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M11c19⚡️
20問 • 2ヶ月前
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  • 通報

    問題一覧

  • 1

    The bandwidth of avionics full duplex switched Ethernet (AFDX) can be up to

    100Mbps

  • 2

    A single Core Processing Input / Output Module (CPIOM) within an Integrated Modular Avionics ( IMA) system hosts

    several avionics applications

  • 3

    In an IMA system, the purpose of an Input / Output Module (IOM) is to

    convert the aircraft system data sent and received by line replaceable units (LRUs) directly connected to them from non-AFDX into AFDX format and vice versa

  • 4

    The Avionics Data Communication Network (ADCN) in an Integrated Modular Avionics(IMA) system uses what communication technology is

    AFDX

  • 5

    A virtual link in an ADCN system is

    a predefined path between two ADCN subscribers

  • 6

    Integrated modular avionics (IMA) technology

    can be combined with older federated type technology on the same aircraft with the use of additional hardware and interfaces to allow the two technologies to communicate

  • 7

    AFDX Ethernet is defined as

    full duplex

  • 8

    The deterministic aspect of AFDX is provided for by the use of

    virtual links

  • 9

    The advantages of using AFDX is

    weight savings

  • 10

    The central feature of an AFDX network is

    its virtual links (VL)

  • 11

    IOM has

    1 CPU

  • 12

    General processor modules (GPMs) each contain

    2 micro- processors for redundant operation

  • 13

    Virtual links are

    unidirectional logic path

  • 14

    The media access control (MAC) address is a unique has

    6-byte

  • 15

    Airbus use the term core processing input/output module CPIOM-B is used to

    air conditioning applications

  • 16

    Airbus use the term

    core processing input/output module CPIOM

  • 17

    A power supply hardware boards of housing module airbus is

    28 VDC

  • 18

    The core processing input /output modules CPIOM-A computers host the

    pneumatic and optional air conditioning applications

  • 19

    Avionics full duplex switched Ethernet (AFDX) virtual link

    has a unique sender and one or more receivers, always follows the frozen route on the network

  • 20

    The General Processor Modules GPM hardware is designed to be ‘fail passive’. This ensures that

    Undetected fault sequences

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    問題一覧

  • 1

    The bandwidth of avionics full duplex switched Ethernet (AFDX) can be up to

    100Mbps

  • 2

    A single Core Processing Input / Output Module (CPIOM) within an Integrated Modular Avionics ( IMA) system hosts

    several avionics applications

  • 3

    In an IMA system, the purpose of an Input / Output Module (IOM) is to

    convert the aircraft system data sent and received by line replaceable units (LRUs) directly connected to them from non-AFDX into AFDX format and vice versa

  • 4

    The Avionics Data Communication Network (ADCN) in an Integrated Modular Avionics(IMA) system uses what communication technology is

    AFDX

  • 5

    A virtual link in an ADCN system is

    a predefined path between two ADCN subscribers

  • 6

    Integrated modular avionics (IMA) technology

    can be combined with older federated type technology on the same aircraft with the use of additional hardware and interfaces to allow the two technologies to communicate

  • 7

    AFDX Ethernet is defined as

    full duplex

  • 8

    The deterministic aspect of AFDX is provided for by the use of

    virtual links

  • 9

    The advantages of using AFDX is

    weight savings

  • 10

    The central feature of an AFDX network is

    its virtual links (VL)

  • 11

    IOM has

    1 CPU

  • 12

    General processor modules (GPMs) each contain

    2 micro- processors for redundant operation

  • 13

    Virtual links are

    unidirectional logic path

  • 14

    The media access control (MAC) address is a unique has

    6-byte

  • 15

    Airbus use the term core processing input/output module CPIOM-B is used to

    air conditioning applications

  • 16

    Airbus use the term

    core processing input/output module CPIOM

  • 17

    A power supply hardware boards of housing module airbus is

    28 VDC

  • 18

    The core processing input /output modules CPIOM-A computers host the

    pneumatic and optional air conditioning applications

  • 19

    Avionics full duplex switched Ethernet (AFDX) virtual link

    has a unique sender and one or more receivers, always follows the frozen route on the network

  • 20

    The General Processor Modules GPM hardware is designed to be ‘fail passive’. This ensures that

    Undetected fault sequences