Jit- Black Box

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    Name:- Jitendra Kumar Sahoo Regd. No. :- 070216120 Branch :- ETE Padmanava College of Engineering, Rourkela.

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    TTHEHE BBLACKLACK BBOXOX

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    INTRODUCTION TO BLACK BOX

    Although they are called "blackboxes," aviation recorders areactually painted bright orange, are a

    group of data collection devicesmounted on the tail of an aircraft.

    Dr. David Warren, a Australian

    aviation scientist proposed a flightrecording device and by 1958 he hadproduced a prototype ARL FlightMemory Unit

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    Data from both the CVR and FDR is stored on

    stacked memory boards inside the crash-survivable memory unit (CSMU)

    The black box is powered by one of two powergenerators that draw their power from the

    plane's engines. One generator is a 28-volt DC

    power source, and the other is a 115-volt, 400-

    hertz (Hz) AC power source

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    TYPICALLY DOUBLE WRAPPED, IN STRONG

    CORROSION-RESISTANT STAINLESS STEEL OR

    TITANIUM,WITH HIGH-TEMPERATUREINSULATION INSIDE

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    GENERATIONS OF DATARECORDER

    First generation - Foil recorder

    Second generation - Tape recorder

    Third generation Solid state recorder

    Components Of Black Box

    CVR - Cockpit Voice Recorder

    FDR Flight Data Recorder

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    A. COCKPITVOICE RECORDERS

    There are several microphones built into

    the cockpit to track the conversation of the

    flight crews.

    These microphones are also designed to

    track any ambient noise in the cockpitsuch as switches being thrown or any

    knocks.

    There may be up to 4 microphones in the

    planes cockpit each connected to CVR.

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    Any sound in the cockpit are picked up by

    these microphones and sent to the CVR, wherethe recordings are digitized and stored.

    The Associated Control Unit in the cockpit

    provides pre amplification to the audio going

    to CVR.

    The positions of 4 microphones are-

    1. Pilots headset

    2. Co-pilot's headset

    3. Headset for 3rd cabin crew4. At the centre of cabin

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    B. FLIGHT DATARECORDER

    The flight data recorder (FDR) is designed to

    record the operating data from the planes

    system.

    There are sensors that are wired from various

    areas on the plane to the flight-data acquisition

    unit, which is wired to the FDR.When a switch is turned on or off, that

    operation is recorded by FDR.

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    FDR Location

    Black boxes are installed in the tail of the plane. The

    entire front of the aircraft acts as a "crush zone" to reduce

    the shock that reaches the recorder. The precise location of the recorders depends on the

    individual plane.

    Sometimes they are located in the ceiling of the galley, in

    the aft cargo hold or in the tail cone that covers the rear

    of the aircraft.

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    FDR LOCATION

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    BUILT TO SURVIVE

    The only device that survive are the Crash

    Survival Memory Unit (CSMU) of the flight datarecorder and cockpit voice recorder

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    CRASH - SURVIVABLE MEMORY UNIT

    The cylindrical compartment on the

    recorder device is engineered to withstand

    extreme heat, violent crashes and tons of

    pressure. In older magnetic-tape recorders,

    the CSMU is inside a rectangular box.

    Using three layers of materials, the CSMU

    in a solid-state black box insulates and

    protects the stack of memory boards that

    store the digitized information.

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    THREE LAYERS OF CRASH - SURVIVABLE

    MEMORY UNIT

    1.Aluminum housing - There is a thin layer of

    aluminum around the stack of memory cards.

    2. High-temperature insulation - This dry-silica

    material is 1 inch (2.54 cm) thick and provideshigh-temperature thermal protection. This is

    what keeps the memory boards safe during post-

    accident fires.

    3. Stainless-steel shell - The high-temperature

    insulation material is contained within a

    stainless-steel cast shell that is about 0.25 inches

    (0.64 cm) thick. Titanium can be used to create

    this outer armor as well.

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    THERE ARE SEVERAL STAGES FOR

    CRASH SURVIVAL SEQUENCE

    Crash impact

    Pin drop

    Static crush

    Fire test

    Deep sea submersion

    Salt water submersion

    Fluid immersion

    After finding the black box, the investigators

    take the recorder to a lab where they can download

    the data from the recorder and attempt to recreate

    the accident.

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    FDR Record Parameters

    prior to September 30, 1969, record six flight

    parameters: altitude; airspeed; heading; vertical

    acceleration; time of day; and the relative time of

    radio transmissions to and from air traffic

    controllers.

    Airplanes certificated after that date were

    required to record a total of 11 parameters,

    adding 5 more to the list.

    Then, it had to record 17 parameters on any

    flight after May 25, 1994. (six additional

    parameters included)

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    FDR Record Parameters

    Currently, there are 88 parameters required as a

    minimum

    a few of the parameters recorded by most FDRs

    - Time - Pressure altitude- Airspeed - Vertical acceleration

    - Magnetic heading - Control-column position

    - Rudder-pedal position- Control-wheel position

    - Horizontal stabilizer - Fuel flow

    - Engine information - Control and actuator

    positions

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    Retrieving Data

    With the data retrieved from the FDR, the Safety

    Board can generate a computer animated video

    reconstruction of the flight.

    The investigator can then visualize the airplane'sattitude, instrument readings, power settings

    and other characteristics of the flight.

    This animation enables the investigating team to

    visualize the last moments of the flight before the

    accident.

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    AFTERA CRASH

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    Locating Black Box

    Underwater Locator Beacon In addition to the paint and reflective tape, black

    boxes are equipped with an underwater locatorbeacon (ULB). If a plane crashes into the water,this beacon sends out an ultrasonic pulse at 37.5

    kilohertz that cannot be heard by human ears butis readily detectable by sonar and acousticallocating equipment. There is a submergencesensoron the side of the beacon that looks like abull's-eye. When water touches this sensor, it

    activates the beacon.

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