Pieteikties, lai skatītu šo digitālo objektu citās valodās
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…
Autors
- Europeana
Digitālais objekts veids
- image
Autors
- Europeana
Digitālais objekts veids
- image
Piegādājošā iestāde
Agregators
Tiesību statuss šim digitālajam objektam (ja nav norādīts citādi)?
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Tiesības
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Identifikators
- dmg:26969023
- http://www.dmg-lib.org/dmglib/handler?image=26969023
Saistības
- Ilmenau University of Technology, Germany
Nodrošinošā valsts
- Europe
Kolekcijas nosaukums
Pirmo reizi publicēts Europeana
- 2013-11-25T17:57:15.908Z
Pēdējoreiz atjaunināts no piegādājošās iestādes
- 2013-11-25T17:57:15.908Z