Flow body of an aircraft and aircraft
View Patent ↗A flow body of an aircraft includes: a flow surface exposed to an airstream during flight of the aircraft, the flow surface generating at least one region of turbulent airflow during flight of the aircraft, at least one perforated area including a plurality of openings extending through the flow surface, a manifold positioned interior to the flow surface in fluid communication with the openings, and at least one suction duct having a first end and a second end, the first end being in fluid communication with the manifold, the second end including a suction opening and being arranged in the at least one region of turbulent airflow, wherein the suction opening is adapted for inducing a suction force in the at least one suction duct when the flow surface is exposed to an airstream during flight, thereby inducing a flow of air from through the plurality of openings.
1. A flow body of an aircraft, comprising:
a flow surface exposed to an airstream during flight of the aircraft, the flow surface generating at least one region of turbulent airflow during flight of the aircraft;
at least one perforated area comprising a plurality of openings extending through the flow surface,
a manifold positioned interior to the flow surface in fluid communication with the openings; and
at least one suction duct having a first end and a second end, the first end in fluid communication with the manifold, the second end comprising a suction opening in the flow surface and arranged in the at least one region of turbulent airflow,
wherein the suction opening is adapted for inducing a suction force in the at least one suction duct when the flow surface is exposed to an airstream during flight, thereby inducing a flow of air from through the plurality of openings,
wherein the flow body is an aerofoil including one or more of an aircraft wing, a winglet, a vertical tailplane, or horizontal tailplane,
wherein the aerofoil is an aircraft wing comprising a lift enhancement device configured to be arranged in the manifold, and
wherein the lift enhancement device is a Krueger lift enhancement device.
2. The flow body according to claim 1 , wherein the flow body comprises a plurality of suction ducts.
3. The flow body according to claim 2 , wherein the flow surface generates a plurality of regions of turbulent airflow during flight of the aircraft spaced apart from each other and wherein each of the plurality of suction ducts is arranged in a separate region of the plurality of regions of turbulent airflow.
4. The flow body according to claim 3 , wherein the manifold comprises a plurality of manifold sections, wherein each of the plurality of manifold sections is arranged on a separate portion of the at least one perforated area.
5. The flow body according to claim 4 , wherein the plurality of suction ducts and the plurality of manifold sections are associated to each other in a one-to-one ratio.
6. The flow body according to claim 4 , wherein the manifold sections are separated by walls.
7. The flow body according to claim 6 , wherein the walls provide an airtight sealing between the manifold sections.
8. The flow body according to claim 1 , wherein each of the at least one suction duct comprises a cross section adapted to a pressure value at a position of the suction opening in the region of turbulent airflow.
9. The flow body according to claim 1 , wherein the flow surface comprises a turbulence generating structure configured to generate the at least one region of turbulent airflow.
10. The flow body according to claim 1 , wherein the flow body comprises a leading edge facing the airstream during flight, wherein the at least one perforated area is arranged at the leading edge.
11. An aircraft comprising at least one flow body according to claim 1 .