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.
Crosswind performance aircraft engine spinner
01.01.2019
Patent
Elektronische Ressource
Englisch
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
IMPROVED CROSSWIND PERFORMANCE AIRCRAFT ENGINE SPINNER
Europäisches Patentamt | 2019
|IMPROVED CROSSWIND PERFORMANCE AIRCRAFT ENGINE SPINNER
Europäisches Patentamt | 2018
|Aircraft Crosswind Performance
NTIS | 1964
|Aircraft crosswind performance
Engineering Index Backfile | 1964
|