| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 141 | Virtual flight recorder hosted by system tracing facility | US11211951 | 2005-08-25 | US08201027B2 | 2012-06-12 | John Michael Attinella; Larry J. Cravens; Michael James Denney; Edwin C. Grazier; Jay Paul Kurtz; David Ferguson Legler |
| A method utilizes a virtual flight recorder to harvest a subset of events being collected by an active system tracing facility during operation of a computer system. The virtual flight recorder is “virtual” from the sense that it is not specifically instrumented into a component with which the virtual flight recorder is associated, which eliminates the burden on developers to specifically instrument components of interest, and minimizes the impact on system performance as a result of performance metric collection. | ||||||
| 142 | Locator Beacon Disposed Internal to an Enclosure of a Flight Data Recorder and Method Therefor | US12206585 | 2008-09-08 | US20100063654A1 | 2010-03-11 | Michael C. Winterhalter; Endre Berecz |
| A flight data recorder includes an enclosure and electronic interface within the enclosure. The electronic interface is coupled for receiving data. A crash survivable memory unit is disposed within the enclosure. The crash survivable memory unit includes a memory module electrically coupled to the electronic interface for storing the data. A locator beacon is disposed within the enclosure or within the crash survivable memory unit. The locator beacon is an acoustic resonator which emits ultrasonic pulses. A battery is disposed within the enclosure or within the crash survivable memory unit for providing operating power to the locator beacon. The battery is rechargeable. The battery status is stored in the memory module. A beacon control circuit is disposed within the enclosure or within the crash survivable memory unit for monitoring the battery. A beacon activation device detects a crash event and notifies the beacon control circuit to activate the locator beacon. | ||||||
| 143 | Self-contained flight data recorder with wireless data retrieval | US09803889 | 2001-03-13 | US20020035416A1 | 2002-03-21 | Hilary Laing De Leon |
| A flight data recorder designed for small aircraft captures various onboard flight data in real-time and stores it in non-volatile memory. Recorded data includes aircraft's instantaneous position, altitude, attitude, engine RPM, G forces, flap position, cockpit voice and others. These data are obtained from various sensors which are integrated into the recorder. At the end of a flight the recorded data is downloaded into a computer using a wireless communications data transceiver also integrated into the recorder. It is an inexpensive system that does not require interfacing to any of the aircraft's instruments. It does not require removal or attaching any equipment to be able to download data. In addition to accident investigation, applications include training, preventive maintenance and asset monitoring. | ||||||
| 144 | Skip-field recorder with electronically controlled stop action capability | US3573357D | 1968-04-24 | US3573357A | 1971-04-06 | TOCE FRANCIS G |
| A system for providing from a helical scan skip-field magnetic tape recorder composite video having iterative portions corresponding to a single frame to enable such frames to be displayed as stable still pictures on a monitor. With the magnetic tape stationary, the video signals developed from a pair of heads spaced apart by 180* plus the arc corresponding to linear tape travel in the time of one field are combined and every other sync pulse is advanced in relation to the video signal such that corresponding portions of video in successive identical fields is in the same time relationship to its synchronizing pulse.
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| 145 | SYSTEM AND METHOD FOR PROVIDING VIRTUAL MACHINE DIAGNOSTIC INFORMATION USING A FLIGHT RECORDER FUNCTIONALITY | US13456028 | 2012-04-25 | US20130111273A1 | 2013-05-02 | Staffan Larsen; Henrik Osterdahl; Mikael Vidstedt |
| A system and method for providing virtual machine diagnostic information. In accordance with an embodiment, a “flight recorder”, for use with a virtual machine, such as a Java virtual machine (JVM), allows a system administrator, software developer or other user experiencing a system problem to “go back in time” and analyze what happened right before a particular problem occurred in their system, and/or obtain an extremely detailed level of profiling without impacting system performance. The flight recorder does this by being tightly integrated into the core of the JVM itself, and by being very conscious of its performance overhead. This allows the flight recorder to provide a large amount of information on the inner workings of the JVM, and on Java programs running in the JVM. | ||||||
| 146 | ELECTRONIC CONTROL MODULE INTEGRATED DIAGNOSTIC FLIGHT RECORDER METHODS AND SYSTEMS | US12015799 | 2008-01-17 | US20090187304A1 | 2009-07-23 | Thomas G. Waypa; Daniel P. Grenn; Joseph M. Stempnik |
| A control system for a vehicle is provided. The system generally includes a first setup module that configures at least one data recording trigger based on data parameters received from at least one of a telematics system and a technician tool. A data logger module records and stores real-time vehicle data based on the at least one data recording trigger. | ||||||
| 147 | Flight Recorder Having Integral Reserve Power Supply Within Form Factor of Enclosure and Method Therefor | US12142129 | 2008-06-19 | US20090319102A1 | 2009-12-24 | Michael C. Winterhalter; Glenn C. Wilson |
| A flight recorder includes an enclosure having a notch formed on one side or corner of the enclosure. An electronic interface is disposed within the enclosure. The electronic interface is coupled for receiving flight data, video data, and audio data. A memory unit is disposed within the enclosure and electrically connected to the electronic interface for storing the data. The memory unit contains a non-volatile memory device. A reserve power supply is physically disposed within the notch of the enclosure. The reserve power supply contains a rechargeable battery. A clamp secures the reserve power supply to the enclosure to make the reserve power supply removable from the enclosure. The reserve power supply has an electrical connector coupled to the enclosure for providing an operating voltage to the electronic interface and memory unit. The reserve power supply and electrical connector physically reside within a form factor of the enclosure. | ||||||
| 148 | Combined rescue beacon and flight recorder device for an aircraft and aircraft provided with such a device | US14128571 | 2012-06-21 | US09187183B2 | 2015-11-17 | Fabien Argillier; Michel Bermudez; Hichem Smaoui; Emmanuel Joubert; Thierry Pelegrin |
| A combined rescue beacon and flight recorder device for an airplane is ejectable, buoyant and/or provided with flotation devices. The combined rescue beacon and flight recorder device comprises a frame provided with at least one outer side surface having a solar panel. The combined rescue beacon and flight recorder device is configured to be placed in a housing created in an airfoil element of the aircraft. | ||||||
| 149 | Flight recorder having integral reserve power supply within form factor of enclosure and method therefor | US12142129 | 2008-06-19 | US08165730B2 | 2012-04-24 | Michael C. Winterhalter; Glenn C. Wilson |
| A flight recorder includes an enclosure having a notch formed on one side or corner of the enclosure. An electronic interface is disposed within the enclosure. The electronic interface is coupled for receiving flight data, video data, and audio data. A memory unit is disposed within the enclosure and electrically connected to the electronic interface for storing the data. The memory unit contains a non-volatile memory device. A reserve power supply is physically disposed within the notch of the enclosure. The reserve power supply contains a rechargeable battery. A clamp secures the reserve power supply to the enclosure to make the reserve power supply removable from the enclosure. The reserve power supply has an electrical connector coupled to the enclosure for providing an operating voltage to the electronic interface and memory unit. The reserve power supply and electrical connector physically reside within a form factor of the enclosure. | ||||||
| 150 | Integrating transient recorder apparatus for time array detection in time-of-flight mass spectrometry | US81731 | 1993-06-23 | US5367162A | 1994-11-22 | John F. Holland; Christie G. Enke; Michael R. Davenport; Lawrence W. Janow |
| An integrating transient recorder for time array detection of ions within an ion source extraction. The arrival times of all ions having various mass-to-charge ratios are calculated and integrating or peak detecting circuitry is activated just prior to the calculated time of arrival of each ion, and then only for a time duration in accordance with a predetermined data collection time window sufficient to enable each ion mass value to be completely measured. An analog-to-digital converter converts the area or peak analog signal for each ion into a corresponding digital signal and outputs the digital signals to a plurality of FIFO buffers. The FIFO buffers are read out for each successive transient by a digital signal processor and summed over a predetermined number of sequential transients in a mass locked registry creating a file of ion intensities versus mass-to-charge ratio of all ions detected. In a preferred embodiment the apparatus includes a mass defect detector which compares the actual arrival time of the ions with the calculated anticipated time of arrival and applies appropriate time delays from a selected one of a plurality of delta-mass tables. This causes the area or peak detection circuity to be turned on either slightly prior to or subsequent to the calculated times of arrival of each of the ions to thus cause each of the ions to be received clearly and completely within each data collection window. Preferred embodiments include combinations of analog or digital peak or area capture and analog or digital successive summations. | ||||||
| 151 | Ink flight state determining device, ink flight state determining method, program, and image recorder | JP2006292442 | 2006-10-27 | JP2008105343A | 2008-05-08 | OGURI ATSUSHI |
| <P>PROBLEM TO BE SOLVED: To provide an ink flight state determining device, an ink flight state determining method, a program, and an image recorder determining whether or not the landing of ink droplets onto recording media becomes proper by detecting the ink droplets during flying discharged from a nozzle. <P>SOLUTION: Flight state detecting sections 22-1-1 to 22-m-n detect the flight states of the ink droplets 41-1 to 41-α during flying discharged from the plurality of nozzles of a nozzle lines 9-1-1 to 9-n-m. A flight state determining section 27 predicts the landing position of the ink droplets 41-1 to 41-α onto the recording medium 15 based on the flight states of the ink droplets detected by the flight state detecting section 22-1-1 to 22-m-n and determines whether or not the landing of the ink droplets onto the recording medium 15 becomes proper based on the predicted result. <P>COPYRIGHT: (C)2008,JPO&INPIT | ||||||
| 152 | 筐体のフォームファクタ内に配置される一体型予備電源装置を備えたフライトレコーダ、データレコーダまたは航空機 | JP2014174828 | 2014-08-29 | JP2015006879A | 2015-01-15 | MICHAEL C WINTERHALTER; GLENN C WILSON |
| 【課題】予備電源装置を備え、適用規格でフライトレコーダに予め決められたフォームファクタ内に収まるフライトレコーダを提供する。【解決手段】フライトレコーダ40は、筐体42の一側または角部に形成した切込み43を有する。電子インターフェースが筐体内部に配置され、飛行データ,映像データおよび音データを受取るのに接続される。メモリユニット70が筐体内部に配置される。メモリユニットは不揮発性メモリデバイスを収容する。補助電源装置46は、筐体の切込み内部に物理的に配置され、再充電可能な電池を収容する。クランプ54は、筐体から補助電源装置を取り外せるように、補助電源装置を筐体に固定する。補助電源装置は、電子インターフェースとメモリユニットに動作電圧を提供するのに、筐体に接続する電気的接続部48を有する。補助電源装置と電気的接続部は、筐体のフォームファクタ内に物理的に存在する。【選択図】図3 | ||||||
| 153 | Power backup application to maintain normal flight recorder operation for a specified period of time in case of aircraft power failure or interruption | US09569375 | 2000-05-11 | US06741896B1 | 2004-05-25 | Richard Olzak; Duncan Schofield; Gary Kersten |
| A device and method to provide backup electrical power to a vehicle data acquisition and recording system. The device operates to control its charging state, discharge state, and interval of discharge to ensure reliable operation of the recording system. The method delineates the process by which continuous electrical power can be supplied to the recording system. | ||||||
| 154 | Crash prevention recorder (CPR)/video-flight data recorder (V-FDR)/cockpit-cabin voice recorder for light aircraft with an add-on option for large commercial jets | US09999589 | 2001-11-15 | US20030152145A1 | 2003-08-14 | Kevin Kawakita |
| FIG. 1 shows a light airplane with the installed invention comprising: an Electronic Rear-view Mirror Component (100) in the cockpit usable by the pilot or co-pilot from the adjustment of twin mechanical arms, a Video Local Area Network (V-LAN) Component (3000), several Bug-Eye Sensor Components (2000) for the front-video camera (2004), rear video camera (2008), right video camera (2012), and left video camera (2016), and a Crash Prevention Recorder (CPR) Component (4000). | ||||||
| 155 | 一种行业应用无人驾驶航空器准飞授权系统及方法 | CN202210893202.8 | 2022-07-27 | CN115223403A | 2022-10-21 | 周海方; 刘志慧; 王兴会; 范毕能; 胡伟建 |
| 本发明为一种行业应用无人驾驶航空器准飞授权系统，属于无人机准飞技术领域，包括飞行综合管理平台，飞行综合管理平台通过云端通讯连接飞行器和飞行控制器，还包括身份认证鉴权器，身份认证鉴权器借助USB接口与飞行控制器通讯连接；飞行控制器还包括准飞授权模块，飞行控制器借助准飞授权模块与飞行综合管理平台的数据链路串接，还包括飞行管控记录仪，飞行管控记录仪借助物理接口嵌于飞行器，飞行管控记录仪设置有多种无线通信接口，飞行管控记录仪的电源模块与无人机的电源相连，飞行管控记录仪还与飞行控制器通讯连接。本方案的系统具有成本低，容易部署的特点，且该系统的应用方法具有操作简单，容错率高，不易出现故障，传输效率高的特点。 | ||||||
| 156 | 一种预防飞行器失联的报警系统 | CN201610965428.9 | 2016-11-05 | CN108074418A | 2018-05-25 | 不公告发明人 |
| 本发明公开了一种预防飞行器失联的报警系统，包括飞行数据记录仪、通讯卫星及地面控制终端。飞行数据记录仪内含飞行信息记录器、无线信号发生器及备用电池，飞行信息包括飞行高度、飞行方向、飞行速度及飞行位置等。无线信号发生器与通讯卫星之间按照事先约定的频段发、收信息，可以规定飞行器每隔半小时发送一次信息，也可以规定更短的时间发送。通讯卫星定时将收集到的飞行器信息发送给地面控制终端，从而能够随时掌握飞行器的准确位置，避免失联事故的发生。 | ||||||
| 157 | 机载综合采集器 | CN202110768405.X | 2021-07-07 | CN113658353B | 2023-05-16 | 王小飞; 袁涛; 刘泽坤; 王元鑫; 嵇绍康; 韩继凯 |
| 本发明涉及一种机载综合采集器，该机载综合采集器包括风速检测计，设置在飞行器上，用以对飞行器所在位置的实时风速进行检测，获取实时风速；振动传感器，设置在仪表参数获取装置上，用以检测在飞行过程中获取参数仪表的振动频率；参数记录仪，参数记录仪与参数仪表连接，其内设置有处理单元，分别与风速检测计和振动传感器连接，参数记录仪用以记录经过处理单元处理的参数信息。在进行参数数据采集的过程中，将仪表中参数进行调整，使得参数记录仪记录的数据接近飞行器的实际状态，飞行过程中的风速会影响飞行器周边气流的变化，而气流的变化会影响飞行器的振动频率，参数记录仪所记录的参数是经过调整的参数数据，数据更为准确。 | ||||||
| 158 | 机载综合采集器 | CN202110768405.X | 2021-07-07 | CN113658353A | 2021-11-16 | 王小飞; 袁涛; 刘泽坤; 王元鑫; 嵇绍康; 韩继凯 |
| 本发明涉及一种机载综合采集器，该机载综合采集器包括风速检测计，设置在飞行器上，用以对飞行器所在位置的实时风速进行检测，获取实时风速；振动传感器，设置在仪表参数获取装置上，用以检测在飞行过程中获取参数仪表的振动频率；参数记录仪，参数记录仪与参数仪表连接，其内设置有处理单元，分别与风速检测计和振动传感器连接，参数记录仪用以记录经过处理单元处理的参数信息。在进行参数数据采集的过程中，将仪表中参数进行调整，使得参数记录仪记录的数据接近飞行器的实际状态，飞行过程中的风速会影响飞行器周边气流的变化，而气流的变化会影响飞行器的振动频率，参数记录仪所记录的参数是经过调整的参数数据，数据更为准确。 | ||||||
| 159 | 弹道参数记录装置 | CN201210194540.9 | 2012-06-14 | CN103486917B | 2016-04-27 | 王金生; 邓泰春; 何永峰; 邓轶; 任业军; 宿世春; 李勇; 杨波; 盖希强; 朱少俊; 洛刚; 李辉; 陈光辉; 吴昱; 汪海涛; 邓德志 |
| 本发明公开了一种弹道参数记录装置。该装置主要由磁体基座1、磁体2、磁体密封盖3、记录仪密封盖4、探测器5、记录仪电路板6、灌封料7、记录仪基座8组成。弹丸飞行过程中，记录仪基座8与弹体位置保持相对固定，刚性尾翼带动磁体基座1旋转，磁体2每经过一次探测器，就会出现一次高电平——低电平——高电平的跳变过程，产生的跳变在记录仪电路板6上会记录下来，同时加速度计9开始工作，存储器10实时记录下这一跳变过程在一定时间内出现的次数、加速度。该装置用途广泛，同时记录弹丸飞行时间、弹丸和尾翼相对转速、弹丸飞行过程中的过载参数。 | ||||||
| 160 | 弹道参数记录装置 | CN201210194540.9 | 2012-06-14 | CN103486917A | 2014-01-01 | 王金生; 邓泰春; 何永峰; 邓轶; 任业军; 宿世春; 李勇; 杨波; 盖希强; 朱少俊; 洛刚; 李辉; 陈光辉; 吴昱; 汪海涛; 邓德志 |
| 本发明公开了一种弹道参数记录装置。该装置主要由磁体基座1、磁体2、磁体密封盖3、记录仪密封盖4、探测器5、记录仪电路板6、灌封料7、记录仪基座8组成。弹丸飞行过程中，记录仪基座8与弹体位置保持相对固定，刚性尾翼带动磁体基座1旋转，磁体2每经过一次探测器，就会出现一次高电平—低电平—高电平的跳变过程，产生的跳变在记录仪电路板6上会记录下来，同时加速度计9开始工作，存储器10实时记录下这一跳变过程在一定时间内出现的次数、加速度。该装置用途广泛，同时记录弹丸飞行时间、弹丸和尾翼相对转速、弹丸飞行过程中的过载参数。 | ||||||
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