专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

WO2015068151A1 ACCELERATOR 审中-公开
标题翻译：加速器
公开(公告)号：WO2015068151A1
公开(公告)日：2015-05-14
申请号：PCT/IL2014/050539
申请日：2014-06-15
申请人： RACHLIN, Felix
发明人： RACHLIN, Felix
IPC分类号： F42B5/10
CPC分类号： F42B30/02 , F41A1/02 , F42B5/02 , F42B5/03 , F42B5/045 , F42B10/38 , F42B15/10
摘要： The invention allows significantly (is several times) to increase the energy of shot on account of additional increase of velocity of movement of throw agent outside of barrel of any firearm, include artillery. The accelerating missile engine realize the additional acceleration - the accelerator that work by energy of compressive powder gases and locate in case of staff ammunition inside of powder filling. It is designed as tube of a high-strength material, that capable of withstanding conditions of shot, with one end of the tube is blocked. This end tolerably install on throw agent stationary way or a throw-down variant. While it is shooting the throw agent of accelerator leaving the barrel with the pressure inside off compare to pressure in the muzzle. It's advised the moment that the bullet leave the barrel pressure of muzzle should be high (100-200 MPa and more), so the length of the barrel should be accordingly reduced to necessary high pressure. Herewith the recoil, dimensions, weight and cost of the gun will decrease, but the energy of the shot will increase. Potentiality of this present method will allow to create the fundamentally new systems of gun that will lightweight, compact, inexpensive, with shot energy is unattainable today. It will be qualitative leap in the evolution of firearms.
摘要翻译：本发明允许显着地（多次）增加射击能量，这是由于任何火器枪枪外部的骰子的移动速度的进一步增加，包括火炮。加速导弹发动机实现额外的加速度 - 加压器是通过压缩粉末气体的能量工作的，并且可以在粉末填充物内的工作人员弹药的情况下进行定位。它被设计为高强度材料的管，能够承受喷射条件，管的一端被阻挡。这个目的可以容忍地安装在抛物剂固定的方式上或一个摔倒的变种。当枪口中的压力与枪口的压力相比时，枪口的加速器离开枪管的压力在内。建议子弹离开枪口压力应高（100-200MPa以上）的时刻，因此应将筒的长度减小到必要的高压。因此，枪的反冲，尺寸，重量和成本会降低，但是射击的能量将增加。这种现有方法的潜力将允许创造出一种基本上新型的枪系统，其轻便，紧凑，便宜，目前射击能量无法实现。火器的发展将会有质的飞跃。

2. 发明申请

WO2011133257A1 SYNCHRONIZED SPIN MULTI-COMPONENT PROJECTILE 审中-公开
标题翻译：同步旋转多分量项目
公开(公告)号：WO2011133257A1
公开(公告)日：2011-10-27
申请号：PCT/US2011/028106
申请日：2011-03-11
申请人： LIBERTY AMMUNITION, INC. , MARX, PJ
发明人： MARX, PJ
IPC分类号： F42B14/02
CPC分类号： F42B10/26 , F42B10/38 , F42B12/34 , F42B14/02
摘要： A projectile includes a leading part formed by a tip and a tip base that form a first annular shoulder where they meet. A trailing part of the projectile is formed by a base having a frusto- conical trailing end and a cylindrical leading end of truncate extent that forms a tail drive. A second annular shoulder is formed where a cylindrical rod meets the tail drive. A flat trailing end of the tip base and a flat leading end of the cylindrical rod abut one another when the projectile is assembled. A cylindrical interface has a leading extent abutting the first annular shoulder and a trailing end abutting the second annular shoulder. The tail drive and the trailing extent of the cylindrical interface are the only parts of the projectile that engage gun barrel rifling when the projectile is positioned in a gun barrel.
摘要翻译：抛射体包括由尖端和尖端基部形成的引导部分，其形成第一环形肩部，在那里它们相遇。抛射体的尾部由具有截头圆锥形尾端和形成尾部驱动的截头范围的圆柱形前端的基部形成。形成第二环形肩部，其中圆柱形杆与尾部驱动器相交。当组装抛射体时，尖端基部的平坦的后端和圆柱形杆的平坦的前端彼此邻接。圆柱形接口具有与第一环形肩部相邻的引导程度和邻接第二环形肩部的后端。当弹丸放置在枪管中时，尾部驱动器和圆柱形接口的尾部范围是射弹的唯一部分，可与枪筒枪膛接合。

3. 发明申请

WO2008010226A1 AIR VEHICLE AND DEPLOYABLE WING ARRANGEMENT THEREFOR 审中-公开
标题翻译：空中车辆和可配置的安排
公开(公告)号：WO2008010226A1
公开(公告)日：2008-01-24
申请号：PCT/IL2007/000916
申请日：2007-07-19
申请人： ISRAEL AEROSPACE INDUSTRIES LTD. , SHAI, Mordechai
发明人： SHAI, Mordechai
IPC分类号： F42B10/18 , F42B10/20 , F42B10/38 , F42B10/62 , B64C19/02 , B64C39/00 , B64C39/08
CPC分类号： F42B10/38 , B64C3/56 , B64C5/12 , B64C9/36 , B64C39/024 , B64C39/068 , B64C39/08 , B64C2201/102 , F42B10/18 , F42B10/20 , F42B10/62 , Y02T50/14
摘要： A deployable wing arrangement or kit is provided for use with a longitudinally extending fuselage (20) having an upper portion and a lower portion. The kit includes a first pair of wings (100) pivotably mountable with respect to said upper portion and capable of being deployed from a first retracted position to a first deployed position, and a second pair of wings (102) pivotably mountable with respect to said lower portion and capable of being deployed from a second retracted position to a second deployed position. A strut arrangement, having at least one pair of struts (104), interconnect the first pair of wings (100) with the said second pair of wings (102). An air vehicle having such a kit, and a method for increasing the range of an air vehicle are also provided.
摘要翻译：提供可展开的机翼装置或套件，用于具有上部和下部的纵向延伸的机身（20）。该套件包括相对于所述上部可枢转地安装并且能够从第一缩回位置展开到第一展开位置的第一对翼（100），以及可相对于所述第一展开位置可枢转地安装的第二对翼下部并且能够从第二缩回位置展开到第二展开位置。具有至少一对支柱（104）的支柱装置将第一对翼（100）与所述第二对翼（102）互连。还提供了一种具有这种套件的空中车辆，以及用于增加空中交通工具的范围的方法。

4. 发明申请

WO2003033988A1 PRECISION GUIDED EXTENDED RANGE ARTILLERY PROJECTILE TACTICAL BASE 审中-公开
标题翻译：精准引导的扩展机器人项目战术基地
公开(公告)号：WO2003033988A1
公开(公告)日：2003-04-24
申请号：PCT/US2002/027012
申请日：2002-08-23
申请人： RAYTHEON COMPANY
发明人： MOORE, James L. , JOHNSON, Gary H. , PETERSON, (DR.) William S. , SHAH, Rajesh H. , DRYER, Richard , QUORTRUP, Conlee O.
IPC分类号： F42B10/14
CPC分类号： F42B10/38 , F42B10/14
摘要： A tactical base for a guided projectile (10) includes a base structure (40), including a plurality of fin slots (46). A plurality of deployable fins (42) are pivotally mounted to the base structure and supported for movement between a stowed position and a deployed position.
摘要翻译：用于引导射弹（10）的战术基座包括基础结构（40），其包括多个鳍槽（46）。多个可展开的翅片（42）可枢转地安装到基座结构上并被支撑以在收起位置和展开位置之间运动。

5. 发明申请

WO1994015167A1 A BREAKING-PROJECTILE BULLET FOR INCREASING THE MUZZLE VELOCITY OF PISTOLS, PREFERABLY OF HAND-GUNS 审中-公开
标题翻译：一个突破性的项目，可以增加手枪的极限速度
公开(公告)号：WO1994015167A1
公开(公告)日：1994-07-07
申请号：PCT/HU1993000074
申请日：1993-12-16
申请人： BREINER, Sándor
IPC分类号： F42B10/00
CPC分类号： F42B5/067 , F42B10/38
摘要： The breaking-projectile bullet comprises a cartridge-case (1), powder-charge (3) inside the cartridge case and a breaking projectile (4) having a remaining part (5) fixed in the cartridge case (1); a projectile part (6); a breaking surface (8) to join said projectile part (6) with said remaining part (5) and to allow the projectile part (6) to become detached from the remaining part (5) along said breaking surface (8) when the compressive force affected by the increasing pressure (p) of the evolving powder gas inside the cartridge case (1) to a surface (S1) of the projectile part (6) exceeds a threshold, and a gas channel (7) connecting said surface (S1) of the projectile part (6) with the inside of said cartridge case (1). Said projectile part (6) comprises an additional accelerator surface (S1') to provide a surface step (S2-S1) for a secondary acceleration force when said projectile part (6) has become detached from the remaining part (5) along said breaking-surface (8).
摘要翻译：破碎弹丸包括在盒壳体内部的盒壳体（1），粉末充电器（3）和具有固定在盒壳体（1）中的剩余部分（5）的破坏抛射体（4）。射弹部分（6）; 将所述抛射体部分（6）与所述剩余部分（5）接合的破坏表面（8），并且当压缩部分（6）沿着所述破裂表面（8）从所述剩余部分（5）脱离时，以及在弹药体（1）内的放出的粉末气体向射弹部件（6）的表面（S1）的增加的压力（p）的影响超过阈值，以及将所述表面（S1 ）与所述盒壳体（1）的内部。所述弹丸部分（6）包括附加的加速器表面（S1'），以在所述弹丸部分（6）沿着所述断裂已经从其余部分（5）脱离时提供用于二次加速力的表面台阶（S2-S1）表面（8）。

6. 发明申请

WO2017116058A1 탄환 审中-公开
标题翻译：镜头
公开(公告)号：WO2017116058A1
公开(公告)日：2017-07-06
申请号：PCT/KR2016/014922
申请日：2016-12-20
申请人： 임채진
发明人： 임채진
IPC分类号： F42B10/32 , F42B10/34 , F42B10/38 , F42B10/04
CPC分类号： F42B10/04 , F42B10/32 , F42B10/34 , F42B10/38
摘要： 본 발명은 화기에서 발사되는 탄환에 관한 것으로, 비행 안정성을 증대시켜 직진성과 사거리를 늘린 탄환과 관련되며 실시예로, 전진 방향에 따라 전후를 관통하는 중앙홀이 형성되어 있는 몸체와, 상기 중앙홀의 단면 중심을 기준으로 등각도로 배치되어 있으며, 상기 몸체의 단면 중심을 기준으로 일방향으로 휘어져 있는 복수의 날개부를 포함하는 탄환을 제시한다.
摘要翻译：
本发明涉及到从武器发射的弹丸，通过增加飞行稳定性与弹丸增加线性度和范围内的实施例中，根据前进方向通过前部和后部的中心孔形成并且多个翼相对于中心孔的横截面的中心以相等的角度设置并且相对于本体的横截面的中心在一个方向上弯曲。

7. 发明申请

WO2017105586A1 BASE DRAG REDUCTION FAIRING USING SHAPE MEMORY MATERIALS 审中-公开
标题翻译：使用形状记忆材料进行基础减载
公开(公告)号：WO2017105586A1
公开(公告)日：2017-06-22
申请号：PCT/US2016/055229
申请日：2016-10-03
申请人： RAYTHEON COMPANY
发明人： SUMMERS, Matthew H. , KOEHLER, Frederick B. , DANFORTH, Jeremy C. , VILLARREAL, James K.
IPC分类号： F42B10/14 , F42B10/40 , F42B10/44
CPC分类号： F42B10/38 , B63G8/00 , F42B10/14 , F42B10/40 , F42B10/44
摘要： A device (100) is provided. The device includes at least one SMM component (115, 120, 130) fabricated from a shape memory material (SMM). The SMM component is configured to change shape in response to receiving a stimulus. The SMM component is also configured to deploy from a device body (105) of the device allowing the device to change shape in an advantageous way. A method (1000) implemented by a device (100) is also provided. The method includes changing (1010) a shape of an SMM component (115, 120, 130) of the device in response to receiving a stimulus. The SMM component is fabricated from an SMM. The method also includes deploying (1015) the SMM component from a device body (105) of the device allowing the device to change shape in an advantageous way.
摘要翻译：提供了一种设备（100）。该装置包括由形状记忆材料（SMM）制造的至少一个SMM部件（115,120,130）。 SMM组件配置为响应接收刺激而改变形状。 SMM部件还被配置为从装置的装置主体（105）展开，允许装置以有利的方式改变形状。还提供了由设备（100）实现的方法（1000）。该方法包括响应于接收刺激而改变（1010）设备的SMM组件（115,120,130）的形状。 SMM组件是由SMM制造的。该方法还包括从设备的设备主体（105）部署（1015）SMM组件，允许设备以有利的方式改变形状。

8. 发明申请

WO2010144008A1 AIR GUIDING MEANS FOR A DISPENSER 审中-公开
标题翻译：空气导向装置
公开(公告)号：WO2010144008A1
公开(公告)日：2010-12-16
申请号：PCT/SE2009/050717
申请日：2009-06-11
申请人： SAAB AB , ZÄTTERQVIST, Christer
发明人： ZÄTTERQVIST, Christer
IPC分类号： F41H11/02 , B64D1/02
CPC分类号： F42B5/155 , F42B4/26 , F42B10/38 , F42B12/62 , F42B12/70
摘要： The present invention relates to an air guiding means for a dispenser, com- prising at least one air scoop (4) to guide an air stream (6) to a feeding out opening (8) for chaffs on the dispenser (2) in order to facilitate packages of chaffs (10) to be released from the dispenser (2). The control means (18) is provided for controlling the air stream (6) through the at least one air scoop (4).
摘要翻译：本发明涉及一种用于分配器的空气引导装置，包括至少一个空气铲斗（4），用于将空气流（6）引导到用于分配器（2）上的谷壳的送出开口（8）以便于从分配器（2）释放的包壳（10）的包装。控制装置（18）用于通过至少一个空气勺（4）控制气流（6）。

9. 发明申请

WO2008091362A3 METHODS AND APPARATUS FOR MISSILE AIR INLET 审中-公开
标题翻译：用于空气入口的方法和装置
公开(公告)号：WO2008091362A3
公开(公告)日：2009-01-08
申请号：PCT/US2007072233
申请日：2007-06-27
申请人： RAYTHEON CO , GESWENDER CHRIS E
发明人： GESWENDER CHRIS E
IPC分类号： F42B10/00
CPC分类号： F02K7/10 , F02K7/105 , F02K7/18 , F42B10/38 , F42B15/10
摘要： Methods and apparatus for delivering a missile may operate in conjunction with a missile comprising an outer skin. The missile may be configured in a closed position and an open position. In the open position, an aperture is opened in the outer skin, for example to supply air to an air-breathing engine. In the closed position, the aperture is closed.
摘要翻译：用于传送导弹的方法和装置可以与包括外部皮肤的导弹一起操作。导弹可以配置在关闭位置和打开位置。在打开位置时，在外皮中开孔，例如将空气供给到空气呼吸引擎。在关闭位置，孔关闭。

10. 发明申请

WO1996021839A1 IMPROVEMENTS IN OR RELATING TO SHOT 审中-公开
标题翻译：改善或相关于拍摄
公开(公告)号：WO1996021839A1
公开(公告)日：1996-07-18
申请号：PCT/GB1996000038
申请日：1996-01-10
申请人： TAYLOR, David, Bradley
IPC分类号： F42B07/04
CPC分类号： A01K95/00 , B22F1/0007 , B22F1/02 , F42B7/046 , F42B10/38
摘要： Shot comprising metallic, e.g. lead, pellets (1) in which each pellet (1) has a surface provided with recesses (3) or projections defining a surface pattern. Each metallic pellet may be provided with one or more layers (4) of one or more coating materials. The invention also relates to a method of producing metallic shot and to a shotgun cartridge incorporating metallic shot.
摘要翻译：射击包括金属，例如铅，颗粒（1），其中每个颗粒（1）具有设置有凹槽（3）的表面或限定表面图案的突起。每个金属颗粒可以设置有一个或多个一个或多个涂层材料层（4）。本发明还涉及一种制造金属镜头的方法和一种结合金属镜头的霰弹枪筒。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式