The invention relates to the design of aviation aerial refueling adapter equipment, in particular to a device for testing the aerial refueling adapter equipment. The device can carry out tests on corresponding functions and pressure of the aerial refueling adapter equipment in the development stage of the aerial refueling adapter equipment. The test device comprises a ground pressure fueling connector, an aerial refueling connector, an oil source pressure fueling header pipe, a first pressure sensor and a second pressure sensor, wherein the ground pressure fueling connector and the aerial refueling connector are connected to an inlet and an outlet of the aerial refueling adapter equipment respectively, the oil source pressure fueling header pipe is connected with the ground pressure fueling connector through a fueling pipeline, an oil outlet of the aerial refueling connector is communicated to an oil inlet of an oil tank through an oil return pipeline, the first pressure sensor is arranged on an oil inlet of the ground pressure fueling connector, and the second pressure sensor is arranged on an oil outlet of the aerial refueling connector. The device for testing the aerial refueling adapter equipment is simple in structure, complete in function, capable of carrying out function tests and pressure tests and convenient to operate and greatly saves manpower resources and labor needed by the tests, and test data are accurate.


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    Titel :

    Device for testing aerial refueling adapter equipment


    Beteiligte:
    ZHAO WEI (Autor:in) / ZHANG SHENG (Autor:in)

    Erscheinungsdatum :

    25.11.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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