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公开(公告)号：US5331627A
公开(公告)日：1994-07-19
申请号：US981072
申请日：1992-11-24
IPC分类号： G11B23/03
CPC分类号： G11B23/0317
摘要： An adaptor cartridge for holding a 90 mm optical disk cartridge for insertion into a 130 mm disk drive apparatus. The cartridge adaptor emulates the external dimensions and features of a 130 mm cartridge so that it can be loaded into and manipulated by the 130 mm drive in the same manner as a normal 130 mm cartridge. The cartridge adaptor contains a shutter arm for opening the 90 mm cartridge door upon insertion of the cartridge into the adaptor cartridge in much the same manner as a 90 mm cartridge door is opened when the cartridge is inserted into a 90 mm drive. The cartridge adaptor also contains a pseudo 90 mm spindle located in an adaptor hub. The pseudo spindle fits within the centering hole of the 90 mm media disk. The adaptor cartridge carries an annular magnet for attracting and holding the 90 mm media disk on the adaptor hub. The underside of the adaptor hub is a simulated 130 mm cartridge hub for mating with the 130 mm drive spindle. The adaptor cartridge may also include a rotating permanent magnet directly above the 90 mm cartridge shutter opening for providing a bias magnetic field to enable writing a magneto-optic disk. Proper orientation of the rotating magnet is provided by the 130 mm drive bias coil.
摘要翻译： 用于保持90mm光盘盒以插入130mm磁盘驱动装置的适配器盒。 墨盒适配器模拟130毫米墨盒的外部尺寸和特征，使其可以以与正常的130毫米墨盒相同的方式装载到130毫米驱动器并由其操纵。 墨盒适配器包含一个快门臂，用于在将墨盒插入适配器墨盒时打开90毫米墨盒门，方式与当墨盒插入90毫米驱动器时打开90毫米墨盒门时相同。 盒式适配器还包含位于适配器集线器中的伪90 mm主轴。 伪主轴装配在90 mm介质盘的定心孔内。 适配器盒带有环形磁体，用于吸引并保持适配器毂上的90毫米介质盘。 适配器集线器的下侧是一个模拟的130毫米磁带轮毂，用于与130毫米驱动主轴配合。 适配器盒还可以包括直接在90mm盒式快门开口上方的旋转永磁体，用于提供偏置磁场以使得能够写入磁光盘。 旋转磁体的正确方向由130 mm驱动偏置线圈提供。
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公开(公告)号：US08417396B2
公开(公告)日：2013-04-09
申请号：US13241189
申请日：2011-09-22
IPC分类号： G01C23/00
CPC分类号： G08G5/0013
摘要： A method of operating an air traffic control system may include receiving, by a control system, an instruction from a control system user. The method may further include providing, by the control system, the instruction to an airplane via a data link between the control system and a system of the airplane. In addition, the method may include adjusting, by the airplane system, at least one airplane control to correspond to the instruction.
摘要翻译： 操作空中交通管制系统的方法可包括由控制系统接收来自控制系统用户的指令。 该方法还可以包括通过控制系统和飞机的系统之间的数据链路向控制系统提供对飞机的指令。 另外，该方法可以包括由飞机系统调整至少一个对应于指令的飞机控制。
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公开(公告)号：US20110046869A1
公开(公告)日：2011-02-24
申请号：US12917424
申请日：2010-11-01
IPC分类号： G08G5/00
CPC分类号： G08G5/0013
摘要： A method of receiving an instruction by an airplane from a control system includes facilitating, by the airplane, a user of a system of the airplane in accepting or rejecting the instruction. The instruction may be received by the airplane via a data link between the control system and the airplane system. If the instruction is accepted, the method may further include loading, by the airplane, the instruction into the airplane system and/or adjusting, by the airplane, at least one airplane control to correspond to the instruction.
摘要翻译： 由飞机从控制系统接收指令的方法包括由飞机帮助飞机系统的用户接受或拒绝该指示。 该指令可以由飞机经由控制系统和飞机系统之间的数据链接接收。 如果该指令被接受，该方法还可以包括由飞机将指令加载到飞机系统中和/或由飞机调整至少一个对应于该指令的飞机控制。
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4.发明授权Focus error detection using an equal path length lateral shearing interferometer 失效使用等径长度横向剪切干涉仪进行聚焦误差检测
公开(公告)号：US5446710A
公开(公告)日：1995-08-29
申请号：US972578
申请日：1992-11-06
CPC分类号： G11B7/0908 , G11B7/0917
摘要： This invention provides an equal path length lateral shearing interferometer and its implementation in focus detection devices, particularly for optical data storage devices. The interferometer comprises a beamsplitter and two abutting roof prisms. Shifting the placement of a roof prism along an axis orthogonal to the direction of light propagation and to the peak of the roof creates a lateral shear between the two output beams. Rotation a roof prism about this axis produces a tilt between the two output beams. This creates an interference pattern with a rotational orientation which is a function of the focus of the beam impinging on the optical storage medium. A pattern sensor is provided to adjust the focus of the beam in an accurate and dynamic manner.
摘要翻译： 本发明提供了一种相等的路径长度横向剪切干涉仪及其在焦点检测装置中的实现，特别是用于光学数据存储装置。 干涉仪包括分束器和两个邻接的屋顶棱镜。 沿着与光传播方向正交的轴线和屋顶的顶部位置移动屋顶棱镜在两个输出光束之间产生横向剪切。 围绕该轴旋转屋顶棱镜在两个输出光束之间产生倾斜。 这产生具有旋转取向的干涉图案，旋转取向是光束入射在光学存储介质上的焦点的函数。 提供图案传感器以精确和动态的方式调整光束的焦点。
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公开(公告)号：US20090267798A1
公开(公告)日：2009-10-29
申请号：US11464642
申请日：2006-08-15
CPC分类号： G08G1/161 , G08G5/0008 , G08G5/0013 , G08G5/025
摘要： The invention discloses differing embodiments of methods, aircraft, and apparatus for communicating the braking conditions of a runway. In one embodiment, braking information may be determined from a first aircraft which has landed on the runway. The braking information may be communicated to air traffic control and/or a second aircraft. Communication of the braking information may take place utilizing an Automatic Dependent Surveillance Broadcast system (ADS-B) and/or other type of automatic networking system.
摘要翻译： 本发明公开了用于传达跑道制动条件的方法，飞行器和装置的不同实施例。 在一个实施例中，可以从已经降落在跑道上的第一飞机确定制动信息。 制动信息可以被传送到空中交通管制和/或第二飞行器。 制动信息的通信可以利用自动相关监视广播系统（ADS-B）和/或其他类型的自动联网系统进行。
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公开(公告)号：US07586422B2
公开(公告)日：2009-09-08
申请号：US11461880
申请日：2006-08-02
IPC分类号： G08B21/00
CPC分类号： B60T8/1703 , B60T8/172 , B64C25/426 , G08G5/0091 , G08G5/025
摘要： The invention discloses differing embodiments of methods, aircraft, and apparatus for determining the landing conditions of a runway. In one embodiment, braking data may be collected from an aircraft which has landed on the runway; a braking performance measurement of the aircraft may be calculated based on the braking data; and a normalized braking performance measurement may be determined based on the braking performance measurement. The invention may be utilized to predict the expected braking performance of various types of aircraft on the runway. The invention may provide landing performance information to a broad host of users, and/or may be used as a basis for the development of a new aviation standard for the reporting of runway braking action.
摘要翻译： 本发明公开了用于确定跑道着陆条件的方法，飞行器和装置的不同实施例。 在一个实施例中，可以从已经降落在跑道上的飞机收集制动数据; 可以基于制动数据来计算飞行器的制动性能测量; 并且可以基于制动性能测量来确定归一化的制动性能测量。 本发明可以用于预测跑道上各种类型的飞机的预期制动性能。 本发明可以向广泛的用户主体提供着陆性能信息，和/或可以用作开发用于报告跑道制动动作的新的航空标准的基础。
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7.发明申请Displaying and/or programming airplane systems based on clearances and/or instructions 有权基于间隙和/或指令显示和/或编程飞机系统公开(公告)号：US20080114504A1
公开(公告)日：2008-05-15
申请号：US11600012
申请日：2006-11-14
CPC分类号： G08G5/0013
摘要： Methods and apparatuses for receiving, by an airplane, one or more clearances and/or instructions from a control system via a data link between the control system and a system of the airplane, are described herein. The system of the airplane may then facilitate a user in accepting or rejecting at least one of the received one or more clearances and/or instructions, and if accepted, may load the clearance and/or instructions and/or adjust controls to correspond to the clearance and/or instructions. Further, the system of the airplane may be adapted to display at least instructionsindicia of whether the received instructions are met to a user.
摘要翻译： 这里描述了用于由飞机从控制系统经由控制系统和飞机系统之间的数据链路接收一个或多个间隙和/或指令的方法和装置。 飞机的系统然后可以方便用户接受或拒绝所接收的一个或多个间隙和/或指令中的至少一个，并且如果被接受，则可以加载间隙和/或指令和/或调整控制以对应于 清关和/或说明。 此外，飞机的系统可以适于至少显示关于所接收的指令是否满足用户的指示。
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公开(公告)号：US20080030073A1
公开(公告)日：2008-02-07
申请号：US11461880
申请日：2006-08-02
IPC分类号： B60T8/32
CPC分类号： B60T8/1703 , B60T8/172 , B64C25/426 , G08G5/0091 , G08G5/025
摘要： The invention discloses differing embodiments of methods, aircraft, and apparatus for determining the landing conditions of a runway. In one embodiment, braking data may be collected from an aircraft which has landed on the runway; a braking performance measurement of the aircraft may be calculated based on the braking data; and a normalized braking performance measurement may be determined based on the braking performance measurement. The invention may be utilized to predict the expected braking performance of various types of aircraft on the runway. The invention may provide landing performance information to a broad host of users, and/or may be used as a basis for the development of a new aviation standard for the reporting of runway braking action.
摘要翻译： 本发明公开了用于确定跑道着陆条件的方法，飞行器和装置的不同实施例。 在一个实施例中，可以从已经降落在跑道上的飞机收集制动数据; 可以基于制动数据来计算飞行器的制动性能测量; 并且可以基于制动性能测量来确定归一化的制动性能测量。 本发明可以用于预测跑道上各种类型的飞机的预期制动性能。 本发明可以向广泛的用户主体提供着陆性能信息，和/或可以用作开发用于报告跑道制动动作的新的航空标准的基础。
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公开(公告)号：US5198944A
公开(公告)日：1993-03-30
申请号：US757423
申请日：1991-09-10
IPC分类号： G11B15/675 , G11B17/035 , G11B17/04 , G11B17/043 , G11B19/00 , G11B25/04
CPC分类号： G11B17/0434 , G11B17/035 , G11B19/00 , G11B25/043
摘要： A recording/playback apparatus in which movable datum pins are held in a base casting. Upon insertion of a cartridge into a holding tray, within the apparatus, the pins are released to move into datum holes in the cartridge when the holes are positioned directly above the pins. The cartridge is then lowered onto the drive spindle and positioned on surfaces of the base casting. During the load cycle, the cartridge is allowed to move relative to the holding tray while continuing to be held in place relative to the base casting by the datum pins.
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公开(公告)号：US20120010763A1
公开(公告)日：2012-01-12
申请号：US13241189
申请日：2011-09-22
CPC分类号： G08G5/0013
摘要： A method of operating an air traffic control system may include receiving, by a control system, an instruction from a control system user. The method may further include providing, by the control system, the instruction to an airplane via a data link between the control system and a system of the airplane. In addition, the method may include adjusting, by the airplane system, at least one airplane control to correspond to the instruction.
摘要翻译： 操作空中交通管制系统的方法可包括由控制系统接收来自控制系统用户的指令。 该方法还可以包括通过控制系统和飞机的系统之间的数据链路向控制系统提供对飞机的指令。 另外，该方法可以包括由飞机系统调整至少一个对应于指令的飞机控制。
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