Refrigeration – Air compressor – cooler and expander type
Reexamination Certificate
2002-04-22
2004-05-04
Bennett, Henry (Department: 3744)
Refrigeration
Air compressor, cooler and expander type
Reexamination Certificate
active
06729156
ABSTRACT:
BACKGROUND OF THE INVENTION
The invention relates to a ram air duct for an aeroplane conditioning system having an inlet channel which can be closed by an inlet valve and in which at least one heat exchanger is arranged, having a blower arranged in a blower chamber and an outlet passage closable by an outlet valve.
Such ram air ducts for aeroplane air conditioning systems are already known from the prior art. A schematic section through such a known air conditioning system in accordance with the prior art is shown in FIG.
1
. An inlet opening
14
is arranged in the aeroplane skin and can be closed via an inlet valve
16
. The inlet valve can be infinitely adjustable in the direction a of the double arrow via an inlet actuator
18
. An inlet passage
20
adjoins the opening
14
and air-to-air heat exchangers
22
and
22
are arranged in it. The inlet passage
20
opens into a blower chamber
26
(plenum). An impeller
28
is arranged in the blower chamber
26
. The impeller
28
is arranged on a shaft
30
on which a compressor
32
and a turbine
34
of a so-called air-cycle machine of the aeroplane air conditioning system are also seated. The impeller
28
is surrounded by a blower outlet passage
36
which opens into an outlet passage
38
. A bypass valve
40
, which can be pivoted in the direction b of the double arrow and allows a bypass flow into the outlet passage
38
by being pivoted open correspondingly, is arranged next to the blower outlet passage
36
in the blower chamber
26
(cf. representation in FIG.
1
). A so-called jet pump
42
is integrated in the blower outlet passage
36
.
The outlet passage can be closed via an outlet valve
44
, with the outlet valve
44
being pivotable via an outlet actuator
46
which moves rods in the double arrow direction c.
The inlet valve
16
serves the control of the stagnation air volume flow which is led via the heat exchangers
22
and
24
.
In addition to the control of the ram air duct volume flow with the inlet valve, the following three functions must usually be satisfied by the ram air duct. For cooling in flight, a part of the stagnation air must be guided in only one direction through a bypass arranged next to the blower. For heating in ground operation and to produce the circulation flow, a bypass must be made possible to the blower in the opposite direction and overall a joint control of the total volume flow from the blower and the bypass must be ensured.
To satisfy these functions, three apparatuses are necessary in the ram air duct in accordance with the prior art. First, the bypass valve is necessary which is arranged parallel to the ventilator. Dependent on the pressure ratio applied, this valve opens and closes automatically. The blower bypass increases the transmission of the ram air duct and thus the total volume flow in flight.
The jet pump is necessary as the second apparatus. This is arranged, as shown in
FIG. 1
, parallel to the impeller. Dependent on the conditions, i.e. the speed and the pressure, a volume flow results in the one or the other direction at the jet pump inlet and outlet or practically no volume flow, with the following three functions being satisfied by the jet pump:
1. avoidance of a blower circular flow on the ground during cooling;
2. achievement of a bypass volume flow (in addition to the above bypass valve) in flight during cooling; and
3. making possible a blower circular flow in interaction with a largely closed inlet valve and a reduced ventilator speed during heating operation.
An infinitely movable outlet valve is necessary as a third apparatus which can be moved by means of an electrical drive and rods.
According to the prior art, three apparatuses are therefore necessary to satisfy the initially defined three functions. This results in some disadvantages which have to be accepted.
For instance, the jet pump causes power losses of 5 to 10% in the blower outlet passage. High noise levels arise due to the mixing losses of the jet pump. The heat output is limited by the relatively low jet pump cross-section. The maximally realisable cross-section is limited due to general design criteria of a functioning jet pump, which thus limits the maximum circuit flow (reversed bypass volume flow) and thus also the heat output. In heating operation, the circuit flow is not sufficient to be able to fully close the stagnation air inlet valve and thus to fully suppress the cooling via the heat exchangers. A complete closing of the inlet valve at too low a circulation flow results in pumping of the blower in ground operation, which has to be prevented at all costs.
The reliability of the apparatus is significantly reduced by the bypass valve, which is formed as a swing-type check valve. In addition, the manufacturing costs increase. The valve is exposed to high cyclic strains. The additional module is difficult to integrate and causes additional weight, primarily in that it has to be made of metal.
Whether a volume flow comes about via the bypass valve, depends only on the pressure conditions at the inlet and outlet. A direct control is therefore not possible.
Finally, the outlet valve, which has a long design to close the whole outlet opening, results in flight in high loads both on the valve and on the valve drive. In addition to the high weight of the valve, the required high motor powers also lead to a correspondingly high weight of the drive. A blocking of the outlet valve in the closed position results in the total failure of the system since no throughput is possible any more when the outlet valve fails in the closed position.
SUMMARY OF THE INVENTION
It is the object of the invention to further develop a generic ram air duct for an aeroplane air conditioning system such that the blower circular flow is increased to improve the heat output. At the same time, the reliability of the apparatus should be increased while reducing the cost price.
This object is solved in accordance with the invention by the combination herein. Accordingly, the outlet passage in the generic ram air duct is divided into two separately running passages of which one is guided as the blower outlet passage up to the blower into the blower chamber and the other is designed as a bypass passage, with the outlet valve only closing the bypass passage in the closed state.
The new stagnation air passage makes possible a blower circular flow for the heating operation or a suction from the outlet passage and the surroundings in interaction with a largely closed inlet valve and a reduced blower speed. Three functions are carried out by means of an apparatus already present. The bypass valve required in accordance with the prior art and the jet pump can be omitted. The system operates more reliably and the heat output of the system is improved since no stagnation air has to be guided over the heat exchangers during heating operation. The heat output can thus be controlled via the outlet valve and the blower pump protection can be adapted via a corresponding control. The loads acting on the outlet valve, in particular during flight, are considerably reduced since the outlet valve has a smaller construction overall. The two lines provided here allow higher flexibility in installation and the total weight of the ram air duct can be reduced overall.
Aspects of the invention result from the dependent claims following the main claim.
For instance, the blower outlet passage can have a guide vane grid in its outlet. This grid improves the flowing off and prevents the penetration of unwanted objects into the blower outlet passage.
The impeller can be arranged such that stagnation air flows through it in the direction of the drive (axial throughflow).
It can, however, also be arranged such that it is flowed through counter to the direction of the drive (180° deflection).
A control apparatus can advantageously be present for the separate control of the inlet valve or the outlet valve. In this way, different operating states of the aeroplane air conditioning system can be set. For instance, the inlet valve can be opened in full or
Brutscher Norbert
Haas Joachim
Hofer Stefan
Sauterleute Alfred
Bennett Henry
Dilworth & Barrese LLP
Drake Malik N.
Liebherr-Aerospace Lindenberg GmbH
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