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    Cryptographic processing with random number generator checking
    1.
    发明授权
    Cryptographic processing with random number generator checking 有权
    随机数发生器检查的加密处理

    公开(公告)号：US09158499B2

    公开(公告)日：2015-10-13

    申请号：US13460719

    申请日：2012-04-30

    申请人： Michael J. Torla ,  Steven D. Millman ,  Thomas E. Tkacik ,  Frank James

    发明人： Michael J. Torla ,  Steven D. Millman ,  Thomas E. Tkacik ,  Frank James

    IPC分类号： G06F7/58 ,  G06F11/07

    CPC分类号： G06F7/58 ,  G06F11/0751

    摘要： Embodiments of an electronic circuit comprise a module, such as a security module, configured to perform cryptographic processing for a predetermined security protocol that includes random number checking. The security module is controlled by a descriptor that includes instructions that cause the security module to access a generated random number, compare the generated random number to a random number stored during a previous execution of the descriptor, and generate an error signal when the generated random number and the previous execution random number are equal.

    摘要翻译： 电子电路的实施例包括被配置为对包括随机数检查的预定安全协议执行密码处理的诸如安全模块的模块。 安全模块由描述符控制，该描述符包括使得安全模块访问生成的随机数的指令，将所生成的随机数与在先前执行描述符期间存储的随机数进行比较，并且当生成的随机数产生随机数时产生错误信号 数字和前一个执行随机数相等。

    CRYPTOGRAPHIC PROCESSING WITH RANDOM NUMBER GENERATOR CHECKING
    2.
    发明申请
    CRYPTOGRAPHIC PROCESSING WITH RANDOM NUMBER GENERATOR CHECKING 有权
    具有随机数发生器检查的图像处理

    公开(公告)号：US20130290792A1

    公开(公告)日：2013-10-31

    申请号：US13460719

    申请日：2012-04-30

    申请人： Michael J. Torla ,  Steven D. Millman ,  Thomas E. Tkacik ,  Frank James

    发明人： Michael J. Torla ,  Steven D. Millman ,  Thomas E. Tkacik ,  Frank James

    IPC分类号： G06F11/07

    CPC分类号： G06F7/58 ,  G06F11/0751

    摘要： Embodiments of an electronic circuit comprise a module, such as a security module, configured to perform cryptographic processing for a predetermined security protocol that includes random number checking. The security module is controlled by a descriptor that includes instructions that cause the security module to access a generated random number, compare the generated random number to a random number stored during a previous execution of the descriptor, and generate an error signal when the generated random number and the previous execution random number are equal.

    摘要翻译： 电子电路的实施例包括被配置为对包括随机数检查的预定安全协议执行密码处理的诸如安全模块的模块。 安全模块由描述符控制，该描述符包括使得安全模块访问生成的随机数的指令，将所生成的随机数与在先前执行描述符期间存储的随机数进行比较，并且当生成的随机数产生随机数时产生错误信号 数字和前一个执行随机数相等。

    ROTARY WING AIRCRAFT ROD END AND METHOD OF MAKING A HELICOPTER VEHICLE ROD END WITH A PRECOCKED ORIENTATION
    5.
    发明申请
    ROTARY WING AIRCRAFT ROD END AND METHOD OF MAKING A HELICOPTER VEHICLE ROD END WITH A PRECOCKED ORIENTATION 失效
    旋转式飞机终点及使用预定方向制造直升机车尾的方法

    公开(公告)号：US20070231140A1

    公开(公告)日：2007-10-04

    申请号：US11036737

    申请日：2005-01-14

    申请人： Frank James ,  Christopher Rajecki

    发明人： Frank James ,  Christopher Rajecki

    IPC分类号： B64C27/50

    CPC分类号： F16F1/40 ,  B64C27/56 ,  B64C27/58 ,  B64C27/59 ,  F16C7/04 ,  F16C11/0614 ,  F16C11/083 ,  F16F1/393 ,  Y10T29/49885 ,  Y10T29/4998 ,  Y10T29/49982 ,  Y10T403/47

    摘要： The invention provides a rotary wing aircraft helicopter vehicle rod end and method of making a rod end. The rotary wing aircraft rod end includes a nonelastomeric inner member having an outer bonding surface segment and an axial bore with a center bore axis, a nonelastomeric outer member having an inner bonding surface segment and an axial bore center bore axis, and molded in place alternating elastomeric shims and nonelastomeric shims connecting the nonelastomeric inner member to the nonelastomeric outer member. The rod end includes a first inner elastomeric shim bonded to the nonelastomeric inner member outer bonding surface segment and to a first inner nonelastomeric shim and a second outer elastomeric shim bonded to the nonelastomeric outer member inner bonding surface segment and to a second outer nonelastomeric shim. The nonelastomeric inner member has a molded misalignment rotary wing aircraft rod end orientation with the outer nonelastomeric outer member.

    摘要翻译： 本发明提供一种旋翼飞机直升机车辆杆端和制造杆端的方法。 旋转翼飞行器杆端包括具有外接合表面段和具有中心孔轴线的轴向孔的非弹性内部构件，具有内部接合表面区段和轴向孔中心孔轴线的非弹性外部构件，并且交替地模制就位 弹性垫片和非弹性垫片将非弹性内部构件连接到非弹性外部构件。 杆端包括结合到非弹性内部构件外部结合表面区段的第一内部弹性垫片和结合到非弹性外部构件内部结合表面区段和第二外部非弹性垫片的第一内部非弹性垫片和第二外部弹性垫片。 非弹性内部构件具有与外部非弹性外部构件的模制未对准旋翼机翼杆端部取向。