초록 ▼

An environment control unit for an airplane is configured so that air is drawn out of a cabin (2), oxygen and water molecules alone are separated from the drawn air by a selective permeable membrane (21), the permeated oxygen and water is supplied to the cabin (2) again. The remaining nitrogen is su

An environment control unit for an airplane is configured so that air is drawn out of a cabin (2), oxygen and water molecules alone are separated from the drawn air by a selective permeable membrane (21), the permeated oxygen and water is supplied to the cabin (2) again. The remaining nitrogen is supplied to a fuel tank (41) in order to prevent explosion, it is possible to reduce the amount of air extracted from an engine (1) that is required to facilitate respiration for passengers and to prevent explosion.

대표청구항 ▼

1. An environment control unit for an airplane wherein air of high-temperature and high-pressure is extracted from an engine or an auxiliary power portion of an airplane, the extracted air is regulated in temperature and pressure by an air conditioning portion and then the regulated air is supplied

1. An environment control unit for an airplane wherein air of high-temperature and high-pressure is extracted from an engine or an auxiliary power portion of an airplane, the extracted air is regulated in temperature and pressure by an air conditioning portion and then the regulated air is supplied to a pressurized chamber, wherein air exhausted from the pressurized chamber or air drawn out of the pressurized chamber is separated into air enriched with nitrogen and air enriched with oxygen, the air enriched with oxygen is supplied to the pressurized chamber again and the air enriched with nitrogen is supplied to an inflammable portion further comprising: an auxiliary air conditioning portion that refrigerates air drawn from the pressurized chamber to a circulation line and supplies the air to the pressurized chamber again and the air enriched with oxygen is supplied to the pressurized chamber by making use of the circulation line of the auxiliary air conditioning portion. 2. The environment control unit for an airplane described in claim 1 and characterized by that the air drawn from the pressurized chamber to the circulation line is refrigerated by a vapor cycle system. 3. The environment control unit for an airplane described in claim 1 or 2 and characterized by that air exhausted from the pressurized chamber or air drawn out of the pressurized chamber is separated into air enriched with nitrogen and air enriched with oxygen and vapor by the use of a permeable membrane which can selectively permeate a molecule by compressing the air. 4. The environment control unit for an airplane described in claim 3, and characterized by that air exhausted from the pressurized chamber or air drawn out of the pressurized chamber is separated into air enriched with nitrogen and air enriched with oxygen and vapor by the use of a material which can selectively adsorb a molecule. 5. The environment control unit for an airplane described in claim 3 and characterized by that air exhausted from the pressurized chamber or air drawn out of the pressurized chamber is separated into air enriched with nitrogen and air enriched with oxygen and vapor by the use of material which can selectively adsorb a molecule. 6. The environment control unit for an airplane described in claim 5, wherein a of materials that selectively adsorb molecules are provided and used by turns. 7. The environment control unit for an airplane described in claim 1, or 2 and characterized by that air exhausted from the pressurized chamber or air drawn out of the pressurized chamber is separated into air enriched with nitrogen and air enriched with oxygen and vapor by the use of a material which can selectively adsorb a molecule. 8. The environment control unit for an airplane described in claim 7, wherein a plurality of materials that selectively adsorb molecules are provided and used by turns.