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    • 1. 发明授权
    • Facsimile machine having a transmission speed selective shiftdown
function
    • 具有传输速度选择性切换功能的计算机
    • US5159465A
    • 1992-10-27
    • US253621
    • 1988-10-05
    • Koichiro MaemuraShigetaka Tanaka
    • Koichiro MaemuraShigetaka Tanaka
    • H04N1/333
    • H04N1/3333H04N2201/3335
    • A facsimile machine includes a data transmission speed shift down function according to which the data transmission speed is shifted down from its initial speed to one of a plurality of new speeds based on a ratio between the total number of data frames initially transmitted to a receiver and the number of data frames requested for retransmission by the receiver. In this manner, an optimal new data transmission speed may be accurately and expeditiously determined. A parameter memory containing information regarding destination areas to which an error correction mode of operation is to be used may be preferably provided in a facsimile machine having both of an error correction mode (ECM) and a normal mode. With this structure, the ECM mode can be automatically set. In such a facsimile machine having both an ECM and a normal transmission modes, a common buffer memory is provided for temporarily storing coded image information either in the ECM or normal transmission mode.
    • 传真机包括数据传输速度降档功能,根据该数据传输速度降档功能,数据传输速度基于最初传送到接收机的数据帧总数之间的比率,以及数据传输速度从初始速度向下移动到多个新速度之一 由接收机请求重传的数据帧的数量。 以这种方式,可以准确和迅速地确定最佳的新的数据传输速度。 可以在具有纠错模式(ECM)和正常模式两者的传真机中优选地提供包含关于要使用纠错操作模式的目的地区域的信息的参数存储器。 通过这种结构,可以自动设置ECM模式。 在具有ECM和正常传输模式的这种传真机中,提供了一个公共缓冲存储器,用于临时存储编码图像信息在ECM或正常传输模式中。
    • 2. 发明授权
    • Digital transmission device having an error correction mode and method
for shifting down a data transmission rate
    • 具有错误校正模式的数字传输设备和用于将数据传输速率降低的方法
    • US5105423A
    • 1992-04-14
    • US352460
    • 1989-05-16
    • Shigetaka TanakaYuichi Saito
    • Shigetaka TanakaYuichi Saito
    • H04L1/00H04L1/18H04N1/32H04N1/333
    • H04L1/0019H04L1/0002H04L1/18H04N1/32619H04N1/3333H04N2201/3335
    • In a method for shifting down a data transmission rate at a transmitter in response to a request from a receiver for retransmission of data frames having data errors in a digital transmission system such as a facsimile system, when transmission errors occur, the receiver transmits a request to the transmitter for retransmission of one or more data frames for which one or more data errors have occurred. At the transmitter, the data transmission rate is shifted down from the first data transmission rate to a second data transmission rate which is used for retransmitting the data frames for which one or more data errors have occurred. The above shift-down operation is controlled by calculating an expected value indicating a possibility of the occurrence of a data error at the time of retransmitting the data frames in which one or more data errors have occurred, on the basis of a number of data frames requested to be retransmitted and a total number of data frames which have been transmitted from the transmitter to the receiver.
    • 在一种用于在发射机处降低数据传输速率的方法中,响应于来自接收机的请求重传在诸如传真系统的数字传输系统中具有数据错误的数据帧的方法,当传输错误发生时,接收机发送请求 发送到发送器,用于重发发生了一个或多个数据错误的一个或多个数据帧。 在发射机处,数据传输速率从第一数据传输速率向下移动到用于重发发生了一个或多个数据错误的数据帧的第二数据传输速率。 通过计算指示在重发发生了一个或多个数据错误的数据帧时基于数据帧的数量发生数据错误的可能性的期望值来控制上述移位操作 请求重新发送和已经从发射机发送到接收机的数据帧的总数。
    • 5. 发明授权
    • Control system for non-linear control of a speed setting and a throttle
valve in an aircraft engine
    • 用于非线性控制飞行器引擎中的速度设定和节流阀的控制系统
    • US5810560A
    • 1998-09-22
    • US656042
    • 1996-05-24
    • Shigetaka Tanaka
    • Shigetaka Tanaka
    • B64C11/40B64C11/34F02D9/02F02D29/02
    • F02D29/02B64C11/34F02D2009/0261
    • A control system for an aircraft that controls the set speed of the propeller governor and the degree of opening of the throttle valve using a single control lever. The speed setting mechanism of the propeller governor is directly connected to the power lever by a push and pull cable, and the set speed of the propeller governor changes in proportion to the stroke of the power lever. Therefore, the propeller speed changes in proportion to the stroke of the power lever. On the other hand, the throttle valve is connected to the power lever by a nonlinear cam and a push and pull cable. Therefore, the degree of opening of the throttle valve does not change in proportion to the stroke of the power lever (i.e., the change in the degree of opening of the throttle valve has a nonlinear characteristic), and the engine output power changes in the nonlinear manner with respect to the change in the propeller speed. By setting the nonlinear characteristic in the change in the engine output power with respect to the change in the propeller speed, an optimum relationship, between the engine speed and engine output power, for the aerodynamic characteristics of the aircraft can be obtained.
    • 用于使用单个控制杆控制螺旋桨调速器的设定速度和节流阀的打开程度的飞机控制系统。 螺旋桨调速器的调速机构通过推拉电缆直接连接到动力杆,螺旋桨调速器的设定速度与动力杆的行程成比例地变化。 因此,螺旋桨速度与动力杆的行程成比例地变化。 另一方面,节流阀通过非线性凸轮和推拉电缆连接到动力杆上。 因此,节流阀的开度与动力杆的冲程成比例地变化(即,节流阀的开度变化具有非线性特性),发动机输出功率在 相对于螺旋桨速度的变化的非线性方式。 通过相对于螺旋桨速度的变化设定发动机输出功率的变化中的非线性特性,可以获得飞机的空气动力特性之间的发动机转速和发动机输出功率之间的最佳关系。
    • 7. 发明授权
    • Facsimile communication method and facsimile machine
    • FACSIMILE通信方法和FACSIMILELE MACHINE
    • US5140439A
    • 1992-08-18
    • US399986
    • 1989-08-29
    • Shigetaka Tanaka
    • Shigetaka Tanaka
    • H04N1/00H04M11/00H04N1/32
    • H04N1/00488H04N1/32614H04N1/32635H04N1/32662H04N2201/3219H04N2201/3261
    • A facsimile communication method includes the steps of transmitting image information from a transmitter facsimile machine to a receiver facsimile machine through a transmission line, determining whether the receiver facsimile machine is successful in receiving the transmitted image information, sending a first station related to the transmitter facsimile machine a first voice message from the transmitter facsimile machine when the receiver facsimile machine is successful in receiving the transmitted image information, and sending a second station related to the receiver facsimile machine a second voice message from the receiver facsimile machine when the receiver facsimile machine has failed to receive the transmitted image information.
    • 传真通信方法包括以下步骤:通过传输线将发送机传真机的图像信息发送到接收机传真机,确定接收机传真机是否成功接收传输的图像信息;发送与发射机传真相关的第一台 当接收机传真机成功接收传送的图像信息时,发送来自发射机传真机的第一语音消息,并且当接收机传真机具有接收机传真机时,从接收机传真机发送与接收机传真机有关的第二话音消息 无法接收传输的图像信息。
    • 8. 发明授权
    • Equalization system tuning device which updates equalizer coefficients
based on selected decision regions
    • 均衡系统调整装置,其基于所选择的决定区域来更新均衡器系数
    • US4679208A
    • 1987-07-07
    • US760116
    • 1985-07-29
    • Shigetaka Tanaka
    • Shigetaka Tanaka
    • H04B3/10H04L27/01
    • H04L27/01
    • An equalization system wherein a signal received over a line is equalized and the quantity of equalization is compensated based on a difference, or error, between the equalized received signal and a signal which is estimated from the received signal, including a tuning device which compensates the amount of equalization by training, which precedes reception of communication data. A difference or error range which is usable for the compensation of the quantity of equalization is set up during a training sequence. The error range sequentially increases as the training sequence proceeds. Thus, decision feedback updating during the training sequence only occurs so long as the difference between the equalized received signal and a signal which is estimated from the received signal is within the error range, which is sequentially increased during a training sequence. After completion of the training sequence decision feedback updating is always allowed.
    • 一种均衡系统,其中通过线路接收的信号被均衡,并且基于均衡的接收信号与从接收信号估计的信号之间的差异或误差来补偿均衡量,包括补偿 在接收通信数据之前通过训练的均衡量。 在训练序列期间建立可用于补偿均衡量的差异或误差范围。 随着训练序列的进行,误差范围依次增加。 因此,仅在均衡的接收信号与从接收信号估计的信号之间的差异在误差范围内时才发生训练序列期间的判定反馈更新,这在训练序列期间依次增加。 训练序列完成后,总是允许更新反馈。
    • 9. 发明授权
    • Method and apparatus for group 3 facsimile capable of properly performing a communications operation using optional frames
    • 用于能够使用可选帧适当地执行通信操作的组3传真机的方法和装置
    • US07227654B1
    • 2007-06-05
    • US09317069
    • 1999-05-13
    • Shigetaka Tanaka
    • Shigetaka Tanaka
    • G06F15/00G06K15/00
    • H04N1/33307H04N1/32016H04N1/33338H04N1/33369H04N1/33392H04N2201/33392
    • A method of a facsimile apparatus includes the steps of providing the facsimile apparatus with a memory which prestores identification information for a plurality of different facsimile machines having common specifications of optional frames, receiving a call for a facsimile communications operation using an optional frame and then identification information from a calling facsimile machine, verifying the identification information sent from the calling facsimile machine with the identification information prestored in the memory, canceling performance of the facsimile communications operation using the optional frame when the identification information sent from the calling facsimile machine is different from the identification information prestored in the memory, and executing the facsimile communications operation using the optional frame when the identification information sent from the calling facsimile machine is identical to the identification information prestored in the memory.
    • 一种传真设备的方法包括以下步骤:向传真设备提供一个存储器,该存储器预先存储具有可选帧的共同规格的多个不同传真机的识别信息,接收使用可选帧的传真通信操作的呼叫, 来自呼叫传真机的信息,使用预先存储在存储器中的识别信息来验证从呼叫传真机发送的识别信息,当从呼叫传真机发送的识别信息不同时,使用可选帧取消传真通信操作的性能 预先存储在存储器中的识别信息,以及当从呼叫传真机发送的识别信息与在存储器中预先存储的识别信息相同时,使用可选帧执行传真通信操作 y。
    • 10. 发明授权
    • Thrust control apparatus and method for an airplane
    • 一种飞机的推力控制装置及方法
    • US06224021B1
    • 2001-05-01
    • US09238280
    • 1999-01-27
    • Shigetaka Tanaka
    • Shigetaka Tanaka
    • B64D3100
    • B64C11/305B64D31/06F02D29/02
    • In an airplane thrust control apparatus, a control unit (EEC) for controlling the throttle valve opening of an internal combustion engine installed in an airplane and the propeller revolution speed is provided in order to control the engine to appropriate conditions suitable to various flight conditions. During normal operation, the EEC sets the throttle valve opening and the propeller revolution speed in accordance to the stroke of a single power lever. However, if it is determined that the airplane is descending, the EEC sets the throttle valve opening to a value less than the normal set opening, and sets the propeller revolution speed to a high revolution speed equal to or higher than a predetermined revolution speed, regardless of the set revolution speed. Therefore, the thrust control apparatus is able to achieve a sufficient descending rate by reducing the engine output while maintaining high supercharger revolution speed high and maintaining required cabin pressurization.
    • 在飞机推力控制装置中,设置用于控制安装在飞机中的内燃机的节气门开度的控制单元(EEC)和螺旋桨转速,以便将发动机控制在适合于各种飞行条件的适当条件。 在正常运行中,EEC根据单个动力杆的行程设置节气门开度和螺旋桨转速。 然而,如果确定飞机正在下降,则EEC将节流阀开度设定为比正常设定开度小的值,将螺旋桨转速设定为等于或高于预定转速的高转速, 无论设定的转速如何。 因此,推力控制装置能够通过降低发动机输出,同时保持高增压器转速高并维持所需的客舱加压来实现足够的下降速率。