Prijava za pregled ovog predmeta na drugim jezicima
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…
Stvorio/la
- Europeana
Vrsta predmet
- image
Stvorio/la
- Europeana
Vrsta predmet
- image
Institucija iz koje dolazi
Agregator
Uvjeti korištenja medija u ovom zapisu (osim ako nije drugačije navedeno)
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Prava
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Identifikator
- dmg:26969023
- http://www.dmg-lib.org/dmglib/handler?image=26969023
Odnosi
- Ilmenau University of Technology, Germany
Država iz koje dolazi
- Europe
Naziv zbirke
Prvi put objavljeno na Europeana
- 2013-11-25T17:57:15.908Z
Zadnji put ažurirano od institucije koja pruža podatke
- 2013-11-25T17:57:15.908Z