Integrated air turbine driven system for providing aircraft environmental control

An integrated environmental control system for an aircraft comprising:

• aircraft mounted accessory drive (AMAD);
• at least one turbine connected to said aircraft accessory mounted drive to provide power to said aircraft accessory mounted drive;
• means for supplying bleed air from an engine to said at least one turbine;
• means for supplying air exiting said at least one turbine to an anti-icing system;
• and
• means for supplying cooled pressurized ram air to at least one of a cabin and a flight deck of said aircraft.

A method for providing environmental control to an aircraft comprising the steps of:

• bleeding air from an aircraft engine;
• delivering said bleed air to at least one turbine;
• using said at least one turbine to provide power to an aircraft mounted accessory drive;
• and
• delivering air from said at least one turbine to an anti-icing system.

A method for providing environmental control to an aircraft comprising the steps of:

• bleeding air from an aircraft engine;
• delivering said bleed air to at least one turbine;
• using said at least one turbine to provide power to an aircraft mounted accessory drive;
• delivering air from said at least one turbine to an anti-icing system;
• and
• supplying cooled pressurized ram air to at least one of a cabin and a flight deck.

An integrated environmental control system for an aircraft comprising:

• aircraft mounted accessory drive for driving at least one of a generator, a pump, a lubrication system and an accessory;
• at least one turbine connected to said aircraft accessory mounted drive to provide power to said aircraft accessory mounted drive;
• means for supplying bleed air from an engine to said at least one turbine;
• and
• means for supplying air exiting said at least one turbine to an anti-icing system.

A method for providing environmental control to an aircraft comprising the steps of:

• bleeding air from an aircraft engine;
• delivering said bleed air to at least one turbine;
• using said at least one turbine to provide power to an aircraft mounted accessory drive for driving at least one of a generator, a pump and a lubrication system;
• and
• delivering air from said at least one turbine to an anti-icing system.