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1. 发明申请

WO2023018008A1 전자 장치 및 그 제어 방법 审中-公开
公开(公告)号：WO2023018008A1
公开(公告)日：2023-02-16
申请号：PCT/KR2022/009346
申请日：2022-06-29
申请人： 삼성전자주식회사
发明人： 김형철 , 김학재 , 문승현 , 박기홍 , 백원준
IPC分类号： G03B21/14 , G09B9/10 , H04N9/31
摘要： 본 전자 장치는 메모리, 셔터부, 투사면에 이미지를 출력하는 프로젝션부 및 컨텐츠에 대응되는 제1 이미지를 메모리로부터 획득하고, 제1 이미지를 키스톤 보정하여 제2 이미지를 획득하고, 제2 이미지에서 컨텐츠에 대응되는 이미지 부분과 컨텐츠에 대응되지 않는 잔여 부분을 식별하고, 잔여 부분이 투사면에 투사되지 않도록 셔터부를 제어하는 프로세서를 포함한다.

2. 发明申请

WO2017153333A1 VORRICHTUNG UND VERFAHREN ZUR SIMULATION VON BESCHLEUNIGUNGSKRÄFTEN 审中-公开
标题翻译：用于模拟加速功率的装置和方法
公开(公告)号：WO2017153333A1
公开(公告)日：2017-09-14
申请号：PCT/EP2017/055184
申请日：2017-03-06
申请人： KEUL, Christian K.
发明人： KEUL, Christian K. , BERTZ, Alexander
IPC分类号： A63F13/28 , G06F3/01 , A61H1/02 , A63B21/06 , A63B21/00 , G09B9/10 , G06F1/16 , G09B9/04
CPC分类号： A63F13/28 , A61H2003/063 , A61H2201/1207 , A61H2201/1604 , A61H2201/165 , A63B21/0058 , A63B21/0608 , A63B21/065 , A63B21/222 , A63B21/4003 , A63B23/025 , A63B24/0087 , A63B2225/50 , G06F3/011 , G06F3/012 , G06F3/016 , G09B9/04 , G09B9/10
摘要： Bereit gestellt wird eine Vorrichtung(1)zur Simulation von am menschlichen Kopf (K) wirkenden Beschleunigungskräften (g), wobei die Vorrichtung (1) aufweist -eine Basiseinheit (10), die am Kopf (K) anordenbar ist, und -ein Gewichtssystem (20), das an der Basiseinheit (10) angeordnet ist, wobei das Gewichtssystem (20) einen Körper (21) aufweist, derrelativ zur Basiseinheit (10) verlagerbar ist. Der Körper kann hierbei in Abhängigkeit eines Drehwinkels(α) des Kopfes oder der Basiseinheit verlagerbar sein. Bereit gestellt wird ferner ein entsprechend ausgestaltetes Verfahren, um von am menschlichen Kopf(K) wirkenden Beschleunigungskräften (g) zu simulieren, insbesondere unter Verwendung einer erfindungsgemäßen Vorrichtung (1).
摘要翻译：提供一种用于模拟作用在人体头部（K）上的加速力（g）的装置（1），所述装置（1）包括附接到所述头部（K）以及设置在所述基座单元（10）上的配重系统（20），所述配重系统（20）包括相对于所述基座单元（10）可移位的主体（21）。在此，主体可以根据头部或基部单元的旋转角度（α）而移位。还提供了用于模拟作用在人体头部（K）上的加速力（g）的合适设计方法，特别是使用根据本发明的装置（1）

3. 发明申请

WO00028505A1 IMPROVEMENTS IN SIMULATORS 审中-公开
标题翻译：模拟器的改进
公开(公告)号：WO00028505A1
公开(公告)日：2000-05-18
申请号：PCT/GB1999/003745
申请日：1999-11-10
IPC分类号： G09B9/12 , A63G31/16 , G09B9/14 , G09B9/10 , G09B9/02
CPC分类号： G09B9/14 , A63G31/16
摘要： Apparatus for simulating motion in the form primarily of a seat having arrangements for providing the user with cues which influence the users perception of apparent motion, particularly sustained movements. A fixed seat frame has a moveable seat from which can tilt about orthogonal roll and pitch axes and be displaced linearly in the heave, surge and sway directions: all movements are small and are accompanied preferably by synchronised variations in the apparent hardness of regions of the contact surface so that a user experiences the small relative displacements and apparent tendency to slip in relation to the seat in synchronisation with other cues which result in an interpretation of the experience to simulate the effects of real motions without actually involving movement. This may reinforce the effects of a convention motion simulator, for example for flight training.
摘要翻译：用于以主要由座椅形式模拟运动的装置，其具有用于向使用者提供影响用户对视在运动，特别是持续运动的感知的线索的布置。固定的座椅框架具有可移动的座椅，从该座椅可以围绕正交的卷轴和俯仰轴线倾斜，并且在起伏，浪涌和摆动方向上线性地移位：所有的移动都很小，并且优选地伴随着接触表面，使得用户体验相对于座椅相对于座椅的小的相对位移和明显的滑动趋势，与其他线索同步，其导致经验的解释以模拟实际运动的效果而不实际涉及运动。这可能会加强惯例运动模拟器的效果，例如飞行训练。

4. 发明申请

WO2021081471A2 AERODYNAMIC INTERACTIONS IN COMPLEX EVTOL FOR FLIGHT SIMULATION 审中-公开
公开(公告)号：WO2021081471A2
公开(公告)日：2021-04-29
申请号：PCT/US2020/057260
申请日：2020-10-25
申请人： JOBY AERO, INC.
发明人： BEVIRT, JoeBen , STOLL, Alex , MIKIC, Gregor, Veble , BAIN, Jeremy
IPC分类号： G09B9/10 , G09B9/12 , G09B9/14 , G09B9/18 , G09B9/206 , G09B9/24
摘要： A method and system for modeling aerodynamic interactions in complex eVTOL configurations for realtime flight simulations and hardware testing which includes decomposing the aircraft into aerodynamic subcomponents, wherein the interactions between these components are handled by flow simulations of the surrounding fluid, which may be Euler flow CFD simulations. A computer generated simulation can be used to analyze the fluid flow and pressures, the forces delivered by an aircraft into the fluid and the forces onto the aircraft from the fluid, to determine the position and attitude of the aircraft, and other aspects. The system may be used as a flight simulator for pilot training in a realtime environment. The system may be used to support component testing using an interface to those components, such as flight electronics and actuators, to test the components in high fidelity simulations of actual flight demands on those components. The system may also be used to support design analysis in non-realtime to run numerous simulations on different designs and to provide comparative output.

5. 发明申请

WO2013109266A1 CENTRIFUGE-BASED-FLIGHT SIMULATOR 审中-公开
标题翻译：基于离散的飞行模拟器
公开(公告)号：WO2013109266A1
公开(公告)日：2013-07-25
申请号：PCT/US2012/021728
申请日：2012-01-18
申请人： ENVIRONMENTAL TECTONICS CORPORATION , COMTOIS, Paul
发明人： COMTOIS, Paul
IPC分类号： G09B9/10 , G09B19/00 , A63G31/16
CPC分类号： G09B9/28
摘要： Some implementations include a method for operating a centrifuge-based-flight simulator in at least one of several different modes: a heightened G-force mode, a normal G-force mode; and transition modes (i.e., ramp-up or ramp-down modes) between the heightened G-force and normal G-force modes. During the normal-G-force mode the simulator ceases planetary motion altogether or substantially decreases rotations to replicate a plurality of flight conditions that physically imparts, on the trainee during operation of the simulator, a G-force that is not greater than approximately one (1) G. The reduction of planetary motion while maintaining realistic motion and force sensations that are appropriate for the virtual-flight conditions being experienced allows realistic flight simulation experience for the trainee and reduces the negative effects of constant planetary motion
摘要翻译：一些实施方案包括用于以几种不同模式中的至少一种操作基于离心机的飞行模拟器的方法：增强的G力模式，正常的G力模式; 以及在增强的G力和正常G力模式之间的过渡模式（即，上升或下降模式）。在正常G力模式期间，模拟器完全停止行星运动或基本上减小旋转以复制多个飞行条件，其在模拟器操作期间在实习者身上施加不大于大约1的G力（ 1）G.行星运动的减少同时保持适合于虚拟飞行条件的现实运动和力感觉，为实习者提供了实际的飞行模拟体验，并减少了恒星行星运动的负面影响

6. 发明申请

WO02003352A2 APPARATUS FOR PRODUCING OR ENHANCING A PERCEIVED SENSATION OF MOTION 审中-公开
标题翻译：用于生产或增强运动感觉的装置
公开(公告)号：WO02003352A2
公开(公告)日：2002-01-10
申请号：PCT/GB2001/002868
申请日：2001-06-29
IPC分类号： A63F13/08 , G09B9/10 , G09B9/16 , G09B
CPC分类号： G09B9/10 , A63F13/08 , A63F13/245 , A63F13/28 , A63F2300/302 , A63F2300/8017 , G09B9/165
摘要： A motion simulator in the form of a seat (11) comprising a seat support frame (12) including a seat back (13), in which a seat pan (19) is movably mounted with respect to the seat support frame (12) via motion actuators (20, 21, 22) which impart to the seat pan (19) motion with respect to the seat support frame (12) with at least three degrees of freedom including sway, and control means (34) for determining the motion of the actuators (20, 21, 22) to move the seat pan (19). Many cues involve moving the seat pan in the opposite sense from the simulated direction of movement.
摘要翻译：一种座椅（11）形式的运动模拟器，包括座椅支撑框架（12），座椅支撑框架（12）包括座椅靠背（13），座椅托盘（19）相对于座椅支撑框架（12）可移动地安装在座椅靠背中，运动致动器（20,21,22），其以至少三个自由度（包括摆动）使座盘（19）相对于座椅支撑框架（12）运动;以及控制装置（34），用于确定致动器（20,21,22）以移动座盘（19）。许多线索涉及将座椅底盘从模拟的运动方向相反的方向移动。

7. 发明申请

WO2022047599A1 一种双人运动转轮机构审中-公开
公开(公告)号：WO2022047599A1
公开(公告)日：2022-03-10
申请号：PCT/CN2020/000297
申请日：2020-12-14
申请人：舒江
发明人：舒江 SHU, Jiang
IPC分类号： G09B9/10
摘要：一种双人运动转轮，包括运动圆环（1）、非等边平行四边连杆机构（3）、拉伸弹簧（4）和悬挂座椅。圆环（1）在转动时，通过摇臂杆（2）带动非等边平行四边连杆机构（3）旋转，两个座椅上人的重力和连接两个座椅之间的拉伸弹簧（4），通过非等边平行四边连杆机构（3）和摇臂杆（2）作用于圆环（1），圆环（1）支撑力来自于地面，通过圆心而作用于非等边平行四边连杆机构（3）上的力，可以阶段错开圆环（1）中心产生前置力矩使圆环（1）转动，座椅上的人借助自身重力和适当使用人力，使圆环（1）不断获得向前转动的动力。拉伸弹簧（4）的作用，就是在转动过程中，在两个座椅处于不同位置关系下，调节它们和圆心之间的力矩关系，有利于克服转动阻力，以达到运动健身游戏娱乐的目的。

8. 发明申请

WO2021224490A1 DISTRIBUTED ELECTRIC PROPULSION AIRCRAFT SIMULATING A SINGLE PROPELLER AIRCRAFT 审中-公开
公开(公告)号：WO2021224490A1
公开(公告)日：2021-11-11
申请号：PCT/EP2021/062217
申请日：2021-05-07
申请人： POLITECNICO DI MILANO
发明人： PASQUALI, Davide , SANTERAMO, Andrea , ALBERTI, Lorenzo , TOMBOLINI, Matteo , TRAINELLI, Lorenzo , RIBOLDI, Carlo Emanuele Dionigi
IPC分类号： B64D27/24 , B64D31/06 , B64D35/08 , G09B9/10 , G09B9/44 , B64D27/02
摘要： It is disclosed a distributed electric propulsion fixed-wing aircraft comprising a plurality of propulsive units, wherein propulsive units are arranged symmetrically with respect to the longitudinal plane, wherein of propulsive units comprises first propulsive units at a first side of the longitudinal plane and second propulsive units at a second side of the longitudinal plane, wherein the distributed propulsion aircraft further comprises a control unit configured to provide a yawing moment so that a sideslip angle is generated, so that the distributed electric propulsion aircraft flies as a fixed-wing aircraft equipped with a single propeller.

9. 发明申请

WO01003583A1 METHOD FOR MONITORING THE FUNCTIONAL STATUS OF A PILOT DURING FLIGHT AND DEVICE THEREFOR 审中-公开
标题翻译：用于监视飞行期间飞行员的功能状态的方法及其装置
公开(公告)号：WO01003583A1
公开(公告)日：2001-01-18
申请号：PCT/RU2000/000051
申请日：2000-02-15
IPC分类号： A61B5/16 , A61B5/18 , G09B9/08 , G09B9/10 , G09B9/28
CPC分类号： G09B9/08 , A61B5/18 , G09B9/28
摘要： The invention relates to medical engineering and more particularly to a method for monitoring the functional status of a pilot in flight conditions. According to this method, the pressure of the pilot's hand on the joystick and the intensity thereof, the changes in joystick trajectory, the pressure of pilot's feet on the directional pedals, the position of the pilot's head, the respiratory process, oxygen pressure and the quality of the mixture in the pipe of the oxygen system, the pressure in the anti-g suit, critical and current altitudes as well as the value of the g are recorded. If the recorded parameters deviate from the reference values, an analysis and control unit generates data on the occurrence of a contingency and transmits such data to the pilot. If the pilot eliminates such a contingency, the analysis unit cancels the command output to the voice synthesizer; if the pilot does not react to said data, a signal is generated in order to activate stimulation systems, to put the plane on a level flight and to activate automatic piloting and landing systems. The inventive device contains a sensor unit, an analysis and control unit and an output unit.
摘要翻译：本发明涉及医疗工程，更具体地说，涉及一种在飞行条件下监视飞行员的功能状态的方法。根据这种方法，驾驶员的手在操纵杆上的压力及其强度，操纵杆轨迹的变化，飞行员的脚在方向踏板上的压力，驾驶员头部的位置，呼吸过程，氧气压力和记录氧气系统管道中混合物的质量，抗反射罩的压力，临界和当前的高度以及g的值。如果所记录的参数偏离参考值，则分析和控制单元产生关于偶发事件的数据，并将该数据发送给飞行员。如果飞行员消除了这种意外事件，则分析单元取消向语音合成器输出的命令; 如果飞行员对所述数据没有反应，则产生信号以激活刺激系统，将飞机置于水平飞行并激活自动驾驶和着陆系统。本发明的装置包含传感器单元，分析和控制单元以及输出单元。

10. 发明申请

WO00077762A1 MOTION SIMULATOR 审中-公开
标题翻译：运动模拟器
公开(公告)号：WO00077762A1
公开(公告)日：2000-12-21
申请号：PCT/KR2000/000600
申请日：2000-06-09
IPC分类号： G09B9/10 , B23Q1/54 , B25J17/02 , G09B9/02 , G09B9/04 , G09B9/12 , G09B9/14 , G09B23/08
CPC分类号： G09B9/04 , G09B9/14
摘要： An improved motion simulator that allows creation of moving sensations closer to the actual situations through the elimination of occurence of undesired moving sensations during creation of moving sensations using the force of gravity is disclosed. The disclosed motion simulator is characterized in that it comprises a stationary frame; a movable frame which is disposed beneath said stationary frame in the direction of gravity, and which has a passenger compartment attached on the bottom surface thereof; and a driving device disposed between said stationary frame and said movable frame, which rotationally or linearly moves the movable frame.
摘要翻译：公开了一种改进的运动模拟器，其允许通过使用重力在创建移动感觉的过程中消除不期望的运动感觉而产生更接近实际情况的运动感觉。所公开的运动模拟器的特征在于它包括一个固定框架; 可动框架，其在重力方向设置在所述固定框架的下方，并且在其底面上具有乘客舱; 以及设置在所述固定框架和所述可移动框架之间的驱动装置，其可旋转或线性地移动所述可移动框架。

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