| 摘要 |
<p>Device for actuation on the ground of aerodynamic turbines for actuating service circuits of aircrafts, particularly circuits for cooling electronic devices, comprising a supporting frame (2), a pneumatic pump (3) provided with an outlet port (4) and with an inlet port (5), and at least one connection conduit (6, 7) that can be associated, with one end thereof, with the outlet port (4) and, with the other end thereof, with an air intake (8), provided on the aircraft, of an aerodynamic turbine for actuating service circuits of aircrafts or which can be associated, with one end thereof, with the inlet port (5) and, with the other end thereof, with the exhaust port (9), provided on the aircraft, of an aerodynamic turbine for actuating service circuits of aircrafts in order to generate an air flow that actuates the aerodynamic turbine which, in turn, actuates the service circuit.</p> |
