Device to control the ventilation and air conditioning of aircraft on the ground

1. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING IN AN AIRCRAFT ON THE GROUND, which must be connected ( 12 ) to an engines' start-up system, comprising a temperature selection system ( 6 ) in a cabin ( 3 ) of the aircraft, a temperature measurement system ( 8 ) in the cabin ( 3 ) of the aircraft, systems including a pneumatic air conditioning system ( 2 ), connected to a pneumatic energy supply system, an electrically powered pneumatic compressor system ( 4 ) connected to an electrical energy supply system and to a pneumatic air conditioning system ( 2 ); and a combination of the above, to control the ventilation and air conditioning of an aircraft based on the difference between a selected temperature ( 6 ) and a measured temperature ( 8 ), said device comprising a system of ( 5 ) ecological operating mode selection for ventilation and air conditioning, a system that detects whether or not an ecological mode has been selected ( 10 , 10 a ), a system to detect the position of the aircraft on the ground ( 10 , 10 b ), a system to detect whether the aircraft's engines are off ( 10 , 10 c ), a system to detect whether a selected energy supply system has been activated ( 10 , 10 d )—this may be either the pneumatic energy supply or electrical energy supply, a system to detect whether air is being supplied ( 10 , 10 e ), a system to detect whether the engine's start up system has been activated ( 13 ), and a system that generates ( 10 ) an ecological operating mode signal ( 16 ), corresponding to an optimal minimum demand for ventilation and air conditioning, which is selectively applied to the pneumatic energy supply system, the electrically powered pneumatic compressor system and the electrical energy supply system, when ecological operating mode has been selected, the aircraft is detected to be on the ground, the engines are detected off and the engines' start up system has not been activated, the selected energy supply—either the pneumatic energy supply system or the electrical energy supply system is activated and supplying air, to control the ventilation and air conditioning in accordance with a minimum level established by the ecological operating mode signal ( 16 ) independent of a difference between the selected temperature ( 6 ) and the temperature measured ( 8 ), to save energy.

2. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 1 , wherein the ecological operating mode ( 16 ) signal depends on at least one parameter.

3. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 2 , wherein the parameter is: outside ambient temperature of the aircraft, outside pressure (barometric height), or a combination of the two.

4. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 1 , wherein the ecological operation section relates to a pre-established fixed value.

5. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 1 , wherein the pneumatic energy supply system represents a choice between an auxiliary power unit ( 1 ) in the aircraft and an electrically powered pneumatic compressor system ( 4 ).

6. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 1 , wherein the electrical energy supply system is a choice between an auxiliary power unit ( 1 a ) in the aircraft and an electrical energy supply unit outside the aircraft.

7. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 1 , wherein the ecological operating mode selection system for ventilation and air conditioning, a system to detect the position of the aircraft on the ground, a system to detect whether the aircraft's engines are off, a system to detect whether the engine's start-up system has been activated, a system to detect whether the selected energy supply system—namely, the pneumatic energy supply or the electrical energy supply—has been activated, a system to detect whether air is being supplied, and a system that generates an ecological operating mode signal, are included in the pneumatic air conditioning system, the pneumatic energy supply system, the electrically powered pneumatic compressor system, in the electrical energy supply system; or in any combination of these.

8. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 7 , wherein the ecological operating mode selection system is comprised of a selector that connects to said ecological operating mode signal generation system selectively by means of cables, an Ethernet, or a combination of the two; and is included selectively in the ecological operating mode signal generation system.

9. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 1 , wherein the inside temperature of the aircraft is selected from an overall temperature or a temperature of a specific section of the aircraft.

10. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 2 , wherein the ecological operating mode selection system for ventilation and air conditioning, a system to detect the position of the aircraft on the ground, a system to detect whether the aircraft's engines are off, a system to detect whether the engine's start-up system has been activated, a system to detect whether the selected energy supply system—namely, the pneumatic energy supply or the electrical energy supply—has been activated, a system to detect whether air is being supplied, and a system that generates an ecological operating mode signal, are included in the pneumatic air conditioning system, the pneumatic energy supply system, the electrically powered pneumatic compressor system, in the electrical energy supply system; or in any combination of these.

11. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 3 , wherein the ecological operating mode selection system for ventilation and air conditioning, a system to detect the position of the aircraft on the ground, a system to detect whether the aircraft's engines are off, a system to detect whether the engine's start-up system has been activated, a system to detect whether the selected energy supply system—namely, the pneumatic energy supply or the electrical energy supply—has been activated, a system to detect whether air is being supplied, and a system that generates an ecological operating mode signal, are included in the pneumatic air conditioning system, the pneumatic energy supply system, the electrically powered pneumatic compressor system, in the electrical energy supply system; or in any combination of these.

12. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 4 , wherein the ecological operating mode selection system for ventilation and air conditioning, a system to detect the position of the aircraft on the ground, a system to detect whether the aircraft's engines are off, a system to detect whether the engine's start-up system has been activated, a system to detect whether the selected energy supply system—namely, the pneumatic energy supply or the electrical energy supply—has been activated, a system to detect whether air is being supplied, and a system that generates an ecological operating mode signal, are included in the pneumatic air conditioning system, the pneumatic energy supply system, the electrically powered pneumatic compressor system, in the electrical energy supply system; or in any combination of these.

13. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 5 , wherein the ecological operating mode selection system for ventilation and air conditioning, a system to detect the position of the aircraft on the ground, a system to detect whether the aircraft's engines are off, a system to detect whether the engine's start-up system has been activated, a system to detect whether the selected energy supply system—namely, the pneumatic energy supply or the electrical energy supply—has been activated, a system to detect whether air is being supplied, and a system that generates an ecological operating mode signal, are included in the pneumatic air conditioning system, the pneumatic energy supply system, the electrically powered pneumatic compressor system, in the electrical energy supply system; or in any combination of these.

14. A DEVICE TO CONTROL VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT ON THE GROUND, in accordance with claim 6 , wherein the ecological operating mode selection system for ventilation and air conditioning, a system to detect the position of the aircraft on the ground, a system to detect whether the aircraft's engines are off, a system to detect whether the engine's start-up system has been activated, a system to detect whether the selected energy supply system—namely, the pneumatic energy supply or the electrical energy supply—has been activated, a system to detect whether air is being supplied, and a system that generates an ecological operating mode signal, are included in the pneumatic air conditioning system, the pneumatic energy supply system, the electrically powered pneumatic compressor system, in the electrical energy supply system; or in any combination of these.