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公开(公告)号：US20060023573A1
公开(公告)日：2006-02-02
申请号：US10901543
申请日：2004-07-29
申请人： Manuel Rivera , David Pereira
发明人： Manuel Rivera , David Pereira
IPC分类号： G11B19/02
摘要： An optical drive reads information from an optical medium by measuring the reflectivity of the optical medium to determine the type of optical medium, setting read parameters associated with the determined type and attempting to read identification information from the optical medium to verify the optical medium type. If the identification information verifies the type of optical medium as determined by the measured reflectivity, the optical drive reads information with the read parameters. If the identification information is not readable or fails to verify the measured optical medium type, an alternative optical medium type read parameters are used to read the identification information. If the alternative optical medium type matches the identification information optical medium type, read parameters associated with the alternative optical medium type are used to read information from the optical medium and the user is provided a warning that the optical medium has substandard quality.
摘要翻译： 光学驱动器通过测量光学介质的反射率来测量光学介质的反射率，从而确定光学介质的类型，设置与所确定的类型相关联的读取参数并尝试从光学介质读取识别信息以验证光学介质类型。 如果识别信息通过测量的反射率确定光学介质的类型，则光驱读取参数的信息。 如果识别信息不可读或无法验证测量的光介质类型，则使用替代的光介质类型读参数来读取识别信息。 如果替代光学介质类型与识别信息光学介质类型匹配，则使用与替代光学介质类型相关联的读取参数来从光学介质读取信息，并且向用户提供光学介质具有不合格质量的警告。
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12.发明授权公开(公告)号：US08955306B2
公开(公告)日：2015-02-17
申请号：US12995399
申请日：2009-04-27
申请人： Hakim Maalioune , David Pereira
发明人： Hakim Maalioune , David Pereira
IPC分类号： F02K1/76
摘要： The invention relates to a method for controlling a plurality of actuators (9a, 9b, 9c) for a movable thrust reverser cowl (1), characterized remarkable in that the position deviation between adjacent actuators is measured in real time, and in that the speed profile of the actuator or actuators in question is adjusted by a position deviation exceeding a predetermined threshold.
摘要翻译： 本发明涉及一种用于控制用于可移动推力反向器罩（1）的多个致动器（9a，9b，9c）的方法，其特征在于，实时地测量相邻致动器之间的位置偏差，并且速度 通过超过预定阈值的位置偏差来调节所讨论的致动器或致动器的轮廓。
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13.发明授权Device for controlling maintenance actuators for the cowlings of a turbojet engine nacelle 有权用于控制涡轮喷气发动机机舱的整流罩维护执行器的装置公开(公告)号：US08686589B2
公开(公告)日：2014-04-01
申请号：US12673868
申请日：2008-07-16
申请人： David Pereira
发明人： David Pereira
IPC分类号： B64D29/00
CPC分类号： B64D29/08 , Y10T307/76
摘要： The invention relates to a device (9) for controlling the maintenance actuators (7a, 7b) of the cowlings of a turbojet engine nacelle of an aircraft, that comprises a first stage (12) to be connected to an electric power network (10) of the aircraft, at least one second power stage (13a, 13b) including converters of a first DC voltage from the first stage (12) into a second DC voltage for powering at least one maintenance actuator (7a, 7b) connected downstream from the device (9), a control means (14) for the first and second stages (12, 13a, 13b), and a means (15) for establishing a communication between the control means (14) and at least one control housing (16a, 16b) so that a user can control the operation of the actuators, the control means being arranged so as to carry out switching operations between a first operation mode in which the second stage(s) (13a, 13b) are powered, and a second standby mode in which the second stage(s) (13a, 13b) are not powered by the first stage (12).
摘要翻译： 本发明涉及一种用于控制飞机的涡轮喷气发动机机舱的整流罩的维护致动器（7a，7b）的装置（9），其包括要连接到电力网络（10）的第一级（12） 所述至少一个第二功率级（13a，13b）包括从所述第一级（12）的第一DC电压的转换器转换成用于为至少一个维护致动器（7a，7b）供电的第二DC电压，所述维护致动器 装置（9），用于第一和第二级（12,13a，13b）的控制装置（14）和用于在控制装置（14）和至少一个控制壳体（16a）之间建立连通的装置 ，16b），使得用户可以控制致动器的操作，控制装置被布置成在第二级（13a，13b）被供电的第一操作模式和 第二待机模式，其中第二级（13a，13b）不由第一级（12）供电 ）。
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公开(公告)号：US20130119664A1
公开(公告)日：2013-05-16
申请号：US13384807
申请日：2010-06-29
申请人： David Pereira , Hakim Maalioune , Vincent Le Coq
发明人： David Pereira , Hakim Maalioune , Vincent Le Coq
CPC分类号： F01D15/10 , B64D29/06 , B64D41/00 , B64D2221/00 , F02N11/04
摘要： The present invention relates to an electric power supply circuit (1) for a turbojet engine nacelle including at least one electric generator (2) mechanically connected to the shaft of a turbojet engine, said generator being capable of directly supplying electric power to a first electric power device other than a simple monitoring or supervising unit, characterized in that said generator is capable of directly supplying electric power to at least one second electric power device other than a monitoring or supervising unit, as well as to a nacelle including such an electric circuit.
摘要翻译： 本发明涉及一种用于涡轮喷气发动机机舱的电力供应回路（1），其包括机械地连接到涡轮喷气发动机的轴的至少一个发电机（2），所述发电机能够直接向第一电动机 除了简单的监视或监督单元之外的功率装置，其特征在于，所述发电机能够直接向除了监视或监督单元之外的至少一个第二电力装置提供电力，以及包括这种电路的机舱 。
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公开(公告)号：US20110225975A1
公开(公告)日：2011-09-22
申请号：US13129719
申请日：2009-08-26
申请人： David Pereira , Laurence Lemains
发明人： David Pereira , Laurence Lemains
IPC分类号： F02C1/00
CPC分类号： B64D15/12 , B64D15/22 , B64D2033/0233 , F02C7/047
摘要： The present invention relates to a method for commanding and controlling at least one resistive heating element (1) belonging to an aircraft turbojet engine nacelle deicing set, characterized in that it involves the steps aimed at: obtaining, from a central control unit (6) of the aircraft, parameters representative of the exterior flight conditions; determining a thermal model corresponding to the flight conditions obtained; as a function of the thermal model, delivering the appropriate corresponding electrical power (4) to the resistive heating element.
摘要翻译： 本发明涉及一种用于命令和控制属于飞机涡轮喷气发动机机舱除冰机组的至少一个电阻加热元件（1）的方法，其特征在于其涉及以下步骤：从中央控制单元（6）获得， 的飞机参数，代表外部飞行情况; 确定与获得的飞行条件相对应的热模型; 作为热模型的函数，将适当的对应的电力（4）传递给电阻加热元件。
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16.发明申请公开(公告)号：US20110088369A1
公开(公告)日：2011-04-21
申请号：US12995399
申请日：2009-04-27
申请人： Hakim Maalioune , David Pereira
发明人： Hakim Maalioune , David Pereira
IPC分类号： F02K1/76
摘要： The invention relates to a method for controlling a plurality of actuators (9a, 9b, 9c) for a movable thrust reverser cowl (1), characterized remarkable in that the position deviation between adjacent actuators is measured in real time, and in that the speed profile of the actuator or actuators in question is adjusted by a position deviation exceeding a predetermined threshold.
摘要翻译： 本发明涉及一种用于控制用于可移动推力反向器罩（1）的多个致动器（9a，9b，9c）的方法，其特征在于，实时地测量相邻致动器之间的位置偏差，并且速度 通过超过预定阈值的位置偏差来调节所讨论的致动器或致动器的轮廓。
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公开(公告)号：US20090019326A1
公开(公告)日：2009-01-15
申请号：US12154188
申请日：2008-05-21
申请人： Gerard Boudon , Didier Malcavet , David Pereira , Andre Steimle
发明人： Gerard Boudon , Didier Malcavet , David Pereira , Andre Steimle
IPC分类号： G06F11/00
CPC分类号： G01R31/3171
摘要： A self-synchronizing data bus analyser is provided which can include a generator linear feedback shift register (LFSR) to generate a first data set, and can include a receiver LFSR to generate a second data set. The data bus analyzer may also include a bit sampler to sample the first data set received through a data bus coupled to the generator LFSR and output a sampled first data set. A comparator can be included to compare the sampled first data set with the second data set generated by the receiver LFSR and provide a signal to the receiver LFSR to adjust a phase of the receiver LFSR until the second data set is substantially the same as the first data set.
摘要翻译： 提供了一种自同步数据总线分析器，其可以包括发生器线性反馈移位寄存器（LFSR）以产生第一数据集，并且可以包括接收器LFSR以生成第二数据集。 数据总线分析器还可以包括比特采样器，以对通过耦合到发生器LFSR的数据总线接收的第一数据集进行采样，并输出采样的第一数据集。 可以包括比较器以将采样的第一数据集与由接收机LFSR生成的第二数据集进行比较，并向接收机LFSR提供信号以调整接收机LFSR的相位，直到第二数据组与第一数据集基本相同 数据集。
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公开(公告)号：US20050256750A1
公开(公告)日：2005-11-17
申请号：US11161467
申请日：2005-08-04
申请人： Richard Hand , Wendy Levitt , David Pereira , Anna Austin , Gregory Coles , Duane Jacobsen , Vinny Khosla , Thomas Lunsford , Renee Richards , Leigh Tomaski
发明人： Richard Hand , Wendy Levitt , David Pereira , Anna Austin , Gregory Coles , Duane Jacobsen , Vinny Khosla , Thomas Lunsford , Renee Richards , Leigh Tomaski
摘要： An automated method and system for refunding the unused portion of an electronic ticket are provided. In accordance with the method, an aging period is set and is added to the scheduled departure date of the issued ticket. If the scheduled departure date plus the aging date is earlier than the current date, a determination is made as to whether the ticket has been used. If the ticket has not been used, the residual value of the ticket is calculated and a refund is issued.
摘要翻译： 提供一种用于退还电子票未使用部分的自动化方法和系统。 根据该方法，设定老化时间，并将其添加到所发行的票的预定出发日期。 如果计划的出发日期加上老化日期早于当前日期，则确定票已被使用。 如果没有使用机票，则计算车票的剩余价值并退还。
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公开(公告)号：US09102411B2
公开(公告)日：2015-08-11
申请号：US13129719
申请日：2009-08-26
申请人： David Pereira , Laurence Lemains
发明人： David Pereira , Laurence Lemains
CPC分类号： B64D15/12 , B64D15/22 , B64D2033/0233 , F02C7/047
摘要： The present invention relates to a method for commanding and controlling at least one resistive heating element (1) belonging to an aircraft turbojet engine nacelle deicing set, characterized in that it involves the steps aimed at: obtaining, from a central control unit (6) of the aircraft, parameters representative of the exterior flight conditions; determining a thermal model corresponding to the flight conditions obtained; as a function of the thermal model, delivering the appropriate corresponding electrical power (4) to the resistive heating element.
摘要翻译： 本发明涉及一种用于命令和控制属于飞机涡轮喷气发动机机舱除冰机组的至少一个电阻加热元件（1）的方法，其特征在于其涉及以下步骤：从中央控制单元（6）获得， 的飞机参数，代表外部飞行情况; 确定与获得的飞行条件相对应的热模型; 作为热模型的函数，将适当的对应的电力（4）传递给电阻加热元件。
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公开(公告)号：US09038363B2
公开(公告)日：2015-05-26
申请号：US13145601
申请日：2010-01-20
申请人： David Pereira , Laurence Lemains
发明人： David Pereira , Laurence Lemains
CPC分类号： B64D15/12 , B64D15/00 , B64D15/20 , B64D2033/0233 , F02C7/047 , H05B3/0014
摘要： The invention relates to a de-icing device for an element of a nacelle of a turbojet engine, including at least one heating resistant mat connected to at least one electrical power source (3) and thus defining an assembly (1) of resistant mats, characterized in that the assembly of resistant mats includes one or more subassemblies of resistant mats, each subassembly in turn including one or more resistant mats of the assembly, and each subassembly of resistive mats having a different ohmic value.
摘要翻译： 本发明涉及一种用于涡轮喷气发动机的机舱的元件的除冰装置，包括至少一个与至少一个电源（3）连接的耐热垫，从而限定了抵抗垫的组件（1） 其特征在于，抵抗垫的组件包括一个或多个抵抗垫的子组件，每个子组件依次包括组件的一个或多个阻力垫，以及具有不同欧姆值的电阻垫的每个子组件。
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