The present invention relates to a fan of the type including:
Many fans are used in airplanes for ensuring air-conditioning of the cabin of the aircraft, or further for ensuring cooling of pieces of equipment of the aircraft.
These fans are powered by the electric network of the airplane. In order to ensure control and powering of the motor of the fan, the fan is equipped with an electric control circuit which, by its operation, produces heat.
For removing heat, it is known how to position electronic components of the electric circuit on a radiator which protrudes inside the vein of air delimited by the external ferrule of the fan. Such a layout degrades the aeraulic performances of the fan.
Document US 2012/0236498 describes a fan comprising means for cooling the electric circuit formed by a tapping aperture opening into the vein of air of the fan and able to take up a secondary cooling flow which circulates between the electronic components of the circuit in order to ensure their cooling.
This layout, even if it gives the possibility of not reducing the aeraulic yield of the fan by the presence of a radiator in the vein of air, is of limited efficiency, the cooling flow rate around the components being low and the layouts may lead to the transmission of contaminating elements towards the components from the vein of air of the fan.
The object of the invention is to propose a fan, notably for aircraft, in which the cooling of the electric control circuit is efficient, without reducing the aeraulic yield of the fan.
For this purpose, the object of the invention is a fan of the aforementioned type, characterized in that:
According to particular embodiments, the fan includes one or several of the following features:
The invention will be better understood upon reading the description which follows, only given as an example and made with reference to the drawings wherein:
The fan 10 illustrated in
It includes an external ferrule 12 delimiting a vein of air 14, circulating from an inlet 16 of the fan to as far as an outlet 18.
The ferrule 12 has an internal surface 20 delimiting the vein of air. This surface is cylindrical with a circular section with a general axis X-X forming the fan axis.
As known per se, a motor 22 is provided along the X-X axis. This motor is borne by supporting arms 24 connecting the stator of the motor to the ferrule 12. A wheel 26 provided with blades 28 is mounted on the rotor of the motor on the air intake 16 side. A nose cone 29 extends the motor 22 opposite to the wheel 26.
A crowd of fins 30 forming an air rectifier extends around the motor 22 downstream from the blades 28 of the wheel. The vein of air 24 produced by rotation of the wheel 26 is circulates between the internal surface 20 of the ferrule and the external surface of the motor 22 and of the nose cone 29.
The fan finally includes a circuit 40 four controlling and powering the motor 22. This circuit is connected to the power supply network 42 specific to the airplane at the inlet and to the motor 22 at the outlet.
The circuit 40 includes a set of electronic components such as coils 44 borne by cores 46 radially extending to the external surface of the ferrule 12. The components are attached on the external surface of the ferrule 12 in thermal contact with the latter.
In this embodiment, the ferrule 12 comprises generally cylindrical tubing 47 and a base 48 for supporting the circuit 40.
The tubing 47 includes an oblong lumen extending along a length of the corresponding tubing, substantially at right angles to the motor 22. The base 48 is received into this lumen and is sealably secured therein for the vein of air.
The surfaces of the tubing 47 and of the base 48 turned towards the motor and both cylindrical with the same curvatures are flush with each other. The base 48 protrudes radially outwards from the tubing 47.
The base 48 is illustrated alone in
Passages for cooling the components are provided through the ferrule 12 and notably through the base 48 in the relevant embodiment.
These passages include continuous conduits 50 circulating in the thickness of the ferrule. They are generally parallel to the X-X axis and open into the vein of air from an inlet tapping aperture 52 and one or several tapping apertures for reintroducing air 54, 56.
The inlet tapping aperture 52 is positioned upstream from the outlet tapping aperture 54, 56, considering the direction of circulation of the vein of air.
The conduits 50 include a main segment 60 extending longitudinally. This segment is rectilinear and extends beyond the end tapping apertures 52 and 56. This segment is obturated at each end with plugs 61 for example formed with a force-fitted polymeric stopper.
The tapping apertures 52, 54, 56 are formed with radial drill holes 62, 64, 66 opening into the main segment 60 and into the vein of air through the internal surface of the ferrule 12 through the corresponding tapping aperture.
Advantageously, the radial drill holes 62, 64, 68 which connect the main segment 60 to the internal surface of the ferrule 12 are made at positions depending on the position of the motor 22 and of the wheel 26. This gives the possibility of using a same base blank in fans of different structure by suitably piercing the tapping apertures. The Earth the same part may be used in several types of fan, by positioning on demand the radial drill holes at right angles to the desired inlet and outlet tapping apertures.
Preferably, according to an alternative embodiment not shown, the external ferrule and notably the base, is formed by extrusion in a die, the rectilinear segments 50 being formed by removable inserts ensuring a recess in the ferrule during its extrusion.
Preferably, the average diameter of each conduit is greater than 4 mm. it is preferably comprised between 4 and 8 mm and advantageously substantially equal to 6 mm.
The conduits 50 are dimensioned so that the velocity in the conduits is greater than 10 m·s−1, and preferably greater than 30 m·s−1.
Further, the dimensioning is such that less than 5% of the total flow from the fan circulates through the cooling conduits 50. Ideally, a flow of about 2% of the total flow circulates through the cooling conduits 50.
In the relevant example, the number of conduits is equal to 7. It is preferably comprised between 2 and 12.
It is conceivable that with such a layout, under the effect of the pressure difference between the downstream tapping aperture 52 and the upstream tapping aperture 54, 56, a cooling flow is established in the conduits 50. As this flow is channeled in conduits of relatively reduced size, the velocity of the cooling flow is relatively high, thereby promoting good removal of the heat produced by the electronic components 44 in thermal contact with the ferrule 12. Further, as the conduits 50 are continuous, the cooling flow does not circulate directly in contact with the components, thereby avoiding their degradation by possible contaminants which may be contained in the gas flow set into motion by the fan.
Number | Date | Country | Kind |
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14 50143 | Jan 2014 | FR | national |