公开(公告)号：US07305911B2

公开(公告)日：2007-12-11

申请号：US10968267

申请日：2004-10-20

Applicant: Christer Regebro

Inventor： Christer Regebro

IPC: F41A1/08

CPC classification number: F41F3/0455 ,  F41A1/10

Abstract: The present invention relates to a method and a device by means of which it has been made possible, without gas discharge to the surrounding environment, to accelerate the speed of a powder-gas-driven projectile from zero to a speed which gives the projectile free-flying characteristics. According to the invention, this has been made possible by utilizing at least some of the expansion force from the propellant powder charge, which discharges gas when it is initiated, for, by a displaceable piston, driving a countermass out of the rear part of the projectile in the direction opposite to the desired flying direction of the projectile.

Abstract translation: 本发明涉及一种方法和装置，通过这种方法和装置，使气体排放到周围环境的可能性使得将粉末 - 气体驱动的射弹的速度从零加速到使射弹释放的速度 相对特征 根据本发明，通过利用来自推进剂粉末装料的至少一些膨胀力，可以实现这一点，该推进剂粉末装料在启动时将气体排出，以便通过可移位活塞将反质量驱动出 在与弹丸的所需飞行方向相反的方向上弹丸。

公开(公告)号：US20070243504A1

公开(公告)日：2007-10-18

申请号：US10594452

申请日：2005-03-15

Applicant: Ulf Bjorkman ,  Anders Holmquist

Inventor： Ulf Bjorkman ,  Anders Holmquist

IPC: F41G3/26

CPC classification number: F41G3/2655 ,  F41G3/265 ,  F41G3/2666

Abstract: A weapon effect simulation system including a fire simulation system and at least one hit simulation system. The fire simulation system includes a transmitter for transmitting electromagnetic waves to simulate real ammunition from a weapon and elements for including information in the electromagnetic waves. The hit simulation system includes both a receiver for receiving the transmitted electromagnetic waves and a processor for determining, based on received electromagnetic waves, whether a target has been hit. The fire simulation system further includes a calculator for calculating the imagined trajectory of the simulated ammunition and a processor for determining the geographical position of the weapon, and wherein the elements for including information in the electromagnetic waves are arranged so as to include information related to coordinates in the three-dimensional space for the calculated ammunition trajectory.

Abstract translation: 一种武器效果模拟系统，包括火灾仿真系统和至少一个命中模拟系统。 火灾模拟系统包括用于传送电磁波以从武器模拟真实弹药的发射机和用于在电磁波中包括信息的元件。 命中模拟系统包括用于接收所发送的电磁波的接收器和用于基于接收的电磁波确定目标是否已被击中的处理器。 火灾模拟系统还包括用于计算模拟弹药的想象轨迹的计算器和用于确定武器的地理位置的处理器，并且其中用于在电磁波中包括信息的元件被布置成包括与坐标有关的信息 在计算弹药轨迹的三维空间中。

公开(公告)号：US20070181129A1

公开(公告)日：2007-08-09

申请号：US10569080

申请日：2004-08-18

Applicant: Fredrik Mattinson ,  Gote Svedenkrans

Inventor： Fredrik Mattinson ,  Gote Svedenkrans

IPC: A62B18/02

CPC classification number: A62B9/006 ,  A62B18/08 ,  G02B27/017 ,  G02B27/0176 ,  G02B2027/0138

Abstract: A breathing mask with a display device can comprise means for providing gas and removing exhaled air from the mask, a visor which permits viewing of the external environment with an adjustment mechanism allowing adjustment of an optics unit with display arranged in the inside of the visor, means for fitting the mask on a wearer, an infrared camera, and an electronic unit with power supply.

Abstract translation: 具有显示装置的呼吸面罩可以包括用于提供气体和从面罩去除呼出的空气的装置，一种允许利用布置在面罩内部的显示器调整光学单元的调节机构来观察外部环境的面罩， 用于将面罩安装在佩戴者，红外线照相机和带有电源的电子单元的装置。

公开(公告)号：US20070176327A1

公开(公告)日：2007-08-02

申请号：US11608850

申请日：2006-12-11

Applicant: Mikael PETERSSON ,  Bjorn WEIDMAN ,  Jonny GUSTAVSSON ,  Max KROGAGER

Inventor： Mikael PETERSSON ,  Bjorn WEIDMAN ,  Jonny GUSTAVSSON ,  Max KROGAGER

IPC: B28B3/02

CPC classification number: B29D99/0014 ,  B29C70/342 ,  B29C70/44 ,  Y10T156/1031

Abstract: Method for manufacturing an elongate stiffening element (12) and a rigid shell structure (10) integrated with at least one elongate stiffening element (12). The method includes the steps of providing a preformed, form-stable reinforcement member (16), which has a hat profile with two inwardly directed, opposing flange portions (20), covering the reinforcement member with a curable composite material to form an external hat profile having outwardly directed flanges (26), and integrating this assembly with either a curable or preformed shell structure (10) of composite material.

Abstract translation: 用于制造细长加强元件（12）和与至少一个细长加强元件（12）成一体的刚性壳结构（10）的方法。 该方法包括以下步骤：提供预成形的，形状稳定的加强件（16），其具有带有两个向内相对的凸缘部分（20）的帽形轮廓，用可固化复合材料覆盖加强件以形成外部帽子 具有向外引导的凸缘（26），并将该组件与复合材料的可固化或预制的壳结构（10）整合。

公开(公告)号：US20070078573A1

公开(公告)日：2007-04-05

申请号：US11535503

申请日：2006-09-27

Applicant: Johan Ivansson ,  Mans Mangard

Inventor： Johan Ivansson ,  Mans Mangard

IPC: G06F19/00

CPC classification number: G01C21/20 ,  G05D1/0223

Abstract: A method for planning the velocity of a craft along a predetermined route, where said method comprises the step of transforming demands and limitations of said route and said craft into a time-distance domain. Said planning subsequently takes place in said domain. The method saves computational time.

Abstract translation: 一种用于沿着预定路线规划飞行器的速度的方法，其中所述方法包括将所述路线和所述飞行器的需求和限制转换为时间域的步骤。 所述规划随后发生在所述领域。 该方法节省了计算时间。

公开(公告)号：US20070039689A1

公开(公告)日：2007-02-22

申请号：US11464834

申请日：2006-08-16

Applicant: Mikael Petersson ,  Bjorn Weidmann ,  Max Krogager ,  Ingemar Turesson

Inventor： Mikael Petersson ,  Bjorn Weidmann ,  Max Krogager ,  Ingemar Turesson

IPC: B32B37/00 ,  B29C65/00 ,  B32B9/04

CPC classification number: B29C70/342 ,  B29C33/52 ,  B29C70/86 ,  Y10T428/31504

Abstract: The present invention relates to a method for the manufacture of a composite article comprising a composite plate (1) and at least one fitting (4). The method is characterized by the steps of arranging at least one former on said composite plate (1), arranging at least one fitting (4) on said composite plate (1), producing a lay-up by applying a composite material layer (9) least partly covering an external surface of the former and of the fitting, and curing the layup in a curing process. After curing, said composite material layer (9) forms the walls of a stiffener and at least partly encloses the fitting so as to support it in a predetermined position.

Abstract translation: 本发明涉及一种复合制品的制造方法，所述复合制品包括复合板（1）和至少一个配件（4）。 该方法的特征在于在所述复合板（1）上布置至少一个成形器，在所述复合板（1）上布置至少一个配件（4），通过施加复合材料层（9 ）最少部分地覆盖前者和配件的外表面，并且在固化过程中固化上层。 固化后，所述复合材料层（9）形成加强件的壁，并且至少部分地包围所述配件以便将其支撑在预定位置。

公开(公告)号：US20060293855A1

公开(公告)日：2006-12-28

申请号：US11162089

申请日：2005-08-29

Applicant: Henrik Hammarlund ,  Bengt-Goran Sundqvist ,  Hasse Persson ,  Jonas Lovgren

Inventor： Henrik Hammarlund ,  Bengt-Goran Sundqvist ,  Hasse Persson ,  Jonas Lovgren

IPC: G08G1/16

CPC classification number: G08G5/045 ,  G01S5/0072 ,  G08G5/0008

Abstract: A method and a system for avoiding collisions between aircrafts. The method comprises: computing a default fly out maneuver regarding how the aircraft shall be maneuvered during a fly out action, predicting a fly away path comprising a prediction of the position of the aircraft during the fly out maneuver, sending information about the own fly away path to the other aircrafts, receiving information about fly away paths from the other aircrafts, detecting an approaching collision, and activating the fly out maneuver upon detecting an approaching collision. The method further comprises carrying out the following steps after activation the fly out maneuver: receiving the current position of the aircraft, and calculating a compensated fly out maneuver for the aircraft based on the current position of the aircraft, said previously predicted position, and the default fly out maneuver.

Abstract translation: 一种避免飞机碰撞的方法和系统。 该方法包括：计算关于飞行器在飞行动作期间如何被操纵的默认飞行操纵，预测飞行路径包括在飞行操纵期间对飞行器的位置的预测，发送关于自己飞行的信息 接收到其他飞机的路径，从其他飞机接收有关飞行路径的信息，检测到接近的碰撞，以及在检测到接近的碰撞时激活飞行操纵。 该方法还包括在激活飞行机动之后执行以下步骤：接收飞行器的当前位置，并且基于飞行器的当前位置，所述先前预测的位置以及飞行器的当前位置计算飞行器的补偿飞出机动 默认飞行机动。

公开(公告)号：US07151999B2

公开(公告)日：2006-12-19

申请号：US10919407

申请日：2004-08-17

Applicant: Fredrik Neregård

Inventor： Fredrik Neregård

IPC: G01S1/00

CPC classification number: G01S13/94 ,  G01C21/165 ,  G01S5/02

Abstract: The present invention relates to terrain navigation wherein an earth-reflected satellite signal is received from at least one reference signal source whose position is known (120), for example a navigation satellite. Based on information contained in the received signal a measured estimate of a shortest reflection distance (d1(tb)) to the satellite (120) is derived. A relative spatial movement (Δx, Δy, Δh) of a relevant craft (110) since a previous positioning instance (ta) is registered onboard the craft (110). Moreover, stored surface information is retrieved pertaining to an elevation (h1b) of the earth surface (130) in relation to the mean sea level (z0) at at least one geographical position (X1b, Y1b). Based on the relative spatial movement (Δx, Δy, Δh) and the retrieved surface information at least one calculated estimate of the shortest reflection distance (d1(tb)) to the satellite (120) is derived. Finally, a geographical position (X1a, Y1a, h1a) is determined on basis of the measured and calculated estimates of the shortest reflection distance (d1(tb)). Thus, a highly reliable and entirely passive positioning may be accomplished on basis of external signals from as few satellites (120) as one.

Abstract translation: 地形导航技术领域本发明涉及地形导航，其中从其位置已知（120），例如导航卫星的至少一个参考信号源接收地球反射的卫星信号。 基于包含在接收信号中的信息，导出对卫星（120）的最短反射距离（d 1 SUB（t B b B））的测量估计。 由于先前的定位实例（t> a ）之后的相关工艺（110）的相对空间运动（Deltax，Deltay，Deltah）被登记在船上（110）上。 此外，至少与平均海平面（z> 0 ）相关的地表面（130）的高度（h1B1）有关的存储表面信息被检索到 一个地理位置（X 1b 1b，Y 1b 1b）。 基于相对空间运动（Deltax，Deltay，Deltah）和所检索的表面信息，至少一个计算出的最短反射距离的估计（d 1 SUB（t B））） 导出到卫星（120）。 最后，基于最短反射的测量和计算的估计来确定地理位置（X 1a，Y 1a，h 1a 1a） 距离（d 1）（t B b））。 因此，可以基于来自少量卫星（120）的外部信号来实现高可靠性和完全被动定位。

公开(公告)号：US07150231B2

公开(公告)日：2006-12-19

申请号：US10809328

申请日：2004-03-26

Applicant: Göran Olofsson

Inventor： Göran Olofsson

IPC: F42B39/14 ,  F42B39/20

CPC classification number: F42B1/036 ,  F42B1/02 ,  F42B1/024 ,  F42B1/028 ,  F42B1/032 ,  F42B39/20

Abstract: An active part of an ammunition device. A casing is provided with a sleeve in association with an opening of the casing. A sprung device is arranged between a locking device arranged at the opening of the casing and the sleeve. The end of the sleeve facing away from the sprung device contacts an explosive charge arranged inside the casing of the active part or a liner arranged on the surface of the explosive charge which faces towards the sleeve and the locking device. The locking device is designed to be released from the casing by the action of a force. The active part keeps the active part intact even if materials in the active part have greatly varying coefficients of thermal expansion, while at the same time, in extreme temperatures, the active part is prevented from detonating by the locking device being released from the casing.

Abstract translation: 弹药装置的活跃部分。 壳体设置有与壳体的开口相关联的套筒。 弹簧装置布置在布置在壳体的开口处的锁定装置和套筒之间。 套筒的远离弹簧装置的端部接触布置在活动部件的壳体内部的炸药，或者布置在面向套筒和锁定装置的炸药的表面上的衬套。 锁定装置设计成通过力的作用从壳体释放。 活性部分即使活性部分中的材料具有大的变化的热膨胀系数，也保持活性部分完整，同时在极端温度下，通过锁定装置从壳体释放而防止有源部分引爆。

公开(公告)号：US07124982B2

公开(公告)日：2006-10-24

申请号：US10479663

申请日：2002-04-23

Applicant: Pär Brofeldt

Inventor： Pär Brofeldt

IPC: B64C1/06

CPC classification number: B64C1/12

Abstract: A device for bracing a shell surface in an aircraft fuselage against deformations and consisting of a continuous profile that is arranged so as, after conformation, to be mounted against the shell surface. Notches are spaced at regular distances apart from each other in at least a portion of the profile. The notches extend through a base surface in the profile, and through an intermediate part perpendicular to the base surface. The notches are delimited upwardly by an upper surface that is not encompassed by the notches.

Abstract translation: 一种用于支撑飞机机身中的壳体表面以防止变形并由连续轮廓构成的装置，其在构造之后被布置成抵靠壳体表面安装。 凹槽在轮廓的至少一部分中彼此间隔规则的距离。 凹口延伸穿过轮廓中的基面，并穿过垂直于基面的中间部分。 凹口由不被凹口包围的上表面向上划定。