.1至0.2。本发明还涉及制造穿甲弹的方法,穿甲弹具有穿甲弹芯(3)由弹壳(1)凸出,上述方法包括将带有衬套(2)的弹芯(3)压配进入弹壳(1)以及压缩上述弹壳(1)的头部(A)以及在压缩弹壳(1)的头部(A)时,本方法还包括同时沿弹芯(3)压缩上述弹壳(1)的尾部(C)。
3 Bandolier having a workpiece away deviated laterally JP2013501375 2011-03-22 JP2013525112A 2013-06-20 ジョーンズ,ディー.パトリック; ウェイン ケリー,マイケル; デュアン ポリック,リチャード; カール ショー,ルイス; ジェイ. マラチーニ,ジェームズ
【解決手段】
順送型(10)を動作させる方法であって、順送型(10)は、一端に、ブランク(68)を有する細長い本体部(60)を有する加工物(1)に作用する。 加工物(1)は、順送型(10)内に形成される弾帯(50)によって支持される。 順送型(10)は、各ブランク(68)に作用する。
【参考図】図6
4 BANDOLIER WITH LATERALLY OFFSET AND SPACED WORK PIECE EP11760032.0 2011-03-22 EP2550503A1 2013-01-30 JONES, D. Patrick; KELLEY, Michael Wayne; POLLICK, Richard Duane; SHAW, Louis Carl; MARRACCINI, James J.
A method of operating a progressive die (10) wherein the progressive die (10) acts on a work piece (1) having an elongated body (60) with a blank (68) at one end. The work piece (1) is supported by a bandolier (50) which is also formed in the progressive die (10). The progressive die (10) acts on each blank (68).
5 Method of manufacture of a metallic sabot EP85102846.4 1985-03-13 EP0158828A1 1985-10-23 Ibach, David R.

The method of manufacture of a sabot component which comprises the steps of severing an aluminum workpiece (50) from bar stock, upsetting the workpiece in a first die, by axial force, to constitute a first preform (51) having a desired uneven mass distribution along the axis thereof, hot forging the first preform in a second die, by transverse force, to constitute a second preform (52) having an unsymmetrical mass distribution transverse to the axis thereof, hot forging the second preform in a third die, by transverse force, to constitute a stamping (60) having opposed unsymmetrical formed surfaces, solution heat treating the stamping to a "W" condition, freezing the stamping to render its metalography dormant, cold forging the stamping in the third die, artificially aging the stamping to a "T8" condition, trimming the stamping in a fourth die, and annodizing the trimmed stamping.

6 THREE COMPONENT BULLET WITH CORE RETENTION FEATURE AND METHOD OF MANUFACTURING THE BULLET EP12743605.3 2012-07-24 EP2737276A1 2014-06-04 BURCZYNSKI, Thomas, J.
A three component bullet with an improved core retention feature and a method of manufacturing the bullet is described including a cylindrical jacket having an open end and a closed end containing a malleable metal core which is forced into a forming die having a bottleneck shaped interior resulting in a bottleneck shaped pre-form wherein the outside diameter of the open-ended forward portion of the jacket is smaller than the outside diameter of its closed rearward portion. The open end of the pre-form may be dropped through or forced through a malleable locking band of appropriate height, diameter and wall thickness. A relatively tight-fitting punch enters the open end of the pre-form generating sufficient axial force against the face of the metal core to radially swell the core and subsequently portions of the jacket fore and aft of the locking band, thereby securing the locking band in place while at the same time producing an inwardly- extending annular band of jacket material which embeds itself into the core material with the result that the core is permanently locked inside the jacket.
7 Verfahren zur Herstellung eines Jagdgeschosses mit Hohlspitze EP95108285.8 1995-05-31 EP0689889A1 1996-01-03 Matysik, Peter; Wiechmann, Heinz

Die vorliegende Erfindung betrifft ein Verfahren zur Herstellung eines Jagdgeschosses mit Hohlspitze. Es soll ein Herstellungsverfahren für ein derartiges Geschoß zur Verfügung gestellt werden, welches nur wenige Arbeitsschritte erfordert, wobei insbesondere die Hohlspitzkonstruktion in nur einem Arbeitsschritt ausgeformt wird. Diese Aufgabe wird erfindungsgemäß dadurch gelöst, daß das gesamte Geschoß auf pulvermetallurgischem Wege aus Metallpulver hergestellt und anschließend kalibriert wird, wobei während des Pulverpressens die Hohlspitzkonstruktion eingebracht wird, die während des Kalibrierens zur endgültigen Geschoßspitze umgeformt wird.

8 Small arms ammunition, and manufacturing process therefor EP83201455 1983-10-11 EP0106411A3 1984-09-05 Kneubühl, Beat; Schwendimann, Hans; Ruf, Max
9 Method for self-propelling projectile manufacturing and resulting projectiles thereof EP81106062 1981-08-03 EP0051717A3 1982-09-08 Galluzzi, Giovanni; Fiocchi, Giuseppe

This invention relates to a self-propelling projectile (20) of the type including a solid nose (21) and a propelling charge housing recess (28) communicating with a hollow space (128) containing the priming charge able to undergo a radial or lateral percussion.

In particular, means (b) are foreseen that assure the projectile rear part (23) seal in respect to the explosion generated gas and further means (c; 34) that permit extraction of the unexploded projectile in case of malfuntionning.

This invention relates also to the method for manufacturing the projectile.

10 Kleinkalibermunition und Verfahren zu ihrer Herstellung EP83201455.9 1983-10-11 EP0106411B1 1987-06-24 Kneubühl, Beat; Schwendimann, Hans; Ruf, Max
11 Method for self-propelling projectile manufacturing and resulting projectiles thereof EP81106062.3 1981-08-03 EP0051717B1 1985-06-05 Galluzzi, Giovanni; Fiocchi, Giuseppe
12 Kleinkalibermunition und Verfahren zu ihrer Herstellung EP83201455.9 1983-10-11 EP0106411A2 1984-04-25 Kneubühl, Beat; Schwendimann, Hans; Ruf, Max

Die Kleinkalibermunition besteht aus einem Mantelgeschoss mit einer aerodynamisch optimierten Gestaltung, die mit Ausnahme der Enden (16) und einem nutförmigen Abschnitt (7) zur Befestigung ein Profil mit einer stetigen Funktion aufweist. Die Trefferwahrscheiniichkeit bei dieser Munition wird zusätzlich vorteilhaft durch die Ausbildung des vorderen (4) und des hinteren Endes (6) des Mantelgeschosses beeinflusst. Die Herstellung des Geschosses erfolgt durch Zugdruckumformen, wobei in einem ersten Zug ein zylindrischer Napf (16) tiefgezogen wird und Weiterzug zuerst die Spitze (12) und dann das hintere Ende (6) des Geschosses geformt werden. Die miteinander verketteten Verfahrensschritte sind auf einer einzigen Stufenpresse realisierbar.

13 Method for self-propelling projectile manufacturing and resulting projectiles thereof EP81106062.3 1981-08-03 EP0051717A2 1982-05-19 Galluzzi, Giovanni; Fiocchi, Giuseppe

This invention relates to a self-propelling projectile (20) of the type including a solid nose (21) and a propelling charge housing recess (28) communicating with a hollow space (128) containing the priming charge able to undergo a radial or lateral percussion.

In particular, means (b) are foreseen that assure the projectile rear part (23) seal in respect to the explosion generated gas and further means (c; 34) that permit extraction of the unexploded projectile in case of malfuntionning.

This invention relates also to the method for manufacturing the projectile.

14 Three component bullet with core retention feature and method of manufacturing the bullet US13190972 2011-07-26 US08752484B2 2014-06-17 Thomas J. Burczynski
A three component bullet with an improved core retention feature and a method of manufacturing the bullet is described including a cylindrical jacket having an open end and a closed end containing a malleable metal core which is forced into a forming die having a bottleneck shaped interior resulting in a bottleneck shaped pre-form wherein the outside diameter of the open-ended forward portion of the jacket is smaller than the outside diameter of its closed rearward portion. The open end of the pre-form may be dropped through or forced through a malleable locking band of appropriate height, diameter and wall thickness. A relatively tight-fitting punch enters the open end of the pre-form generating sufficient axial force against the face of the metal core to radially swell the core and subsequently portions of the jacket fore and aft of the locking band, thereby securing the locking band in place while at the same time producing an inwardly-extending annular band of jacket material which embeds itself into the core material with the result that the core is permanently locked inside the jacket.
15 Ultra precision net forming process employing controlled plastic deformation of metals at elevated temperatures US09389626 1999-09-03 US06230539B1 2001-05-15 Jerry M. Dickson; William R. Baschnagel; Mark C. Bagley
An ultra precision net shape forming process is disclosed which can satisfy the requirements of MMW and sub-MMW components and sabots for small caliber armor piercing ammunition. The process is well suited to both moderate and high volume applications, and offers the potential for dramatically reducing piece part fabrication costs. The process involves closely controlled high temperature compression forming of metals with cycle times of the order of one minute or less, precise replication of all die features, and very low residual stresses. The ultra precision net shape forming cycle starts following insertion of the billet/blank into an open die. In the preheat phase the press is closed to preheat position where the billet/blank is enclosed in both halves of the die but no force is applied. Following preheat the part is formed employing displacement and force control to insure a fully formed part. After holding for a preset time at the peak force, the press is then commanded back to the loading position. The process has many of the attributes of conventional compression molding of plastics and is well suited to high volume, automated production of complex precision parts.
16 Method of manufacturing a hollow point bullet US963752 1997-11-04 US5943749A 1999-08-31 Brian Eugene Swank
A method of manufacturing a hollow point bullet is disclosed. A cavity is formed in an end portion of a slug of generally solid material. A plurality of grooves are formed on an outer surface of the end portion of the slug. A slit is cut through a portion of each of the grooves substantially adjacent a peripheral edge of the end portion. The end portion of the slug is contoured so that the bullet has a desired shape and geometry.
17 Method of producing hunting projectile with hollow point US489891 1995-06-13 US5722035A 1998-02-24 Peter Matysik; Heinz Wiechmann
A hunting projectile with a hollow point is produced with a only few working steps, and in particular a hollow point construction is formed out only in one working step. For this purpose the whole projectile is made of a metal powder by a powder-metallurgical process and then calibrated and during the powder pressing, the hollow tip construction is brought in so that during the calibration it is deformed to produce a final projectile tip.
18 Bullet fabricating means US47263565 1965-07-16 US3322020A 1967-05-30 ECKERT CHARLES F
19 Bullet making US61302556 1956-10-01 US3069748A 1962-12-25 NOSLER JOHN A
20 Method of making bullets US54788055 1955-11-01 US2898666A 1959-08-11 FROST GEORGE E
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