Air-oil heat exchanger comprising divergent parietal channels
An air/oil heat exchanger arranged in a vein. The exchanger includes internal parietal corridors and/or external parietal corridors and central corridors, the radial height of the internal and/or external parietal corridors increasing from the inlet of the exchanger to its outlet.
1 . An air/oil heat exchanger, comprising:
a radially internal wall,
a radially external wall, and
a plurality of partitions, some of the partitions are hollow and through which oil passes, the partitions, the radially internal wall, and the radially external wall are delimiting corridors, among which internal parietal corridors and/or external parietal corridors delimited by the radially internal and/or external walls and the adjoining partitions, and central corridors at a distance from the radially internal wall and the radially external wall and delimited only by the partitions, each corridor allowing air flow to pass through the air/oil heat exchanger, wherein the internal parietal corridors and/or the external parietal corridors each define a radial height that increases monotonically from an entrance of the air/oil heat exchanger to an exit of the air/oil heat exchanger, and wherein each of the central corridors defines a central corridor radial height that is maintained constant or decreases from the entrance to the exit.
2 . The air/oil heat exchanger according to claim 1 , wherein at an inlet of the air/oil heat exchanger, the radial height of the internal and/or external parietal corridors is less than the central corridor radial height.
3 . The air/oil heat exchanger according to claim 1 , wherein at an outlet of the air/oil heat exchanger, the radial height of the internal and/or external parietal corridors is greater than the central corridors radial height, and a height of the internal and/or external parietal corridors is double that of a height of the central corridors.
4 . The air/oil heat exchanger according to claim 1 , wherein on a radially central portion of the air/oil heat exchanger, certain partitions concentric or perpendicular to a radius of the turbomachine have an upstream end arranged downstream of an inlet of the air/oil heat exchanger, distant from the inlet of the air/oil heat exchanger by a distance of at least 20% of a length of the air/oil heat exchanger.
5 . The air/oil heat exchanger according to claim 4 , wherein in the radially central portion and in a radial direction, one partition out of two has an upstream end coinciding with the inlet of the air/oil heat exchanger, and one partition out of two has an upstream end downstream of the inlet of the air/oil heat exchanger.
6 . The air/oil heat exchanger according to claim 4 , wherein the radially central portion extends over a height of approximately two thirds of the height of the air/oil heat exchanger at the inlet.
7 . The air/oil heat exchanger according to claim 1 , wherein in a downstream portion of the air/oil heat exchanger, the radially internal wall is concave and approaches the radially external wall.
8 . The air/oil heat exchanger according to claim 1 , wherein a height of the air/oil heat exchanger increases from an inlet thereof to a maximum height at two thirds of a length of the air/oil heat exchanger then decreases.
9 . The air/oil heat exchanger according to claim 1 , wherein a length of the air/oil heat exchanger is three times a maximum height thereof.
10 . The air/oil heat exchanger according to claim 1 , further comprising an inlet plane and an outlet plane which form between them an angle of between 5 and 15°.
11 . The air/oil heat exchanger according to claim 1 , wherein the plurality of partitions among the hollow or solid partitions are flat and arranged radially.
12 . The air/oil heat exchanger according to claim 1 , wherein the plurality of partitions among the hollow or solid partitions are curved and concentric, or are flat and perpendicular to a respective radius of the turbomachine.
13 . A turbomachine, comprising:
an air vein in which the air/oil heat exchanger of claim 1 is arranged, and
a rotor is arranged upstream of or in the air vein, upstream of the air/oil heat exchanger.
14 . The turbomachine according to claim 13 , further comprising:
a stator arranged downstream of the rotor and upstream of the air/oil heat exchanger and positioned in the air vein.
15 . The turbomachine according to 13 , wherein directly downstream of the air/oil heat exchanger, a height of the air vein decreases over a distance of at least 30% of a length of the air/oil heat exchanger.
16 . The turbomachine according to claim 13 , wherein the air flow has a main direction which is inclined at an angle of 20° with an axis of the turbomachine.
17 . The air/oil heat exchanger according to claim 2 , wherein the height of the internal and/or external parietal corridors is half that of the central corridors.