[0001] The screw compressor is a rotary volumetric compressor consisting of two parallel
rotors fitted externally with several helical profiles (screws) such that they can
engage in each other. The two rotors are housed in a stator consisting of two longitudinally
intersecting cylinders, in which the rotors turn with a clearance that cannot be reduced
beyond a certain limit.
[0002] The rotor shafts are supported by rolling bearings, and generally one rotor leads
the other by meshing the same helical profiles. Sometimes both can be controlled by
a pair of external gears, to reduce the friction otherwise present. During rotation,
the profiles of the screws uncover an intake gap, located at one end of the stator,
through which air or gas enters to fill the volume between the profiles up to the
maximum extension thereof.
[0003] On the opposite side, the profiles penetrate each other, reduce the volume and compress
the gas enclosed therein until the delivery gap is uncovered. The operation of the
screw compressor is based on the counter-rotating action of two helical rotors that
compress the gas or air taken from the intake duct and bring it towards the delivery
duct. During this path the space is reduced and, consequently, the pressure rises.
[0004] The screw compressor is very popular thanks to the diffusion of the technology of
its construction. Many manufacturers and assemblers offer this product in many different
variants: single-stage, two-stage for high pressure with and without oil for oil-free
applications. The speed of rotation is normally higher than that of the motor to which
it is connected due to gearboxes or the ratio of pulleys when a belt is present.
[0005] These types of industrial compressors deliver gas or compressed air continuously,
are very well controllable, extremely efficient and silent (in terms of safety at
work, environmental protection and noise emissions).
[0006] The current technology involves the use of metallic materials (spheroidal cast iron
or steel) for the production of screws and the correct operation of the compressor
is linked to the presence of clearances between the profile of the screws and the
screws with the compression chamber. However, the presence of such clearances still
leads to a lower efficiency of the machine due to the leakages that bring gas from
high-pressure zones (delivery) and lower-pressure zones (intake).
[0007] As mentioned above, the compression ratios can be increased by injection of lubricating
oil, which helps both the surfaces of the profiles in contact, which acts as a refrigerant
to maintain temperature limits suitable for the materials used, and as a sealing fluid
between the elements in relative motion between them.
[0008] Patent
CN1032383 describes propellers with a steel shaft, aluminium body and fibre-filled polyamide
coating; this composition of different materials is used to ensure a reduction in
the overall weight of the finished body, to take full advantage of the special characteristics
of the polymeric materials and also to use a higher-performing lubricating fluid.
[0009] For this purpose, patent
CN107448383A uses water as lubricant and not-filled PEEK (polyether ether ketone) to coat the
rotor.
[0010] In the patents cited, the production of the rotor, both as a coating and as a finished
piece is obtained by injection molding.
[0011] The present invention aims to improve the performance of a compressor of this type
by using entirely polymeric material for the propellers.
[0012] An aspect of the present invention concerns a screw compressor having the characteristics
of claim 1.
[0013] Further features of the present invention are contained in the dependent claims.
The characteristics and advantages of the present invention will become more apparent
from the following description of an embodiment of the invention, provided by way
of non-limiting example, with reference to the schematic attached drawings, wherein:
- figure 1 illustrates a screw compressor in side view according to the present invention;
- figure 2 illustrates a section of the compressor of figure 1 taken along line A-A;
- figure 3 illustrates a cross-section of the compressor of figure 1;
- figure 4 illustrates the male rotor and the female rotor of the compressor of figure
1;
- figures 5a, 5b and 5c illustrate, for male and female rotors respectively, and for
the coupled rotors, the means for locking the axial displacement;
- figure 6 schematically illustrates the various parts of the screw compressor;
- figure 7 schematically illustrates a detail of a separate lubrication system for the
mechanical parts (bearings, seals and gears) of the compressor.
[0014] With reference to the mentioned figures, the screw compressor according to the present
invention comprises two rotors or helical screws, respectively male rotor 2 and female
rotor 3 enclosed in a casing 4 inside which they counter-rotate. A gas passes through
an intake duct 5 created between the two rotors, and the rotation closes this duct
at the intake and the compressed gas is pushed towards a delivery 6.
[0015] Each rotor includes a rotation shaft 21 and 31 which rotates in the case thanks to
special bearings which is surrounded by propellers 22 and 32 which engage with each
other. The propellers are made in such a way as to reduce progressively the space
between rotors and stator, so that the gas sucked in by the suction duct compresses
in the direction of the delivery 6.
[0016] The two rotors are usually designed with different profiles. The male rotor is usually
provided with convex lobes, while the female rotor has usually concave cavities. It
is thanks to these characteristics that they are engage on to each other. A special
motor supplies the compressor with the necessary supply. The motor is used to impart
the rotation to the male rotor, which in turn drives the female rotor. The casing
is provided with special bearings that are used to keep the rotors in the correct
position. They are located at the ends of both rotors, of which they ensure the uniform
rotation and constant balance.
[0017] There are also intake and discharge valves, which regulate the initial recovery and
the removal of gas from the compressor. The intake valve opens to allow gas to enter
the system, while the discharge valve receives the compressed gas at the end of the
process.
[0018] According to the present invention the propellers 22 and 32 are made of a polymeric
material.
[0019] The choice of a polymeric material for the realization of the propellers, in fact,
brings significant advantages on the performance side, exploiting the behaviour in
temperature and the greater deformability of the material itself, able to lead to
a reduction of the clearance among the propellers during operation. Unlike metals,
in fact, it is possible to have a greater contact, therefore adaptation of the profiles
during the meshing process, in relation to the properties of surface friction and
non-stick reduction.
[0020] Furthermore, in order to minimize the fatigue and/or deformation problems of the
propeller shaft, in relation to more critical application conditions, in terms of
mechanical resistance, the central body of the screw, in particular the shaft 21 and
31 including external projections, can be produced in a more resistant material and
subsequently mechanically connected to the polymeric helical parts.
[0021] The polymeric propellers can be produced starting from a 3D molding process (e.g.
FDM) or from a solid profile.
[0022] The production process of the propellers can include both the use of FDM (Fused Deposition
Modeling) and the mechanical processing of a solid cylinder.
[0023] 3D molding, by means of FDM, has excellent piece finishes and a good production speed,
but at the same time, the mechanical and chemical characteristics of the polymer remain
unchanged. In the molding process, a further finishing step of the obtained rotor
may be necessary, to ensure compliance with the geometric and dimensional tolerances
of the piece necessary for the correct operation of the machine, in the transients
and at operating speed.
[0024] The shaft is preferably made with a material different from that of the propellers,
for example from a more resistant material, in order to absorb most of the bending
load generated by compression and the torque imposed by the motor, minimizing the
deformations that could be encountered by using a body made solely starting from the
same material.
[0025] The shafts are mechanically connected to the respective propellers in order to transmit
the torque of the motor through a suitable locking system. In order to obtain an effective
transmission of the torque, this system comprises tabs and relative slots made both
on the rotor and on the shaft, with a variable number depending on the diameter of
the shaft and of the torque value to be transmitted, up to the use of a splined shaft.
[0026] With regards to the transmission line of the axial and radial loads connected to
the compression process itself, the coupling between propeller and shaft envisages
the presence of contact surfaces designed to resist the forces at play. In particular,
radial thrusts were taken into account by appropriately calibrating the diametrical
coupling between shaft and propeller. From the point of view of the axial thrusts,
from delivery towards intake, under operating conditions, means for locking the relative
axial displacement between the two parts comprising a projection 211 and 311 on the
shaft which fits a groove made in the propeller were created. In relation to the inverted
axial thrusts (from intake towards the delivery), connected instead to transitory
situations at the start-up of the direct coupling and gear machines, a locking ring
212 and 312 of the propeller side delivery on each rotor is provided. This system
has the task of avoiding both the slippage between screw and shaft during torque transmission,
and to prevent the axial translations of the rotor along the shaft in both directions,
in relation to the loads generated by the mechanics of the meshing between the two
rotors and by the fluid dynamics of the compression process itself, taking into account
the expansions at play.
[0027] Considering the anisotropic behaviour of the material obtained by means of 3D molding,
the internal stator bodies (rotor case-diametrical seat and delivery and suction planes)
of the compressor can be coated with an abradable polymeric film. This film not only
reduces the space between rotor and respective cylinder, further decreasing the leakages,
but also ensures, in case of contact of the rotor with the above-mentioned surfaces,
the formation of a groove, preventing plastic deformation or the breakage of the tooth
of the rotor due to excessive overheating caused by the friction of the different
materials. So the purpose of the polymeric film is also to create a thin "sacrificial"
barrier between the rotors and the bodies of the compressor.
[0028] A suitable polymer that can be used for both male and female screws is PEEK (polyether
ether ketone), filled with both long and short fibres, which has the right properties
of compatibility both with the shaft and with the processed gases, as well as the
mechanical and chemical properties such that it can be subjected to both 3D molding
(such as FDM) and traditional mechanical machining, starting from the solid (bar or
cylinder) and for geometric finishes.
[0029] Polyamides as well as polyolefins, suitably functionalised and/or filled with appropriate
fillers and fibres, can also be used to obtain the profiles. These polymers must have
properties of compatibility with both the processed fluids and the shafts on which
they are installed, as well as an adequate affinity among them. A category of polymers
suitable for coating stator bodies, on the other hand, are fluorinated or perfluorinated
compounds, as well as the suitably functionalised polyolefins and polyamides.
[0030] In addition to a chemical compatibility with the material of the propellers, in order
to ensure good adhesion, this coating must also be fully compatible with the temperatures
and the processed gases in order to avoid a premature and unwanted deterioration.
[0031] Sprays, powders or plasma can be used to apply the film.
[0032] The use of high-performance polymers makes it possible, in the case of oil-injected
machines, to use higher-performing refrigerant fluid, as well as to improve the mechanical
and functional behaviour in the presence of corrosive and/or aggressive gas components.
[0033] The polymeric propellers are therefore compatible with:
- process gas;
- lubricating fluid;
- operating conditions of the compressor (temperature, pressure, loads generated);
At the same time, in relation to the characteristics identified in relation to deformability
under the conditions of use, they are able to reduce the previously mentioned clearances,
in order to improve performance without however affecting the correct mechanical operation,
thanks to a higher coefficient of thermal expansion of the polymer than the metal.
[0034] The choice of a polymeric material for the realization of the propellers, in fact,
brings significant advantages on the performance side, exploiting the behaviour in
temperature and the greater deformability of the material itself, able to lead to
a reduction of the clearances among the propellers during operation. Unlike metals,
in fact, a greater contact is possible, therefore adaptation of the profiles during
the meshing process, in relation to the properties of surface friction and non-stick
reduction.
[0035] These aspects are inevitably expressed, for the oil-injected machine version, in
a more flexible choice of lubricant, which, on the rotor side, performs less and less
both the function of anti-friction/anti-seize film during the mechanical meshing process
and the function of clearance reduction, which is more effectively covered by materials/coatings.
[0036] In terms of quantity and functionality, therefore, the injected fluid becomes, as
far as the compression chamber is concerned, primarily a thermodynamic vector, of
temperature reduction in the process, in relation to purely energetic heat balances.
Where it is not possible to change the characteristics of the fluid used also for
lubrication of the other mechanical parts (e.g. bearings/gears/seals...) it is possible
to resort to separate lubrication solutions. The screw compressor of the present invention
can comprise lubrication channels 7, accessible from the outside, which transport
the suitable lubricant to such mechanical parts such as bearings 71, gears, or seals
73. In this machine configuration, the chamber where the meshing takes place between
the rotors is to be isolated, thus being able to use different fluids for each specific
purpose (only refrigerant for rotors or lubricant/refrigerant for other mechanical
parts). This insulation is created by placing internal seals between the compression
chamber and the bearings.
1. Screw compressor comprising a male rotor (2) and a female rotor (3) enclosed in a
casing (4) inside which they counter-rotate, to drive the male rotor from a motor,
a gas passes through an intake duct (5) created between the two rotors, and the rotation
closes this duct at the intake and the compressed gas is pushed towards a delivery
(6),
each rotor includes a rotation shaft (21,31) which rotates in the case thanks to special
bearings which is surrounded by propellers (22,32) which engage each other, the screws
being made in such a way as to reduce progressively the space between rotors and casing,
so that the gas sucked in by the suction duct compresses in the direction of the delivery
(6),
characterized in that the propellers are made of a polymeric material.
2. Compressor according to claim 1, wherein the shafts (21,31) of the rotors are made
of a material more resistant than that of the propellers.
3. Compressor according to claim 1, wherein the shafts (21,31) are mechanically connected
to the respective propellers (22,32) in order to transmit the torque of the engine
through a suitable locking system.
4. Compressor according to claim 1, wherein said polymeric material of the propellers
is PEEK.
5. Compressor according to claim 1, wherein the propellers are made by 3D molding.
6. Compressor according to claim 1, in which said 3D molding is carried out by means
of the FDM technique.
7. Compressor according to claim 1, in which the internal stator bodies, rotor case-diametrical
seat and delivery and suction planes are coated with an abradable polymeric film.
8. Compressor according to claim 1, comprising lubrication channels (7), accessible from
the outside, which carry suitable lubricant to bearings and / or gears and / or seals.
9. Compressor according to claim 1, comprising means for locking the relative axial displacement
between propellers and shafts comprising a projection (211,311) on the shaft which
fits a groove made in the propeller and a locking ring (212,312) of the propeller
side delivery.