Aircraft dynamic loads and vibrations resulting from landing impact and from runway and taxiway unevenness are recognized as significant in causing fatigue damage, dynamic stress on the airframe, crew and passenger discomfort, and reduction of the pilot's ability to control the aircraft during ground operations. One potential method for improving operational characteistics of aircraft on the ground is the application of active control technology to the landing gears to reduce ground loads applied to the airframe. An experimental investigation was conducted which simulated the landing dynamics of a light airplane to determine the feasibility and potential of a series hydraulic active control main landing gear. The experiments involved a passive gear and an active control gear. Results of this investigation show that a series hydraulically controlled gear is feasible and that such a gear is very effective in reducing the loads transmitted by the gear to the airframe during ground operations.
Experimental Investigation of Active Loads Control for Aircraft Landing Gear
1982
72 pages
Report
Keine Angabe
Englisch
Active control landing gear for ground loads alleviation
NTRS | 1985
|AIRCRAFT LANDING GEAR CONFIGURATIONS FOR TRANSFERRING LOADS TO FUSELAGE
Europäisches Patentamt | 2023
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