Method and device for reducing the increase in temperature at the surface of the terrestrial globe, vehicle and station for implementing said method

An engine for propulsion of an aircraft, the engine enabling a reduction in an increase in the temperature of the air of the atmosphere and the temperature of the water of the oceans and seas of the Earth, the engine comprising:

• a combustion chamber (C1) containing fossil or non-fossil fuel, use of which fuel generates, by consumption of oxygen from atmospheric air or by consumption of oxygen from atmospheric air enriched with pure oxygen or by consumption of pure oxygen, a gas containing heat and water vapor, the combustion chamber having an inlet (E1);
• a propeller (H1);
• a tank (R1) connected to the combustion chamber (C1);
• a fuel pump (P1);
• at least one fuel shut-off and adjustment valve (V);
• and
• an ambient air inlet equipped with a shut-off and adjustment valve,
• the combustion chamber C1:
• using the fossil or non-fossil fuel from the tank (R1) arriving in the combustion chamber via inlet (E1),
• generating by consumption of oxygen from atmospheric air or by consumption of oxygen from atmospheric air enriched with pure oxygen or by consumption of pure oxygen, entering the combustion chamber through the inlet (E2), a combustion gas leaving the combustion chamber through outlet S1 and containing heat, sensible heat and latent heat, and water vapor, which water vapor has a triple effect on increasing the temperature of the air of the atmosphere and the temperature of the water of the oceans and seas of the Earth by:
• direct heating of the air of the Earth's atmosphere from latent heat in the vapor,
• indirect heating of the Earth's atmosphere by the greenhouse effect by absorption of infrared radiation emitted by the Earth's surface of water vapor,
• increase in the temperature of the water of the oceans and seas on the surface of the Earth by reducing the blocking of evaporation of the water of the oceans and seas on the surface of the Earth, which reduction of evaporation is done by decreasing the concentration gradient of water vapor between the surface of the water of the seas and oceans and the atmospheric air above the water;
• and
• a heat exchanger (X1) with ambient air condensation (A1)-combustion gas or ambient air condensation (A1)-liquid-combustion gas or liquid-combustion gas condensation, which heat exchanger removes heat contained in the combustion gas and the condensation of water vapor in the form of liquid water.