| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 341 | 車載用カメラモジュール | PCT/JP2008/069639 | 2008-10-29 | WO2010050012A1 | 2010-05-06 | 瀬戸 秀行; 梅田 英敏; 中田 圭俊 |
車の走行状況と運転手の状況とから運転手の居眠りやよそ見などを検知し、危険を知らせたり、前の車との車間距離や道に飛び出してくる物体を検知して危険がある場合は知らせたり、ドライブレコーダとして機能し、事故の際に運転手の状況、車の状況、道路状況などの撮像結果を証拠として使うことができ、かつ、複雑な画像処理を必要とせずに車の前方と車内の両方の撮像を可能とした、車載用カメラモジュールをコストを抑えながら提供することが課題であり、撮像素子と、その撮像素子に車内の映像を結像させる車内撮像用光学系と、前記撮像素子に車前方の車外映像を結像させる反射鏡を含んだ車外撮像用光学系とで構成され、車内に設けられて車内及び車外とを監視するようにした。 |
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| 342 | SMART AVIONICS SYSTEM | US14641299 | 2015-03-06 | US20160176538A1 | 2016-06-23 | Joseph Bekanich |
| An aircraft communication network comprises: avionics monitoring software in communication with aircraft avionics, the aircraft avionics including a flight data recorder and an emergency location transmitter; the avionics monitoring software functioning to acquire real-time aircraft operating parameters from the flight data recorder; the avionics monitoring software further functioning to activate the emergency location transmitter upon detection of an anomaly in the aircraft operating parameters, a processor/compiler in communication with the avionics monitoring software; and a transmitter in communication with the processor/compiler, the processor/compiler functioning to transmit real-time data obtained from the aircraft flight data recorder to the transmitter for transmission to ground-based facilities. | ||||||
| 343 | 综合数据显控记录仪 | CN202230106367.7 | 2022-03-03 | CN307316312S | 2022-05-06 | 陕桥梁; 李强 |
| 1.本外观设计产品的名称：综合数据显控记录仪。 2.本外观设计产品的用途：本外观产品用于航空飞行器上记录数据和显示数据参数。 3.本外观设计产品的设计要点：在于形状。 4.最能表明设计要点的图片或照片：立体图。 | ||||||
| 344 | Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system | US13507470 | 2012-06-28 | US08412434B2 | 2013-04-02 | Zolán Iván Radó |
| This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making. | ||||||
| 345 | Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system. | US12927393 | 2010-11-12 | US20110077833A1 | 2011-03-31 | Zoltan Ivan Rado |
| This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making. | ||||||
| 346 | Method And Device Of Calculating Aircraft Braking Friction And Other Relating Landing Performance Parameters Based On The Data Received From Aircraft's On Board Flight Data Management System | US13694866 | 2013-01-11 | US20130138292A1 | 2013-05-30 | Zoltan Ivan Rado |
| This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making. | ||||||
| 347 | Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system | US12802065 | 2010-05-28 | US08121771B2 | 2012-02-21 | Zolta'n Iva'n Rado' |
| This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making. | ||||||
| 348 | Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system | US12802101 | 2010-05-28 | US08050840B2 | 2011-11-01 | Zoltán Iván Radó |
| This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making. | ||||||
| 349 | Method and device of calculating aircraft braking friction and other relating landing performance parameters based on the data received from aircraft's on board flight data management system | US12802065 | 2010-05-28 | US20100299038A1 | 2010-11-25 | Zoltan Ivan Rado |
| This invention relates to a method and apparatus for the calculation of aircraft braking friction and other relating landing parameters, including but not limited to aircraft braking action, aircraft takeoff distance, aircraft landing distance, runway surface conditions and runway surface friction based on the data collected by and available in the aircraft Flight Data Recorder (FDR) or other flight data management system, for example, the Quick Access Recorder (QAR), to provide all involved personnel in the ground operations of an airport and airline operations, including but not limited to aircraft pilots, airline operation officers and airline managers as well as airport operators, managers and maintenance crews, with the most accurate and most recent information on the true aircraft landing performance parameters to help better and more accurate safety and economical decision making. | ||||||
| 350 | Methods for timing pigeon races | EP82200491.7 | 1982-04-23 | EP0064787A2 | 1982-11-17 | De Oude, Johannes |
The conventional, mechanically operated pigeon recorder is replaced by an electronic recorder of small size and light weight, if any including a memory and display, and cooperating with a specific data-carrier, taken along by the pigeon during its transport to the competition starting point and on its home flight and bearing - whether or not in code - a competition number, which after the flight, is put into the recorder and produces a time signal, in which the sensing and/or recording of the data-carrier may be done visually, magnetically, optically and/or electrically, whereby means are provided allowing to have the time registration done by the homing pigeons themselves. |
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| 351 | Method and device for flight supplying test of optical fiber | JP14011490 | 1990-05-31 | JPH0323407A | 1991-01-31 | DEII KEE SHIYOTSUTAA; JII AARU RETSUDOFUOODO |
| PURPOSE: To realize supplying test for a high-speed optical fiber by providing a winding frame to be fixed to an aircraft, maintaining the coil of the optical fiber and a parachute to thrown out in the middle of a flight. CONSTITUTION: The fiber 14 is coiled around a block 22 and fixed to a transmitter inside a tube 20. A pod 12 is fixed to the aircraft, and a canister 20 with the parachute 18 is discharged from the tip of the pod, when the speed and the altitude of the aircraft reaches a prescribed value. A circuit 81 inputs directly from load cells 36, 37 and 50 to a recording meter 80 through a transmitter 55 and a receiver 78, a rotary counter 40, a microphone 84, which are fixed to the parachute tube 20, and a thermistor 86 fixed to the pod 12. Thereby critical engineering data concerning the optical characteristics of the fiber in the middle of supplying is obtained as a precise simulation of an actual flight. COPYRIGHT: (C)1991,JPO | ||||||
| 352 | Airborne microwave path modeling system | US679082 | 1976-04-21 | US4050067A | 1977-09-20 | Ethelbert P. Elmore, Jr. |
| An airborne geophysical measurement and recording system and apparatus in which radar signals are focused onto terrain below an aircraft flying in a straight line between microwave tower sites. The echo signals are detected and signals produced and recorded on a strip chart recorder indicating path profile and terrain reflectivity. In addition, atmospheric pressure, temperature and humidity data are recorded as functions of aircraft altitude, so that atmospheric refractivity gradients can be calculated, either by an on-board computer or later, and this factor taken into account during path design or performance simulation. | ||||||
| 353 | Wireless transducer data capture and retrieval system for aircraft | US745536 | 1996-11-12 | US6009356A | 1999-12-28 | David A. Monroe |
| A wireless safety and surveillance recorder system for aircraft incorporates a plurality of strategically spaced wireless sensors for monitoring critical components and operational characteristics of the aircraft. The captured data and a wireless image are transmitted to a monitor in the cockpit and recorded on a "black box" flight recorder, and may be transmitted to ground control stations for real time or near real time surveillance. The system may include a second recorder for providing redundancy and may include redundant sensors. | ||||||
| 354 | System and method for providing virtual machine diagnostic information using a flight recorder functionality | US13456028 | 2012-04-25 | US08924789B2 | 2014-12-30 | 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. | ||||||
| 355 | Image recording method | JP2000321833 | 2000-09-18 | JP2002087393A | 2002-03-27 | MORIYA TADASHI |
| PROBLEM TO BE SOLVED: To solve the problem on a conventional voice recorder or a flight data recorder mounted in an aircraft for searching the causes of accidents, where the voices of occupants, interior sounds or electric signals picked out of structures including mountings in the aircraft are recorded but images are not recorded, that it is insufficient for searching the causes of accidents and it is also sufficient for usually inspecting troubles in flight and serving additional roles. SOLUTION: This image recording method comprises processing image data in the aircraft photographed by a camera installed in the aircraft for at certain time intervals with data compressed by a signal converter and reserving the image data in various data recorders to be taken, reproduced and displayed as required. COPYRIGHT: (C)2002,JPO | ||||||
| 356 | Image recorder | JP842192 | 1992-01-21 | JPH05197312A | 1993-08-06 | YASUTOMI HIDEO |
| PURPOSE:To provide the image recorder which is small in size, light in weight, low in cost and where a good quality image can be obtained. CONSTITUTION:Powder toner 5 inside a casing 12 is carried to a part facing an opening 13 on a surface of a photoconductive member 1 by utilizing electric field curtain force based on non-uniform alternating electric field generated by an electric field curtain forming electrode 15. This powder toner 5 flys from the surface of the photoconductive member 1 by having the photoconductive member 1 exposed by an optical writing head 17 based on image signals, and then they are attracted to the surface of recording paper 8 by an electrostatic field generated by an attracting bias platen 19. | ||||||
| 357 | DIGITAL RECORDING AND REPLAY SYSTEM FOR AN AIRCRAFT AND METHOD FOR REPRODUCTION OF ONBOARD INSTRUMENTATION OF AN AIRCRAFT | US14468747 | 2014-08-26 | US20150051791A1 | 2015-02-19 | Daniel O'Connor; Bruno Cervia; Robert Milns; Paul Gibson |
| Digital recording and replay system for an aircraft, comprising a Mission Computer with an Operational Flight Program for generating instrument data for onboard instruments of the aircraft; a Mission Data Recorder connected to said Mission Computer for recording said instrument data; and a Mission Debriefing System; wherein the Mission Debriefing System is configured to reproduce the onboard instruments of the aircraft based on instrument data retrieved from the Mission Data Recorder. Method for reproduction of onboard instrumentation of an aircraft, comprising the steps of connecting a Mission Data Recorder to a Mission Computer of an aircraft having an Operational Flight Program for generating instrument data for onboard instruments; recording instrument data; providing a Mission Debrief System and causing it to reproduce the onboard instruments of the aircraft based on instrument data retrieved from the Mission Data Recorder. | ||||||
| 358 | Infeed system for lumber | US773694 | 1996-12-27 | US5765617A | 1998-06-16 | Cameron Dean Mierau; Aki Juhani Anttila; Richard Ichiro Komori |
| An infeed system that orients a log for a processing unit. A flight conveyor, a log turner and a sharp chain are in an overlapping arraignment. The flight conveyor conveys a log past a scanner which inputs scan data into a computer which determines the profile and orientation on the flight conveyor. The computer determines the desired orientation of the log for the processing unit. The log turner is arranged to rotate and skew the log to the desired orientation. The log is then transferred to the sharp chain conveyor. The overlapping arrangement of the flight conveyor, log turner and sharp chain maintains full control of the log at all times. The sharp chain conveys the log past a second scanner which inputs the scan data to the computer to determine the actual orientation of the log on the sharp chain. The infeed system may also be provided with a shift and lift mechanism for further controlling the log position relative to the processing unit. | ||||||
| 359 | Voice recorder with emergency transmitting function | JP32525595 | 1995-11-21 | JPH09142398A | 1997-06-03 | WATANABE OSAMU; SASAKI SEIJI |
| PROBLEM TO BE SOLVED: To attain early solution of an event by transmitting a condition in an aircraft, when its hijack is generated, to outside the aircraft, made to serve as an aid for determining a means and a change arresting a hijacker. SOLUTION: In this constitution, a voice recorder amplifies outputs of microphones 1, 2, 3 for use of a pilot, copilot and a sound in an aircraft by amplifiers 4, 5, 6 input to a recorder 7 in a particular vessel 8, an emergency transmitter 9 transmitting from an antenna 11 a radio wave of preset emergency channel, with outputs of the amplifiers 4, 5, 6 serving as a modulation wave, is provided, a switch 10, provided in a position not detected by a hijacker, is operated when hijack is generated, so as to wirelessly inform the outside of the aircraft of giving/taking with the hijacker. COPYRIGHT: (C)1997,JPO | ||||||
| 360 | Time-of-flight analyzer | JP2004211558 | 2004-07-20 | JP2006032207A | 2006-02-02 | KAWATO EIZO |
| <P>PROBLEM TO BE SOLVED: To provide a time-of-flight analyzer capable of making timing of an ion generator coincide with that of an ion signal recorder to accurately determine a peak center position even in the case where the number of measurement is small. <P>SOLUTION: This time-of-flight analyzer is provide with the ion generator and the ion signal recorder operating by synchronizing with clocks. A trigger signal synchronizing with the clocks is generated by the ion signal recorder and ions are generated by the ion generator by using the trigger signal. Since timing for accelerating the ions is synchronized with timing for digitally converting a signal of the ions detected by an ion detector by the ion signal recorder to record it, occurrence of a timing error becoming a problem in a conventional technique can be suppressed. <P>COPYRIGHT: (C)2006,JPO&NCIPI | ||||||
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