公开(公告)号：US20170025032A1

公开(公告)日：2017-01-26

申请号：US15290441

申请日：2016-10-11

Applicant: AIRBUS HELICOPTERS

Inventor： Guillaume DUMAR ,  Regis ROSSOTTO ,  Hilario VIEIRA

IPC: G09B9/46 ,  G09B9/08 ,  G09B9/44

CPC classification number: G09B9/46 ,  G09B9/085 ,  G09B9/44

Abstract: A method of driving a main rotor of a rotorcraft in rotation while implementing an in-flight simulation mode that simulates failure of one of the engines of the rotorcraft. In simulation mode, and when a current speed of rotation (NR) of the main rotor is detected as being lower than a predetermined threshold speed of rotation (S), the simulation mode is kept active and a regulation command is generated in order to perform a controlled operation (A) of gradually increasing the power delivered by the engines by authorizing the limit imposed by a setpoint (OEI/2) for regulating operation of the engine in simulation mode to be exceeded. Said gradually increasing power is interrupted by the pilot staying under training and operating a collective pitch manoeuver of the blade of the main rotor providing a rotation of main rotor at the predetermined threshold speed in rotation.

Abstract translation: 一种在实现模拟旋翼航空器中的一个发动机的故障的飞行中模拟模式的同时驱动旋翼航空器的主转子旋转的方法。 在模拟模式中，当主转子的当前旋转速度（NR）被检测为低于预定的阈值旋转速度（S）时，模拟模式保持活动，并且产生调节命令以执行 控制操作（A）通过授权超过在模拟模式下调节发动机运转的设定值（OEI / 2）施加的限制来逐渐增加发动机所输送的功率。 所述逐渐增加的动力被飞行员停留在训练中，并且操作主转子叶片的集体桨距操纵器，以主旋转的旋转方式以预定的阈值速度旋转。

公开(公告)号：US20140322675A1

公开(公告)日：2014-10-30

申请号：US14359270

申请日：2012-11-11

Applicant: BIOMEDTECH AUSTRALIA PTY LTD

Inventor： Oleg Bassovitch

IPC: G09B9/10

CPC classification number: G09B9/10 ,  G09B9/085

Abstract: The present invention provides a system for training a subject to recognise the onset of hypoxia, the system including (i) a flight simulation system, and (ii) a hypoxia induction system, wherein the flight simulation system is operably linked to the hypoxia induction system. The system provides a tool for pilot training to a pilot, allowing for the delivery of standardised training programs where the tasks required for the operation of an aircraft are able to be coordinated with an induction of hypoxia in the subject. Such a system is also able to provide an assessment tool to demonstrate when a pilot has had sufficient training in recognising the effects of hypoxia.

Abstract translation: 本发明提供了一种用于训练受试者以识别缺氧发作的系统，该系统包括（i）飞行模拟系统和（ii）缺氧诱导系统，其中飞行模拟系统可操作地连接到缺氧诱导系统 。 该系统为飞行员提供了飞行员培训的工具，允许提供标准化的培训计划，其中飞机运行所需的任务能够与受试者的缺氧诱导相协调。 这样一个系统也能够提供一个评估工具来证明飞行员何时有足够的训练来认识缺氧的影响。

公开(公告)号：US20140255879A1

公开(公告)日：2014-09-11

申请号：US13885198

申请日：2012-05-07

Applicant: Ming Lu

Inventor： Ming Lu

IPC: G09B9/08

CPC classification number: G09B9/085

Abstract: This invention supplies a flight-icing simulator to train the pilots with skills under flight-icing conditions. This simulator is composed of several modules to provide pilots the information of ice distribution and strength on aircrafts, the distance of the aircraft to the icing dangerous zone, the perturbation of the points with feedback function, etc.

Abstract translation: 本发明提供飞行测试模拟器，以在飞行情况下训练飞行员的技能。 该模拟器由几个模块组成，为飞行员提供飞机上的冰分布和强度信息，飞机到结冰危险区域的距离，反馈功能点的扰动等。

公开(公告)号：US20120315602A1

公开(公告)日：2012-12-13

申请号：US13223181

申请日：2011-08-31

Applicant: Philip M. Tenning ,  Greg Cass

Inventor： Philip M. Tenning ,  Greg Cass

IPC: G09B9/08

CPC classification number: G09B9/085 ,  G09B25/02

Abstract: A vehicle pneumatic system training aid comprises simulated controls and indicators and a pneumatic circuit. The simulated controls and indicators correspond to at least a portion of controls and indicators on an actual vehicle. The pneumatic circuit comprises a connection to a source of pressurized fluid, and at least one fluid flow control device. The fluid flow control device is positionable in at least two different positions corresponding to different actual vehicle conditions that are simulatable. The simulated controls are actuatable to change a condition of the pneumatic circuit and the simulated indicators are operable to display an indication of the condition of the pneumatic circuit.

Abstract translation: 车辆气动系统训练辅助装置包括模拟控制和指示器以及气动回路。 模拟控制和指示符对应于实际车辆上的控制和指示器的至少一部分。 气动回路包括与加压流体源的连接以及至少一个流体流动控制装置。 流体流量控制装置可位于对应于可模拟的不同实际车辆状况的至少两个不同位置。 模拟控制器可致动以改变气动回路的状态，并且模拟指示器可操作以显示气动回路状况的指示。

公开(公告)号：US20060177798A1

公开(公告)日：2006-08-10

申请号：US11226146

申请日：2005-09-14

Applicant: Carl Dworman

Inventor： Carl Dworman

IPC: G09B9/02

CPC classification number: G09B9/08 ,  G09B9/085 ,  G09B19/165

Abstract: A pilot aid that includes a sheet material having indicia thereon indicative of a plurality of predetermined flying parameters including at least wind velocity and direction. A plurality of indicia wheels are each separately mounted from the sheet material and each are associated with a different flying parameter. A plurality of windows are disposed on the sheet material, each positioned to overly a corresponding indicia wheel and each for observing one of a plurality of predetermined characteristics that define the flying parameter.

Abstract translation: 一种辅助助剂，其包括其上具有标记的片材材料，其指示包括至少风速和方向的多个预定飞行参数。 多个标记轮分别从片材安装，并且每个标记轮与不同的飞行参数相关联。 多个窗口设置在片材上，每个窗口定位成过度对应的标记轮，并且每个窗口用于观察限定飞行参数的多个预定特征中的一个。

公开(公告)号：US20030190588A1

公开(公告)日：2003-10-09

申请号：US10408430

申请日：2003-04-07

Applicant: The Boeing Company

Inventor： Robert J. Lechner

IPC: G09B009/08 ,  G09B019/16

CPC classification number: G09B9/085

Abstract: A method and apparatus are provided for automatically generating a terrain model for display during a simulated flight along a predefined mission route. The apparatus includes a mission profiler that automatically determines the area containing the mission route for which the terrain source data is required and the respective resolution of different regions within the area. The apparatus also includes an apparatus for automatically collecting the terrain source data including a search engine for automatically searching electronic collections of terrain source data to identify terrain source data covering the area containing the mission route. The apparatus also includes an image engine for processing the terrain source data into one or more predefined formats and a terrain engine for automatically compiling the processed data to create a terrain model for display during flight simulation.

Abstract translation: 提供了一种方法和装置，用于在沿着预定义的任务路线的模拟飞行期间自动生成用于显示的地形模型。 该装置包括任务分析器，其自动确定包含需要地形源数据的任务路线的区域以及区域内不同区域的相应分辨率。 该装置还包括用于自动收集地形源数据的装置，包括用于自动搜索地形源数据的电子集合的搜索引擎，以识别覆盖包含任务路线的区域的地形源数据。 该装置还包括用于将地形源数据处理成一个或多个预定义格式的图像引擎和用于自动编译处理数据的地形引擎，以在飞行模拟期间创建用于显示的地形模型。

公开(公告)号：US20030059743A1

公开(公告)日：2003-03-27

申请号：US09942179

申请日：2001-08-29

Applicant: The Boeing Company

Inventor： Robert J. Lechner

IPC: G09B009/08 ,  G09B019/16

CPC classification number: G09B9/085

Abstract: A method and apparatus are provided for automatically generating a terrain model for display during a simulated flight along a predefined mission route. The apparatus includes a mission profiler that automatically determines the area containing the mission route for which the terrain source data is required and the respective resolution of different regions within the area. The apparatus also includes an apparatus for automatically collecting the terrain source data including a search engine for automatically searching electronic collections of terrain source data to identify terrain source data covering the area containing the mission route. The apparatus also includes an image engine for processing the terrain source data into one or more predefined formats and a terrain engine for automatically compiling the processed data to create a terrain model for display during flight simulation.

Abstract translation: 提供了一种方法和装置，用于在沿着预定义的任务路线的模拟飞行期间自动生成用于显示的地形模型。 该装置包括任务分析器，其自动确定包含需要地形源数据的任务路线的区域以及区域内不同区域的相应分辨率。 该装置还包括用于自动收集地形源数据的装置，包括用于自动搜索地形源数据的电子集合的搜索引擎，以识别覆盖包含任务路线的区域的地形源数据。 该装置还包括用于将地形源数据处理成一个或多个预定义格式的图像引擎和用于自动编译处理数据的地形引擎，以在飞行模拟期间创建用于显示的地形模型。

公开(公告)号：US06195626B1

公开(公告)日：2001-02-27

申请号：US09099923

申请日：1998-06-19

Applicant: Jeremy D. Stone

Inventor： Jeremy D. Stone

IPC: G06G748

CPC classification number: A63F13/56 ,  A63F13/10 ,  A63F13/67 ,  A63F13/803 ,  A63F2300/6027 ,  A63F2300/64 ,  A63F2300/8017 ,  G09B9/085

Abstract: Enhanced realism of a real-time simulator having multiple computer-controlled units results from making the units capable of reacting to only those other units that each of them can be aware of because of their spatial relationships to the unit. Awareness is based upon probabilities; it can persist after a relationship changes; and it can be influenced by a units designation of a target. Each unit selects a target based upon a score incorporating multiple aspects of its tactical situation, and can change targets when the situation changes. A unit selects a strategy in response to which of a set of tactical configurations exist between the unit and its target; the strategy can change short of completion when the configuration changes. A plan produces guidance commands from the high-level strategy. The guidance commands are converted into control settings for guiding the subject unit using a physics engine for simulating the physical dynamics of the unit. The control settings can interact with each other under certain conditions. The time rate at which each computer-controlled unit performs the above operations varies with the tactical situation, and can be different for different units. The operator for each unit precomputes some data required for multiple calculations in performing the operations.

Abstract translation: 具有多个计算机控制单元的实时模拟器的增强的现实性是由于使得单元能够仅响应于它们中的每个单元，因为它们与该单元的空间关系可以察觉。 意识是基于概率; 关系变化后可以持续; 并且它可能受到目标的单位指定的影响。 每个单位根据包含其战术情况的多个方面的分数来选择目标，并且可以在情况改变时改变目标。 单位选择一种战略，以响应单位和目标之间存在一组战术配置的策略; 当配置发生变化时，该策略可能会改变不完整。 计划从高层次战略中制定指导指令。 引导命令被转换成用于引导主体单元的控制设置，使用物理引擎来模拟单元的物理动力学。 控制设置可以在某些条件下相互交互。 每个计算机控制单元执行上述操作的时间速率随战术情况而变化，并且对于不同的单元可以是不同的。 每个单元的操作员预先计算执行操作时进行多次计算所需的一些数据。

公开(公告)号：US06179618B2

公开(公告)日：2001-01-30

申请号：US09100502

申请日：1998-06-19

Applicant: Jeremy D. Stone

Inventor： Jeremy D. Stone

IPC: G09B908

CPC classification number: G09B9/085 ,  G09B9/003

Abstract: Enhanced realism of a real-time simulator having multiple computer-controlled units results from making the units capable of reacting to only those other units that each of them can be aware of because of their spatial relationships to the unit. Awareness is based upon probabilities; it can persist after a relationship changes; and it can be influenced by a unit's designation of a target. Each unit selects a target based upon a score incorporating multiple aspects of its tactical situation, and can change targets when the situation changes. A unit selects a strategy in response to which of a set of tactical configurations exist between the unit and its target; the strategy can change short of completion when the configuration changes. A plan produces guidance commands from the high-level strategy. The guidance commands are converted into control settings for guiding the subject unit using a physics engine for simulating the physical dynamics of the unit. The control settings can interact with each other under certain conditions. The time rate at which each computer-controlled unit performs the above operations varies with the tactical situation, and can be different for different units. The operator for each unit precomputes some data required for multiple calculations in performing the operations.

公开(公告)号：US5584696A

公开(公告)日：1996-12-17

申请号：US282925

申请日：1994-07-28

Applicant: Joe L. Walker ,  Paul C. Lyon ,  Richard B. Linton ,  Rulon Nye ,  Ralph W. Fisher ,  Jeffrey B. Edwards ,  Clifford N. Cox

Inventor： Joe L. Walker ,  Paul C. Lyon ,  Richard B. Linton ,  Rulon Nye ,  Ralph W. Fisher ,  Jeffrey B. Edwards ,  Clifford N. Cox

IPC: G09B9/08 ,  G09B9/34 ,  H04N13/00 ,  G09B9/24

CPC classification number: G02B27/0172 ,  G02B27/017 ,  G09B9/085 ,  G09B9/34 ,  H04N13/0014 ,  H04N13/0278 ,  H04N13/044 ,  H04N13/0497 ,  G02B2027/0134 ,  H04N13/0051 ,  H04N13/0289 ,  H04N13/0296

Abstract: The present invention is directed to a simulation system for simulating virtual reality experiences such as for the sport of hang gliding or the like. The simulation system has a stereoscopic and collimated virtual image display, for providing pupil forming simulated images to a rider at a fixed point of reference relative to the stereoscopic display. In the disclosed embodiment, the simulation system comprises a mechanical support structure for suspending the rider in a harness so as to allow freedom of movement. The rider is suspended to face a visual display over a movable control bar coupled to the mechanical support structure. By maneuvering the control bar, riders may view the results of their actions as by a simulated display. The visual display is coupled to the control bar to receive electrical signals indicative of the movements initiated by the riders as they maneuver through a programmed environment. The visual display provides stereoscopic "pupil forming" images of positional states of the hang glider to the riders at a fixed point of reference relative to the visual display. The fixed point of reference is provided by limiting movement of the rider's head relative to the visual display, as for example with a head rest disposed directly above the viewing area of the visual display.

Abstract translation: 本发明涉及一种用于模拟虚拟现实体验的仿真系统，例如用于滑翔运动等。 仿真系统具有立体和准直的虚拟图像显示器，用于在相对于立体显示器的固定参考点处为驾驶者提供形成模拟图像的瞳孔。 在所公开的实施例中，模拟系统包括用于将骑手悬挂在吊带中以允许移动自由的机械支撑结构。 骑乘者被悬挂以面对耦合到机械支撑结构的可移动控制杆的视觉显示器。 通过操纵控制杆，骑手可以通过模拟显示来查看其动作的结果。 视觉显示器耦合到控制杆以接收指示由骑手在通过编程环境操纵时发起的运动的电信号。 视觉显示器以相对于视觉显示器的固定参考点为骑手提供了悬挂滑翔机的位置状态的立体“瞳孔形成”图像。 通过限制骑手的头部相对于视觉显示器的运动来提供固定的参考点，例如用位于视觉显示器的观看区域正上方的头枕。