Classifications

• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
  • G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
  • G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
  • G01S1/68—Marker, boundary, call-sign, or like beacons transmitting signals not carrying directional information
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
  • G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
  • G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
  • G01S19/13—Receivers
  • G01S19/14—Receivers specially adapted for specific applications
  • G01S19/17—Emergency applications
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
  • G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
  • G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
  • G01S5/14—Determining absolute distances from a plurality of spaced points of known location
• • G—PHYSICS
  • G08—SIGNALLING
  • G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
  • G08B25/00—Alarm systems in which the location of the alarm condition is signalled to a central station, e.g. fire or police telegraphic systems
  • G08B25/01—Alarm systems in which the location of the alarm condition is signalled to a central station, e.g. fire or police telegraphic systems characterised by the transmission medium
  • G08B25/10—Alarm systems in which the location of the alarm condition is signalled to a central station, e.g. fire or police telegraphic systems characterised by the transmission medium using wireless transmission systems
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B64—AIRCRAFT; AVIATION; COSMONAUTICS
  • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
  • B64D45/00—Aircraft indicators or protectors not otherwise provided for
  • B64D2045/0065—Black boxes, devices automatically broadcasting distress signals

Definitions

• the present invention relates to a method and a device for remotely collecting data from aircraft or ship recorders.
• the field of the invention is therefore that of the safety of air or sea transport.
• the invention relates to an ejection buoy from an aircraft or a ship when the latter is in distress.
• VDR voyage Data Recorder
• the invention thus relates to the remote collection of data from recorders of aircraft, ships or submarines inhabited or not.
• the object of the invention is to enable a reconnaissance aircraft, in a single flight, to bring back the data of the recorders as well as the precise coordinates of the point of sinking while driving in parallel and without interruption the search visual floating debris drifting.
• the collection of data requires the recovery of the recorder at the sea surface, either by a ship sent to the area or by helicopter using, for example, a device such as that described in US Patent 5,086,998.
• This operation can not be conducted by a fixed-wing aircraft such as an aircraft of recognition that alone has the radius of action allowing it to reach any area of the ocean.
• US Pat. No. 4,981,453 describes a warning buoy and a guide for rescue means. It does not include a data storage device and therefore does not allow the remote collection of data from recorders.
• the present invention therefore has the main purpose of solving the difficulties presented by the methods and devices of the prior art by proposing a method and a device for remote data collection of aircraft or ship recorders.
• the invention proposes a device for remotely collecting data from aircraft or ship recorders, characterized in that it comprises an ejection buoy equipped with a bidirectional radio channel making it possible to ensure digital data exchanges with a remote data collection means, this buoy being provided with a satellite location receiver and a local memory in which its successive positions are stored during its drift to the surface of the sea, said buoy further comprising a memory in which are stored, prior to its ejection, information such as those stored in flight recorders for aircraft, or travel for ships, said buoy also comprising a power source and a device onboard electronic sound activation.
• the method of remotely collecting data from aircraft or ship recorders according to the invention is remarkable in that it comprises the following steps:
• FIG 1 is an overview of the device according to the invention.
• FIG. 2 represents a functional block diagram of the subsets of the ejection buoy.
• Figure 3 shows a block diagram of the remote data collection equipment.
• FIG. 1 shows an overview of the device.
• An aircraft 1 is damaged on the seabed. Near the point of impact 2 of said aircraft with the surface of the water is illustrated a buoy 3 drifting surface after its ejection of the aircraft. Its position 4 at the time of the radio session with the remote means is representative of its drift after its ejection.
• the geolocation satellites 5 allow the buoy to record at regular time intervals, its drift 6.
• different means of communication with the buoy 4 at a distance such as a maritime patrol aircraft 7, a communication satellite 8 and its control station installed on land 9 or on a ship 10.
• the reference 1 1 designates a satellite dedicated to the location of distress transmitters forming part of an international network such as the COSPAS-SARSAT system.
• the remote data collection means may also be constituted by a fixed or rotary wing aircraft, a communication satellite, a periscopic immersion submarine.
• FIG. 2 which represents a functional block diagram of the subsets of the ejection buoy, is represented a source of electrical energy such as a battery, a central unit constituted by a microprocessor, a device for energizing the internal electronic buoy at the end of the ejection.
• This activation device 22 may consist of electrodes detecting contact with seawater or an activated contactor during ejection.
• a first memory 23 nonvolatile information is recorded which is characteristic of the flight or journey, received via an interface 24 inside the buoy and a communication electronics 25 provided, if necessary, with an external device for encrypting the data. .
• the data from a satellite location receiver 27 passes through the microprocessor 21 to a second memory 28 where the drift of the buoy is stored since its ejection, if necessary in encrypted form using the internal circuit 32.
• radio transmitter 29 serves to communicate with the remote means of data collection. On receipt of orders, it securely transmits the contents of the memories 23 and 28.
• the buoy may be provided with a distress transmitter 30 set on the international frequencies of a distress transmitter locating device, facilitating thus its detection and identification very quickly from a center on the ground.
• a flash lamp 31 may be activated at dusk for a visual location of the buoy by an overhead or surface means such as a ship.
• a test interface 33 is used to verify in the workshop or in flight the proper operation of the electronics inside the buoy.
• the various components mentioned are integrated into a shockproof sealed enclosure 36 providing buoyancy by buoyancy.
• An optional remote controlled device 34 makes it possible to scuttle the buoy once the contents of its memories have been transferred remotely.
• FIG. 3 shows a block diagram of the remote data collection equipment. It comprises a computer 40, powered by a source of electrical energy 41, which communicates via a radio transmitter 42, with the buoy. The communications being direct or relayed if necessary by one or more satellites 8. The data relating to the trajectory of the buoy during its drift and flight information or travel are, if necessary after decryption by an encryption device 44, are transferred on a mass storage medium 43 removable or not.
• a GPS receiver 45 can be used by the remote information gathering means when last is an aircraft or a ship to join the shortest buoy.
• the collecting means is, prior to the establishment of bidirectional communication with the buoy, guided near the search area from information transmitted to the ground, by the aircraft or the aircraft. ship in distress before it sank.
• a reconnaissance aircraft may, in a single flight:
• the buoy does not make spontaneous emissions. As a result, it can not be located by an undesirable third party who, after having retrieved it, will subtract the content from those for whom it is intended.
• the data stored in the memories 23 and 28 can be encrypted using the device inside the buoy 32 or external 26, the recovery of the buoy by a third party does not allow it to operate unauthorized.

Landscapes

• Engineering & Computer Science (AREA)
• Radar, Positioning & Navigation (AREA)
• Remote Sensing (AREA)
• Physics & Mathematics (AREA)
• General Physics & Mathematics (AREA)
• Computer Networks & Wireless Communication (AREA)
• Business, Economics & Management (AREA)
• Emergency Management (AREA)
• Position Fixing By Use Of Radio Waves (AREA)
• Arrangements For Transmission Of Measured Signals (AREA)
• Recording Measured Values (AREA)
• Mobile Radio Communication Systems (AREA)
• Traffic Control Systems (AREA)

Applications Claiming Priority (2)

Publications (1)

Family

ID=42320178

Family Applications (1)

Country Status (10)

Cited By (1)

Families Citing this family (30)

Family Cites Families (16)

• 2009
  • 2009-11-13 FR FR0905456A patent/FR2952747B1/fr active Active
• 2010
  • 2010-11-12 CN CN2010800592930A patent/CN102713660A/zh active Pending
  • 2010-11-12 RU RU2012123978/07A patent/RU2012123978A/ru not_active Application Discontinuation
  • 2010-11-12 BR BR112012011192A patent/BR112012011192A2/pt not_active IP Right Cessation
  • 2010-11-12 WO PCT/FR2010/052418 patent/WO2011058281A1/fr active Application Filing
  • 2010-11-12 CA CA2780836A patent/CA2780836A1/fr not_active Abandoned
  • 2010-11-12 KR KR1020127015215A patent/KR20120101067A/ko not_active Application Discontinuation
  • 2010-11-12 JP JP2012538388A patent/JP2013510762A/ja active Pending
  • 2010-11-12 US US13/509,326 patent/US8509998B2/en not_active Expired - Fee Related
  • 2010-11-12 EP EP10792993A patent/EP2499510A1/fr not_active Withdrawn

Non-Patent Citations (1)

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