Log ind for at se denne genstand på andre sprog.
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…
Skaberen
- Europeana
Type af genstand
- image
Skaberen
- Europeana
Type af genstand
- image
Ejerinstiution
Aggregator
Rettigheder for medierne i denne optagelse (medmindre andet er angivet)
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Rettigheder
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Identifikator
- dmg:26969023
- http://www.dmg-lib.org/dmglib/handler?image=26969023
Forbindelser
- Ilmenau University of Technology, Germany
Leverende land
- Europe
Navn på samling
Første gang offentliggjort på Europeana
- 2013-11-25T17:57:15.908Z
Sidste gang opdateret fra den ejerinstiution
- 2013-11-25T17:57:15.908Z