Air de prélèvement (Bleed Air)

Qu'est-ce que l'air de prélèvement ?

Bleed air is compressed, hot air extracted from intermediate or high-pressure compressor stages of a gas turbine engine. At those stages, air has been compressed to pressures of 30–45 psi and temperatures of 200–250 °C — energetic enough to run cabin pressurization, heating, anti-icing systems, and engine starting without additional pumps or heaters. Extracting bleed air reduces available engine thrust and efficiency, which is why some aircraft have eliminated bleed air entirely.

Fonctionnement

Bleed air is tapped at one of two compressor stages depending on flight conditions:

• Intermediate pressure (IP) port: Lower-energy air used at high power settings where the engine compresses air sufficiently at intermediate stages.
• High pressure (HP) port: Used at low power settings (descent, idle) when IP stage pressure is insufficient. Automatically switches via Pressure Regulating Shutoff Valves (PRSOV).

After extraction, bleed air travels through the Pneumatic Distribution System to:

• Air Conditioning Packs: Air cycle machines cool and regulate bleed air for cabin distribution
• Pressurization: Maintains cabin altitude (typically 6,000–8,000 ft equivalent) by pressurizing the fuselage
• Wing and engine inlet anti-icing: Hot bleed air flows through leading edge D-sections to prevent ice accumulation
• Engine starting: Bleed air from the APU or a ground cart spins the starter turbine to accelerate the engine to self-sustaining speed
• Hydraulic reservoir pressurization and potable water tank pressurization

Spécifications de performance

• Efficiency penalty: Bleed air extraction costs 1–3% fuel burn on a typical flight
• Pressure: Delivered to packs at approximately 30–45 psi after regulation
• Temperature: Pre-cooled by fuel-air heat exchangers to ~200 °C before distribution
• Flow rate: Up to 2 lb/sec per engine on large twins at maximum bleed demand

Exemples d'aéronefs

• Airbus A320: Conventional bleed air from CFM56/LEAP engines — industry-standard architecture
• Boeing 787 Dreamliner (bleedless): No bleed air extracted from engines. Instead, electric compressors (powered by generators) provide all pressurization and anti-icing — saving 2–3% fuel burn and improving cabin air quality (no risk of engine oil contamination)
• Airbus A350 (partial bleedless): Uses bleed air for cabin conditioning but electric wing anti-icing (hybrid approach)
• Boeing 737 / Airbus A320: APU provides bleed air for engine starting and ground air conditioning before main engines start

Bleed air management is controlled automatically by FADEC in coordination with the aircraft's pneumatic and environmental control systems.