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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…
Makers
- Europeana
Type object
- image
Makers
- Europeana
Type object
- image
Deelnemende erfgoedorganisatie
Informatienetwerk
Rechtenstatus van de media in dit record (tenzij anders vermeld)
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Rechten
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Identificatie
- dmg:26969023
- http://www.dmg-lib.org/dmglib/handler?image=26969023
Relaties
- Ilmenau University of Technology, Germany
Land
- Europe
Naam van de collectie
Voor het eerst gepubliceerd op Europeana
- 2013-11-25T17:57:15.908Z
Laatste keer bijgewerkt door deelnemende erfgoedorganisatie
- 2013-11-25T17:57:15.908Z