An aircraft parachute system includes an aircraft that has a fuselage, a pair of wings, a tail section and a plurality of engines. A plurality of parachute units is provided and each of the parachute units is coupled to the aircraft. Each of the parachute units is selectively deployed when the aircraft experiences an in-flight emergency such that the plurality of parachute units inhibits the aircraft from crashing. A plurality of balloon units is provided and each of the balloon units is coupled to the aircraft. Each of the balloon units is selectively deployed when the aircraft experiences the in-flight emergency. In this way each of the balloon units floats the aircraft in water when the aircraft lands in water.


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    Title :

    Aircraft Parachute System


    Contributors:

    Publication date :

    2018-06-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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