公开(公告)号：WO2015094059A1

公开(公告)日：2015-06-25

申请号：PCT/SE2013/051586

申请日：2013-12-20

Applicant: SAAB AB

Inventor： HALLANDER, Per ,  LUNDBERG, Anders ,  NYMAN, Tonny ,  PETERSSON, Mikael

IPC: B64C1/12 ,  B29C43/02 ,  B29C65/70 ,  B29C70/50 ,  B29C70/68 ,  B29D99/00

CPC classification number: B29C65/48 ,  B29C65/02 ,  B29C66/00145 ,  B29C70/382 ,  B29C70/386 ,  B29D99/0014 ,  B29K2105/06 ,  B29L2031/3076 ,  B64C1/061 ,  B64C1/064 ,  B64C1/12 ,  Y02T50/43

Abstract: A stiffening element 11 comprising at least a first stiffening profile 1and at least a second stiffening profile 2. The first stiffening profile 1 comprises a profile member 4, at least one structural flange 8 is connected to the profile member 4, a through-passage 9 extending through the profile member 4,and at least one support flange 10 is connected to the profile member 4.The second stiffening profile 2 comprises a bottom portion 12 and at least one support side portion 13 connected to the bottom portion 12. Furthermore, the invention relates to a method for manufacturing a stiffening element 11 and a method for manufacturing a reinforced structure 15, wherein the reinforced structure 15 comprises at least one structural element 14 and at least one stiffening element 11.

Abstract translation: 包括至少第一加强轮廓1和至少第二加强轮廓2的加强元件11.第一加强轮廓1包括轮廓构件4，至少一个结构凸缘8连接到轮廓构件4，通道9 延伸穿过轮廓构件4，并且至少一个支撑凸缘10连接到轮廓构件4.第二加强轮廓2包括底部12和连接到底部12的至少一个支撑侧部13。 本发明涉及一种用于制造加强元件11的方法和用于制造加强结构15的方法，其中加强结构15包括至少一个结构元件14和至少一个加强元件11。

公开(公告)号：WO2015069152A1

公开(公告)日：2015-05-14

申请号：PCT/SE2013/000171

申请日：2013-11-07

Applicant: SAAB AB (publ)

Inventor： EDSTRÖM, Karl ,  ÖSTLUND, Johan

IPC: F42C19/12 ,  F42B3/12

CPC classification number: F42C19/12 ,  F42B3/103 ,  F42B3/124 ,  F42B3/128 ,  F42B33/001

Abstract: The present invention relates to an electric detonator (1) comprising a cap (2), comprising a priming charge (3) and an electrode (4), comprising a positive pole, a negative pole and a resistor element (8), the said priming charge (3) comprising at least two primary explosives, a first primary explosive (9) and a second primary explosive (10), and at least one secondary explosive (11). The electric detonator is characterized in that the two primary explosives (9, 10) and the secondary explosive (11) are arranged in layers, in an increasing degree of sensitivity, bearing one against the other, wherein the first primary explosive (9), constituting the most sensitive of the two primary explosives (9, 10), is arranged closest to the resistor element (8), and in that the second primary explosive (10) is arranged thereafter between the first primary explosive (10) and the secondary explosive (11). The invention also relates to a production method for the said electric detonator (1).

Abstract translation: 本发明涉及一种电雷管（1），其包括盖（2），包括起动电荷（3）和电极（4），包括正极，负极和电阻元件（8），所述 包括至少两个主要爆炸物，第一主要爆炸物（9）和第二主要爆炸物（10）以及至少一个次要炸药（11）的起动炸药（3）。 电雷管的特征在于，两个主要爆炸物（9,10）和二次爆炸物（11）以增加的灵敏度排列成层叠，其中第一爆炸物（9）， 构成两个主要爆炸物（9,10）中最敏感的最靠近电阻元件（8）的位置，其中第二主要爆炸物（10）之后设置在第一主要爆炸物（10）和次要爆炸物 爆炸物（11）。 本发明还涉及所述电雷管（1）的制造方法。

公开(公告)号：WO2015038045A1

公开(公告)日：2015-03-19

申请号：PCT/SE2013/051075

申请日：2013-09-16

Applicant: SAAB AB

Inventor： ENMAR, Mats

IPC: B23Q3/06 ,  B25B11/02 ,  B64F5/00

CPC classification number: B23Q3/103 ,  B23Q1/5456 ,  B25B11/02 ,  B64F5/10

Abstract: The invention relates to an end-effector body (210, 252, 310) for a fixture device comprising a first fixing point (218, 262, 318) for attachment to an article (270, 370, 470), wherein the end-effector body (210, 252, 310) comprises a second fixing point (220, 262, 320) for article (270, 370, 470) attachment. The fixing points (218, 220, 262, 318, 320) are arranged to face away from the end-effector body (210, 252, 310) in different directions. The invention also regards an adjustable fixture device (400) comprising such end-effector body (210, 252, 310).

Abstract translation: 本发明涉及一种用于固定装置的末端执行器本体（210,252,310），其包括用于附接到制品（270,370,470）的第一固定点（218,262,318），其中末端执行器 主体（210,252,310）包括用于制品（270,370,470）连接的第二固定点（220,262,320）。 固定点（218,220,262,318,320）布置成在不同方向上远离末端执行器本体（210,252,310）。 本发明还涉及一种包括这种末端执行器本体（210,252,310）的可调节固定装置（400）。

公开(公告)号：WO2015038038A1

公开(公告)日：2015-03-19

申请号：PCT/SE2013/051049

申请日：2013-09-10

Applicant: SAAB AB

Inventor： BERGLUND, Pär

IPC: H01Q1/27

CPC classification number: H01Q1/27 ,  H01Q1/243 ,  H01Q5/378 ,  H01Q9/42

Abstract: The present invention relates to a portable device comprising a protective housing and antenna. The antenna comprises an antenna element and a ground plane. Further the antenna is integrally arranged along the protective housing. The protective housing is designed as a spacing element between the antenna element and the ground plane. Further the protective housing is adapted to hold a radio unit. The invention further relates to a garment adapted to house the portable device and the radio unit.

Abstract translation: 本发明涉及一种包括保护壳体和天线的便携式设备。 天线包括天线元件和接地平面。 此外，天线沿着保护壳体一体地布置。 保护壳被设计为天线元件和接地平面之间的间隔元件。 此外，保护壳体适于保持无线电单元。 本发明还涉及适于容纳便携式设备和无线电单元的衣服。

公开(公告)号：WO2014204361A1

公开(公告)日：2014-12-24

申请号：PCT/SE2013/050705

申请日：2013-06-17

Applicant: SAAB AB

Inventor： ANDERSSON, Stefan ,  FREDRIKSSON, Arnold ,  ZANDÉN, Johan

IPC: G02B27/01

CPC classification number: G02B27/0101 ,  G02B2027/0112 ,  G02B2027/0118 ,  G02B2027/0138 ,  G02B2027/0194 ,  G03B21/2013 ,  G03B21/206 ,  G03B21/28

Abstract: A head-up display system for a vehicle facilitating the use of night vision goggles for a person in the vehicle during night vision conditions, the system comprising a light source for providing light to an image source, which image source is arranged to project an image on a semi-transparent combiner mirror; the combiner mirror being arranged to superimpose the projected image onto a view of the environment in front of the vehicle by transmitting light rays from the environment and at the same time reflecting the projected image towards the eyes of an observer wherein the system comprises a first and a second light source for alternatively providing light to the image source; the first light source being arranged to emit light of a first colour to be used during daylight conditions, and the second light source being arranged to emit light of a second colour to be used during night vision conditions, wherein the first colour is in a first light emission spectrum and perceived as green and the second colour is in a second emission spectrum and perceived as yellow or orange.

Abstract translation: 一种用于车辆的平视显示系统，其有助于在夜视状态期间为车辆中的人使用夜视护目镜，该系统包括用于向图像源提供光的光源，该图像源被布置成投射图像 在半透明组合镜上; 组合器镜被布置成通过从环境透射光线并且同时将投影图像反射到观察者的眼睛，将投影图像叠加在车辆前方的环境视图上，其中系统包括第一和第二 用于替代地向所述图像源提供光的第二光源; 所述第一光源被布置成在日光条件期间发射要使用的第一颜色的光，并且所述第二光源被布置成发射将在夜间视觉条件期间使用的第二颜色的光，其中所述第一颜色处于第一 发光光谱并被感知为绿色，第二种颜色处于第二个发射光谱，并被认为是黄色或橙色。

公开(公告)号：WO2014171867A1

公开(公告)日：2014-10-23

申请号：PCT/SE2013/050425

申请日：2013-04-19

Applicant: SAAB AB

Inventor： BEJERYD, Johan ,  BORG, Johan ,  ISAKSSON, Folke ,  HAGLUND, Leif ,  CARLBOM, Per ,  NYGREN, Ola ,  ANDERSSON, Ingmar

IPC: G06T17/05 ,  G01C11/02 ,  G06K9/00 ,  G06T3/00 ,  G06T5/00

CPC classification number: G01C11/12 ,  G06T7/55 ,  G06T17/05 ,  G06T2207/10016 ,  G06T2207/10032

Abstract: The invention relates to a method for analysing images generated from at least one imaging system on at least one satellite. The method comprises providing at least three images of an area of interest from the at least one imaging system, where the at least three provided images are provided from at least three different angles,establishing point correspondence between the at least three provided images,generating at least two sets of three-dimensional information based on the at least three provided images, wherein the at least two sets of three-dimensional information are generated based on at least two different combinations of at least two of the at least three provided images of the area of interest,and comparing the at least two sets of three-dimensional information so as to determine discrepancies and providing information related to the imaging system and/or errors in the images based on the determined discrepancies. The invention also relates to a method for image correction, a system, a computer program and a computer program product.

Abstract translation: 本发明涉及一种用于分析由至少一个卫星上的至少一个成像系统产生的图像的方法。 该方法包括从至少一个成像系统提供感兴趣区域的至少三个图像，其中至少三个提供的图像从至少三个不同的角度提供，建立至少三个提供的图像之间的点对应， 基于至少三个提供的图像的至少两组三维信息，其中基于所述至少三个提供的图像中的至少两个的至少两个的至少两个不同的组合来生成所述至少两组三维信息 并且比较所述至少两组三维信息，以便基于所确定的差异来确定差异并提供与成像系统相关的信息和/或图像中的错误。 本发明还涉及一种用于图像校正的方法，系统，计算机程序和计算机程序产品。

公开(公告)号：WO2014081356A1

公开(公告)日：2014-05-30

申请号：PCT/SE2012/051280

申请日：2012-11-20

Applicant: SAAB AB

Inventor： NORDIN, Pontus ,  STRINDBERG, Göte

IPC: B64C3/28 ,  F01D5/28 ,  B64C27/473

CPC classification number: B64C1/062 ,  B64C1/12 ,  B64C3/28 ,  B64D2045/0095

Abstract: The invention regards an airframe leading edge part designed to be replaceable fixed to a structural portion (20, 21, 33) which during use moves through the air, the airframe leading edge part (19, 19') comprises a first (39) and a second (41) longitudinal joint edge adapted to fit the structural portion (20, 21,33). A joint (47)or a multitude of joints (45, 47, 47', 47'') is provided between the structural portion (20, 21, 33) and at least one of the longitudinal joint edges (39, 41). The joint(47) being adapted to break in the event of an eventual object (26, 26'), such as a bird, strikes and deforms the airframe leading edge part (19, 19') during said use. The joint(47) being designed to break at beforehand determined maximum joint strength (Pmax) of the joint (47). The invention also regards a repairing method for exchanging a damaged leading edge.

Abstract translation: 本发明涉及一种机身前缘部分，其被设计成可替换地固定到结构部分（20,21,33），在结构部分（20,21,33）期间，通过空气运动，机身前缘部分（19,19'）包括第一（39）和 适于装配结构部分（20,21,33）的第二（41）纵向接合边缘。 在所述结构部分（20,21,33）和所述纵向接合边缘（39,41）中的至少一个之间设置有接头（47）或多个接头（45,47,47'，47“）。 适于在诸如鸟的最终物体（26,26'）的情况下中断的接头（47）在所述使用期间撞击和变形机身前缘部分（19,19'）。 接头（47）被设计成以预先确定的接头（47）的最大接头强度（Pmax）断裂。 本发明还涉及用于更换损坏的前缘的修理方法。

公开(公告)号：WO2014074034A1

公开(公告)日：2014-05-15

申请号：PCT/SE2012/051211

申请日：2012-11-08

Applicant: SAAB AB

Inventor： HÅDÉN, Bertil ,  BÄCKSTRÖM, Mats

IPC: B64D15/00

CPC classification number: H01L41/042 ,  B64D15/163 ,  F03D80/40

Abstract: The present invention relates to a de-icing arrangement (400) and a method for de-icing a structural element (610). The de-icing arrangement comprises at least one electromagnetic actuator (404),a capacitive storage bank (403),a control unit (401) arranged to provide an excitation pulse to the at least one electromagnetic actuator,and a charging circuit (402) arranged to charge the capacitive storage bank (403). The at least one electromagnetic actuator (404) is arranged to expand in at least one direction when fed with the excitation pulse. The at least one electromagnetic actuator (404) is arranged in abutting relation to said structural element so as to apply a mechanical force caused by the expansion on the structural element. The control unit (401) is arranged to control current discharge of the capacitive storage bank into the at least one electromagnetic actuator so as to abort the excitation pulse at a predetermined timing after start of the pulse.

Abstract translation: 本发明涉及一种除冰装置（400）和一种用于除冰结构元件（610）的方法。 除冰装置包括至少一个电磁致动器（404），电容存储体（403），被布置成向至少一个电磁致动器提供激励脉冲的控制单元（401），以及充电电路（402） 布置成对电容性存储体（403）充电。 所述至少一个电磁致动器（404）布置成在馈送有激励脉冲时在至少一个方向上膨胀。 所述至少一个电磁致动器（404）以与所述结构元件邻接的方式设置，以便将由膨胀引起的机械力施加到所述结构元件上。 控制单元（401）被布置成控制电容性存储组的电流放电到至少一个电磁致动器中，以便在脉冲开始之后的预定定时中止激励脉冲。

公开(公告)号：WO2014070051A1

公开(公告)日：2014-05-08

申请号：PCT/SE2012/051183

申请日：2012-10-31

Applicant: SAAB AB

Inventor： NORDIN, Pontus ,  HALLANDER, Per ,  BOHLIN, Jonas ,  HELLSTRÖM, Thomas

IPC: B64C3/36 ,  C23C4/06 ,  C23C16/06 ,  F01D5/28 ,  B29C70/00

CPC classification number: C23C4/06 ,  B64C11/205 ,  B64C21/10 ,  B64C23/005 ,  B64C2230/12 ,  B64D15/12 ,  B64D45/00 ,  B64D45/02 ,  B64D2045/009 ,  C23C4/08 ,  C23C4/12 ,  C23C4/18 ,  C23C14/34 ,  C23C14/5886 ,  C23C24/04 ,  F01D5/288 ,  F05D2300/514 ,  F05D2300/6032 ,  Y02T50/166 ,  Y02T50/43 ,  Y02T50/672 ,  Y02T50/673

Abstract: The present invention regards an aerial article comprising a composite skin (5), a leading edge (1) facing the airflow (a) during the use of the aerial article (3), an erosion resistant coating (7) comprising a metallic material, and an aerodynamic surface (9). The coating (7) partly or entirely covers the composite skin (5) of the aerial article (3), wherein the coating (7) is of such high porosity that moisture transportation (MT) is permitted from the composite skin (5) to the aerodynamic surface (9) of the coating (7), and of such low porosity that erosion protection of the composite skin (5) still is achieved during said use. It also regards a method of applying an erosion resistant coating (7) comprising a metallic material to a composite skin (5) of an aerial article (3). It is made by providing an erosion resistant coating material (45) onto the composite skin (5) over a selected area of the article (3) wherein the coating is porous. Finally, polishing the outer surface (9) of the coating (7) is made so that a smooth aerodynamic surface is achieved.

Abstract translation: 本发明涉及一种包括复合蒙皮（5）的空中制品，在使用地空制品（3）期间面向气流（a）的前缘（1）），包括金属材料的抗侵蚀涂层（7） 和空气动力学表面（9）。 涂层（7）部分地或完全地覆盖空中物品（3）的复合皮肤（5），其中涂层（7）具有如此高的孔隙率，允许从复合皮肤（5）到 所述涂层（7）的空气动力学表面（9）以及在所述使用过程中实现复合表皮（5）的侵蚀保护的这种低孔隙率。 还涉及将包含金属材料的耐侵蚀涂层（7）施加到空中物品（3）的复合皮肤（5）的方法。 其通过在复合表皮（5）上在制品（3）的选定区域上提供防腐蚀涂层材料（45）制成，其中涂层是多孔的。 最后，抛光涂层（7）的外表面（9），使得获得平滑的空气动力学表面。

公开(公告)号：WO2014065718A1

公开(公告)日：2014-05-01

申请号：PCT/SE2012/051126

申请日：2012-10-22

Applicant: SAAB AB

Inventor： NORDIN, Pontus ,  RYDBOM, Anders ,  VÅNGELL, Tomas

IPC: B29C70/08 ,  B29C70/14 ,  B29C70/30 ,  B32B5/28 ,  B64C23/06

CPC classification number: B29C70/14 ,  B29C70/081 ,  B29C70/30 ,  B29L2031/3085 ,  B32B5/024 ,  B32B5/12 ,  B32B5/26 ,  B32B7/12 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/0269 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2307/558 ,  B32B2605/18 ,  B64C23/069 ,  Y02T50/164

Abstract: The present invention regards a structurally integrated curved structure (13, 13', 13'') comprising a curved transition region (15) being defined between a tip section (42) and a root section (11, 21), an upper and lower composite skin (27, 29) comprising an inner surface (45) fixed to a substructure (31) of said transition region (15), the substructure (31) and skins (27, 29) are, during use of the structure (13, 13', 13''), subjected to a bending moment (M), each skin (27, 29) of said transition region (15) comprises elongated reinforcement fiber-like elements. The lower composite skin (29) comprises reinforcing fibersand/or nano tubes(41, 43), which are oriented transverse to the inner surface (45). The invention also regard sa method for producing the structurally integrated curved structure (13, 13', 13'').

Abstract translation: 本发明涉及一种结构上整合的弯曲结构（13,13'，13“），其包括限定在尖端部分（42）和根部部分（11,21）之间的弯曲过渡区域（15），上部和下部 在所述结构（13）的使用期间，包括固定到所述过渡区域（15）的子结构（31）的内表面（45），所述子结构（31）和表面（27,29）的复合皮肤（27,29） ，13'，13“），经受弯矩（M），所述过渡区域（15）的每个皮肤（27,29）包括细长的加强纤维状元件。 下复合皮肤（29）包括横向于内表面（45）定向的增强纤维和/或纳米管（41,43）。 本发明还涉及用于制造结构一体化的弯曲结构（13,13'，13“）的方法。