1. An aircraft hydraulic system for operating a plurality of hydraulically-operated actuators in the aircraft, comprising: a hydraulic reservoir in which hydraulic fluid is stored; a hydraulic distribution system coupling the hydraulic reservoir to the actuators and having a main flow line coupled to...
1. A system for on-site storage and purification of used hydraulic fluid removed from an aircraft hydraulic fluid system, comprising: a transportable cart; a salvage tank mounted on the transportable cart, the salvage tank having an inner volume dimensioned to contain at least the used hydraulic...
AMC25.1309SystemDesignandAnalysis AMC25.1435HydraulicSystems-Design,τest,AnalysisandCertification AMC25.1453ProtectionofOxygenEquipmentfromRupture CS25.1309Equipment,SystemsandInstallations CS25.1435HydraulicSystems CS25.1453ProtectionofOxygenEquipmentfromRupture 2.1.3EUROCAEPublications AvailablefromEUROCAE,102rueEtienneDolet...
The schematic of the pneumatic duct system is shown in Fig.1.During service operation,the pneumatic duct system of a commercial aircraft is subjected to thermodynamic and pressure cycles,accompanied with the pressure and thermal loss that may cause the shortage of bleeding mass flow for the anti-...
Nevertheless, in this particular incident, the leaked hydraulic oil managed to enter the regulating air system, leading to its impact on the cabin and cockpit personnel. Read more View article Industrial Applications (Except Road Vehicles) Gianfranco Pistoia, in Battery Operated Devices and Systems, ...
One of the objectives of the MEA is the replacement of hydraulic and pneumatic devices with their electric counterpart. The increased number of electric and electronic devices onboard calls for the need of automated control algorithms aimed at achieving specific control goals. A multi-objective ...
Stall warning test requires AC power. Also, with no hydraulic pressure, the leading edge flaps may droop enough to cause an asymmetry signal, resulting in a failure of the stall warning system test. If this happens, switch the “B” system electric pump ON to fully retract all flaps and ...
The arrestor hook actuation schematic is a simple and reliable electrical-hydraulic system circuit which can be used in Navy aircraft operated on ship dec... S Meera,KS Robin,BK Subrahmanya,... 被引量: 0发表: 2016年 Induction for the Birds NASA and the Navy explore magnetic fields in sear...
A control system for an aircraft includes a hydraulic pump, first hydraulic line, second hydraulic line, a first actuator coupled with a first control surface, a second actuator cou
Besides the pneumatic systems, the hydraulic systems, like flight control and landing gear actuators, can also be replaced with electric alternatives. The changes in the system masses and the power requirements for such MEA architecture for an A320neo-category aircraft have previously been investigated...