Embodiments of the subject matter disclosed herein correspond to a reciprocating compressor.
In particular, the disclosure relates to a reciprocating compressor comprising valves having at least a valve axis that is perpendicular to a cylinder axis.
In the field of “Oil & Gas”, reciprocating compressors are widely used.
US2002/0141884-A1 describes an unloader system is provided for a reciprocating gas compressor. The system includes an unloader valve assembly including a valve member controlling flow between compressor cylinder and a clearance bottle. Opening and closing of the valve member is controlled by manipulating a control pressure acting through a manifold against the stem of the valve member by means of a pressure regulator connected in series with a pressure source. When the pressure in the compressor cylinder acting on the heads of the poppet valve members exceeds the control pressure acting on the stems, the poppet valve members open, partially unloading the compressor.
Each cylinder head of the reciprocating compressor described in the cited document has an annular chamfer with a concave surface partially facing the valve openings.
In different known designs, the cylinder head may a have plurality of slots, each facing a valve opening. Each slot have a concave surface, shaped as a part of a sphere (therefore with a constant radius).
The fluid, when aspired into the compression chamber and when leaving it, runs onto the concave surface of the chamfer or of the slots. This generates pressure losses that lower the efficiency of the compressor.
Therefore, there is a general need for an improved reciprocating compressor, which may have reduced pressure losses and improved adiabatic efficiency with respect the known reciprocating compressors.
An important idea is to create a recessed surface at least partially facing the valve opening that have a convex part facing the valve opening.
This new shape may lead to decreased aerodynamic resistance with a clearance volume comparable to the one of the known compressors.
A first embodiment of the subject matter disclosed herein corresponds to a reciprocating compressor.
The accompanying drawings, which are incorporated herein and constitute a part of the specification, illustrate exemplary embodiments of the present invention and, together with the detailed description, explain these embodiments. In the drawings:
The following description of exemplary embodiments refers to the accompanying drawings.
The following description does not limit the invention. Instead, the scope of the invention is defined by the appended claims.
The description relates to a reciprocating compressor having a plurality of valves. A recessed surface is positioned in front of at least one valve, having at least a convex part facing the valve. The shape of the recessed surface optimizes the trade-off between the cylinder dead volume and the pressure losses.
A piston 4 is movable inside the cylinder 2, and is coupled to a piston rod 5 extending through a cylinder head 10. The piston rod 5 may be conventionally connected to a system designed to transmit a reciprocating movement to the piston 4.
At least one valve 6, may be provided to selectively open and close a valve opening 7 formed in the cylinder lateral wall 3. The valve opening 7 may be at least partially formed in the cylinder liner 31 and/or in the liner spacer 31A. The valve 6 that may be of the type represented in
As it may be seen in
The shape of the recessed surface 12 is schematically shown in
According to one aspect of the present embodiment, an intersection between at least a plane containing the cylinder axis A and the recessed surface 12 is a first curve 13 (see
Moreover the intersection between at least a plane P1, P2, P3 perpendicular to the cylinder axis A and the recessed surface 12 is a further curve 14A, 14B, 14C (see
The intersection between the recessed surface 12 and at least a first plane P1 perpendicular to the cylinder axis A and further containing (or located in proximity of) a free end 15 of the cylinder head 10, 11 may be a second curve 14A (shown in
i·y=A3x2+B3x+C3,
wherein A3, B3 and C3 are constants. Their value can be either positive of negative depending on the position of the coordinate system. A3 shall be different from zero.
As shown in
i·y=A1x2+B1x+C1
wherein A1, B1 and C1 are constants. Their value can be either positive of negative depending on the position of the coordinate system. A1 shall be different from zero.
i·y=A2x2+B2x+C2
wherein A2, B2 and C2 are constants. Their value can be either positive of negative depending on the position of the coordinate system. A2 shall be different from zero.
The distance G from the valve axis B to the plane P3 may be >0, and up to L-D/2.
Basically the shape of the recessed surface 12 is defined by the interpolation of at least a base curve 7A of the valve opening 7 and the second curve 14A.
Moreover the shape of the recessed surface 12 may be further defined by the interpolation of the third curve 14B and/or of the fourth curve 14C.
The base curve 7A may be defined by an opening formed in the cylinder lateral wall 3 or in the cylinder liner 31.
In one embodiment the base curve 7A may be the intersection of a first cylinder of axis B and diameter Dv, and a second cylinder of axis A and diameter equal to the one of the cylinder 2.
In a different embodiment, the base curve 7A may be the intersection of the first cylinder (having axis B and diameter Dv), with and a plane perpendicular to the plane containing axes A and B.
In again a different embodiment, the base curve 7A may be the intersection of the first cylinder (having axis B and diameter Dv), with a third cylinder with same diameter of cylinder 2, but with an axis lying on the same plane of axes A and B and inclined with respect to both axis A and B.
In an embodiment, the described reciprocating compressor may be configured to work at a pressure comprised between atmospheric pressure (or slightly lower) and 600 Bar.
For those kind of compressors, the valve axis B may be perpendicular to the cylinder axis A.
According to one aspect, the vertices of the second curve 14A, of the third curve 14B, and of the fourth curve 14C, may belong to the first curve 13, having a convexity facing, or at least partially facing the valve opening 7.
The reciprocating compressor 1, as above described, may comprise a plurality of valve openings 7 facing (or at least partially facing) a plurality of recessed surfaces 12 located on each cylinder head 10, 11.
In an embodiment the shape of all the recessed surfaces facing the valve openings 7 of the reciprocating compressor is identical or almost identical.
In an embodiment, a number from two to ten valve openings 7 may be located at one side of the piston 4, and the same number of valve openings 7 may be located on the other side. For each side, half of the valve openings 7 may be dedicated to the inlet of the fluid to be compressed in the compression chamber, and the other half number of valve openings 7 may be dedicated to the outlet of the fluid from the compression chamber. The shape of the recessed surface 12 provided in front of the inlet valve openings 7 and on the outlet valve openings 7 may be identical or very similar.
Moreover one 10 of the cylinder heads may be formed in one piece with the cylinder body 30. Another cylinder head 11 may be removably fixed (for example by bolts or any other suitable means) to the cylinder body 30.
The reciprocating compressor as above described may have a valve diameter Dv (see
The piston diameter P may vary from 80 mm to 1300 mm, and the maximum height H1 of the recessed surface 12 may be comprised between 10 mm and P/2. (where P is the piston diameter). As it may be clear from the drawings, the maximum height H1 is taken on the plane P1.
The aerodynamic profile of the recessed surface 12 as above described, is now an extension of the valve space, that may help in avoiding abrupt discontinuities in the flow path from gas chamber to cylinder 2 in case of suction valves and vice-versa in case of discharge ones (which in the prior art led to an increase in pressure losses). The present recessed surface 12 leaves no reflux zones or useless dead volume, giving an increased cylinder adiabatic efficiency.
The proposed design offers less aerodynamic resistance than the known designs, maintaining the same cylinder clearance volume.
The required clearance volume is minimized due to the variable cross-section of the recessed surface, which leaves no reflux zones from the cylinder valve to the cylinder bore.
The proposed shape of the recessed surface 12, is derived form a surface connecting the cylinder valve hole (or the cylinder liner/spacer) with two (or more) consecutives custom profiles (i.e. polynomial, etc.) with different cross-section.
As described, the recessed surface shape, could be realized within a cylinder head 10 formed in the same piece of the cylinder body 30 or in a removable cylinder head 11 by casting, machining or other tools.
The recessed surface shape can also be obtained by the assembly of different parts, e.g. cylinder head, cylinder liner, liner spacer and the cylinder itself, or different combinations thereof.
The component with the recessed surface 12 may be made of metallic, plastic and/or composite materials.
The improvements given from the described design may lead to:
a reduced power needed at the crankshaft;
a more efficient use of the cylinder dead volume;
an improved Cylinder Adiabatic Efficiency (without reduction of Volumetric Efficiency);
to a more uniform flow through valves; and
it may help in avoiding Piston Masking effects (piston masking occurs when the piston approaches the dead center, gradually closing the openings 7, thereby decreasing the passage area for the gas).
Reference throughout the specification to “one embodiment” or “an embodiment” means that a particular feature, structure, or characteristic described in connection with an embodiment is included in at least one embodiment of the subject matter disclosed. Thus, the appearance of the phrases “in one embodiment” or “in an embodiment” in various places throughout the specification is not necessarily referring to the same embodiment. Further, the particular features, structures or characteristics may be combined in any suitable manner in one or more embodiments.
One or more embodiments of the disclosure may comprise one or more of the following clauses, alone or in combination.
In particular, an embodiment refers to a reciprocating compressor 1, comprising:
a cylinder body 30 defining a cylinder 2, the cylinder 2 having a cylinder lateral wall 3 and a cylinder axis A, a piston 4 movable inside the cylinder 2, at least one valve 6 configured to selectively open and close a valve opening 7 formed in the cylinder lateral wall 3, at least a cylinder head 10, 11 that at least partially protrudes towards the piston 4 inside the cylinder 2,
the cylinder head 10, 11 having a recessed surface 12 at least partially facing the valve opening 7; an intersection between at least a plane containing the cylinder axis A and the recessed surface 12 is a first curve 13 having at least a convex part facing the valve opening 7.
According to one aspect the intersection between at least a plane P1, P2, P3 perpendicular to the cylinder axis A and the recessed surface 12 is a further curve 14A, 14B, 14C having a concavity facing the valve opening 7.
According to again another aspect intersection between the recessed surface (12) and at least a first plane (P1) perpendicular to the cylinder axis (A) and further containing a free end (15) of the cylinder head (10, 11) is a second curve (14A) at least partially defined by the equation: y=A3x2+B3x+C3, wherein A3, B3 and C3 are constants, and the value of A3 is ≠0.
According to a further aspect the intersection between the recessed surface 12 and at least a second plane P2 perpendicular to the cylinder axis A and further containing a valve axis B is a third curve 14B at least partially defined by the equation: y=A1x2+B1x+C1, wherein A1, B1 and C1 are constants, and the value of A1 is ≠0.
According to again another aspect the intersection between the recessed surface 12 and at least a third plane P3 perpendicular to the cylinder axis A and further lying between the valve axis B and the free end 15 of the cylinder head 10, 11 is a fourth curve 14C least partially defined by the equation: y=A2x2+B2x+C2, wherein A2, B2 and C2 are constants, and the value of A2 is ≠0.
According to a further aspect the shape of the recessed surface 12 is defined by the interpolation of at least a base curve 7A of the valve opening 7 and the second curve 14A.
According to again another aspect the shape of the recessed surface 12 is further defined by the interpolation of the third curve 14B and/or of the fourth curve 14C.
According to a further aspect the base curve 7A is defined by an opening formed in the cylinder lateral wall 3.
According to again another aspect a valve axis B is perpendicular to the cylinder axis A.
According to a further aspect the vertexes of the second curve 14A, of the third curve 14B, and of the fourth curve 14C belong to the first curve 13.
According to again another aspect the valve opening 7 houses a valve 6 comprising a plurality of valve passages 22 formed in a valve seat 21, the valve passages 22 facing the valve opening 7.
According to a further aspect a cylinder head 10 is formed in one piece with a cylinder body 30.
According to again another aspect a cylinder head 11 is removably fixed to the cylinder body 30.
According to a further aspect the cylinder lateral wall 3 is defined by a cylinder liner 31 coupled to the cylinder body 30.
According to again another aspect a liner spacer 31A extents from the cylinder head 10 to the cylinder liner 31, the valve opening 7 being at least partially formed in the cylinder liner 31 and/or in the liner spacer 31A.
While the disclosed embodiments of the subject matter described herein have been shown in the drawings and fully described above with particularity and detail in connection with several exemplary embodiments, it will be apparent to those of ordinary skill in the art that many modifications, changes, and omissions are possible without materially departing from the novel teachings, the principles and concepts set forth herein, and advantages of the subject matter recited in the appended claims. Hence, the proper scope of the disclosed innovations should be determined only by the broadest interpretation of the appended claims so as to encompass all such modifications, changes, and omissions. In addition, the order or sequence of any process or method steps may be varied or re-sequenced according to alternative embodiments.
Number | Date | Country | Kind |
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102015000060102 | Oct 2015 | IT | national |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2016/073694 | 10/4/2016 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2017/060253 | 4/13/2017 | WO | A |
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677474 | Russell | Jul 1901 | A |
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1719998 | Prellwitz | Jul 1929 | A |
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5622486 | McDuffie | Apr 1997 | A |
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8118574 | Sperry | Feb 2012 | B1 |
20020141884 | Sperry | Oct 2002 | A1 |
20090238699 | Sanford | Sep 2009 | A1 |
Number | Date | Country |
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106634 | Sep 1924 | CH |
1367164 | Sep 1974 | GB |
Entry |
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Italian Search Report and Written Opinion issued in connection with corresponding IT Application No. 102015000060102 dated May 31, 2016 (English Translation not available). |
International Search Report and Written Opinion issued in connection with corresponding PCT Application No. PCT/EP2016/073694 dated Dec. 14, 2016. |
International Preliminary Report on Patentability issued in connection with corresponding PCT Application No. PCT/EP2016/073694 dated Apr. 10, 2018. |
Number | Date | Country | |
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20180291884 A1 | Oct 2018 | US |