A device includes a harness system configured to be attached to a parachute harness of a parachute. The device also includes a propulsion system connected to the harness system, wherein the propulsion system is configured to be off when undeployed and during freefall, and wherein the propulsion system is configured to deploy during canopy flight stage to generate thrust for a parachutist of the parachute. The device further includes a circuitry configured to control power generation by the propulsion system to control the thrust. The device includes a power source configured to power the circuitry and the propulsion system.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    PARACHUTE RANGE AUGMENTER


    Beteiligte:

    Erscheinungsdatum :

    26.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    PARACHUTE RANGE AUGMENTER

    RHEA DAVID MICHAEL / FOX BENJAMIN MICHAEL | Europäisches Patentamt | 2024

    Freier Zugriff

    Augmenter la cadence

    IuD Bahn | 2010



    Jet-Engine Test Cell Augmenter Performance

    C. A. Kodres / G. L. Murphy | AIAA | 1998


    Jet-Engine Test Cell Augmenter Performance

    Kodres, C.A. | Online Contents | 1998