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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…
Créateur
- Europeana
Type d'item
- image
Créateur
- Europeana
Type d'item
- image
Institution partenaire
Agrégateur
Licence du support dans cet enregistrement (sauf indication contraire)
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Droits
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Identificateur
- dmg:26969023
- http://www.dmg-lib.org/dmglib/handler?image=26969023
Relations
- Ilmenau University of Technology, Germany
Pays fournisseur
- Europe
Nom de la collection
Première publication sur Europeana
- 2013-11-25T17:57:15.908Z
Dernière mise à jour de l'Institution partenaire
- 2013-11-25T17:57:15.908Z