An aircraft engine 1, for mounting on an aircraft wing, comprises a fan or propeller 7 attached to an axial shaft 3. The fan or propeller comprises a plurality of blades 16 arranged around the shaft of which at least one has an internal channel. The axial shaft has an internal channel formed therein that extends from an opening 15 at a front end towards, and in communication with, the channel in the blade(s). The opening can be selectively opened and closed so that air is received into the shaft channel when open and is diverted through the internal channel of the blade(s) and exhausted through a further opening. The channelled air is used for blowing over the surface of an aircraft wing to enhance lift at lower airspeeds.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft engine and wing assembly


    Beteiligte:

    Erscheinungsdatum :

    2016-01-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft having an engine wing assembly

    MONDAL BHASKAR NANDA / NAMADEVAN ARVIND / JAYARAMAN SHANKAR et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT HAVING AN ENGINE WING ASSEMBLY

    MONDAL BHASKAR NANDA / NAMADEVAN ARVIND / JAYARAMAN SHANKAR et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT ENGINE PYLON TO WING MOUNTING ASSEMBLY

    DA SILVA JULIO ANTONIO BELTRAMI / FERREIRA CLOVIS AUGUSTO EÇA / MONTORO WANDERLEY et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft engine pylon to wing mounting assembly

    CASTELLI ALBERTO DEI / FERREIRA CLOVIS AUGUSTO EÇA / MONTORO WANDERLEY et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    AIRCRAFT ENGINE PYLON TO WING MOUNTING ASSEMBLY

    CASTELLI ALBERTO DEI / FERREIRA CLOVIS AUGUSTO EÇA / MONTORO WANDERLEY et al. | Europäisches Patentamt | 2017

    Freier Zugriff