Aircraft landing gear with electromagnetic damper

The article describes the design and computation of the aircraft landing gear with an electromagnetic-gas shock absorber. A numerical simulation of the landing impact was carried out at different values of the initial vertical velocity. The dependence of the optimal electric current in the winding o...

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Veröffentlicht in:	IOP conference series. Materials Science and Engineering 2021-01, Vol.1019 (1), p.12069
Hauptverfasser:	Zagidulin, A R, Podruzhin, E G
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft landing Electromagnets Landing gear Shock absorbers
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Beschreibung
Zusammenfassung:	The article describes the design and computation of the aircraft landing gear with an electromagnetic-gas shock absorber. A numerical simulation of the landing impact was carried out at different values of the initial vertical velocity. The dependence of the optimal electric current in the winding of the shock absorber electromagnet on the vertical speed is obtained.
ISSN:	1757-8981 1757-899X
DOI:	10.1088/1757-899X/1019/1/012069