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AIRCRAFT LANDING GEAR AND SKID MECHANISM WITH AN EMERGENCY LOWERING FEATURE
Pump 1 delivers hydraulic fluid, at a pressure controlled by relief valve 2, through check valve 3 into a directional valve with spool 4 which directs the fluid to ends A of power cylinders 5. This moves pistons 6 which retract the landing ghear and skid. From ends D of the cylinders, fluid is discharged through valves 7 and the directional valve to the tank. When the landing gear is in the retrac…
Urheber
- Europeana
Art des Objekts
- image
Urheber
- Europeana
Art des Objekts
- image
Datenpartner
Aggregator
Rechtehinweise der Medien in diesem Datensatz (sofern nicht anders angegeben)
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Rechte
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Kennung
- dmg:26969023
- http://www.dmg-lib.org/dmglib/handler?image=26969023
Beziehungen
- Ilmenau University of Technology, Germany
Bereitstellendes Land
- Europe
Name der Sammlung
Erstmals auf Europeana veröffentlicht
- 2013-11-25T17:57:15.908Z
Zuletzt aktualisiert vom Datenpartner
- 2013-11-25T17:57:15.908Z