EUR 23,00 gastos de envío desde Alemania a Estados Unidos de America
Destinos, gastos y plazos de envíoLibrería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -A hydraulic drive system is a quasi-hydrostatic drive or transmission system that uses pressurized hydraulic fluid to power hydraulic machinery. The term hydrostatic refers to the transfer of energy from pressure differences, not from the kinetic energy of the flow. A hydraulic drive system consists of three parts: The Pump, driven by an electric motor or a combustion engine or a windmill; valves, filters, piping etc. and the actuator.An aircraft hydraulic system just like all other hydraulic system is used to control some mechanical movements in the system. The hydraulic system if used for controlling the movement of the control surfaces of the aircraft. These are the most crucial of the mechanical movements in an aircraft as they involve direction control of the aircraft itself. Along with these other movements that are supported by the aircraft hydraulic system are extension and retraction of the landing gear, direction control of the swivelling nozzle, movement of the air intake hatch cover and mechanical movement of air brakes (if any).In operation of all these components, most crucial of the components as mentioned above are pump, valves, pipelines and the actuators. 60 pp. Englisch. Nº de ref. del artículo: 9786206787327
Cantidad disponible: 2 disponibles
Librería: moluna, Greven, Alemania
Condición: New. Nº de ref. del artículo: 1207952108
Cantidad disponible: Más de 20 disponibles
Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemania
Taschenbuch. Condición: Neu. Neuware -A hydraulic drive system is a quasi-hydrostatic drive or transmission system that uses pressurized hydraulic fluid to power hydraulic machinery. The term hydrostatic refers to the transfer of energy from pressure differences, not from the kinetic energy of the flow. A hydraulic drive system consists of three parts: The Pump, driven by an electric motor or a combustion engine or a windmill; valves, filters, piping etc. and the actuator.An aircraft hydraulic system just like all other hydraulic system is used to control some mechanical movements in the system. The hydraulic system if used for controlling the movement of the control surfaces of the aircraft. These are the most crucial of the mechanical movements in an aircraft as they involve direction control of the aircraft itself. Along with these other movements that are supported by the aircraft hydraulic system are extension and retraction of the landing gear, direction control of the swivelling nozzle, movement of the air intake hatch cover and mechanical movement of air brakes (if any).In operation of all these components, most crucial of the components as mentioned above are pump, valves, pipelines and the actuators.Books on Demand GmbH, Überseering 33, 22297 Hamburg 60 pp. Englisch. Nº de ref. del artículo: 9786206787327
Cantidad disponible: 2 disponibles
Librería: AHA-BUCH GmbH, Einbeck, Alemania
Taschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - A hydraulic drive system is a quasi-hydrostatic drive or transmission system that uses pressurized hydraulic fluid to power hydraulic machinery. The term hydrostatic refers to the transfer of energy from pressure differences, not from the kinetic energy of the flow. A hydraulic drive system consists of three parts: The Pump, driven by an electric motor or a combustion engine or a windmill; valves, filters, piping etc. and the actuator.An aircraft hydraulic system just like all other hydraulic system is used to control some mechanical movements in the system. The hydraulic system if used for controlling the movement of the control surfaces of the aircraft. These are the most crucial of the mechanical movements in an aircraft as they involve direction control of the aircraft itself. Along with these other movements that are supported by the aircraft hydraulic system are extension and retraction of the landing gear, direction control of the swivelling nozzle, movement of the air intake hatch cover and mechanical movement of air brakes (if any).In operation of all these components, most crucial of the components as mentioned above are pump, valves, pipelines and the actuators. Nº de ref. del artículo: 9786206787327
Cantidad disponible: 1 disponibles