AUS EINEM DRALLSTABILISIERTEN TRÄGERGESCHOSS AUSSTOSSBARE SUBMUNITION, INSBESONDERE LEUCHTMUNITION
    3.
    发明公开
    AUS EINEM DRALLSTABILISIERTEN TRÄGERGESCHOSS AUSSTOSSBARE SUBMUNITION, INSBESONDERE LEUCHTMUNITION 有权
    澳大利亚金融监督管理局(TRAGERGESCHOSS)澳大利亚证券监督管理委员会(INSBESONDERE LEUCHEMUNITION)

    公开(公告)号:EP3017271A1

    公开(公告)日:2016-05-11

    申请号:EP14730896.9

    申请日:2014-06-17

    发明人: GUTH, Sven

    IPC分类号: F42B15/36 F42B12/62 F42B4/28

    摘要: The invention relates to a submunition (1), in particular luminous munition, that can be discharged from a spin-stabilized carrier projectile and has a submunition body (2) and a parachute housing (3) arranged on the rear side of the submunition body (2) with a main parachute located therein. To achieve the effect that the main parachute is activated when there is a predeterminable spin of the submunition (1), the invention proposes connecting the submunition body (2) and the parachute housing (3) releasably to one another by way of a centrifugal coupling (4) in such a way that the submunition body (2) and the parachute housing (3) are non-positively and/or positively connected to one another by the centrifugal coupling (4) as a result of the centrifugal force occurring when the carrier projectile is fired, and in such a way that the centrifugal coupling (4) releases the connection between the submunition body (2) and the parachute housing (3) after the centrifugal force has subsided to a predeterminable value.

    摘要翻译: 本发明涉及一种子弹药(1),特别是发射弹药,其可以从旋转稳定的载体射弹排出,并具有子弹体(2)和设置在子弹体背面的降落伞壳体(3) (2)位于其中的主降落伞。 为了实现当子弹药(1)存在可预定的旋转时主降落伞被激活的效果,本发明提出通过离心联轴器将子弹药体(2)和降落伞壳体(3)可释放地彼此连接 (4),使得子弹药体(2)和降落伞壳体(3)通过离心联轴器(4)彼此不正和/或正相关,这是由于当离心力联轴器 在离心力已经下降到可预定的值之后,离心联轴器(4)以离散联接器(4)释放子弹药体(2)和降落伞壳体(3)之间的连接的方式被发射。

    WAFFE, INSBESONDERE REICHWEITENGESTEUERTE DRUCKLUFTWAFFE
    4.
    发明公开
    WAFFE, INSBESONDERE REICHWEITENGESTEUERTE DRUCKLUFTWAFFE 审中-公开
    武器,特别是范围控制的压力,空军

    公开(公告)号:EP2459955A1

    公开(公告)日:2012-06-06

    申请号:EP10734706.4

    申请日:2010-07-21

    IPC分类号: F41B11/32

    CPC分类号: F41B11/723 F41B11/724

    摘要: The invention relates to a range control (2), making it possible to determine the launch and impact speed of the ammunition or explosive bodies (10) to the required distance in such a way that the in particular non-lethal ammunition (10) remains non-lethal. Therefore, a kind of air weapon (1) is provided having an infinitely variable range control using a shooting pressure control, for example by means of a proportional pressure control (3) and/or additionally in connection with a closure technique and a valve technique.

    AUS EINER TRAGBAREN, RÜCKSTOßFREIEN WAFFE VERSCHIEßBARER LEUCHTMUNITIONSKÖRPER
    6.
    发明公开
    AUS EINER TRAGBAREN, RÜCKSTOßFREIEN WAFFE VERSCHIEßBARER LEUCHTMUNITIONSKÖRPER 有权
    从便携式反弹无核武器VERSCHIESSBARER灯壳体

    公开(公告)号:EP2893287A1

    公开(公告)日:2015-07-15

    申请号:EP13752875.8

    申请日:2013-08-09

    发明人: GUTH, Sven

    IPC分类号: F42B4/28 F42B12/42

    CPC分类号: F42B4/28 F42B12/42

    摘要: The invention relates to a flare ammunition body (1) shootable from a portable, recoil-free weapon, said flare ammunition body having a projectile case (2) in which a flare body (3), a parachute (5) attached to the flare body (3) and a fuse (6) for activating an ejection charge (7) for ejecting the flare body (3) and the parachute (5) from the projectile case (2) above a target area are provided. In order to achieve an arrangement of the fuse (6) for activating the ejection charge (7) at the rear end of the projectile case (2) without impairing the ejection and deployment process of the parachute (5) after activation of the ejection charge (7), according to the invention the parachute (5), viewed in the shooting direction, is arranged inside a front case portion (8), which can be separated from the adjoining portion of the projectile case (2) when the ejection charge (7) is activated. On the peripheral side of the flare body (3), an air brake (10) is fixed, which deploys during ejection of the flare body (3) out of the projectile case (2) and decelerates the flare body relative to the front case portion (8) in such a manner that the parachute (5) is pulled out of the front case portion (8) from the rear by the flare body (3).

    NEBELSPRENGGRANATE
    8.
    发明公开
    NEBELSPRENGGRANATE 审中-公开
    FOG爆炸的手榴弹

    公开(公告)号:EP3314201A1

    公开(公告)日:2018-05-02

    申请号:EP16729215.0

    申请日:2016-05-31

    发明人: GUTH, Sven

    摘要: In order to obtain an explosive smoke grenade (1), which can be fired from a portable anti-tank weapon, in particular a recoilless infantry weapon, and which permits an enemy position or a vehicle to be fogged as quickly as possible, so that the enemy has only a very limited radius of action, the invention proposes providing the explosive smoke grenade (1) with a time fuse (6) which can be programmed such that the burst charge (5) detonates in the direct vicinity of the enemy position but before the grenade has reached the ground, and there releases the smoke-generating active material (7). In addition, the pyrotechnic active substance (7) arranged between the burst charge (5) and the grenade casing (2) consists of a plurality of film strips, which are coated with a red-phosphorus-containing incendiary composition (flares). For this purpose, the dimensions of the flares are selected such that they generate a visibility barrier in both the visible and the infrared wavelength regions.

    WAFFENSYSTEM MIT EINER RÜCKSTOßFREIEN ODER RÜCKSTOßARMEN WAFFE UND EINER MIT DER WAFFE VERSCHIEßBAREN GRANATE
    10.
    发明公开
    WAFFENSYSTEM MIT EINER RÜCKSTOßFREIEN ODER RÜCKSTOßARMEN WAFFE UND EINER MIT DER WAFFE VERSCHIEßBAREN GRANATE 审中-公开
    WITH A反弹室外武器系统或武器后坐力武器和带有武器VERSCHIEßBARENGRENADE

    公开(公告)号:EP2856064A1

    公开(公告)日:2015-04-08

    申请号:EP13726140.0

    申请日:2013-05-21

    发明人: GUTH, Sven

    IPC分类号: F41A1/02 F41A1/08

    CPC分类号: F41A1/02 F41A1/10

    摘要: The invention relates to weapon system (1) comprising a recoil-free or low-recoil weapon (2), which has a weapon barrel (3), and further comprising a shell (4) that can be shot by means of the weapon (2) and which has a rod-shaped rear region (5) that protrudes into the weapon barrel at the opening end. According to the invention, in order for the shell (4) to have an increased exit speed in comparison with comparable known weapon systems having a recoil-free or low-recoil weapon for such a weapon system (1), the weapon (2) is designed as a light-gas accelerator in order to pre-accelerate the shell (4). Thus, exit speeds of the shell (4) above the speed of sound can be produced in a simple manner. The post-acceleration of the shell (4) then occurs outside of the weapon barrel (3) by means of an athodyd (ramjet drive) associated with the shell (4).