Enhanced piccolo ducting with sidewall air outlets

1. A ventilating system for ventilating an aircraft cabin, comprising:

an air supply pipe connected to an air source, and

a plurality of air distribution lines connected to and branching off from the air supply pipe,

wherein the ventilating system is adapted to blow out the air, flowing through the air supply pipe, directly from the air distribution lines into the aircraft cabin, and when operating in a first operating state

wherein when operating in a second operating state at least some of the air distribution lines are connected to connecting lines which supply the air, flowing from the air supply pipe, to air outlets arranged in a distributed manner in the aircraft cabin, wherein the air supply pipes rotates to move from the first operating state to the second operating state.

2. The ventilating system according to claim 1 , wherein the air distribution lines include connecting stubs extending from the air supply pipe.

3. The ventilating system according to claim 1 , wherein the air distribution lines are inclined at an angle of approximately 30° relative to a circumferential surface of the air supply pipe.

4. The ventilating system according to claim 1 , wherein a first group of the air distribution lines extends substantially in the direction of a first aircraft cabin sidewall when the ventilating system is mounted in an aircraft, and a second group of the air distribution lines extends substantially in the direction of a second aircraft cabin sidewall when the ventilating system is mounted in an aircraft.

5. The ventilating system according to claim 4 , wherein the air outlets are positioned at the first and/or the second aircraft cabin sidewall when the ventilating system is mounted in an aircraft.

6. The ventilating system according to claim 1 , wherein when the ventilating system is mounted in an aircraft, an air outlet is positioned at least in a partial region of the aircraft cabin in every second space between two ribs of the aircraft cabin.

7. The ventilating system according to claim 1 , wherein the air supply pipe is positioned at a ceiling of the aircraft cabin when the ventilating system is mounted in an aircraft.

8. The ventilating system according to claim 1 , wherein an orifice is included in least some of the air distribution lines.

9. The ventilating system according to claim 1 , wherein the air outlets have a substantially square-shaped cross-section.

10. The ventilating system according to claim 1 , further comprising:

a fastening device for fastening the air supply pipe to an aircraft structure, the fastening device being adapted to fasten the air supply pipe, in the first operating state of the ventilating system, in a first position to the aircraft structure and to fasten the air supply pipe, in the second operating state of the ventilating system, in a second position, rotated relative to the first position, to the aircraft structure.

11. A method for ventilating an aircraft cabin with a ventilating system, comprising:

supplying air from an air source into an air supply pipe,

distributing the air, flowing through the air supply pipe, to a plurality of air distribution lines connected to and branching off from the air supply pipe,

blowing the air flowing through the air supply pipe directly from the air distribution lines into the aircraft cabin in a first operating state of the ventilating system, and

blowing the air flowing through the air supply pipe through connecting lines connected to at least some of the air distribution lines and through air outlets arranged in a distributed manner in the aircraft cabin in a second operating state of the ventilating system wherein the air supply pipe is rotated between the first operating state and the second operating state.

12. The method according to claim 11 , further comprising:

rotating the air supply pipe between a first position out of communication with the connecting lines in the first operating state of the ventilating system, and a second position in communication with the connecting lines in the second operating state of the ventilating system.

13. The method according to claim 11 , further comprising:

removing the connecting lines and the air outlets from the aircraft cabin in the first operating state of the ventilating system.

14. The ventilating system according to claim 1 , wherein the connecting lines and the air outlets are removably connected to the aircraft cabin so that in the first operating state, the connecting lines and the air outlets are removed to reduce space and weight constraints added by the connecting lines and the air outlets.