公开(公告)号：WO2005121692A1

公开(公告)日：2005-12-22

申请号：PCT/EP2005/052676

申请日：2005-06-09

Applicant: SAAB AB ,  HENRIKSSON, Johan ,  WIBERG, Jesper ,  EMRICSSON, Ingemar ,  MALM, Jonas

Inventor： HENRIKSSON, Johan ,  WIBERG, Jesper ,  EMRICSSON, Ingemar ,  MALM, Jonas

IPC: F42B8/12

CPC classification number: F42B12/382 ,  F42B8/12 ,  F42B12/48

Abstract: An impact cartridge unit for military exercise comprises a cartridge (1) containing a propulsive agent and on top thereof a member (2) simulating a low velocity grenade to be fired by a firearm or the like. Said grenade simulating member comprises an arrangement (5) adapted to simulate a detonation of a low velocity grenade and means associated therewith for triggering said detonation.

Abstract translation: 用于军事演习的冲击筒单元包括容纳推进剂的盒（1），并且在其上方具有模拟由枪支等点燃的低速手榴弹的构件（2）。 所述手榴弹模拟构件包括适于模拟低速手榴弹的爆震的装置（5），以及用于触发所述爆震的装置。

公开(公告)号：WO0236955A8

公开(公告)日：2005-11-10

申请号：PCT/SE0102381

申请日：2001-10-30

Applicant: SAAB AB ,  NILSSON LARS ,  AX LARS

Inventor： NILSSON LARS ,  AX LARS

IPC: F02K9/08 ,  F02K9/32 ,  F02K9/70 ,  F02K9/76 ,  F02K9/95 ,  F02K9/97 ,  F42B15/36

CPC classification number: F42B15/36 ,  F02K9/08 ,  F02K9/32 ,  F02K9/70 ,  F02K9/76 ,  F02K9/763 ,  F02K9/95 ,  F02K9/978

Abstract: The present invention relates to a method and an arrangement for, in multi-stage rockets (3) provided with a number of successively ignitable rocket engines (7, 13) arranged one in front of another in the flying direction of the rocket and joined together detachably with one another, each following rocket engine (13) in the ignition sequence depending, for its ignition, on being initiated after a preceding rocket engine (7) has been able to bun out, causing each preceding rocket engine (7) included in the ignition sequence to be jettisoned by virtue of the next engine having reached its working pressure. According to the invention, each preceding rocket engine is designed with a preferably conical guide part (11) which is directed forwards in the flying direction of the rocket and geometrically adapted to the exhaust nozzle (12) of the following rocket engine (13) and which, in the initial position, is fitted into said exhaust nozzle (12) and fixed in this position by means of at least one blocking part (15) which is deformable or capable of elastic recovery.

Abstract translation: 本发明涉及一种多级火箭（3）中的方法和装置，该多级火箭（3）具有在火箭的飞行方向上一个在另一个前方排列并连接在一起的若干连续可点燃的火箭发动机（7,13） 每个随后的火箭发动机（13）在点火顺序中依赖于其点火，在先前的火箭发动机（7）能够蹦出之后被启动，使得每个先前的火箭发动机（7）包括在 由于下一个发动机已经达到其工作压力而要排出的点火顺序。 根据本发明，每个先前的火箭发动机被设计成具有优选的圆锥形引导部分（11），其沿着火箭的飞行方向向前指向并几何地适应于随后的火箭发动机（13）的排气喷嘴（12）和 其在初始位置被装配到所述排气喷嘴（12）中并且通过至少一个可变形或能够弹性恢复的阻挡部分（15）固定在该位置。

公开(公告)号：WO2005093363A1

公开(公告)日：2005-10-06

申请号：PCT/EP2005/002728

申请日：2005-03-15

Applicant: SAAB AB ,  BJÖRKMAN, Ulf ,  HOLMQUIST, Anders

Inventor： BJÖRKMAN, Ulf ,  HOLMQUIST, Anders

IPC: F41G3/26

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

Abstract: This invention concerns a weapon effect simulation system comprising a fire simulation system and at least one hit simulation system. The fire simulation system comprises both means (2) for transmitting electromagnetic waves to simulate real ammunition from a weapon and means (21) for including information in the electromagnetic waves. The hit simulation system contains both means for receiving the transmitted electromagnetic waves and means (33) for determining, based on received electromagnetic waves, whether a target has been hit. The weapon effect simulation system is characterized in that the fire simulation system further comprises means (17) for calculating the imagined trajectory of the simulated ammunition and means (20) for determining the geographical position of the weapon, and in that the means (21) 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: 本发明涉及一种包括火灾模拟系统和至少一个命中模拟系统的武器效果模拟系统。 火灾仿真系统包括用于发射电磁波以模拟来自武器的真实弹药的装置（2）和用于在电磁波中包括信息的装置（21）。 命中模拟系统包含用于接收所发射的电磁波的装置和用于基于接收到的电磁波确定目标是否已被击中的装置（33）。 武器效应模拟系统的特征在于，火灾模拟系统还包括用于计算模拟弹药的想象轨迹的装置（17）和用于确定武器的地理位置的装置（20），并且手段（21） 在电磁波中包含信息被布置为包括与用于所计算的弹药轨迹的三维空间中的坐标有关的信息。

公开(公告)号：WO2005088505A1

公开(公告)日：2005-09-22

申请号：PCT/SE2005/000358

申请日：2005-03-14

Applicant: SAAB AB ,  OLSSON, Kjell

Inventor： SAAB AB ,  OLSSON, Kjell

IPC: G06F17/60

CPC classification number: G06Q40/08

Abstract: The invention relates to a method and an arrangement in electronic systems. The application can concern smaller systems for control, monitoring and regulation, and can also concern larger systems, such as, for example, systems for police, fire services, rescue services, etc. The application can also relate to a subsystem or a function in a very large system, for example comprised in management systems for military operations. The invention is charaterized in that it handles uncertainties within its area of application in a special way. These can be uncertainties regarding the parameter that is to be determined or uncertainties in the signals or data that constitute the basis for the determination of the sought parameter. There is often also a time-critically within the application. In certain applications, changes can be rapid and the invention can also handle such dynamic processes. The benefit of the invention is particularly marked in the difficult cases when the dynamic processes are associated with uncertainties. The invention carries out detection and prediction in electronic systems.

Abstract translation: 本发明涉及一种电子系统中的方法和装置。 该应用可以涉及用于控制，监控和调节的较小系统，并且还可以涉及较大的系统，例如用于警察，消防服务，救援服务等的系统。该应用还可以涉及子系统或功能 一个非常大的系统，例如包括在军事行动的管理系统中。 本发明的特征在于它以特殊的方式处理其应用领域的不确定性。 这些可能是关于要确定的参数或构成确定所寻求参数的依据的信号或数据中的不确定性的不确定性。 在应用程序中通常也有时间关键。 在某些应用中，变化可以很快，本发明也可以处理这种动态过程。 当动态过程与不确定性相关联的困难情况下，本发明的益处特别明显。 本发明在电子系统中进行检测和预测。

公开(公告)号：WO03106263A8

公开(公告)日：2005-03-10

申请号：PCT/SE0300670

申请日：2003-04-25

Applicant: SAAB AB ,  SARIN SOHAN ,  NORDIN PONTUS

Inventor： SARIN SOHAN ,  NORDIN PONTUS

IPC: F02K1/82 ,  G10K11/172 ,  B64D33/04 ,  F01N1/24 ,  G10K11/162

CPC classification number: F02K1/827 ,  G10K11/172 ,  Y02T50/671

Abstract: The present invention relates to an acoustic liner (1) arranged to attenuate sound. The acoustic liner (1) comprises a top sheet (5) having substantially linear characteristics and a liner core (2) or cavity. The top sheet (5) comprises a layer (3) of a metallic foam. The invention also relates to the use of said acoustic liner in a hot stream environment such as the outlet of an aircraft engine, and to the manufacture of an acoustic liner.

Abstract translation: 本发明涉及一种被设置为衰减声音的声学衬垫（1）。 声学衬垫（1）包括具有基本线性特征的顶片（5）和衬垫芯（2）或空腔。 顶片（5）包括金属泡沫的层（3）。 本发明还涉及在诸如飞机发动机的出口的热流环境中的所述声衬垫的使用以及声衬垫的制造。

公开(公告)号：WO2004022328A1

公开(公告)日：2004-03-18

申请号：PCT/SE2003/001353

申请日：2003-09-01

Applicant: SAAB AB ,  KROGAGER, Max ,  WESTERDAHL, Anders

Inventor： KROGAGER, Max ,  WESTERDAHL, Anders

IPC: B32B3/12

CPC classification number: B29C66/1142 ,  B29C65/483 ,  B29C65/54 ,  B29C65/7829 ,  B29C66/112 ,  B29C66/114 ,  B29C66/43 ,  B29C66/435 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72525 ,  B29K2105/06 ,  B29L2031/30 ,  B29L2031/307 ,  B29L2031/3076 ,  Y10T428/19 ,  B29C65/00 ,  B29K2307/04 ,  B29K2309/08

Abstract: This invention concerns a method for reinforcing a core (2) constructed of at least two core parts (2a, 2b, 2c, 2d), each of which exhibits a top side, a bottom side and walls joining the top side and bottom side. The core parts (2a, 2b, 2c, 2d) are arranged joined wall-to-wall with one another along a joint seam (4a, 4b, 4c) filled with glue, preferably in the form of a glue film. The method is characterized in that notches (5a, 5b, 5c) are realized in a number of places in the glue joint, which notches extent between the walls from the top side to the bottom side of the core parts so that the glue joint can be divided into pieces. The invention also encompasses an article fabricated in accordance with the aforementioned method.

Abstract translation: 本发明涉及一种用于加强由至少两个芯部分（2a，2b，2c，2d）构成的芯体（2）的方法，每个芯部分表现出顶侧，底侧和连接顶侧和底侧的壁。 核心部分（2a，2b，2c，2d）沿着填充有胶水的接缝（4a，4b，4c）彼此成壁连接，优选为胶膜形式。 该方法的特征在于，在胶接头中的多个位置上实现了切口（5a，5b，5c），其从芯部的顶侧到底侧的壁之间切割的程度，使得胶接合 分为几块。 本发明还包括根据上述方法制造的制品。

公开(公告)号：WO2004004253A1

公开(公告)日：2004-01-08

申请号：PCT/SE2003/000978

申请日：2003-06-12

Applicant: SAAB AB ,  PETTERSSON, Martin

Inventor： PETTERSSON, Martin

IPC: H04L12/56

CPC classification number: H04W72/0446 ,  H04W84/18

Abstract: The invention relates to communication of data in a time division multiple access system where the data is transmitted wirelessly between station (MS1-MS6; BS1-BS3) in time slots. The time slots are arranged in frames of a repeating frame structure. The stations (MS1-MS6; BS1-BS3) autonomously select time slots for transmission of data according to a self-organizing transmission algorithm, which allows a first station (MS1) to reuse a time slot that is allocated to a second station (MS2-MS6, BS2, BS3). According to the invention an addressed message (M M1 Adr ) is sent from a first base station (BS1) to a mobile station (MS1). This station transmits am acknowledgement message (Ack M1 B1 ) in response to the addressed message (M M1 Adr ) in order to confirm a safe receipt of the addressed message (M M1 Adr ). If due to for example a high traffic load, the acknowledgement message (Ack M1 B1 ) cannot be received directly by the first base station (BS1), the mobile station (MS1) sends this message (Ack M1 B1 ) via a second base station (BS2) to a message handling entity (MHE) in a network (N), which is responsible for the transmission of the addressed message (M M1 Adr ). The message handling entity (MHE) may either be a separate node in the network (N) or be included in the first station (BS1). Thanks to the proposed solution, unnecessary repeated transmissions of the addressed message (M M1 Adr ) can be avoided, and consequently valuable wireless bandwidth be saved.

Abstract translation: 本发明涉及在时分多址系统中的数据通信，其中数据在时隙中在站（MS1-MS6; BS1-BS3）之间无线地发送。 时隙以重复帧结构的帧布置。 站（MS1-MS6; BS1-BS3）根据自组织传输算法自主选择用于传输数据的时隙，这允许第一站（MS1）重用分配给第二站（MS2）的时隙 -MS6，BS2，BS3）。 根据本发明，将寻址消息（M Adr）从第一基站（BS1）发送到移动台（MS1）。 响应于寻址的消息（M Adr），该站发送确认消息（Ack B1），以确认寻址消息（M Adr）的安全接收。 如果由于例如高业务负载，则确认消息（Ack B1）不能被第一基站（BS1）直接接收，所以移动台（MS1）发送该消息（Ack B1）经由 第二基站（BS2）到网络（N）中的消息处理实体（MHE），负责传送寻址消息（M Adr）。 消息处理实体（MHE）可以是网络中的单独节点（N），也可以包括在第一站（BS1）中。 由于提出的解决方案，可以避免寻址消息（M Adr）的不必要的重复传输，从而节省有价值的无线带宽。

公开(公告)号：WO2003067192A1

公开(公告)日：2003-08-14

申请号：PCT/SE2003/000149

申请日：2003-01-29

Applicant: SAAB AB ,  SJANIC, Zoran

Inventor： SJANIC, Zoran

IPC: G01C21/20

CPC classification number: G01C21/20

Abstract: The invention concerns a method and a system for calculating a flight route between a first position and a second position. According to the method, the first position is chosen as the current position, and the following steps are then repeated until the second position is reached: a loss function is determined corresponding to each flight path in a set of flight paths that are predefined in relation to the current direction of flight; a flight path that yields the most advantageous value for the loss function is selected; a subsection from the current position and a predetermined number of positions forward are registered for the selected flight path, and the position at the end of the subsection is chosen as the new current position.

Abstract translation: 本发明涉及一种用于计算第一位置和第二位置之间的飞行路线的方法和系统。 根据该方法，选择第一位置作为当前位置，然后重复以下步骤直到达到第二位置：对应于在关系中预定义的一组飞行路径中的每个飞行路径确定损失函数 对于目前的飞行方向，从当前位置选择产生损失函数最有利值的飞行路径，并向所选择的飞行路径登记向前的预定数量的位置，并且在末尾处的位置 小节被选为新的当前位置。

公开(公告)号：WO2003064130A1

公开(公告)日：2003-08-07

申请号：PCT/SE2003/000027

申请日：2003-01-13

Applicant: SAAB AB ,  KROGAGER, Max ,  VAARA, Jan

Inventor： KROGAGER, Max ,  VAARA, Jan

IPC: B29C33/76

CPC classification number: B29C33/3821 ,  B29C33/54

Abstract: The subject invention concerns a method of manufacturing mould sections or mould inserts of the type used as interior support and moulding parts during the manufacture of products of malleable materials, such as fibre armoured polymer materials and such as are similar thereto, inclusive of the empty spaces in the final state of the products, such as integrated support profiles, built-in tank spaces etc. Thus, the relevant mould sections or mould inserts, according to the subject invention, shall be produced of a particulate material, in itself hard, that can consist, e.g., of sand, metallic powder or another similar product and that, contained in a gas-tight bag, gives the mould insert the desired exterior shape in a matrix or device equivalent thereto while the bag is vacuum sealed such that the particulate material forms a body of firm cohesion, after which the opening used for the vacuum sealing of the bag is hermetically sealed. The subject invention entails the method of manufacture of said mould inserts in question as well as the method of utilising the same.

Abstract translation: 本发明涉及在制造可延展材料的产品（例如纤维铠装聚合物材料）和类似于其中的包括空位的制造中用作内部支撑和模制部件的模具部分或模具插入件的制造方法 在产品的最终状态下，例如集成支撑型材，内置罐空间等。因此，根据本发明的相关模具部件或模具插入件应由颗粒材料本身制成，其本身是硬的，即 可以包括例如沙子，金属粉末或另一类似产品，并且包含在气密袋中的模具将模具插入件放置在与其相当的基质或装置中的期望的外部形状，同时袋被真空密封，使得颗粒 材料形成牢固的内聚力，之后用于袋的真空密封的开口被气密密封。 本发明涉及制造所讨论的所述模具插入件的方法以及使用该模具插入件的方法。

公开(公告)号：WO2003054389A1

公开(公告)日：2003-07-03

申请号：PCT/SE2002/001997

申请日：2002-11-04

Applicant: SAAB AB ,  KROGAGER, Max ,  VAARA, Jan

Inventor： KROGAGER, Max ,  VAARA, Jan

IPC: F03D11/02

CPC classification number: F03D80/30 ,  F03D80/00 ,  Y02E10/72

Abstract: The invention concerns a device for overvoltage protection in a wind turbine comprising a drive shaft (7) that is arranged to operatively connect one or a plurality of rotor blades (12) to a generator (9). The invention includes a drive shaft (7) containing a core of carbon fiber composite (7a) with a longitudinally through-passing cavity. In one end a connector (5) for a hub (4) that connects the rotor blades (12) is arranged to be introduced, and in the other end a coupling part (10) to the generator (9) is arranged to be introduced. An inner layer of fiberglass composite (7b), which is integrated with a core of carbon fiber composite (7a) in the drive shaft (7), surrounds the cavity and is arranged so as to electrically insulate the connector (5) and the coupling (10) from the drive shaft (7), which is electrically connected to ground.

Abstract translation: 本发明涉及一种用于风力涡轮机中的过电压保护的装置，包括驱动轴（7），该驱动轴被设置成将一个或多个转子叶片（12）可操作地连接到发电机（9）。 本发明包括一个包含碳纤维复合材料芯体（7a）的驱动轴（7），其具有纵向通孔。 在一端，用于连接转子叶片（12）的毂（4）的连接器（5）被布置成被引入，并且在另一端中，与发生器（9）的联接部分（10）被布置成被引入 。 与驱动轴（7）中的碳纤维复合材料（7a）的芯体一体化的玻璃纤维复合材料（7b）的内层包围空腔并且被布置成使得连接器（5）和联接器 （10）从与驱动轴（7）电连接的地面。