| 摘要 |
#CMT# #/CMT# The part (100) has a cylindrical shaped air inlet (102) such as vertical open cylinder, and an air transmitting conduit (107 for transmitting airflow from the exterior of the part into an internal volume of the part. The air inlet is arranged on a wall (116) of the part to locally form a line of a leading edge of the part. The longitudinal axis of the air inlet is parallel to the line of the leading edge of the part. The air inlet has a radius equal to the curvature radius of the leading edge. The air inlet is provided with a cone shaped air passage jet pipe. #CMT#USE : #/CMT# Aircraft part e.g. strut fairing for fixing jet engine located under fixation strut to airfoil located on top of strut, wing of airfoil of aircraft, fixation strut, engine strut fairing, system fairing or vertical or horizontal tail empennage, for aeronautical field for holding an air system e.g. heat exchanger (claimed), air blower and de-icer, that is utilized for transmitting air from an area located in the air flow to another area more or less confined to the aircraft. #CMT#ADVANTAGE : #/CMT# The air inlet does not disturb the flow of the air flow. The air inlet has the radius equal to the curvature radius of the leading edge, thus limiting the aerodynamic disturbance in the environmental flow regardless of the opening angle of the air inlet. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a schematic transversal sectional view of a top of an aircraft part in a closed position. 100 : Aircraft part 102 : Cylindrical shaped air let 103 : External opening 107 : Air transmitting conduit 108 : Internal opening 116 : Wall. |
