Patent Application
20130193271
The present invention relates to the Auxiliary Power Unit of an aircraft in general and, more particularly, to the drainage mast of the compartment of an Auxiliary Power Unit of an aircraft.
Known drainage systems of the auxiliary power unit (APU) of an aircraft comprise a mast for evacuating any liquid accumulated in the APU compartment to the atmosphere by gravity.
One of the effects of the ventilation of the APU compartment typically induced by a jet pump mechanism generated by the APU itself is a depression (less pressure in the APU compartment than outside) generated in the APU compartment.
Some of the drawbacks of a pressure impact in the drainage system are mainly related to the difficulties in priming the drainage mast. That is, the draining capacity of the mast is sufficient once it is working fully filled with liquid, but if the ingestion of air into the APU compartment starts before the mast is filled with liquid, because there is a lower pressure in the APU compartment than outside, the stresses induced by the air flow impede the flow of liquid, and it may well happen that the mast never gets filled or primed. Rather, typically, air entering the APU compartment almost completely prevents any outflow of liquid until the liquid height inside the APU compartment is enough to balance the suction in the APU compartment, rendering the mast ineffective. Once this height is reached, only a reduced cross section of the mast will be useful for draining and, in addition, the liquid height in the APU compartment will be as large as what would be reached without a drainage mast.
U.S. Pat. No. 5,996,938 proposes a drainage system comprising a drain tube which is in fluid communication at its upper end with a liquid collecting floor and at its lower end to a check valve selectively open and placed as closely as possible to the aircraft overboard drain port. Liquids collected by the collecting floor are gravitationally directed into the drain tube upper end. The check valve is configured to be open to fluid drainage from the tube out of the drain port when the pressure head of fluid upstream of the check valve exceeds fluid pressure at the drain port due to aircraft operating conditions. This drainage system is therefore dependent of the said check-valve.
An object of the present invention is to provide a drainage mast capable of draining an APU compartment of an aircraft both when the pressure inside the APU compartment is higher than the pressure outside the APU compartment and when the pressure outside the APU compartment is higher than the pressure inside the APU compartment without any active pressure control device.
In one aspect, this and another objects are met by a drainage mast with a first end connected to the APU compartment and a second end for discharging the liquids to the atmosphere; the drainage mast being configured with at least a sector having decreasing cross section areas towards the second end; the area of the initial cross section of said sector being smaller than the area of any cross section of the drainage mast closer to the first end.
Said sector may be the whole drainage mast, a sector located in the second half of the drainage mast or an outlet sector at the end of the drainage mast.
In an embodiment in which said sector is the outlet sector and the drainage mast is arranged at an acute angle with respect to a horizontal plane at the first end, the outlet sector comprises an inner obstruction on the lower wall that completely obstructs a fraction of the cross sections along the outlet sector. The performance and operational characteristics of a drainage mast according to this embodiment are a function of the ratio between the areas of the final and the initial cross section of the outlet sector.
Advantageously, said ratio is comprised between 0.5-0.8.
In an embodiment in which said sector is the outlet sector and the drainage mast is arranged at an acute angle with respect to a horizontal plane at the first end, the outlet sector comprises an inner obstruction that divides the outlet sector into an upper outlet sub-sector, right below the upper wall, and a lower outlet sub-sector, right above the lower wall. The performance and operational characteristics of a drainage mast according to this embodiment are a function of the ratio between the areas of the final and initial cross section of the upper outlet sub-sector and the lower outlet sub-sector.
Advantageously, said ratio is comprised between 0.2-0.4.
Advantageously, said inner obstruction has a conical shape and is arranged with its base in a central position at the exit cross section of the outlet sector on the second end.
In an embodiment in which said sector is the outlet sector, the outlet sector is configured with a nozzle streamlined shape so that the streamlines of the liquid in the second end are very closely parallel to the axis of the drainage mast. The performance and operational characteristics of a drainage mast configured as a nozzle according to this embodiment are a function of the ratios between the effective diameters and areas of the final and the initial cross section of the nozzle.
Advantageously, said nozzle has a dome-ended rectangular shape or an oval shape at the second end and said ratios are comprised respectively between 0.8-0.90 and 0.6-0.8.
In another aspect, the above-mentioned object is met by an aircraft comprising a drainage mast with the above-mentioned features.
Other desirable features and characteristics of the invention will become apparent from the subsequent detailed description of the invention and the appended claims, in relation with the enclosed drawings.
a is an enlarged frontal view of the outlet sector of the drainage mast.
a and 3b are schematic side views of two situations of the drainage system of an APU compartment of an aircraft according to the first embodiment of the invention when the atmospheric pressure is higher than the pressure inside the APU compartment.
a and 5b are schematic side views of two situations of the drainage system of an APU compartment of an aircraft according to the second embodiment of the invention when the atmospheric pressure is higher than the pressure inside the APU compartment.
In other configurations the lower wall of the APU compartment is in itself the fuselage skin.
As shown in
The length L of the drainage mast 13 and the inclination angle α with respect to a hypothetical horizontal plane at the first end 15 controls the effective height Heft of the liquid in the APU compartment 11 according to the equation:
ρg Heff=ρg (Ho+L sin(α))=Pout−Pin
where:
ρ: liquid density at ambient conditions;
g: gravity acceleration;
Heff: liquid height in the APU compartment 11 measured from the second end 17 of the drainage mast 13;
Pout: pressure outside of the APU compartment 11 (atmospheric pressure);
Pin: pressure inside of the APU compartment 11.
On the other hand, Ho is the liquid height in the APU compartment 11 measured from the first end 15 of the drainage mast 13.
The basic idea of the present invention for priming the drainage mast 13 when there is a lower pressure in the APU compartment 11 than outside is configuring a sector of the drainage mast 13 with decreasing cross section areas compared to the cross section areas found upstream along the drainage mast 13. The reason for this is that the flow rate supported by the drainage mast 13 upstream of said sector will then be larger than what said sector can accommodate and, as a result, liquid will be accumulated along the drainage mast 13 upstream of said sector, therefore priming it.
Therefore when Pout>Pin, the drainage mast 13 will get primed when Heft is large enough to compensate the pressure difference.
We will now describe several embodiments of the present invention in reference to Figures showing the aircraft fuselage as the lower wall of the APU compartment 11 but the invention also comprises embodiments with a separate APU compartment 11 such as in
Once this channel for the air flow is set about working the liquid will fill the rest of the cross section of the drainage mast 13 (see
APU compartment 11 if there were no air inflow. However the pressure forces due to the air inflow still prevent the liquid from spilling over the obstacle 31. It is the growth of Heft which eventually provides a level enough to overcome these pressure forces and finally prevents the air inflow. At this moment, the drainage mast 13 priming is complete and the drainage system starts to work at its full capacity (see
When Pout>Pin the reduced area of the outlet sector 21 involves a reduction of the draining effectiveness.
The dynamics of the drainage mast 13 according to this embodiment is somewhat more complex than that of the previous embodiment and that of the bare drainage mast. The complexity arises due to the possibility of two modes of operation, namely the partially-primed mode and the fully-primed one.
The last one is the mode in which the whole section of the drainage mast 13 is draining liquid (see
In the partially-primed mode only the lower outlet sub-sector 43 is discharging liquid (see
The general evolution when Pout>Pin is as follows. At the beginning, when no fluid is present in the drainage mast 13, the air flow enters through both the upper outlet sub-sector 41 and the lower outlet sub-sector 43. When the liquid leakage inside the compartment starts, the height of the liquid in the APU compartment 11 begins to grow because there is no liquid outflow through the drainage mast 13.
However, when the height Ho of the liquid at the APU compartment 11 reaches a few centimeters above the first end 15 of the drainage mast 13, the air is prevented from flowing upstream the drainage mast 13 through the lower outlet sub-sector 43, so a channel of liquid is established which pours out liquid continuously, although the drainage mast is not yet fully-primed, that is, there is still ingestion of air. This outflow is low because of both the reduced height and the reduced area of the exit cross section of the lower outlet sub-sector 43. However, it is effective in keeping low the level Ho of the liquid in the APU compartment 11 for low leakage rates, despite the ingestion of air. For larger leakage flow rates, the liquid level in the APU compartment 11 keeps on growing, although with a slower rate than at the start of the system. When the height Ho of the liquid reaches the level needed for balancing the suction Pout−Pin, the drainage mast 13 becomes fully-primed. Then, the drainage flow rate from the APU compartment 11 through the drainage mast 13 increases significantly. Now two possibilities arise according to whether the drainage flow rate in the fully-primed mode is larger or smaller than the liquid leakage flow rate. If the leakage flow rate is larger than the drainage one in the fully-primed mode, the height Ho of the liquid will keep on increasing. Since the drainage flow rate is proportional to the height, the liquid level Ho will increase until the drainage flow rate balances the leakage finally reaching a steady state with no ingestion of air.
On the other hand, if the drainage flow rate in the fully-primed mode is larger than the leakage one, then once the mast becomes fully-primed the liquid level Ho will start to decrease until the ingestion of air F1 sets in again through the upper outlet sub-sector 41. The drainage mast 13 turns then back again to operate in the partially-primed mode, that is, with only the lower outlet sub-sector 43 pouring out liquid. The drainage flow rate is reduced, so if the new one is larger than the leakage one, the liquid level Ho begins to increase once again until the mast succeeds to get fully-primed and the cycle repeats once and again.
b and 7c show two examples of the final cross section of a nozzle having respectively a dome-ended rectangular shape and an oval shape. The initial cross section in both cases would be the circular section shown in
In one embodiment, the effective diameter De of the final cross section of the nozzle (De=(4×A/π)1/2, being A the area of the final cross section) is comprised between the 80-90% of the diameter D of the initial circular section and the area of the final cross section is comprised between the 60-80% of the area of the initial circular section.
This embodiment provides better discharge times than the above-mentioned embodiments for a given discharge area in the outlet sector 21.
Although the present invention has been described in connection with various embodiments, it will be appreciated from the specification that various combinations of elements, variations or improvements therein may be made, and are within the scope of the invention.
| Number | Date | Country | Kind |
|---|---|---|---|
| 12382027.6 | Jan 2012 | EP | regional |
