| 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 | CRASH SURVIVABLE ENCLOSURE FOR FLIGHT RECORDER | EP90914461 | 1990-08-10 | EP0445270A4 | 1992-10-21 | GROENEWEGE, JOHANNES, B. |
| 102 | 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. | ||||||
| 103 | 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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| 104 | Recording method in flight recorder | JP8434796 | 1996-04-05 | JPH09282863A | 1997-10-31 | KAWAMURA MASANORI |
| PROBLEM TO BE SOLVED: To minimize loss of recording capacity to effectively use a memory by inspecting failure of a flash memory in unit of an erasing block before recording of data. SOLUTION: A memory management means 1 administrates a flash memory 2 for each erasing block and sequentially records data toward the end portion from the leading portion of the erasing block. In this case, the management means 1 inspects whether the erasing block at the destination to store the data is defective or not. When the relevant erasing block is normal, data is recorded in this block but if it is defective, the next erasing block as the destination is inspected whether it is defective or not. When it is normal, the recording process is continued. COPYRIGHT: (C)1997,JPO | ||||||
| 105 | Flight recorder emitting device | JP30459391 | 1991-11-20 | JPH05139388A | 1993-06-08 | KAWASE MAMORU |
| PURPOSE: To easily collect a flight recorder even in a state where an airframe sinks beneath the waves. CONSTITUTION: The memory section 10 of a flight recorder is accommodated in a case 9. The memory section 10 is held in the case 9 by an electromagnet 16 supplied with electric power from a power source inside an airframe and a clamp 17. The clamp 17 is locked on the hook-shaped part of an acceleration detector 21, and released by giving abnormal acceleration. The memory section 10 is energized so as to be emitted outside the case 9 by a spring 18 against force to hold the memory section 10 through the electromagnet 16 and the clamp 17. The memory section 10 is emitted outside by the spring 18 in the case where the supply of electric power from the power source inside the airframe is stopped, and the abnormal acceleration is given. COPYRIGHT: (C)1993,JPO&Japio | ||||||
| 106 | Flying head helical scanning magnetic recorder reproducer | JP10434576 | 1976-09-02 | JPS5230411A | 1977-03-08 | SUTEFUAN EMU BOOGERU |
| 107 | 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. |
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| 108 | FLIGHT RECORDER WITH REDUNDANT EJECTABLE FLIGHT DATA MEMORY MODULES | US15106076 | 2014-12-05 | US20160318616A1 | 2016-11-03 | HARALD FISCHER |
| A flight data memory module (1) has a data memory device (2) for storing data, a data receiver device (3, 4) for receiving the data and a sheath (8) enclosing the data memory device (2). The sheath (8) has a spherical, ellipsoid, ovoid and/or rounded convex wall. A flight data memory device (11) has a plurality of flight data memory modules (1), a receptacle for arranging the plurality of flight data memory modules (1) in and/or on an aircraft and an ejector device (12) for mechanically ejecting the flight data memory modules (1). A flight data storage system (10) has a flight data memory device (11), a data-collecting device (16) for collecting data in a flight data system (17) and a data-transmitting device (15) for transmitting the data collected by the data-collecting device (16) to at least one of the flight data memory modules (1). | ||||||
| 109 | Flight crash survivable storage unit with boiler for flight recorder memory | US317687 | 1994-10-05 | US5750925A | 1998-05-12 | 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) a thermal insulator located within the inner cavity defining at least a portion of a second interior cavity, with the at least one heat sensitive item being located within the second interior cavity; and (c) a boiler located within the second interior cavity including at least one containment compartment for containing a thermal mass and at least one protective compartment within which the at least one heat sensitive item is located. 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 a boiler per se for use in a FCSSU of the type contemplated by the invention. | ||||||
| 110 | Automatically ejecting flight data recorder | US12764374 | 2010-04-21 | US08493715B1 | 2013-07-23 | Marc T. Angelucci |
| An apparatus for holding a flight data recorder in an aircraft includes a housing that defines a compartment enclosing the flight data recorder and a flotation device attached to the flight data recorder. If the aircraft crashes into a body of water and become submerged, one or more releasable fasteners holding the compartment's cover in place are triggered thereby removing the cover over an opening in the compartment and ejecting the flotation device and the flight data recorder out of the compartment. The floatation device then floats the flight data recorder to the surface of the water where it can be located by the rescuers. | ||||||
| 111 | 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). | ||||||
| 112 | 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. | ||||||
| 113 | 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. | ||||||
| 114 | Automatically ejecting flight data recorder | US12868867 | 2010-08-26 | US08670879B1 | 2014-03-11 | Marc T. Angelucci |
| An apparatus for holding a flight data recorder in an aircraft includes a housing that defines a compartment enclosing the flight data recorder and a flotation device encapsulating the flight data recorder. If the aircraft crashes into a body of water and become submerged, one or more releasable fasteners holding the compartment's cover in place are triggered thereby removing the cover over an opening in the compartment and ejecting the flotation device and the flight data recorder out of the compartment. The floatation device then floats the flight data recorder to the surface of the water where it can be located by the rescuers. | ||||||
| 115 | SYSTEMS AND METHODS FOR PROTECTING A FLIGHT RECORDER | US13552275 | 2012-07-18 | US20140022722A1 | 2014-01-23 | 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. | ||||||
| 116 | Ejection Device for a Flight Data Recorder | US13805270 | 2011-06-16 | US20130092795A1 | 2013-04-18 | Reinhold Grewe; Stefan Feierabend |
| An ejection device for a flight data recorder includes an ejection spindle, which can be detachably connected to the flight data recorder by means of a bayonet coupling. The bayonet coupling can be released by means of force application by the ejection spindle, a disengaging device, which has a compression-resistant housing and into which the ejection spindle can be screwed, and a gas pressure generator, a valve, which is located within the disengaging device and which permits a flow connection between the outlet of the gas pressure generator and the ejection spindle when the ejection spindle is screwed in and which disables the flow connection between the outlet of the gas pressure generator and the ejection spindle when the ejection spindle is unscrewed. | ||||||
| 117 | Application Software Flight Recorder Tester Client | US11685592 | 2007-03-13 | US20080229283A1 | 2008-09-18 | Steve Nelson |
| Apparatus for testing a first software application, the apparatus having corresponding methods and computer-readable media, comprises a processor to execute the first software application and a second software application concurrently; a user interface circuit to receive first signals representing actions of a tester of the first software application; and a display circuit to generate second signals representing a display produced in accordance with the first software application; wherein the second software application collects first and second data representing the first and second signals, respectively, during a test interval of execution of the first software application; and wherein a motion picture is generated comprising a synchronized representation of the first and second data. | ||||||
| 118 | Kernel-mode in-flight recorder tracing mechanism | US11069786 | 2005-03-01 | US20060200701A1 | 2006-09-07 | Robin Callender |
| The subject invention relates to systems and methods that automatically monitor and record component-related activities to support remote diagnostic capabilities. In one aspect, an automated computer diagnostic system is provided. The system includes a trace component that monitors computer-related activities between a driver and an operating system component. The trace component can be embedded within the driver or coupled thereto but, generally records activities relating to a given driver in contrast to generically for the entire operating system. A log records the computer-related activities to facilitate problem diagnosis with respect to the driver or the operating system component. | ||||||
| 119 | 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). | ||||||
| 120 | Flight recorders with static electronics memory | US706766 | 1991-05-29 | US5508922A | 1996-04-16 | 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. | ||||||
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