Particle separator for an air conduit, air distribution system, use of a particle separator and aircraft
A particle separator comprises a pipeline that allows a fluid to flow in a curved direction of flow. The particle separator includes an inlet region, a curved deflection region, which in the direction of flow follows on from the inlet region, with an inside wall and an outside wall, and a delimitation body. The delimitation body at least in some sections extends between the inside wall and the outside wall in the interior of the deflection region and is curved in the same direction as the deflection region.
1. A particle separator, including a pipeline that allows a fluid to flow in a curved direction of flow, the pipeline comprising:
an inlet region;
a curved deflection region, which in the direction of flow follows on from the inlet region, with an inside wall and an outside wall;
a plurality of particle reflection bodies; and
a delimitation body which at least in some sections extends between the inside wall and the outside wall in the interior of the deflection region and is curved in the same direction as the deflection region,
wherein the delimitation body in the direction of flow is curved to a lesser extent than the outside wall so that between the delimitation body and the outside wall a pocket for collecting particles forms, which pocket is open towards the inlet region and which tapers off in the direction of flow, and
wherein the particle reflection bodies are arranged directly and only on an inside wall of the inlet region, the inside wall of the inlet region makes a transition to the inside wall of the deflection region, and the particle reflection bodies are designed to deflect impinging particles into the pocket.
2. The particle separator of claim 1 ,
wherein the delimitation body is permeable to air at least in some regions.
3. The particle separator of claim 1 , wherein the delimitation body extends in the direction of flow, starting from the transition between the inlet region and the deflection region.
4. The particle separator of claim 1 , wherein the delimitation body in the downstream direction closes off with the outside wall the pocket for collecting particles.
5. The particle separator of claim 1 , wherein the particle reflection bodies comprise a plurality of bulges that are arranged one behind the other in the direction of flow, and each of the plurality of bulges include an elevation that projects into the interior of the pipeline.
6. The particle separator of claim 5 , wherein the plurality of bulges are of a bead-like design.
7. The particle separator of claim 1 , further comprising:
a drain that is arranged in a transition region between the inlet region and the outside wall of the deflection region.
8. The particle separator of claim 1 ,
wherein the cross section of the delimitation body, at least in some sections, is curved in the same direction as the outside wall of the deflection region, except at a lesser curvature than the outside wall.
9. The particle separator of claim 8 , wherein the cross section of the pocket at least in some sections is crescent-shaped.
10. The particle separator of claim 1 , wherein the delimitation body extends along the entire deflection region.
11. The particle separator of claim 1 , wherein an opening of the pocket is situated in a transition between the inlet region and the deflection region or further upstream.
12. An air distribution system for an aircraft, comprising:
at least one air conduit;
at least one particle separator integrated as an ice separator in the at least one air conduit, the at least one particle separator including a pipeline comprising:
an inlet region a curved deflection region, which in the direction of flow follows on from the inlet region, with an inside wall and an outside wall;
a plurality of particle reflection bodies; and
a delimitation body which at least in some sections extends between the inside wall and the outside wall in the interior of the deflection region and is curved in the same direction as the deflection region,
wherein the delimitation body in the direction of flow is curved to a lesser extent than the outside wall so that between the delimitation body and the outside wall a pocket for collecting particles forms, which pocket is open towards the inlet region and which tapers off in the direction of flow, and
wherein the particle reflection bodies arranged directly and only on an inside wall of the inlet region, the inside wall of the inlet region makes a transition to the inside wall of the deflection region, and the particle reflection bodies are designed to deflect impinging particles into the pocket.
13. An aircraft, comprising:
an air distribution system including at least one air conduit for directing air from a mixer unit to at least one air outlet in a passenger cabin of the aircraft;
at least one particle separator integrated as an ice separator in the at least one air conduit, the at least one particle separator including a pipeline comprising:
an inlet region a curved deflection region, which in the direction of flow follows on from the inlet region, with an inside wall and an outside wall;
a plurality of particle reflection bodies; and
a delimitation body which at least in some sections extends between the inside wall and the outside wall in the interior of the deflection region and is curved in the same direction as the deflection region,
wherein the delimitation body in the direction of flow is curved to a lesser extent than the outside wall so that between the delimitation body and the outside wall a pocket for collecting particles forms, which pocket is open towards the inlet region and which tapers off in the direction of flow, and
wherein the particle reflection bodies arranged directly and only on an inside wall of the inlet region, the inside wall of the inlet region makes a transition to the inside wall of the deflection region, and the particle reflection bodies are designed to deflect impinging particles into the pocket.
14. The aircraft of claim 13 , wherein the delimitation body is permeable to air at least in some regions.
15. The aircraft of claim 13 , wherein the delimitation body extends in the direction of flow, starting from the transition between the inlet region and the deflection region.
16. The aircraft of claim 13 , wherein the delimitation body in the downstream direction closes off with the outside wall the pocket for collecting particles.
17. The aircraft of claim 13 , wherein the particle reflection bodies comprise a plurality of bulges that are arranged one behind the other in the direction of flow, and each of the plurality of bulges include an elevation that projects into the interior of the pipeline.
18. The aircraft of claim 17 , wherein the plurality of bulges are of a bead-like design.