Aircraft Pressurization System

Aircraft Pressurization

Aircraft pressurization is the process of maintaining a safe and comfortable internal pressure in an aircraft cabin.

Reasons for Pressurization:

• To prevent hypoxia (oxygen deficiency) at high altitudes
• To reduce fatigue and improve passenger comfort
• To protect against extreme temperatures and weather conditions
• To prevent damage to aircraft structures due to pressure differences

Pressurization Systems:

• Cabin Pressurization System: Maintains a constant pressure difference between the cabin and the outside environment
  • Uses air from the engines or auxiliary power unit (APU) to pressurize the cabin
  • Controlled by the cabin pressure controller and pressure sensors
• Cabin Altitude Control System: Regulates the cabin altitude (pressure) to maintain a safe and comfortable level
  • Typically set to a cabin altitude of 8,000-10,000 feet (2,400-3,000 meters)

Pressurization Process:

1. Air Intake: Air is drawn from the engines or APU into the cabin pressurization system
2. Compression: Air is compressed to increase its pressure
3. Cooling: Compressed air is cooled to remove excess heat
4. Expansion: Cooled air is expanded to reduce its pressure to a safe level
5. Distribution: Pressurized air is distributed throughout the cabin
6. Ventilation: Excess air is vented out of the cabin to maintain a safe pressure level

Safety Features:

• Pressure Relief Valves: Prevent over-pressurization of the cabin
• Cabin Pressure Sensors: Monitor cabin pressure and alert the crew to any anomalies
• Emergency Decompression: Allows for rapid decompression of the cabin in emergency situations

Effects of Pressure Changes:

• Ear Pain: Caused by pressure changes during ascent and descent
• Altitude Sickness: Caused by rapid changes in cabin pressure
• Decompression Sickness: Caused by rapid loss of cabin pressure

Aircraft Pressurization

• The process of maintaining a safe and comfortable internal pressure in an aircraft cabin

Reasons for Pressurization

• Prevents hypoxia (oxygen deficiency) at high altitudes
• Reduces fatigue and improves passenger comfort
• Protects against extreme temperatures and weather conditions
• Prevents damage to aircraft structures due to pressure differences

Pressurization Systems

• Cabin Pressurization System: maintains a constant pressure difference between the cabin and outside environment
• Uses air from engines or APU to pressurize the cabin
• Controlled by cabin pressure controller and pressure sensors
• Cabin Altitude Control System: regulates cabin altitude to maintain a safe and comfortable level

Cabin Altitude

• Typically set to a cabin altitude of 8,000-10,000 feet (2,400-3,000 meters)

Pressurization Process

• Air Intake: draws air from engines or APU into the cabin pressurization system
• Compression: increases air pressure
• Cooling: removes excess heat from compressed air
• Expansion: reduces air pressure to a safe level
• Distribution: distributes pressurized air throughout the cabin
• Ventilation: vents excess air out of the cabin to maintain safe pressure level

Safety Features

• Pressure Relief Valves: prevent over-pressurization of the cabin
• Cabin Pressure Sensors: monitor cabin pressure and alert crew to anomalies
• Emergency Decompression: allows rapid decompression of the cabin in emergency situations

Effects of Pressure Changes

• Ear Pain: caused by pressure changes during ascent and descent
• Altitude Sickness: caused by rapid changes in cabin pressure
• Decompression Sickness: caused by rapid loss of cabin pressure

Aircraft Pressurization

Reasons for Pressurization

• Prevents hypoxia at high altitudes by maintaining a safe internal pressure
• Reduces fatigue and improves passenger comfort by controlling temperature and humidity
• Protects against extreme temperatures and weather conditions
• Prevents damage to aircraft structures due to pressure differences

Pressurization Systems

• Cabin Pressurization System maintains a constant pressure difference between the cabin and outside environment
• Uses air from engines or APU to pressurize the cabin
• Controlled by cabin pressure controller and pressure sensors
• Cabin Altitude Control System regulates cabin altitude to maintain a safe and comfortable level
• Typically set to a cabin altitude of 8,000-10,000 feet (2,400-3,000 meters)

Pressurization Process

• Air is drawn from engines or APU into the cabin pressurization system
• Air is compressed to increase its pressure
• Compressed air is cooled to remove excess heat
• Cooled air is expanded to reduce its pressure to a safe level
• Pressurized air is distributed throughout the cabin
• Excess air is vented out of the cabin to maintain a safe pressure level

Safety Features

• Pressure Relief Valves prevent over-pressurization of the cabin
• Cabin Pressure Sensors monitor cabin pressure and alert the crew to any anomalies
• Emergency Decompression allows for rapid decompression of the cabin in emergency situations

Effects of Pressure Changes

• Ear pain is caused by pressure changes during ascent and descent
• Altitude sickness is caused by rapid changes in cabin pressure
• Decompression sickness is caused by rapid loss of cabin pressure