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公开(公告)号：US10439274B2
公开(公告)日：2019-10-08
申请号：US15537300
申请日：2014-12-19
Applicant: SAAB AB
Inventor： Daniel Cedertorn , Johan Östberg
Abstract: The disclosure relates to a pivot axle arrangement for providing the two structural elements are pivotally movable in relation to each other. The pivot axle arrangement comprises a first and a second axle spindle for holding an outer axle, a first and a second bearing element and the outer axle. The outer axle is formed as a hollow cylinder. An inner axle is concentrically arranged in a longitudinal direction inside of the outer axle such that the inner axle extends between said first and second axle spindle. The ends of the inner axle are fastened to the first and second axle spindles by a first and second fastening means such that the first and second axle spindles are interconnected via said inner axle.
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312.发明申请公开(公告)号：US20190219076A1
公开(公告)日：2019-07-18
申请号：US16303012
申请日：2016-05-19
Applicant: SAAB AB
Inventor： Magnus LANDBERG , Thomas JERVALL
CPC classification number: F15B15/262 , B64C13/40 , F15B11/127 , F15B15/148
Abstract: An aircraft secondary control system comprises a rod arrangement of a driving actuator, configured for performing the motion. The rod arrangement is coupled to the aircraft secondary control member via a linkage arrangement. The driving actuator comprises a first engagement and disengagement device of a piston body and comprises a second engagement and disengagement device, each of which being configured for alternately and/or simultaneously engaging said rod arrangement. The piston body is arranged in a cylinder body and is configured to make a working stroke from a first position to a second position.
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313.发明申请公开(公告)号：US20190203741A1
公开(公告)日：2019-07-04
申请号：US16302901
申请日：2016-05-19
Applicant: SAAB AB
Inventor： Magnus LANDBERG , Martin HOCHWALLNER
CPC classification number: F15B15/148 , F15B11/183 , F15B15/262 , F15B2015/268
Abstract: A fluid actuator arrangement comprises a piston rod member, at least two cylinders each said cylinder having a piston body, and a clamping mechanism associated to each cylinder. Each clamping mechanism is arranged to engage and disengage the piston body of the cylinder to the piston rod member. The fluid actuator arrangement comprises further a control element arranged to control a back and forward movement of the respective piston body so that forward movement is slower than the backward movement and to control the movement of the respective piston bodies in relation to each other such that at least one piston body is always moving forward and such that an overlap exists wherein at least two of the piston bodies are moving forward simultaneously during a cycle.
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314.发明申请公开(公告)号：US20190178613A1
公开(公告)日：2019-06-13
申请号：US16301170
申请日：2017-05-05
Applicant: SAAB AB
Inventor： Christer ZAETTERQVIST
Abstract: A magazine for storing and launching countermeasures arranged in cartridges, comprising a plurality of longitudinal cartridge cases forming the magazine, where the magazine comprises a tilting means adapted to tilt the cartridge cases, such that the openings of the cartridge cases can be directed in a selected direction, and where a countermeasure comprises multiple projectiles, and where the magazine is adapted to launch a first countermeasure and a second countermeasure, where the projectile cluster density of the first countermeasure is lower than the projectile cluster density of the second countermeasure. The advantage of the invention is that a countermeasure can be directed towards an incoming object and can be adapted for the distance to the object before it is launched.
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315.发明申请公开(公告)号：US20190162840A1
公开(公告)日：2019-05-30
申请号：US16092382
申请日：2016-04-20
Applicant: SAAB AB
Inventor： Lars Sundell
Abstract: The present invention refers to a method for controlling transmission of an electronically steerable antenna system, wherein the electronically steerable antenna system comprises a signal generator configured to generate electromagnetic waveforms, and an antenna. The antenna comprises an even number of antenna columns symmetrically arranged about a centerline of the antenna and thereby forming two symmetrical antenna halves. Respective antenna column comprises at least one antenna element configured at least for transmitting electromagnetic waves. The electronically steerable antenna system is configured for transmitting at least interrogation signals and ISLS control signals, and the method comprises the method steps of, when transmitting the ISLS control signals: generating an electromagnetic waveform; applying a first transmission phase offset to the electromagnetic waveform, wherein the first transmission phase offset determines the phase offset between each antenna column pair; applying a second transmission phase offset to each antenna column of the second antenna half, wherein the second transmission phase offset of the second antenna half offset is 180 degrees in relation to the first antenna half; and transmitting the generated electromagnetic waveform whereto the first and the second phase offsets have been applied. The present invention also relates to an electronically steerable antenna system configured to execute the method.
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Patent Agency Ranking
公开(公告)号：US10302742B2
公开(公告)日：2019-05-28
申请号：US15760760
申请日：2015-09-21
Applicant: SAAB AB
Inventor： Max Wallen , Bruno Lumetzberger
Abstract: The present disclosure relates to exemplary embodiments of radar systems for providing increased robustness against radar interference transmissions and methods for controlling such radar systems. The radar system comprises at least one radar antenna configured at least for receiving a radar signal, a radar signal dividing means, a first receiver device and a second receiver device. The first receiver device is configured for monitoring a first frequency range and the second receiver device is configured for monitoring a second frequency range, wherein the second frequency range is wider than the first frequency range and the first frequency range is a subset of the second frequency range. The second receiver device is configured for measuring interference levels within the second frequency range. The present disclosure further relates to exemplary embodiments of methods for controlling the radar system, wherein the methods refer to measuring interference levels within the second frequency range, analysing measured interference levels, determining favorable frequency channels within the second frequency range in respect to interference level and possibly changing operating frequency channel in respect to measured interference levels.
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公开(公告)号：US20190131760A1
公开(公告)日：2019-05-02
申请号：US16083685
申请日：2016-03-30
Applicant: SAAB AB
Inventor： Peter BANE , Marcus GUSTAFSSON
Abstract: The present disclosure relates a laser arrangement (1) and a method of the laser arrangement, arranged to output energy in the form of laser emission, for emitting controlled Q-switched laser emission. The laser arrangement comprises a gain medium (2) arranged to be excited when pumped, an optical resonator (3), an active Q-switch (4) arranged in the optical resonator, said active Q-switch (4) being controllable between at least a high loss state and a low loss state, and being arranged to introduce loss in the optical resonator to prevent lasing in the high loss state and to affect lasing minimally in the low loss state, a photo detector (5) arranged to detect the presence of a free running pulse (1′) generated by the optical resonator and which occurs when a lasing threshold is reached and a processing circuitry (6) arranged to control (S4) of the state of the active Q-switch based on the detection of the free running pulse.
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公开(公告)号：US20180370602A1
公开(公告)日：2018-12-27
申请号：US16062294
申请日：2015-12-16
Applicant: SAAB AB
Inventor： Bernt Norrman
CPC classification number: B63B17/0081 , B63B3/10 , B63B49/00 , B63G9/00 , F16F3/02 , F16F3/04 , F16F15/04 , F16F15/067 , F16F2230/0041 , G01S7/03 , H01Q1/002 , H01Q1/18 , H01Q1/34 , H01Q3/04
Abstract: The present disclosure relates to a shock absorbing arrangement suitable e.g. for ship installed structures comprising a rod, a resilient member arranged in connection to the rod, a structure element and a locking member arranged in connection to the structure element. The locking member is arranged to detachably lock the structure element at a resting position at the rod and the locking member, or the structure element, is supported by the resilient member. The resilient member is configured such that a spring force of the resilient member acts to maintain the structure element essentially at the resting position at the rod. The locking member is further configured to release the structure element from the resting position when being exposed to a force exceeding a predetermined holding force, whereupon the resilient member acts to reinstate the locking of the structure element at the resting position at the rod. The present disclosure further relates to a shock absorbing structure comprising such shock absorbing arrangements.
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公开(公告)号：US20180365407A1
公开(公告)日：2018-12-20
申请号：US16063054
申请日：2016-12-15
Applicant: SAAB AB
Inventor： Mats JONSSON
Abstract: The present invention relates to a method for authenticating software. The method comprises defining a set of parameters to use for trace mapping the software, wherein the set of parameters represents the software functionality when executed. The method further comprises: a) creating a trusted fingerprint that is created by trace mapping the software using the set of parameters when executed in a trusted environment; b) creating an operating fingerprint that is created by trace mapping the software using the set of parameters when executed in an operating environment; c) comparing the operating fingerprint with the trusted fingerprint, and identifying any difference between the trusted fingerprint and the operating fingerprint; and d) when said operating fingerprint is non-identical with the trusted fingerprint, initiating predefined action(s) in response to the identified differences between the trusted fingerprint and the operating fingerprint.
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公开(公告)号：US20180267163A1
公开(公告)日：2018-09-20
申请号：US15761955
申请日：2015-09-21
Applicant: SAAB AB
Inventor： Hans HELLSTEN
CPC classification number: G01S13/90 , G01S7/414 , G06K9/0063 , G06K9/6278 , G06K2209/21
Abstract: A method and a device for detecting at least one target in an image, wherein the image comprises a set of pixels with a magnitude assigned to each pixel is provided. The method comprises an iterative process until the K+1th target does not show a probability increase above a predetermined threshold value. The method is performed by creating a candidate free image, calculating, for the candidate free image, the probability of there being a target at each pixel, by using Bayes theorem, determining a location of the candidate target K+1 in the image, determining the probability that there is a target at the determined location, by determining the calculated probability of there being a target at the determined location. By performing the above, the most probable locations for targets in the image are located together with the probability that the location holds a true target.
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