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公开(公告)号：US20060130951A1
公开(公告)日：2006-06-22
申请号：US11017123
申请日：2004-12-20
IPC分类号： B60C3/06
CPC分类号： B60C11/0083 , B29D30/0601 , B29D2030/201 , B60C3/06 , B60C17/0009 , B60C17/0018 , Y10T152/10504
摘要： A pneumatic tire is capable of operation during underinflated condition and the construction of sidewalls are configured to compensate for negative cambers acting upon the tire. The inboard side of the tire is softened in comparison to the outboard side of the tire. This is achieved by either forming an asymmetrical tire in either the tire profile or the internal construction.
摘要翻译： 充气轮胎能够在欠充气状态下操作，并且侧壁的构造被构造成补偿作用在轮胎上的负弯矩。 轮胎的内侧与轮胎的外侧相比软化。 这可以通过在轮胎轮廓或内部结构中形成不对称轮胎来实现。
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公开(公告)号：US20050092415A1
公开(公告)日：2005-05-05
申请号：US10696620
申请日：2003-10-29
CPC分类号： B60C3/04 , B60C17/0009 , B60C17/0018 , Y10T29/49494
摘要： A self-supporting pneumatic tire is molded in such a manner that ride comfort is improved, durability is increased, and a greater run-flat capability can be achieved. The self-supporting run-flat tire is molded such that the molded bead base width is equal or less than the rim width of the intended rim upon which the tire is to be mounted. By molding the tire with a bead width less than or equal to the rim width, the sidewall inserts are not subjected to additional stress during and after inflation of the tire and the strain energy is more evenly distributed through the sidewall pillar construction.
摘要翻译： 自支撑充气轮胎以提高乘坐舒适度，耐久性提高的方式模制，并且可以实现更大的跑平能力。 自支撑漏气保用轮胎被模制成使得模制胎圈基座宽度等于或小于要安装轮胎的预期轮辋的轮辋宽度。 通过使胎圈宽度小于或等于轮辋宽度的轮胎成型，胎侧插入件在轮胎充气期间和充气后不会受到额外的应力，并且应变能更均匀地分布在侧壁支柱结构中。
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公开(公告)号：USD731870S1
公开(公告)日：2015-06-16
申请号：US29467482
申请日：2013-09-19
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公开(公告)号：USD705033S1
公开(公告)日：2014-05-20
申请号：US29423751
申请日：2012-06-05
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公开(公告)号：USD731282S1
公开(公告)日：2015-06-09
申请号：US29467489
申请日：2013-09-19
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公开(公告)号：US20120097060A1
公开(公告)日：2012-04-26
申请号：US13079392
申请日：2011-04-04
申请人： Johan Dahlberg
发明人： Johan Dahlberg
IPC分类号： F42B5/26
CPC分类号： F42B5/16
摘要： A method for producing propellant charges with progressive combustion characteristic and a higher charge density than previously considered possible to achieve, intended in the first instance for direct-firing barrel weapons such as tank cannons. Combined in the charge are at least two radially perforated propellant tubes, which are arranged in their entirety inside or after one another, and which have at an e-dimension selected in relation to the actual type of propellant and its desired combustion characteristic, combustion or ignition channels, and which have circular outer and inner boundary surfaces, in conjunction with which, before initiation of the charge, at least one of the total number of outer surfaces of these propellant tubes that are available for initiation has been treated with an inhibition, surface treatment or surface intended to delay the propagation of ignition to that surface so that the combustion of the propellant tubes is partially mutually overlapping.
摘要翻译： 一种用于产生具有逐步燃烧特性和较先前认为可能达到的较高电荷密度的推进剂电荷的方法，其首先用于直接燃烧炮弹武器如坦克炮。 在充电中组合的是至少两个径向穿透的推进剂管，其全部内部或彼此排列，并且具有相对于实际类型的推进剂选择的e维度及其期望的燃烧特性，燃烧或 点火通道，并且具有圆形的外部和内部边界表面，在开始充电之前，这些可用于引发的这些推进剂管的外表面的总数中的至少一个已经被抑制地处理， 表面处理或表面，旨在延迟点火到该表面的传播，使得推进剂管的燃烧部分地相互重叠。
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7.发明授权Method and arrangement for producing propellant for charges with high charge density and high progressivity 失效用于生产具有高电荷密度和高渐进性的电荷的推进剂的方法和装置公开(公告)号：US07921777B2
公开(公告)日：2011-04-12
申请号：US10582114
申请日：2004-12-08
申请人： Johan Dahlberg
发明人： Johan Dahlberg
摘要： The present invention relates to a method and an arrangement for the production of radially perforated, cylindrical propellant tubes (1, 23, 31). The invention is based on the underlying idea that the respective propellant tube (1, 23, 31) must be fixed and centred between its own open ends and thereafter to be perforated in stages in a large number of consecutive perforation operations by means of one or more pins (13) capable of displacement in a pin die (10) relative to the propellant tube towards and at least through the major proportion of the cylindrical wall of the propellant tube. Also included in the invention is the requirement for the displacement, between each perforation operation, of the propellant tube and the pin die (10) used for the preparation operation in such a way relative to one another that the propellant tube, after a complete perforation operation, shall be covered in its entirely by perforations (32, 33, 35, 36), which lie at a predetermined e-dimension distance from one another.
摘要翻译： 本发明涉及用于生产径向穿孔的圆柱形推进剂管（1，23,31）的方法和装置。 本发明基于以下基本思想：相应的推进剂管（1,23,31）必须固定并居中在其自身的开放端之间，然后通过一个或多个连续穿孔操作在大量连续的穿孔操作中分阶段穿孔 更多的销（13）能够相对于推进剂管朝向并且至少通过推进剂管的圆柱形壁的主要部分在销模（10）中移位。 在本发明中还包括要求在每次穿孔操作之间，推进剂管与用于准备操作的销模（10）之间相对于彼此的移位，使得推进剂管在完全穿孔之后 操作应完全由穿孔（32,33,35,36）覆盖，穿孔彼此处于预定的e维距离。
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公开(公告)号：USD731280S1
公开(公告)日：2015-06-09
申请号：US29467484
申请日：2013-09-19
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9.发明授权公开(公告)号：US08607704B2
公开(公告)日：2013-12-17
申请号：US12934154
申请日：2009-03-23
CPC分类号： F41A19/58 , F42B5/08 , F42C19/0811
摘要： The invention relates to a method of, in the electrical ignition of a propellent charge (1) provided with an electrically conductive surface coating (5) and comprising one or more propellant components (3), ensuring that ignition and progressive combustion of the propellent charge take place. The method is characterized in that said electrically conductive surface coating, when ignition of the propellent charge is desired, is connected to an electrical high-voltage source (6), in that said high-voltage source is made to generate at least one high electrical pulse to said connected electrically conductive surface coating, and in that said at least one high electrical pulse produces an instantaneous flashover ignition of the electrically conductive surface coating of the propellent charge and of all its propellant components, simultaneously. The invention also relates to a propellent charge and to an ammunition shot comprising the propellent charge.
摘要翻译： 本发明涉及一种在具有导电表面涂层（5）并且包括一个或多个推进剂组分（3）的推进剂装料（1）的电点火中的方法，确保推进剂装料的点燃和逐步燃烧 发生。 该方法的特征在于，当需要推进剂电荷的点燃时，所述导电表面涂层连接到电气高压源（6），因为所述高压源被制成以产生至少一个高电 脉冲到所述连接的导电表面涂层，并且所述至少一个高电脉冲同时产生推进剂电荷及其所有推进剂组分的导电表面涂层的瞬时闪络点火。 本发明还涉及一种推进剂装药和一种包括推进剂装药的弹药射流。
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公开(公告)号：US08544387B2
公开(公告)日：2013-10-01
申请号：US13079392
申请日：2011-04-04
申请人： Johan Dahlberg
发明人： Johan Dahlberg
IPC分类号： C06B45/12
CPC分类号： F42B5/16
摘要： A method for producing propellant charges with progressive combustion characteristic and a higher charge density than previously considered possible to achieve, intended in the first instance for direct-firing barrel weapons such as tank cannons. Combined in the charge are at least two radially perforated propellant tubes, which are arranged in their entirety inside or after one another, and which have at an e-dimension selected in relation to the actual type of propellant and its desired combustion characteristic, combustion or ignition channels, and which have circular outer and inner boundary surfaces, in conjunction with which, before initiation of the charge, at least one of the total number of outer surfaces of these propellant tubes that are available for initiation has been treated with an inhibition, surface treatment or surface intended to delay the propagation of ignition to that surface so that the combustion of the propellant tubes is partially mutually overlapping.
摘要翻译： 一种用于产生具有逐步燃烧特性和较先前认为可能达到的较高电荷密度的推进剂电荷的方法，其首先用于直接燃烧炮弹武器如坦克炮。 在充电中组合的是至少两个径向穿透的推进剂管，其全部内部或彼此排列，并且具有相对于实际类型的推进剂选择的e维度及其期望的燃烧特性，燃烧或 点火通道，并且具有圆形的外部和内部边界表面，在开始充电之前，这些可用于引发的这些推进剂管的外表面的总数中的至少一个已经被抑制地处理， 表面处理或表面，旨在延迟点火到该表面的传播，使得推进剂管的燃烧部分地相互重叠。
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