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序号 专利名 申请号 申请日 公开(公告)号 公开(公告)日 发明人
61 FLIGHT RECORDER US13702850 2011-05-26 US20130208111A1 2013-08-15 Nicholas Kidd; Paul Chamberlain
The present invention describes a flight recorder for an aircraft with an instrument display panel for displaying aircraft status data to a pilot. The flight recorder comprises one or more sensors that monitor one or more flight conditions of the aircraft, a camera unit for providing image data and a data storage unit for storing the aircraft status data and image data from the camera. The flight recorder additionally comprises a control unit for monitoring the flight condition data supplied by the sensors.
62 Flight recorder US37234353 1953-08-04 US2959459A 1960-11-08 RYAN JAMES J
63 Flight track recorder US37369753 1953-08-11 US2916202A 1959-12-08 BEISHLINE ALLEN W
64 Flight recording instrument US40054541 1941-06-30 US2414976A 1947-01-28 REDHED WILLIAM S
65 EINRICHTUNG ZUR BERGUNG EINES FLUGSCHREIBERS PCT/DE2014/100220 2014-07-01 WO2016000670A1 2016-01-07 BERNECKER, Hermann

Die vorliegende Erfindung betrifft eine Einrichtung (1) zur Bergung eines Flugschreibers (3), beinhaltend zumindest ein an Bord eines Fugzeugs mitgeführtes Aufzeichnungsgerät in Form eines Flugdatenschreibers und/oder eines Stimmenrecorders, welches relevante Flug- und Flugzeugparameter während eines Fluges mit einer Zeitachse speichert. Die erfindungsgemäße Einrichtung (1) ist dadurch gekennzeichnet, dass sie eine schwimmfähige Kapsel (2) umfasst, von welcher der Flugschreiber (3) umschlossen ist, wobei mindestens ein Mittel (4) zur Abtrennung der Kapsel (2) vom Flugzeug vorgesehen ist und die Einrichtung (1) eine Sensorik zur Steuerung des mindestens einen Mittels (4) zur Abtrennung der Kapsel (2) aufweist, die zur Auswertung eine so der mehrerer durch den Flugunfall erzeugter Parameter bestimmt ist.

66 FLIGHT DATA RECORDER WIRELESS INTERFACE PCT/US2006/037428 2006-09-26 WO2007041091A1 2007-04-12 FROST, Wendell, A.; DUNCAN, Schofield

Methods and systems for wirelessly offloading data recorded on a flight recorder. In one embodiment, a method of offloading data recorded on a flight recorder includes determining whether to enable a wireless transmitter and wirelessly transmitting previously stored data on the flight recorder via the wireless transmitter according to the determination. In one aspect, wireless transmission is determined by wireless parameters, such as weight on wheels, air speed, ground speed, engine speed, open compartments and sensed forces. Wireless transmission may be performed either manually or automatically.

67 CRASH SURVIVABLE ENCLOSURE FOR FLIGHT RECORDER PCT/US1990004511 1990-08-10 WO1991004921A1 1991-04-18 SUNDSTRAND DATA CONTROL, INC.; GROENEWEGE, Johannes, B.
A crash survivable enclosure (10) includes a flight data recorder or memory device (14) physically supported and protected by a solid synthetic wax filler (46) contained in an inner metal shell (24). A second filler (60) of high efficiency heat insulating material is contained in an outer shell (50) for physically supporting the inner shell (24) and its contents.
68 TRANSIENT RECORDER IN TIME-OF-FLIGHT MASS SPECTROMETER PCT/US1994006892 1994-06-17 WO1995000236A1 1995-01-05 MERIDIAN INSTRUMENTS, INC.; HOLLAND, John, F.; ENKE, Christie, G.; DAVENPORT, Michael, R.; JANOW, Lawrence, W.
An integrating transient recorder (10, 78, 106, 120) 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 (18, 84, 90, 128) 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 (22, 24, 86, 92, 130). The FIFO buffers (22, 24, 86, 92, 130) are read out for each successive transient by a digital signal processor (26, 88, 94) 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 (16, 100) 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.
69 Flight recorder JP11580675 1975-09-25 JPS5239299A 1977-03-26 MURATA KINYA; YAMAZAKI YOSHIHIRO
PURPOSE: To record especially a number of informations from a cockpit at the time of take-off and landing at which accidents occur frequently, by combining a video camera, a video tape recorder and a manual VTR operation switch. COPYRIGHT: (C)1977,JPO&Japio
70 Fault-tolerant solid-state flight recorder EP92305494.4 1992-06-16 EP0528518A3 1993-09-08 Yokote, Timothy Alan; Upton, Eric Lawrence; Enyedy, Arthur Gustav; Stockton, Grant Joseph

A fault-tolerant solid-state flight data recorder providing reliable, high-speed storage of flight data. The flight data recorder employs a distributed, modular architecture in which an array of controller/memory modules is arranged in parallel controller/memory chains and the memory in the individual controller/memory modules is partitioned into submodules. This distributed architecture allows failed controller/memory modules or failed memory submodules to be bypassed, thus providing fault tolerance for both controller and memory functions. The modular architecture allows the number of controller/memory modules to be easily configured to accommodate any required storage size, while the number of parallel controller/memory chains can be configured to accommodate any required data rate.

71 Flight data recorder US14132202 2013-12-18 US09321540B2 2016-04-26 Laurent Barizza; Frederic Aubespin
The invention relates to a flight data recorder. It is equipped with capsules designed to break at determined depths. The capsules release hydraulic tracing elements, generating a luminous streak in the water, when they are broken, so that the searches for the flight data recorders, or black boxes, are made easier.
72 FLIGHT DATA RECORDER US14132202 2013-12-18 US20140177146A1 2014-06-26 Laurent BARIZZA; Frederic AUBESPIN
The invention relates to a flight data recorder. It is equipped with capsules designed to break at determined depths. The capsules release hydraulic tracing elements, generating a luminous streak in the water, when they are broken, so that the searches for the flight data recorders, or black boxes, are made easier.
73 Ejectable flight recorder US11012561 1961-05-15 US3140847A 1964-07-14 AMES JR HENRY P
74 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。
75 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。
76 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。
77 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。
78 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。
79 Flight data recorder JP3187995 1995-01-30 JPH08198197A 1996-08-06 NARUSE OSAMU
PURPOSE: To obtain data of performance evaluation corresponding to various flight modes of an airframe, an engine, etc., in a flight data recorder mounted to obtain data for clarifying the use of accident of an aircraft. CONSTITUTION: On/off information from a flight mode selection switch (mode S) and a flight mode write switch (wright S), both being disposed in a control device 2, is inputted to a signal processing portion 1 where detection information from air frame sensors attached at necessary points of an airframe is converted to a singles as required and then automatically recorded in a recorder 3. By depressing the mode S, high speed sampling rates corresponding to various flight modes are specified. By depressing the write S, flight mode data and data of specific sensor outputs detected at specified high speed sampling rats are recorded in the recording device 3. COPYRIGHT: (C)1996,JPO
80 Flight data recorder JP13697893 1993-05-17 JPH06321195A 1994-11-22 NARUSE OSAMU
PURPOSE: To easily regenerate and collect the recorded data of a flight data recorder loaded to provide a data for analyzing the cause at generating an accident of an aircraft every general flight so as to apply it for the maintenance of airframe and engine. CONSTITUTION: A recorder control part 2 for applying a prescribed signal conversion to the detection information from an airframe sensor 1 mounted on the essential part of an airframe and automatically recording the result in a memory 9 of a special vessel 8 has a memory card writing part 5. A memory card 10 is inserted thereto from the outside, the data of the same content as the data recorded in the memory 9 during a flight is recorded thereon, and the memory card 10 is pulled out after the flight is finished. COPYRIGHT: (C)1994,JPO
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