公开(公告)号：US09214092B2

公开(公告)日：2015-12-15

申请号：US13834707

申请日：2013-03-15

申请人： Environmental Tectonics Corporation

发明人： Michael Charles Newman

IPC分类号： G09B9/12 ,  G09B9/10

CPC分类号： G09B9/10 ,  G09B9/12

摘要： A system and method for minimizing or eliminating Coriolis-tumbling sensations on a trainee in a centrifuge-based simulator is described. In one example methodology, a simulator transitions its rate of rotation to replicate flight conditions in which G-forces are unloaded on a trainee from a first-G-force value to a nominal-G-force value. Before reaching the nominal-G-force value, an intermediate-G-force value—which is more than the nominal-G-force value, but less than the first-G-force value—is imparted and maintained on the trainee for a suitable duration of time. This intermediate-G-force value may be determined based on several factors including: (i) the angle of rotation of a gondola at during the first-G-force value, and/or (ii) the first-G-force value. After the intermediate-G-force value is imparted and maintained for a suitable duration of time, the G-forces imparted on the trainee may be further unloaded till the nominal-G force value is reached.

摘要翻译： 描述了一种用于在基于离心机的模拟器中最小化或消除科里奥利滚筒感觉的系统和方法。 在一个示例性方法中，模拟器将其旋转速率转换成复制飞行条件，其中G力从实验者从第一G力值卸载到标称G力值。 在达到标称G力值之前，给予和保持在实习者身上的中间G力值 - 其大于标称G力值但小于第一G力值 合适的持续时间。 该中间G力值可以基于几个因素来确定，包括：（i）在第一G力值期间的缆车的旋转角度和/或（ii）第一G力值。 在赋予中间G力值并保持适当的持续时间之后，赋予实习者的G力可以进一步卸载，直到达到标称G力值。

公开(公告)号：US20110028872A1

公开(公告)日：2011-02-03

申请号：US12744896

申请日：2008-11-26

申请人： Maher Kevin

发明人： Maher Kevin

IPC分类号： A61H99/00

CPC分类号： G09B19/00 ,  A61B5/01 ,  A61B5/024 ,  A61B5/0531 ,  A61B5/08 ,  A61B5/11 ,  A61H1/001 ,  A61H2203/0431 ,  B64G7/00 ,  G07F17/3216 ,  G09B9/10

摘要： A vestibular stimulation system, computer controls, methods, and doses are provided.

摘要翻译： 提供前庭刺激系统，计算机控制，方法和剂量。

公开(公告)号：US20100112535A1

公开(公告)日：2010-05-06

申请号：US12290630

申请日：2008-10-31

申请人： Alistair K. Chan ,  Roderick A. Hyde ,  Jordin T. Kare ,  Lowell L. Wood, JR.

发明人： Alistair K. Chan ,  Roderick A. Hyde ,  Jordin T. Kare ,  Lowell L. Wood, JR.

IPC分类号： G09B19/00

CPC分类号： A61M21/00 ,  A61M2021/0027 ,  A61M2021/005 ,  A61M2021/0072 ,  A61M2230/63 ,  A61N1/36014 ,  A63F2300/1037 ,  G09B9/10 ,  G09B9/28

摘要： A method is generally described which includes detecting motions associated with a user, by a feedback sensor device. The method of also includes receiving information by a control program, the information being related to an objective of the user's motion from an objective information source and receiving data representative of the detected motions by the control program. Further, the method includes generating control data based on the data representative of the detected motions and the information, by a control algorithm of the control program. Further still, a method includes running the control program by a controller. Yet further still, the method includes outputting control signals based on the control data and delivering current from a current source to the vestibular system of the user in response to the control signals.

摘要翻译： 通常描述一种通过反馈传感器装置检测与用户相关联的运动的方法。 所述方法还包括通过控制程序接收信息，所述信息与来自客观信息源的用户运动的目标相关，并且接收由所述控制程序表示检测到的运动的数据。 此外，该方法包括通过控制程序的控制算法基于表示检测到的运动和信息的数据生成控制数据。 此外，一种方法包括通过控制器运行控制程序。 此外，该方法还包括基于控制数据输出控制信号，并响应于控制信号将电流从当前源传送到用户的前庭系统。

公开(公告)号：US06331114B1

公开(公告)日：2001-12-18

申请号：US09378911

申请日：1999-08-23

申请人： Fred Massey

发明人： Fred Massey

IPC分类号： G09B908

CPC分类号： G09B9/28 ,  G09B9/08 ,  G09B9/10

摘要： An apparatus for operating a remote controlled airplane including a frame, a remote control unit received within the frame and having first and second joystick elements, a joystick controller cantably mounted to the frame so as to have a forward/backward movement and a side-to-side movement, a first linkage connected to the joystick controller and to the first joystick element and adapted to cause an up-and-down movement of tie first joystick element relative to the forward/backward movement of the joystick controller, and a second linkage connected to the joystick controller and to the first joystick element. The second linkage is adapted to cause a side-to-side movement of the first joystick element relative to the side-to-side movement of the joystick controller. A pedal structure is pivotally mounted to the frame so as to be pivotable about a central axis. A third linkage connects the pedal structure to the second joystick element. A throttle member is pivotally connected to the frame and has a fourth linkage connected to the second joystick element. A pair of front wheels are rotatably mounted to a forward end of the frame and a third wheel is rotatably mounted in a transverse plane to a rearward end of the frame. An actuator mounted on the joystick controller causes a motor to drive the rear wheel.

摘要翻译： 一种用于操作遥控飞机的装置，包括框架，容纳在框架内并具有第一和第二操纵杆元件的遥控单元，可悬挂地安装到框架的操纵杆控制器，以便具有向前/向后运动，以及侧向 连接到操纵杆控制器和第一操纵杆元件的第一连杆，并且适于相对于操纵杆控制器的向前/向后运动引起系带第一操纵杆元件的上下移动;以及第二连杆 连接到操纵杆控制器和第一操纵杆元件。 第二连杆机构适于引起第一操纵杆元件相对于操纵杆控制器的侧向运动的侧向运动。 踏板结构枢转地安装到框架上，以便围绕中心轴线枢转。 第三连杆将踏板结构连接到第二操纵杆元件。 节流构件枢转地连接到框架并且具有连接到第二操纵杆元件的第四连杆。 一对前轮可旋转地安装在框架的前端，并且第三轮可旋转地安装在框架的后端的横向平面中。 安装在操纵杆控制器上的执行器使电机驱动后轮。

公开(公告)号：US5980255A

公开(公告)日：1999-11-09

申请号：US39245

申请日：1998-03-16

申请人： Louis-Joseph Mathieu ,  Pascal Le-Huu

发明人： Louis-Joseph Mathieu ,  Pascal Le-Huu

IPC分类号： A47C7/72 ,  A63F13/08 ,  A63G31/16 ,  G09B9/10 ,  G09B9/14 ,  G09B9/00

CPC分类号： A63F13/28 ,  A47C7/72 ,  A63F13/08 ,  A63F13/803 ,  G09B9/10 ,  G09B9/12 ,  G09B9/14 ,  A63F2300/302 ,  A63F2300/8082 ,  A63G31/16

摘要： A new motion cueing scheme has been found and adapted to an actual aircraft production seat to provide both transient and sustained heave acceleration cues. The mechanism is simple and compact enough to be easily implemented on G-seats. Changes in seat pan pitch angle synchronized with seat back vertical displacement result in a cue which feels realistic and reproduces consistently a number of the physiological and physical effects experienced by the pilot submitted to a real heave acceleration.

摘要翻译： 已经发现了一种新的运动提示方案，并适用于实际的飞机生产座椅，以提供瞬时和持续的起重加速提示。 该机构简单紧凑，可以方便地在G座上实施。 与座椅靠背垂直位移同步的座舱俯仰角的变化导致一个提示现实的提示，并一致地再现了飞行员提交给真正的起伏加速度的一些生理和物理效应。

公开(公告)号：US5498161A

公开(公告)日：1996-03-12

申请号：US311178

申请日：1994-09-23

申请人： Walter E. Noble, Jr.

发明人： Walter E. Noble, Jr.

IPC分类号： G09B9/10 ,  G09B9/16 ,  G09B9/08

CPC分类号： G09B9/10 ,  G09B9/165

摘要： An anti-G suit simulation system and especially pertains to an arrangement or system for simulating realistic acceleration conditions which are normally encountered during strenuous maneuvers carried out by pilots operating high-performance aircraft, such as jet fighter aircraft. More particularly, there is disclosed an anti-G simulation system wherein aircraft simulator pilots are exposed to physical conditions which rapidly and faithfully simulate and compensate for changes in high-intensity accelerations and gravitational effects or so-called G-conditions which are ordinarily encountered by the pilots of high-performance aircraft during the execution of aircraft maneuvers. Provided is a novel high/low-pressure vacuum system in which a series of solenoid valves are controllably connected to a source of high-pressure operating air and respectively, in a selective mode to high-pressure and low-pressure pumps which are adapted to be actuated responsive to signals received from a simulator computer so as to controllably evacuate the anti-G suit in conformance with specific reductions in G-forces simulated by the system.

摘要翻译： 一种反G型西装仿真系统，特别涉及一种用于模拟在操作高性能飞行器（如喷气式战斗机）的飞行员进行的艰苦演习中通常遇到的现实加速度条件的装置或系统。 更具体地，公开了一种抗G仿真系统，其中飞行器模拟器飞行员暴露于物理条件，其迅速且忠实地模拟并补偿高强度加速度和重力作用或所谓的G状态的变化，这些变化通常由 在执行飞机机动时高性能飞机的飞行员。 提供了一种新型的高/低压真空系统，其中一系列电磁阀可控制地连接到高压操作空气源，并且以选择方式分别连接到高压和低压泵，适用于 响应于从模拟器计算机接收到的信号而被响应，以便可控制地抽出符合系统模拟的G力的特定减小的防G服。

公开(公告)号：US5490784A

公开(公告)日：1996-02-13

申请号：US145413

申请日：1993-10-29

申请人： David E. E. Carmein

发明人： David E. E. Carmein

IPC分类号： A63B22/02 ,  G06F3/00 ,  G06F3/01 ,  G09B9/02 ,  G09B9/08 ,  G09B9/10 ,  G09B9/12 ,  G09B9/16 ,  G09B9/00

CPC分类号： G06F3/011 ,  A63B22/02 ,  G09B9/02 ,  G09B9/08 ,  G09B9/10 ,  G09B9/12 ,  G09B9/165 ,  A63B2071/0666 ,  G06F2203/012

摘要： A motion simulating device which is capable of creating motion with up to six degrees of freedom; three rotational degrees of freedom and three linear-translational degrees of freedom. The motion simulating device includes a generally spherical capsule abuttively supported on a plurality of rollers that are connected to a translatable frame. At least one of the rollers is a multi-directional active roller that frictionally engages the capsule to impart rotational motion to the capsule in any direction. The frame is optionally attached to a number of actuator legs which are capable of translating the frame along three orthogonal axes. Optimally, sights, sounds and physical sensations may be electronically coordinated and reproduced in the capsule so that a user may interactively control and respond to a variety of environments while simultaneously experiencing the corresponding motion and physical sensations associated with the interactive environment.

摘要翻译： 一种运动模拟装置，能够产生高达六个自由度的运动; 三个旋转自由度和三个线性 - 平移自由度。 运动模拟装置包括一个大体上球形的胶囊，其邻接地支撑在连接到可平移框架的多个辊上。 至少一个辊是多向有源辊，其摩擦地接合胶囊以在任何方向上向胶囊提供旋转运动。 框架可选地附接到能够沿着三个正交轴平移框架的多个致动器腿。 最佳地，视觉，声音和物理感觉可以在胶囊中电子协调和再现，使得用户可以交互地控制和响应各种环境，同时经历与交互式环境相关联的相应运动和物理感觉。

公开(公告)号：US5009598A

公开(公告)日：1991-04-23

申请号：US274838

申请日：1988-11-23

申请人： Thomas E. Bennington

发明人： Thomas E. Bennington

IPC分类号： G09B9/08 ,  G09B9/10 ,  G09B9/16 ,  G09B9/28

CPC分类号： G09B9/28 ,  G09B9/08 ,  G09B9/10 ,  G09B9/16

摘要： An aircraft flight simulator system adaptable to an actual inoperative aircraft not in flight provides instrument displays driven by a computer flight simulator program interacting with inputs from sensors attached to the actual aircraft control system and overlay switches. The computer may also drive visual displays placed in the cockpit windshield and side windows, as well as provide audio output and output for the operation of aircraft jacks to simulate inflight motion. All equipment may be relatively quickly and easily installed or removed so as to make maximum use of an otherwise inoperative aircraft on the ground, and by the use of computer program modifications, may be used to simulate a wide variety of aircraft. Realistic control handling is provided by feedback mechanisms attached to various aircraft control surfaces and the control column and which are coupled to the computer.

公开(公告)号：US4340371A

公开(公告)日：1982-07-20

申请号：US244842

申请日：1981-03-18

申请人： Gerald J. Kron

发明人： Gerald J. Kron

IPC分类号： G09B9/10 ,  G09B9/00

CPC分类号： G09B9/10

摘要： An apparatus for simulating the loads acting on the arms of an aircraft pilot under high G conditions including a first torque motor of pancake-like configuration attached to the flight suit near the elbow area of the pilot. A second torque motor positioned near the pilot's waist operates through a tether line to apply a force to the shoulder of the pilot. With both torque motors operating, the upper and lower arms of the pilot are loaded in a manner to simulate the effect of acceleration loading of primary consequence, +Gz.

摘要翻译： 一种用于模拟在高G条件下作用在飞行器飞行员的臂上的负载的装置，包括附接到飞行员肘部附近的飞行服的薄煎饼状构造的第一扭矩马达。 定位在飞行员腰部附近的第二扭矩马达通过系绳运行，以向飞行员的肩膀施加力。 在两个扭矩电机工作的情况下，导向装置的上臂和下臂以一种方式加载，以模拟加速载荷对主要结果+ Gz的影响。

公开(公告)号：US4321044A

公开(公告)日：1982-03-23

申请号：US960525

申请日：1978-11-14

申请人： Gerald J. Kron

发明人： Gerald J. Kron

IPC分类号： G09B9/08 ,  G09B9/10 ,  A47C1/00

CPC分类号： G09B9/10 ,  Y10S297/08

摘要： An improved G-seat system for providing kinesthetic cues to the operator of a vehicle simulator in which the motion sensations associated with the "G" forces are simulated by the motion of a single seat plate (62) having a pair of passive thigh ramps (78) mounted thereon and the variation in the degree of inflation of thin bladders (82A,B) which overlie the seat plate. Raised surfaces (80) may be provided on the plate beneath the ischial tuberosity region of the operator to increase the dynamic range of perceived g-loading effects. A backrest plate (92) may be provided for motion in conjunction with the seat plate and a thin bladder (128) may likewise be provided theron. Driven radial elements (108,110) may then be positioned on the lower part of the backrest plate to augment pressure cues at selected areas of the operator's back.

摘要翻译： 一种改进的G座系统，用于向车辆模拟器的操作者提供动觉线索，其中通过具有一对被动大腿坡道的单个座板（62）的运动来模拟与“G”力相关联的运动感觉 78）和覆盖在座板上的薄气囊（82A，B）的膨胀程度的变化。 凸起的表面（80）可以设置在操作者的坐骨结节区域下面的板上，以增加感知的g-加载效应的动态范围。 可以设置靠背板（92）以与座板一起运动，并且同样可以提供细气囊（128）。 驱动的径向元件（108,110）然后可以定位在靠背板的下部，以增加操作者背部的选定区域处的压力线索。