Spinner axial cross-section may have longer spinner axial distance compared to baseline axial distance of baseline cross-section and spinner aspect ratio greater than baseline aspect ratio of baseline cross-section.


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    Title :

    Crosswind performance aircraft engine spinner


    Contributors:

    Publication date :

    2019-01-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    CROSSWIND PERFORMANCE AIRCRAFT ENGINE SPINNER

    CLARK ADAM WAYNE / CEDAR RICHARD DAVID / RIDDLE DAVID BAKER | European Patent Office | 2017

    Free access

    IMPROVED CROSSWIND PERFORMANCE AIRCRAFT ENGINE SPINNER

    CLARK ADAM WAYNE / CEDAR RICHARD DAVID / RIDDLE DAVID BAKER | European Patent Office | 2019

    Free access

    IMPROVED CROSSWIND PERFORMANCE AIRCRAFT ENGINE SPINNER

    CLARK ADAM WAYNE / CEDAR RICHARD DAVID / RIDDLE DAVID BAKER | European Patent Office | 2018

    Free access

    Aircraft Crosswind Performance

    J. F. O'Gara | NTIS | 1964


    Aircraft crosswind performance

    O'Gara, J.F. | Engineering Index Backfile | 1964