Hydraulic Systems Summary
Hydraulic Systems Overview
Advantages of Hydraulic Systems
Lightweight: More efficient power-to-weight ratio.
High Reliability: Reliable operation with minimal failure rates.
Low Maintenance: Easier upkeep compared to electric systems.
Flexibility: Small pipe diameters allow flexible installation.
Load Tolerance: Can withstand overloads without damage.
Hydraulic Circuit Design
Critical vs Non-Critical Systems:
Critical: Primary flight controls; must function reliably.
Non-Critical: Utility functions (e.g., cargo doors) can tolerate some failure.
Components of Hydraulic Systems
Main Components:
Reservoir
Pump
Accumulator
Valves (Directional, Pressure Control, Flow Control)
Actuator
Hydraulic Fluids
Types:
Vegetable-based: Used in older aircraft.
Mineral-based: Common in general aviation (e.g., MIL-H-5606).
Synthetic fluids: For high-performance aircraft (e.g., Skydrol).
Properties:
High flash point
Optimal viscosity over temperature range
Hydraulic Actuators
Types:
Single-acting: Moves in one direction; requires external force to return.
Double-acting: Moves in both directions; can be balanced or unbalanced based on piston area.
Applications in Aircraft
Simple aircraft: wheel brakes, landing gear.
Larger aircraft: flight controls, flaps, thrust reversers.
Emergency Power Sources
Accumulators: Provide short-term pressure.
Electric Motor Pumps: Serve essential functions briefly during failures.
Ram Air Turbines (RAT): Used for continuous emergency power; deployed during failures.
Monitoring and Status Indications
Pressure transducers, filter blockage indicators, and temperature warnings ensure system health.
Hydraulic System Design Questions
Key parameters: pressure, flow rate, duty cycle, emergency power needs.
System must accommodate heat load and dissipation requirements.
Common Aircraft Systems Examples
A320 and B767 utilize multiple independent hydraulic systems for redundancy and safety.