Hydraulics in the aircraft
Hydraulics uses an incompressible fluid (hydraulic oil) to transmit force. The basic principle is Pascal's law: pressure in an enclosed fluid acts equally in all directions — a small force on a small piston area can produce a large force on a larger piston area.
Formulas:
- Pressure: p = F / A (force / area). Unit: bar, psi, Pa.
- Force amplification: F₂ = p × A₂ (with p = F₁ / A₁).
- Volume / stroke relation: V₁ = V₂ (small volume at small piston = large volume at large piston) → smaller stroke at the larger piston.
Example: small piston 1 cm² × 100 N force → pressure 10 bar (10⁶ Pa); large piston 10 cm² × 10 bar = 1 000 N. → 10× force amplification.
Properties of hydraulic fluid
Requirements:
- Incompressible — compressible fluid would behave elastically and lose control precision.
- High thermal stability — hydraulic systems heat up in operation.
- Anti-wear additives — lubricate pumps, valves, cylinders.
- Corrosion protection.
Common hydraulic fluids:
- Mineral oil (MIL-PRF-5606) — red dye, older standard.
- Synthetic phosphate ester (Skydrol, MIL-PRF-83282) — fire-resistant, yellow-purple dye, in modern airliners.
- Water-glycol — rare, fire-safe.
Mixing forbidden: different hydraulic fluids must never be mixed — gel formation, seal damage.
Components of a hydraulic system
1. Reservoir — stores hydraulic oil, level shown through sight glass.
2. Pump — generates hydraulic pressure. Types:
- Engine-driven pump — driven by the engine (airliners).
- Electrical pump — for backup or small systems.
- Hand pump — backup on pump failure.
3. Pressure relief valve — protects against overpressure; opens above limit.
4. Accumulator — pressure reservoir with gas pre-charge (usually nitrogen), absorbs pressure peaks and provides short-term reserve.
5. Selector valves — direct pressure to actuators per pilot input.
6. Actuators — hydraulic cylinders that produce mechanical motion (gear, flaps, brakes).
7. Filters — remove contaminants.
8. Lines — connect components; high-pressure tubing (typically 2 000–3 000 psi / 140–210 bar).
Hydraulics in PPL aircraft
In light aircraft (C172, PA-28, DA40) hydraulics is rare and limited to simple applications:
Brakes — almost always hydraulic:
- The brake pedal pushes a small master cylinder → hydraulic fluid transmits force to the brake caliper at the wheel.
Variable-pitch propellers — constant-speed propellers use oil pressure for blade pitch (engine oil, not a separate hydraulic system).
Retractable gear — on retractable types (C172RG, C182RG, Mooney, Bonanza) hydraulic or electric.
Flaps — rarely hydraulic in PPL aircraft; usually electric or mechanical (PA-28 flaps by hand lever).
Pneumatics in the aircraft
Pneumatics uses compressed air instead of fluid. Differences from hydraulics:
- Compressible — springy behaviour, less precise control.
- Cleaner — no oil leaks in the cockpit.
- Lighter — no heavy fluid.
- Higher pressures difficult — air is harder to compress.
Applications:
- Pneumatic de-icing boots: inflatable rubber tubes on leading edges crack ice off.
- Gyro drive by suction pump (vacuum system): vacuum pump creates suction (~5 inHg), air flows through gyro nozzles and spins the gyro.
- Pressurised cabin (airliners): bleed air from the engine maintains cabin pressure.
- Starters (turbines): pneumatic starters on some types.
Vacuum system in PPL aircraft
Many classic PPL aircraft have a vacuum system for gyro instruments:
- Vacuum pump (engine-driven) creates suction.
- Vacuum gauge in the cockpit (4.5–5.5 inHg normal).
- Powers attitude indicator (AI) and directional gyro (DG) with airflow.
- Turn coordinator is electrically driven — redundancy on vacuum failure.
Vacuum failure: AI and DG slowly fail (gyros spin down). The pilot must use electrically driven instruments (turn coordinator) and the magnetic compass.
Safety aspects
- High-pressure hydraulics: injury hazard from oil jet on leaks; hydraulics maintenance only in approved shops.
- Contamination: foreign matter clogs valves; check filters regularly.
- Water ingress: causes corrosion and foaming — hydraulic fluid must remain dry.