中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

27 records (took 0.028 seconds)

    Angle of attack based pitch generator and head up display
    1.
    发明授权
    Angle of attack based pitch generator and head up display 失效
    基于角度的俯仰发生器和抬头显示

    公开(公告)号：US4390950A

    公开(公告)日：1983-06-28

    申请号：US210771

    申请日：1980-11-28

    Applicant: Hans R. Muller

    Inventor： Hans R. Muller

    IPC: B64D43/00 ,  G01C21/00 ,  G01C21/20 ,  G05D1/06 ,  G01C23/00 ,  G06G7/78

    CPC classification number: G05D1/0615

    Abstract: A circuit for computing a signal representing the pitch attitude of an aircraft utilizes angle of attack based information and the output of a gyroscope to produce a calculated pitch signal which has a long term component dependent upon the angle of attack based information and a short term component dependent upon the gyroscope output signal. The calculated pitch signal may be used to pitch stabilize a head up display in the aircraft and in this event is modified with a correction signal derived from the pitch signal and the output of a head up display mounted accelerometer. Alternatively, the pitch signal may be combined with a signal representing the difference between the output of the display mounted accelerometer and the output of an angle of attack vane mounted accelerometer to provide a pitch stabilization signal which is free of turn and shear errors.

    Abstract translation: 用于计算表示飞行器的俯仰姿态的信号的电路利用基于攻角的信息和陀螺仪的输出来产生计算的俯仰信号，其具有取决于基于攻角的信息的长期分量和短期分量 取决于陀螺仪的输出信号。 所计算出的俯仰信号可以用于对飞机中的抬头显示进行俯仰稳定，并且在这种情况下，使用从俯仰信号导出的校正信号和头部显示安装的加速度计的输出进行修正。 或者，音调信号可以与表示显示器安装的加速度计的输出与迎角附加加速度计的输出之间的差的信号组合，以提供无转弯和剪切误差的音调稳定信号。

    Cable structure with cable sheath
    2.
    发明授权
    Cable structure with cable sheath 失效
    带电缆护套的电缆结构

    公开(公告)号：US4246937A

    公开(公告)日：1981-01-27

    申请号：US971494

    申请日：1978-12-20

    Applicant: Hans R. Muller

    Inventor： Hans R. Muller

    IPC: H01B7/24 ,  D07B1/00 ,  D07B1/14 ,  D07B1/16 ,  E04C5/08 ,  E04C5/10 ,  F16C1/26 ,  E04H12/20 ,  F16G11/00 ,  H01B11/18

    CPC classification number: F16C1/26 ,  E04C5/08 ,  E04C5/10

    Abstract: A cable structure comprising a cable provided with a cable sheath in the form of a flexible corrugated or undulated tube. Between the cable and the sheath there are arranged guide bodies at predetermined locations. The guide bodies are fixed at the inside of the sheath and are provided with domed or arched guide surfaces at the side of the cable, in order to guide the cable both in a straight and bent condition.

    Abstract translation: 一种电缆结构，包括设置有柔性波纹或波状管形式的电缆护套的电缆。 在电缆和护套之间，在预定位置处布置有引导体。 引导体固定在护套的内部，并且在电缆侧面设置有拱形或拱形的引导表面，以便将电缆引导成直线和弯曲的状态。

    Process for the preparation of (6S)- and (6R)-tetrahydrofolic acid
    3.
    发明授权
    Process for the preparation of (6S)- and (6R)-tetrahydrofolic acid 失效
    制备（6S） - 和（6R） - 四氢叶酸的方法

    公开(公告)号：US5324836A

    公开(公告)日：1994-06-28

    申请号：US44886

    申请日：1993-04-08

    Applicant: Hans R. Muller ,  Martin Ulmann ,  Josef Conti ,  Gunter Murdel

    Inventor： Hans R. Muller ,  Martin Ulmann ,  Josef Conti ,  Gunter Murdel

    IPC: C07B57/00 ,  C07D475/04

    CPC classification number: C07D475/04

    Abstract: For the preparation of (6S)- and (6R)-tetrahydrofolic acid and their addition salts with a sulfonic acid or with sulfuric acid, (6R,S)-tetrahydrofolic acid is reacted with a sulfonic acid or with sulfuric acid, the resulting acid addition salt is fractionally crystallized and, if desired, the (6S)- or (6R)-tetrahydrofolic acid is liberated from the resulting diastereomeric acid addition salts by treatment with a base and isolated.

    Abstract translation: 为了制备（6S） - 和（6R） - 四氢叶酸及其与磺酸或硫酸的加成盐，（6R，S） - 四氢叶酸与磺酸或硫酸反应，得到的酸 加成盐分数结晶，如果需要，通过用碱处理并分离得到的（6S） - 或（6R） - 四氢叶酸从所得非对映异构酸加成盐中释放出来。

    Solid state memory for aircraft flight data recorder systems
    4.
    发明授权
    Solid state memory for aircraft flight data recorder systems 失效
    飞机数据记录仪系统的固态存储器

    公开(公告)号：US4644494A

    公开(公告)日：1987-02-17

    申请号：US577215

    申请日：1984-02-06

    Applicant: Hans R. Muller

    Inventor： Hans R. Muller

    IPC: B64D47/00 ,  G06F17/40 ,  G11C5/00 ,  G11C7/00 ,  G11C16/06 ,  G11C16/20 ,  G11C16/22 ,  G11C16/30 ,  G11C17/00 ,  G11C29/00 ,  G06F3/00 ,  G06F13/00

    CPC classification number: G11C29/765 ,  G11C16/06 ,  G11C16/20 ,  G11C16/225 ,  G11C16/30

    Abstract: A memory unit for a aircraft flight data recorder system uses an electronically erasable solid state memory for storing the flight data and a memory controller circuit are housed in a penetration resistant, thermally insulated enclosure. Power dissipation within the insulated enclosure is minimized by an external switching circuit that applies operating potential to the solid state memory only when data are being transferred to and from the memory circuit. A data protection circuit, located within the insulated enclosure inhibits memory write and erase operations whenever the system operating potential falls below a predetermined level. In continuously storing flight data, the oldest stored data is overwritten with newly arriving flight data and the memory controller maintains an erased boundary that defines the beginning and end of the recorded data. A power monitor circuit, located outside the insulated enclosure, resets the memory controller to the erased boundary following a power interruption. A dedicated portion of the memory space is utilized to store the address of faulty memory locations (detected during the data storage sequence) and stores the beginning and ending memory address of selected portions of the data record. The memory controller is sequenced to skip both the faulty memory locations and memory storage locations associated with the selected portions of the data record when new flight data is being stored.

    Abstract translation: 用于飞机飞行数据记录器系统的存储器单元使用电子可擦除固态存储器来存储飞行数据，并且存储器控制器电路容纳在防穿透绝热外壳中。 只有当数据传输到存储器电路和从存储器电路传输时，外部开关电路才能将绝缘外壳内的功率消耗降至最低。 位于绝缘外壳内的数据保护电路每当系统工作电位低于预定电平时就禁止存储器写入和擦除操作。 在连续存储飞行数据时，最新的存储数据被新到达的飞行数据覆盖，并且存储器控制器保持定义记录数据的开始和结束的擦除边界。 位于绝缘外壳外部的电源监控电路在电源中断后将存储器控制器复位到擦除的边界。 存储器空间的专用部分用于存储故障存储器位置的地址（在数据存储序列期间检测），并存储数据记录的选定部分的开始和结束存储器地址。 当存储新的航班数据时，存储器控制器被排序以跳过与数据记录的选定部分相关联的故障存储器位置和存储器存储位置。

    Terrain data retrieval system
    6.
    发明授权
    Terrain data retrieval system 失效
    地形数据检索系统

    公开(公告)号：US06710723B2

    公开(公告)日：2004-03-23

    申请号：US09955419

    申请日：2001-09-17

    Applicant: Hans R. Muller ,  Kevin J. Conner ,  Steven C. Johnson

    Inventor： Hans R. Muller ,  Kevin J. Conner ,  Steven C. Johnson

    IPC: G08B2300

    CPC classification number: G08G5/0086 ,  G01S7/12 ,  G01S7/22 ,  G01S13/953 ,  G01S19/41 ,  G01S19/47 ,  Y02A90/18

    Abstract: A terrain-awareness system (TAS) provides LOOK-AHEAD/LOOK-DOWN as well as LOOK-UP terrain advisory and warning indications to the pilot of an aircraft of a hazardous flight condition. The TAS includes an airport data base as well as a terrain data base that is structured to provide various resolutions depending on the topography of the particular geographic area of interest. Navigational data from a satellite-based navigational system, such as a global positioning system (GPS), is used to provide a LOOK-AHEAD/LOOK-DOWN and LOOK-UP terrain advisory and terrain warning indications based upon the current position and projected flight path of the aircraft. Since the terrain advisory and the warning signals are a function of the flight path of the aircraft, nuisance warnings are minimized.

    Abstract translation: 地形识别系统（TAS）为飞行员提供了LOOK-AHEAD / LOOK-DOWN以及LOOK-UP地形咨询和警告指示。 TAS包括一个机场数据库，以及一个地形数据库，其结构是根据特定地理区域的地形提供各种分辨率。 来自基于卫星的导航系统（例如全球定位系统（GPS））的导航数据用于根据当前位置和预计航班提供LOOK-AHEAD / LOOK-DOWN和LOOK-UP地形咨询和地形警告指示 飞机的路径。 由于地形咨询和警告信号是飞机的飞行路径的功能，妨碍了警报。

    Method and apparatus for alerting a pilot to a hazardous condition during approach to land
    7.
    发明授权
    Method and apparatus for alerting a pilot to a hazardous condition during approach to land 失效
    在接近陆地期间将飞行员提醒危险状况的方法和装置

    公开(公告)号：US06088634A

    公开(公告)日：2000-07-11

    申请号：US31146

    申请日：1998-02-26

    Applicant: Hans R. Muller ,  Kevin J. Conner ,  Steven C. Johnson

    Inventor： Hans R. Muller ,  Kevin J. Conner ,  Steven C. Johnson

    IPC: G01C5/00 ,  G05D1/06 ,  B64D45/04

    CPC classification number: G05D1/0676 ,  G01C5/005

    Abstract: A terrain-awareness system (TAS) provides LOOK-AHEAD/LOOK-DOWN as well as LOOK-UP terrain advisory and warning indications to the pilot of an aircraft of a hazardous flight condition. The TAS includes an airport data base as well as a terrain data base that is structured to provide various resolutions depending on the topography of the particular geographic area of interest. Navigational data from a satellite-based navigational system, such as a global positioning system (GPS), is used to provide a LOOK-AHEAD/LOOK-DOWN and LOOK-UP terrain advisory and terrain warning indications based upon the current position and projected flight path of the aircraft. Since the terrain advisory and the warning signals are a function of the flight path of the aircraft, nuisance warnings are minimized.

    Abstract translation: 地形识别系统（TAS）为飞行员提供了LOOK-AHEAD / LOOK-DOWN以及LOOK-UP地形咨询和警告指示。 TAS包括一个机场数据库，以及一个地形数据库，其结构是根据特定地理区域的地形提供各种分辨率。 来自基于卫星的导航系统（例如全球定位系统（GPS））的导航数据用于根据当前位置和预计航班提供LOOK-AHEAD / LOOK-DOWN和LOOK-UP地形咨询和地形警告指示 飞机的路径。 由于地形咨询和警告信号是飞机的飞行路径的功能，妨碍了警报。

    Terrain awareness system
    8.
    发明授权
    Terrain awareness system 失效

    公开(公告)号：US5839080A

    公开(公告)日：1998-11-17

    申请号：US509642

    申请日：1995-07-31

    Applicant: Hans R. Muller ,  Kevin J. Conner ,  Steven C. Johnson

    Inventor： Hans R. Muller ,  Kevin J. Conner ,  Steven C. Johnson

    IPC: G01C5/00 ,  G05D1/06 ,  G08G5/04

    CPC classification number: G05D1/0676 ,  G01C5/005

    Abstract: A terrain awareness system (TAS) provides LOOK-AHEAD/LOOK-DOWN as well as LOOK-UP terrain advisory and warning indications to the pilot of an aircraft of a hazardous flight condition. The TAS includes an airport data base as well as a terrain data base that is structured to provide various resolutions depending on the topography of the particular geographic area of interest. Navigational data from a satellite-based navigational system, such as a global positioning system (GPS), is used to provide a LOOK-AHEAD/LOOK-DOWN and LOOK-UP terrain advisory and terrain warning indications based upon the current position and projected flight path of the aircraft. Since the terrain advisory and the warning signals are a function of the flight path of the aircraft, nuisance warnings are minimized.

Patent Agency Ranking