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
101	Remote aircraft flight recorder and advisory system	US768313	1996-12-17	US5890079A	1999-03-30	Seymour Levine
This invention is a system that monitors many performance parameters and many aircraft operational parameters, and broadcasts this information along with aircraft identification, audio, video, global positioning and altitude data, to a world wide two-way rf network. This information is monitored and recorded at a remote, centralized location. At this location, this information is combined with archived data, ATC data, weather data, topological data, map data, and manufacturers' data. Analysis of this combined data allows identification of problems and generation of advisories. Six types of advisories are generated: maintenance, safety of flight, flight efficiency, flight separation, safe to fly and safe to take off. In the event of a crash the remotely recorded data provides an instant indication of the cause of the crash as well as where the crashed plane can be found. Use of this invention allows replacement of the current, on-board flight data recorders thus saving costs and weight. Having the recorded data at a remote site eliminates the need to search for flight data recorders. Other advantages are back-up for ATC radar position data, better control of aircraft separation, improved flight efficiency, and allowing use of simpler and lower power radar.
102	Flight recorder with static electronic memory	US455812	1989-12-20	US5053967A	1991-10-01	Michel Clavelloux; Maurice Ropert
A flight recorder (MPV) is contained within a two-walled chassis (11, 13), of which the walls are separated by a fire-resistant material (12). The memory means consist of hybrid circuits (H1-H8) of the EEPROM type. These are associated with a control card that may act as a fuse. The hybrid circuits (H1-H8) are mounted so as to be pressure-resistant. The flight parameters are alternating recorded on two memory cards (MC1 and MC2) and also in their hybrid circuits.
103	Systems and methods for protecting a flight recorder	US13552275	2012-07-18	US08723057B2	2014-05-13	David Lowell Miller; Gary Kersten; Wendell A. Frost
Systems and methods for protecting a flight recorder are provided. In certain embodiments, a crash survivable memory unit, comprises a memory device that records flight data; a flexible insulation layer that inhibits thermal energy from conducting from an external side of the flexible insulation layer to an internal side of the flexible insulation layer, wherein the internal side faces the memory device; a microlattice layer abutting the internal side and enclosing the memory device, the microlattice layer configured to distribute thermal energy that passes through the flexible insulation layer substantially throughout the microlattice layer; and a heat absorbing material that impregnates the microlattice layer, the heat absorbing material configured to absorb the thermal energy in the microlattice layer; and an impact resistant layer encircling the flexible insulation layer, wherein the impact resistant layer absorbs shocks that result from other objects contacting the impact resistant layer.
104	Flight crash survivable storage unit with aquarium container for flight recorder memory	US320265	1994-10-11	US5756934A	1998-05-26	Gregory W. Purdom
An enclosure for protecting a heat sensitive item from high temperatures and shock which includes: (a) an outer housing including an inner cavity for containing at least one heat sensitive item; (b) an aquarium located within the inner cavity including at least one protective compartment within which the at least one heat sensitive item is located; (c) a thermal mass, located within the inner cavity and covering at least a portion of the exterior surface of the aquarium; and (d) a venting mechanism for venting any moisture, that penetrates the aquarium and enters the at least one protective compartment included therein, to the ambient air outside the outer housing. The invention finds particular utility in the Flight Recorder field where heat sensitive components, such as solid state memories, may be subject to fire and shock often resulting from an aircraft crash. The invention also features a corrosion protection capability which is effective when the item being protected is in close proximity to a source of moisture. Further aspects of the invention are directed to processes for fabricating enclosures of then type contemplated by the invention (a Flight Crash Survival Storage Unit (FCSSU) in the Flight Recorder context), and to an aquarium per se for use in a FCSSU of the type contemplated by the invention.
105	Wireless supplement and/or substitute for aircraft flight recorders	US10331258	2002-12-30	US07039509B2	2006-05-02	Robert Richard Podowski
A method for preserving information from an airborne aircraft (10) includes receiving an activation signal, and in response thereto, establishing a call from the aircraft (10) to a ground support facility (210) over a wireless telecommunications network (200). Sounds within the aircraft (10) are monitored, and an audio signal reflecting the same is generated. Flight data from the aircraft (10) is obtained and encoded. The audio signal and encoded flight data are multiplexed to generate a combined output signal (300) which is transmitted via the call from the aircraft (10) to the ground support facility (210).
106	Wireless supplement and/or substitute for aircraft flight recorders	US10331258	2002-12-30	US20040128039A1	2004-07-01	Robert Richard Podowski
A method for preserving information from an airborne aircraft (10) includes receiving an activation signal, and in response thereto, establishing a call from the aircraft (10) to a ground support facility (210) over a wireless telecommunications network (200). Sounds within the aircraft (10) are monitored, and an audio signal reflecting the same is generated. Flight data from the aircraft (10) is obtained and encoded. The audio signal and encoded flight data are multiplexed to generate a combined output signal (300) which is transmitted via the call from the aircraft (10) to the ground support facility (210).
107	Flight recorder having capability of storing intermediate data	US453554	1982-12-27	US4510803A	1985-04-16	Thomas E. Perara
A flight recorder (11) for a vehicle such as an airborne vehicle is provided in which various data is recorded, along with on-board time data (from 38) in order to be processed by ground based equipment (13). The on-board time data is synchronized by using a telemetry signal (DT) which is received by a ground based tracking system so that the timing of the events recorded by the flight recorder (11) may be synchronized with the timing of events recorded by the ground based tracking system. This combined data is provided to the ground based equipment (13) in order that the data at (12) obtained on-board the vehicle can be analyzed. By the use of digital techniques, various measurements, such as acceleration and angular rate may be accurately stored and reproduced. This arrangement reduces repeat costs for multiple tests and increases reliability of test data.
108	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.
109	COMPUTER FLIGHT RECORDER WITH ACTIVE ERROR DETECTION	US14158146	2014-01-17	US20150205654A1	2015-07-23	Leon E. Gregg; James L. Tilbury
A method, apparatus and program product utilize a flight recorder having active error detection functionality to proactively detect errors in a computer or a sub-system or component thereof. The active error detection may be based on one or more trends detected in the trace data logged by the flight recorder and reflective of particular types of errors that may be present in a computer during operation, such that an error may be logged, and in some instances, an exception may be triggered.
110	Virtual flight recorder hosted by system tracing facility	US11211951	2005-08-25	US20070050683A1	2007-03-01	John Attinella; Larry Cravens; Michael Denney; Edwin Grazier; Jay Kurtz; David Legler
An apparatus, program product and method utilize 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.
111	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.
112	Method and apparatus for a crash survivable flight data recorder	US11978837	2007-10-30	US20090112381A1	2009-04-30	Daniel J. Schwinn; Steven W. Jacobson; Joseph Weihs
Common practice in the aviation industry is to place a single Flight Data Recorder (FDR) in an aircraft for the purpose of aiding an investigation of an aircraft accident or incident. In contrast, a system employing ‘an example’ embodiment of the invention uses multiple flight data recorders by having a primary node or first FDR, and one or more secondary nodes or one or more additional FDRs configured to store flight data. Each FDR is placed in a different location so as to ensure backup of the recorded and stored data. In this way, the invention system provides redundancy of information for an aircraft accident or incident and more reliable data storage.
113	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.
114	FLIGHT RECORDER HAVING INTEGRAL RESERVE POWER SUPPLY WITHIN FORM FACTOR OF ENCLOSURE AND METHOD THEREFOR	PCT/US2009046815	2009-06-10	WO2009155176A3	2010-03-25	WINTERHALTER MICHAEL C; WILSON GLENN C
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.
115	Self-contained flight data recorder with wireless data retrieval	US09803889	2001-03-13	US06898492B2	2005-05-24	Hilary Laing de Leon; Roland E. Quiros
A flight 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 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.
116	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.
117	FLIGHT RECORDER HAVING INTEGRAL RESERVE POWER SUPPLY WITHIN FORM FACTOR OF ENCLOSURE AND METHOD THEREFOR	PCT/US2009/046815	2009-06-10	WO2009155176A2	2009-12-23	WINTERHALTER, Michael, C.; WILSON, Glenn, C.
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.
118	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.
119	인클로져의 형상 인자 내에 일체형 예비 전력 공급장치를 구비한 비행 기록기 및 이를 위한 방법	KR1020117001296	2009-06-10	KR101626298B1	2016-06-01	윈터홀터마이클씨.; 윌슨그렌씨.
비행기록기는인클로져의일 측부또는코너에형성된절결부를갖는인클로져를포함한다. 전자인터페이스는인클로져내에배치된다. 전자인터페이스는비행데이터, 비디오데이터및 오디오데이터를수신하도록결합된다. 메모리유닛이인클로져내에배치되고데이터를저장하기위해전자인터페이스에전기적으로접속된다. 메모리유닛은비휘발성메모리장치를포함한다. 예비전력공급장치는인클로져의절결부내에물리적으로배치된다. 예비전력공급장치는재충전가능한배터리를포함한다. 클램프가예비전력공급장치를인클로져에고정하여예비전력공급장치가인클로져로부터제거될수 있게한다. 예비전력공급장치는전자인터페이스및 메모리유닛에작동전압을제공하기위해인클로져에결합된전기커넥터를구비한다. 예비전력공급장치및 전기커넥터는물리적으로인클로져의형상인자내에존재한다.
120	인클로져의 형상 인자 내에 일체형 예비 전력 공급장치를 구비한 비행 기록기 및 이를 위한 방법	KR1020117001296	2009-06-10	KR1020110033921A	2011-04-01	윈터홀터마이클씨.; 윌슨그렌씨.
비행 기록기는 인클로져의 일 측부 또는 코너에 형성된 절결부를 갖는 인클로져를 포함한다. 전자 인터페이스는 인클로져 내에 배치된다. 전자 인터페이스는 비행 데이터, 비디오 데이터 및 오디오 데이터를 수신하도록 결합된다. 메모리 유닛이 인클로져 내에 배치되고 데이터를 저장하기 위해 전자 인터페이스에 전기적으로 접속된다. 메모리 유닛은 불휘발성 메모리 장치를 포함한다. 예비 전력 공급장치는 인클로져의 절결부 내에 물리적으로 배치된다. 예비 전력 공급장치는 재충전가능한 배터리를 포함한다. 클램프가 예비 전력 공급장치를 인클로져에 고정하여 예비 전력 공급장치가 인클로져로부터 제거될 수 있게 한다. 예비 전력 공급장치는 전자 인터페이스 및 메모리 유닛에 작동 전압을 제공하기 위해 인클로져에 결합된 전기 커넥터를 구비한다. 예비 전력 공급장치 및 전기 커넥터는 물리적으로 인클로져의 형상 인자 내에 존재한다.

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