飞行记录仪相关的专利数据

序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
121	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.
122	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.
123	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
124	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.
125	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.
126	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
127	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.
128	EINSATZFAHRZEUG ODER FLUGGERÄT MIT EINER TRÄGERPLATTFORM UND EINEM MAUTKONTROLLGERÄT, MAUTKONTROLLSYSTEM UND VERFAHREN ZUM KONTROLLIEREN EINER MAUTZAHLUNG	PCT/EP2017/061842	2017-05-17	WO2017198710A1	2017-11-23	LEHNING, Michael; SCHIFFER, Lukas; DOHMANN, Bernhard; LEIJSSEN, Marco; REISS, Maik; GRAW, Peter
Die Erfindung betrifft ein Einsatzfahrzeug oder Fluggerät mit einer Trägerplattform und einem Mautkontrollgerät (102) für eine Trägerplattform (100). Das Mautkontrollgerät (102) umfasst eine Sensoreinrichtung (106) zum Erzeugen einer Fahrzeuginformation (110), die ein im Umfeld des Einsatzfahrzeuges oder Fluggeräts befindliches Fahrzeug (200) repräsentiert, sowie ein Steuergerät (108) mit einer Schnittstelle zu einer Mautdatenverarbeitungseinrichtung (112). Das Steuergerät (108) ist ausgebildet, um über die Schnittstelle die Fahrzeuginformation (110) an die Mautdatenverarbeitungseinrichtung (112) zu senden und eine unter Verwendung der Fahrzeuginformation (110) erzeugte Mautzahlungsinformation (114), die eine dem Fahrzeug (200) zugeordnete Mautzahlung repräsentiert, von der Mautdatenverarbeitungseinrichtung (112) zu empfangen. Das Mautkontrollgerät (102) ist an der Trägerplattform (100) angeordnet oder anordenbar und ist von der Trägerplattform (100) abnehmbar.
129	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.
130	飞行数据记录仪	CN201530294609.X	2015-08-07	CN303492811S	2015-12-09	李晓宇; 李星辉
1、本外观设计产品的名称：飞行数据记录仪。2、本外观设计产品的用途：用于无人机飞行数据等记录。3、本外观设计的设计要点：在于该外观设计产品的形状。4、最能表明设计要点的图片或者照片：立体图。
131	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).
132	无人机飞行数据记录仪	CN201630138201.8	2016-04-22	CN303853150S	2016-09-14	张瑜; 李诗杨; 熊杰
1．本外观设计产品的名称：无人机飞行数据记录仪。2．本外观设计产品的用途：本外观设计产品用于记录、存储、发送和统计无人机飞行状态和数据，实现位置监测、高度信息采集、飞行累计时间记录、坠机检测、飞行架次进行记录、飞行预警功能。3．本外观设计产品的设计要点：产品的外形结构。4．最能表明本外观设计设计要点的图片或照片：主视图。
133	无人机飞行数据记录仪	CN201630138193.7	2016-04-22	CN303853148S	2016-09-14	张瑜; 李诗杨; 熊杰
1．本外观设计产品的名称：无人机飞行数据记录仪。2．本外观设计产品的用途：本外观设计产品用于记录、存储、发送和统计无人机飞行状态和数据，实现位置监测、高度信息采集、飞行累计时间记录、坠机检测、飞行架次进行记录、飞行预警功能。3．本外观设计产品的设计要点：产品的外形结构。4．最能表明本外观设计设计要点的图片或照片：主视图。
134	无人机飞行数据记录仪	CN201630138194.1	2016-04-22	CN303853149S	2016-09-14	张瑜; 李诗杨; 熊杰
1．本外观设计产品的名称：无人机飞行数据记录仪。2．本外观设计产品的用途：本外观设计产品用于记录、存储、发送和统计无人机飞行状态和数据，实现位置监测、高度信息采集、飞行累计时间记录、坠机检测、飞行架次进行记录、飞行预警功能。3．本外观设计产品的设计要点：产品的外形结构。4．最能表明本外观设计设计要点的图片或照片：主视图。
135	无人机飞行数据记录仪	CN201630138203.7	2016-04-22	CN303853151S	2016-09-14	张瑜; 李诗杨; 熊杰
1．本外观设计产品的名称：无人机飞行数据记录仪。2．本外观设计产品的用途：本外观设计产品用于记录、存储、发送和统计无人机飞行状态和数据，实现位置监测、高度信息采集、飞行累计时间记录、坠机检测、飞行架次进行记录、飞行预警功能。3．本外观设计产品的设计要点：产品的外形结构。4．最能表明本外观设计设计要点的图片或照片：主视图。
136	无人机飞行数据记录仪	CN201630138195.6	2016-04-22	CN303886106S	2016-10-12	张瑜; 李诗杨; 熊杰
1．本外观设计产品的名称：无人机飞行数据记录仪。2．本外观设计产品的用途：本外观设计产品用于记录、存储、发送和统计无人机飞行状态和数据，实现位置监测、高度信息采集、飞行累计时间记录、坠机检测、飞行架次进行记录、飞行预警功能。3．本外观设计产品的设计要点：产品的外形结构。4．最能表明本外观设计设计要点的图片或照片：主视图。5．省略视图：后视图为不常用视图，故省略。
137	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。
138	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。
139	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。
140	一种分离式记录仪	CN201510513905.3	2015-08-20	CN106469473A	2017-03-01	管鹏; 冯九胜; 仇胜斌
本发明涉及飞行记录仪领域，提供一种在发生飞行事故时对飞行所采数据进行保护的抛放式记录器，通过它所保护的数据，可以对事故原因进行科学、客观的分析。该发明综合了多项幸存方法，防护性能高，可以在各类喷气式飞机上长期使用，可靠性高。所述的分离式记录仪具有腔体结构和翼型结构；记录仪的各个功能模块安装于记录仪的腔体内，保证记录仪的重心靠近迎风面且处在记录仪整体的对称中心线上，各个功能模块包括信标、储能模块、数据管理模块、数据存储单元，所述的分离式记录仪还具有盖板，盖板封闭所述的腔体结构并固定在上表面上，并与上表面整体形成气动外形。

2 3 4 5 6 7 8 9 10 11

IPRDB

热门服务

关于我们

友情链接

联系方式