AIRCRAFT CABIN PNEUMATIC AIR CONDITIONING SYSTEM INCLUDING AN AMBIENT AIR COMPRESSOR
The pneumatic air conditioning system optimizes airflow by switching between ground and flight modes, using bleed and ambient air sources, to reduce engine load and energy consumption, ensuring efficient cabin temperature and pressure control across flight phases.
Patent Information
- Application Number
- FR2024005416
- Authority / Receiving Office
- FR · FR
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2024-05-27
- Publication Date
- 2025-11-28
AI Technical Summary
Existing aircraft air conditioning systems face challenges in minimizing air withdrawal from propulsion engines to reduce fuel consumption and maintain cabin temperature and pressure control across various flight phases, while also optimizing energy consumption and system integration.
A pneumatic air conditioning system with a network of pipes and control valves that switches between ground and flight modes, utilizing bleed air and ambient air sources, along with heat exchangers and an air cycle turbomachine, to optimize airflow and reduce engine load.
The system achieves efficient air conditioning with reduced energy consumption, compact integration, and adaptability to flight conditions, while maintaining cabin pressure and temperature control.