Scroll type positive displacement compressors and pumps include spiral wraps (scrolls) for compressing or pumping a fluid or gas, such as for refrigeration and other applications. Typically, a scroll type compressor or pump includes a stationary scroll, an orbiting scroll, an anti-rotation device (e.g., an Oldham ring) to prevent rotation of the orbiting scroll and bearings, a crankshaft, and an eccentrically mounted shaft. Generally, the scroll shape consists of a spiral wall with a radius increasing in proportion to the wrap angle. The scroll walls begin adjacent to a discharge port near the center of the scroll plate to minimize dead space, maximize compression ratio, and provide a flow path to the discharge port.
A scroll type positive displacement assembly includes a first scroll and a second scroll, where the second scroll is configured to orbit with respect to a center of the first scroll without rotating with respect to the first scroll. Together, the first scroll and the second scroll define a compression chamber between two seal points where the first scroll and the second scroll contact one another as the second scroll orbits with respect to the first scroll during a compression cycle, and the two seal points come together proximate to a discharge port between the first scroll and the second scroll such that there is at least substantially no dead space between the first scroll and the second scroll at an end of the compression cycle. For example, the two seal points remain in sealing contact during at least one hundred and eighty (180) degrees of the compression cycle.
This Summary is provided to introduce a selection of concepts in a simplified form that are further described below in the Detailed Description. This Summary is not intended to identify key features or essential features of the claimed subject matter, nor is it intended to be used as an aid in determining the scope of the claimed subject matter.
The Detailed Description is described with reference to the accompanying figures. The use of the same reference numbers in different instances in the description and the figures may indicate similar or identical items.
Referring to
The first compression chamber 60 is formed between a first seal point 64 and a second seal point 66, positioned at first and second locations where the fixed scroll 52 contacts the orbiting scroll 54. The second compression chamber 62 is formed between a third seal point 68 and a fourth seal point 70, positioned at third and fourth locations where the fixed scroll 52 contacts the orbiting scroll 54. As the orbiting scroll 54 continues to orbit about the center of the fixed scroll 52, the fluid or gas contained within the first and second compression chambers 60 and 62 migrates toward a discharge port 72. The fluid or gas is then expelled via the discharge port 72. As shown in
In such a configuration, the compressor shaft is cantilevered because there is no room to pass the shaft and eccentric through the center of the scroll. Thus, the plane of the eccentric bearing is axially offset from the plane of the scrolls, inducing a moment on the orbiting scroll causing additional non-symmetric axial thrust between the scrolls. The cantilevered shaft also causes increased radial shaft and bearing loading which requires a larger shaft and bearings and reduces mechanical efficiency. To compensate for axial thrust on the orbiting scroll, a thrust bearing system is incorporated.
Referring now to
In the embodiment illustrated in
One feature of the scroll type positive displacement assembly 100 of the present disclosure is that the first one hundred and eighty (180) degrees of compression cavity, beginning at the discharge port area and moving outward, which is formed during the last one hundred and eighty (180) degrees of the compression cycle, is defined by four constant radius one hundred and eighty (180) degree arcs, two inside surfaces on the fixed scroll 102 and two outside surfaces on the orbiting scroll 104. A series of mathematical equations can be used to define the relationships between the scroll geometry and the four radii and their locations. These relationships may ensure that the correct sequence of sealing contact is maintained between the fixed and orbiting scrolls in the compression cavities, and that the compression cavity has no dead space at the end of the compression cycle except for the space remaining in the discharge port 110 and passages. These equations are listed and explained below. The remaining scroll surfaces, beyond the first one hundred and eighty (180) degrees, may be defined by conventional scroll equations.
Referring now to
Let “C1” equal the distance from the scroll centerline on the fixed scroll to the starting point of the inside wall of the conventional scroll surface. Let “C2” equal the distance from the scroll centerline to the starting point of the outside wall of the conventional scroll surface. Let “C3” equal the distance from the scroll centerline on the orbiting scroll to the starting point of constant radius “R3”. “C3” is an independent design variable chosen based on space requirements and design practices. If the central region of the orbiting scroll is enlarged to pass the crankshaft through the center, the value of “C3” is determined by space requirements for the compressor shaft 108, eccentric 106, and eccentric bearing plus minimum wall thickness, “C3” may be reduced for non-thru shaft design. For symmetric scroll geometry, where the orbiting and fixed scroll surfaces are formed as mirror images of each other, let “C3” equal negative “S” divided by four.
Let “R1” equal the constant radius of the beginning inside wall surface 136 one hundred and eighty (180) degree arc of a first wall 128 of the fixed scroll. Let “R2” equal the constant radius of the one hundred and eighty (180) degree arc connecting “R1” to the starting wrap of the outside surface 138 of the conventional scroll wall on the fixed scroll. Let “R3” equal the constant radius of the beginning outside wall surface 140 one hundred and eighty (180) degree arc of a second wall 130 of the orbiting scroll. Finally, let “R4” equal the constant radius of the one hundred and eighty (180) degree arc connecting “R3” to the starting wrap of the inside surface 142 of the conventional scroll wall on the orbiting scroll. Let “Y1” equal the offset from the scroll center 132 which defines the focal point for “R1” on the fixed scroll and the offset from the scroll center 134 which defines the focal point for “R3” on the orbiting scroll. Let “Y2” equal the offset from the scroll center 132 which defines the focal point for “R2” on the fixed scroll and the offset from the scroll center 134 which defines the focal point for “R4” on the orbiting scroll.
Then, example equations for relating the geometrical properties of the fixed and orbiting scrolls 102 and 104 to one another are as follows (it will be appreciated that stroke “S”, wall thickness “W”, starting wrap count “SW”, ending wrap count “EW”, and “C3” are independent design variables):
P=S+2*W
C1=(SW+1/2)*P−W/2
C2=SW*P+W/2
Y1=(C2−C3)/2
Y2=(C1+C3)/2
R1=C1+(C3−C2)/2
R2=C2−(C1+C3)/2
R3=C1+(C3−C2)/2−S/2
R4=S/2+C2−(C1+C3)/2
It should be noted that the scroll type positive displacement assembly 100 may include other dimensional relationships. For example, it will be appreciated that these dimensional relationships describe scroll geometry in a two-dimensional plane. Thus, the depth of the fixed and orbiting scroll members 102 and 104 in a third dimension is another independent design variable which may be chosen based on space requirements and design practices.
It should also be noted that while the scroll type positive displacement assembly 100 illustrated in
Conventional scroll designs experience seal separation of the innermost cavity seals during the last one hundred and eighty (180) degrees of the compression cycle. This characteristic causes dead space at the end of the compression cycle, which reduces the compression ratio and efficiency of the compressor. In contrast, the inner sealing surface of the fixed scroll of the scroll type positive displacement assembly 100, shown in
Additionally, the center regions of both scrolls of the scroll type positive displacement assembly 100 may be enlarged, moving the discharge port and compression cavities radially outward, without increasing the dead space adjacent to the discharge port at the end of the compression cycle. This feature yields a high compression ratio design with fewer scroll wraps. Enlarging the central region may be done to allow room for the eccentric 106, the eccentric bearing, the shaft 108, and shaft bearings, with the shaft 108 passing through the scrolls and the eccentric 106 and supported by shaft bearings on each side of the eccentric. This feature reduces the radial forces on the shaft bearings allowing the use of smaller bearings and shafting. Further, the eccentric 106 may be located axially within the scroll plane allowing the radial pressure forces between the scrolls to pass through the plane of the eccentric bearing and reducing non-symmetric axial thrust between the scrolls.
Conventional scroll machines require precision machining to match the mating surfaces of the orbiting and stationary scrolls and achieve minimum clearance at the sealing surfaces. As described herein, one or both scroll members of the scroll type positive displacement assembly 100 may be coated with an abradable coating of sufficient thickness to cause interference at all sealing surfaces between the scroll members. During the manufacturing or assembly sequence, the two scroll members can be assembled and operated, causing the excess coating to abrade away, leaving a near-perfect match between the surfaces of both scroll members. This process may reduce the need for precise machining of the scroll members.
Although the subject matter has been described in language specific to structural features and/or process operations, it is to be understood that the subject matter defined in the appended claims is not necessarily limited to the specific features or acts described above. Rather, the specific features and acts described above are disclosed as example forms of implementing the claims.
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Child | 17751575 | US |