A fitting for attaching the horizontal tail stabilizer of an aircraft, allowing the formation of a lighter component, without a fatigue failure mode and with a significant reduction in the installation time. The fitting comprises: a core piece having a regular thickness, the core piece having a U configuration, according to a plan view, thereby being composed of two lateral areas and a central area located between the lateral areas, at least one central reinforcement having a regular thickness and joined to one side of the central area and comprising a flange located on an inner edge of the core piece, at least two lateral reinforcements having a regular thickness and each lateral reinforcement being joined to one side of a different lateral area and comprising a flange located on the inner edge of the core piece.


    Access

    Download


    Export, share and cite



    Title :

    FITTING FOR ATTACHING THE HORIZONTAL TAIL STABILIZER OF AN AIRCRAFT


    Contributors:

    Publication date :

    2020-02-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / 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



    FITTING FOR ATTACHING THE HORIZONTAL TAIL STABILIZER OF AN AIRCRAFT

    JURADO MEDINA MANUEL | European Patent Office | 2022

    Free access

    FITTING FOR TRIMMING A HORIZONTAL STABILIZER OF AN AIRCRAFT

    AREVALO RODRIGUEZ ELENA | European Patent Office | 2017

    Free access

    STABILIZER ATTACHING STRUCTURE

    MATSUMOTO YOICHI / INAGAKI YUICHI / SUZUKI HIKARU et al. | European Patent Office | 2015

    Free access

    AIRCRAFT HORIZONTAL STABILIZER DESIGN

    LANIGAN BRENDAN P / O'NEIL JOSHUA R | European Patent Office | 2018

    Free access

    AIRCRAFT HORIZONTAL STABILIZER SURFACE

    LLAMAS SANDIN RAUL CARLOS / LUQUE BUZO MIGUEL | European Patent Office | 2018

    Free access