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    Adjustable miniature panoramic illumination and infusion system for retinal surgery
    2.
    发明授权
    Adjustable miniature panoramic illumination and infusion system for retinal surgery 失效
    适用于视网膜手术的微型全景照明和输注系统

    公开(公告)号：US5725514A

    公开(公告)日：1998-03-10

    申请号：US700560

    申请日：1996-08-08

    申请人： Avi Grinblat ,  Stanley Chang

    发明人： Avi Grinblat ,  Stanley Chang

    IPC分类号： A61B19/00 ,  A61F9/007 ,  A61M3/02 ,  A61N1/30 ,  A61M35/00

    CPC分类号： A61F9/007 ,  A61F9/00727 ,  A61B2090/306 ,  A61M3/0279

    摘要： A medical device and method for eye surgery and method for illumination and fluid flow, particularly retinal surgery, combines a flow of infusing fluid and optical fiber illumination. The device uses a single strand of plastic optical fiber which extends through bores in a juncture device tube and needle cannula with sufficient clearance to permit the flow of the infusing fluid. The illuminating tip of the optical fiber is moved, during surgery, by loosening a cap of the junction device to release the optical fiber, moving the optical fiber within the junction device, and then re-tightening the cap to re-secure the optical fiber.

    摘要翻译： 用于眼科手术的医疗装置和方法以及用于照明和流体流动的方法，特别是视网膜手术，其结合了输注流体和光纤照明。 该装置使用单股塑料光纤，其延伸穿过具有足够间隙的接合装置管和针插管中的孔，以允许输注流体的流动。 在手术过程中，光纤的照明尖端通过松开接合装置的帽来移动，以释放光纤，将光纤移动到接合装置内，然后重新拧紧帽以重新固定光纤 。

    SYSTEMS, DEVICES, AND METHODS FOR ROBOT-ASSISTED MICRO-SURGICAL STENTING
    3.
    发明申请
    SYSTEMS, DEVICES, AND METHODS FOR ROBOT-ASSISTED MICRO-SURGICAL STENTING 审中-公开
    机器人辅助微创手术的系统，设备和方法

    公开(公告)号：US20100331858A1

    公开(公告)日：2010-12-30

    申请号：US12811506

    申请日：2009-01-30

    申请人： Nabil Simaan ,  Howard Fine ,  Wei Wei ,  Stanley Chang

    发明人： Nabil Simaan ,  Howard Fine ,  Wei Wei ,  Stanley Chang

    IPC分类号： A61B19/00 ,  A61F2/84

    CPC分类号： A61F2/82 ,  A61B34/30 ,  A61B34/37 ,  A61B34/71 ,  A61B34/77 ,  A61B2017/00331 ,  A61B2017/00345 ,  A61B2017/00991 ,  A61B2034/304 ,  A61B2090/064 ,  A61F2/966 ,  A61F9/007

    摘要： Systems, devices, and methods for robot-assisted microsurgical stenting are described herein. In some embodiments a tele-robotic microsurgical system for eye surgery include: a tele-robotic master and a slave hybrid-robot; wherein the tele-robotic master has at least one master slave interface controlled by a medical professional; wherein the slave hybrid-robot has at least one robotic arm attached to a frame releasably attached to a patient's head; wherein the at least one robotic arm has a parallel robot and a serial robot; and wherein the serial robot includes a stenting unit which includes a support tube, a pre-bent tube mounted within the support tube and a guide wire extending from the support tube for carrying a stent and for piercing a blood vessel.

    摘要翻译： 本文描述了用于机器人辅助显微外科支架置入术的系统，装置和方法。 在一些实施例中，用于眼科手术的远程机器人显微手术系统包括远程机器人主机和从属混合机器人; 其中远程机器人主机具有由医疗专业人员控制的至少一个主从接口; 其中所述从动混合机器人具有附接到可释放地附接到患者头部的框架的至​​少一个机器人手臂; 其中所述至少一个机器臂具有并联机器人和串行机器人; 并且其中所述串联机器人包括支架单元，所述支架单元包括支撑管，安装在所述支撑管内的预弯曲管和从所述支撑管延伸以用于承载支架和用于刺穿血管的导丝。

    Disk drive with fast error correction validation
    4.
    发明授权
    Disk drive with fast error correction validation 失效
    具有快速纠错验证的磁盘驱动器

    公开(公告)号：US5691994A

    公开(公告)日：1997-11-25

    申请号：US436516

    申请日：1995-05-08

    申请人： Marc Acosta ,  Carl Bonke ,  Trinh Bui ,  Stanley Chang ,  Patrick Lee ,  Phong Tran ,  Joanne Wu

    发明人： Marc Acosta ,  Carl Bonke ,  Trinh Bui ,  Stanley Chang ,  Patrick Lee ,  Phong Tran ,  Joanne Wu

    IPC分类号： G11B20/18 ,  G11C29/00

    CPC分类号： G11B20/1866

    摘要： An intelligent disk drive employing a controller which performs high speed error correction and miscorrection detection using a finite field processor. The error correction code is defined over a finite field and the error detection code is defined over an extension field of the finite field. The finite field processor performs calculation over both the finite field and extension field to provide high speed error correction and correction validation.

    摘要翻译： 一种采用控制器的智能磁盘驱动器，其使用有限场处理器执行高速误差校正和误差检测。 纠错码是在有限域上定义的，错误检测码是在有限域的扩展域上定义的。 有限域处理器对有限域和扩展域进行计算，以提供高速纠错和校正验证。

    Air Compression Type Engine For Aviation
    5.
    发明申请
    Air Compression Type Engine For Aviation 有权
    航空压缩式发动机

    公开(公告)号：US20080127629A1

    公开(公告)日：2008-06-05

    申请号：US11659888

    申请日：2006-04-19

    申请人： Stanley Chang

    发明人： Stanley Chang

    IPC分类号： F02K1/00

    CPC分类号： F02K1/002 ,  F02C3/04 ,  F02C3/107 ,  F05D2220/90 ,  Y02T50/671

    摘要： The present invention relates to an air compression type engine for aviation. The conventional aircraft engine is complicated in structure, consumes expensive aero fuel, and produces extremely loud noise during operation. Therefore, the present invention employs a turbo-charged air compressor to generate high temperature and high pressure gas in the pressure chamber, and uses the reaction thrust force generated by ejecting the compressed air through the nozzle to make the aircraft vertically take off/land, suspend in the air and fly forwardly. Benefited from the simple structure, the manufacture cost of the aircraft engine can be dramatically decreased. Vertically raising and landing the aircraft can be achieved by changing the ejection directed of the compressed air in the pressure chamber. The commonly used gasoline or diesel, which is cost saving and capable of combusting with a high combustion value, can be used instead of the expensive aviation kerosene. Further, the generated noise is quite small. By means of above arrangement, it is possible to manufacture a jet type manned craft like a car, which can be operated by common people to vertically take off/land and shuttle conveniently in the downtown area through simple operation procedure.

    摘要翻译： 本发明涉及一种用于航空的空气压缩式发动机。 传统的飞机发动机结构复杂，消耗昂贵的航空燃料，在运行中产生极大的噪音。 因此，本发明采用涡轮增压空气压缩机在压力室中产生高温高压气体，并且使用通过喷嘴喷射压缩空气而产生的反作用力使飞机垂直起飞/降落， 悬挂在空中，向前飞。 受益于简单的结构，飞机发动机的制造成本可以大大降低。 可以通过改变在压力室中的压缩空气的喷射来实现垂直升降飞机。 可以使用常用的汽油或柴油，其成本节省并且能够燃烧高燃烧值，而不是昂贵的航空煤油。 此外，产生的噪声相当小。 通过上述安排，可以制造像汽车这样的喷气式载人飞船，可以由普通人通过简单的操作程序在市区方便地垂直起飞/陆地和穿梭。

    Two-level error correction encoder
    7.
    发明授权
    Two-level error correction encoder 失效
    两级纠错编码器

    公开(公告)号：US5889794A

    公开(公告)日：1999-03-30

    申请号：US940187

    申请日：1997-09-30

    申请人： Shih Mo ,  Stanley Chang ,  Lih-Jyh Weng ,  Ba-Zhong Shen

    发明人： Shih Mo ,  Stanley Chang ,  Lih-Jyh Weng ,  Ba-Zhong Shen

    IPC分类号： H03M13/00 ,  H03M13/15

    CPC分类号： H03M13/15 ,  H03M13/00

    摘要： A two-level error correction encoder encodes m-bit data symbols in a first level of encoding in accordance with a distance d ECC over GF(2.sup.m+i) to produce (m+i)-bit ECC redundancy symbols and, during a second level of encoding, both modifies the set of ECC redundancy symbols, as necessary, to set i selected bits in each symbol in a predetermined truncation pattern and appends to the set of ECC symbols one or more pseudo redundancy symbols. The encoder includes d-1 Galois Field multipliers, and d-1 associated redundancy-symbol registers and an ECC symbol modifier lookup table that has stored therein information that the encoder uses during the second level of encoding. After the first level of encoding, the d-1 registers contain the (m+i)-bit ECC redundancy symbols. These symbols are used to enter the look-up table and select information that the encoder then encodes along with the ECC redundancy symbols, to produce the modified ECC redundancy symbols and append thereto one or more pseudo redundancy symbols. As the ECC redundancy symbols are modified, the encoding system removes them from the two-level encoder and appends them to the data. The last symbol(s) removed from the encoder and appended to the data are the one or more pseudo redundancy symbols. The system then truncates the i-bit pattern from each of the redundancy symbols to produce, at the end of the two-level encoding operation, a data code word that includes the m-bit data symbols, the m-bit modified ECC redundancy symbols and one or more m-bit pseudo redundancy symbols.

    摘要翻译： 两级纠错编码器根据GF（2m + i）上的距离d ECC编码第一编码级别的m位数据符号，以产生（m + i）位ECC冗余符号，并且在第二级 根据需要，根据需要修改ECC冗余符号集合，以预定的截断模式设置每个符号中的所选择的比特，并将附加到ECC符号的集合中的一个或多个伪冗余符号。 编码器包括d-1伽罗瓦域乘法器和d-1相关联的冗余符号寄存器和ECC符号修改器查找表，其中存储编码器在第二编码级别期间使用的信息。 在第一级编码之后，d-1寄存器包含（m + i）位ECC冗余符号。 这些符号用于输入查找表并选择编码器随后与ECC冗余符号一起被编码的信息，以产生经修改的ECC冗余符号并附加到一个或多个伪冗余符号。 随着ECC冗余符号的修改，编码系统将它们从二级编码器中删除，并将它们附加到数据中。 从编码器移除并附加到数据的最后一个符号是一个或多个伪冗余符号。 系统然后从每个冗余符号中截断i比特模式，以在两级编码操作结束时产生包括m比特数据符号的数据码字，m位修改的ECC冗余符号 和一个或多个m位伪冗余符号。

    Air compression type engine for aviation
    10.
    发明授权
    Air compression type engine for aviation 有权
    空气压缩式发动机

    公开(公告)号：US07980058B2

    公开(公告)日：2011-07-19

    申请号：US11659888

    申请日：2006-04-19

    申请人： Stanley Chang

    发明人： Stanley Chang

    IPC分类号： F02K1/00

    CPC分类号： F02K1/002 ,  F02C3/04 ,  F02C3/107 ,  F05D2220/90 ,  Y02T50/671

    摘要： The present invention relates to an air compression type engine for aviation. The conventional aircraft engine is complicated in structure, consumes expensive aero fuel, and produces extremely loud noise during operation. Therefore, the present invention employs a turbo-charged air compressor to generate high temperature and high pressure gas in the pressure chamber, and uses the reaction thrust force generated by ejecting the compressed air through the nozzle to make the aircraft vertically take off/land, suspend in the air and fly forwardly. Benefited from the simple structure, the manufacture cost of the aircraft engine can be dramatically decreased. Vertically raising and landing the aircraft can be achieved by changing the ejection directed of the compressed air in the pressure chamber. The commonly used gasoline or diesel, which is cost saving and capable of combusting with a high combustion value, can be used instead of the expensive aviation kerosene. Further, the generated noise is quite small. By means of above arrangement, it is possible to manufacture a jet type manned craft like a car, which can be operated by common people to vertically take off/land and shuttle conveniently in the downtown area through simple operation procedure.

    摘要翻译： 本发明涉及一种用于航空的空气压缩式发动机。 传统的飞机发动机结构复杂，消耗昂贵的航空燃料，在运行中产生极大的噪音。 因此，本发明采用涡轮增压空气压缩机在压力室中产生高温高压气体，并且使用通过喷嘴喷射压缩空气而产生的反作用力使飞机垂直起飞/降落， 悬挂在空中，向前飞。 受益于简单的结构，飞机发动机的制造成本可以大大降低。 可以通过改变在压力室中的压缩空气的喷射来实现垂直升降飞机。 可以使用常用的汽油或柴油，其成本节省并且能够燃烧高燃烧值，而不是昂贵的航空煤油。 此外，产生的噪声相当小。 通过上述安排，可以制造像汽车这样的喷气式载人飞船，可以由普通人通过简单的操作程序在市区方便地垂直起飞/陆地和穿梭。