PAIR OF CO-OPERATING SCREW ROTORS
20170227009 · 2017-08-10
Inventors
Cpc classification
F04C2240/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01C1/084
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C2250/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C18/084
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F04C18/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A pair of co-operating screw rotors including a male rotor and a female rotor. The male rotor and the female rotor have helically extending lobes and intermediate grooves configured to intermesh with one another. Each groove of the female rotor has a first flank including at least three concave sections. A first section includes or is disposed immediately adjacent the radially innermost point of the groove. A second section is shaped as a circular arc with a radius having its center located outside the pitch circle. A third section is shaped as a circular arc with a radius having its center located outside the pitch circle. The radius of the third section is greater than the radius of the second section, which is greater than the radial distance between a pitch circle of the female rotor and the radially innermost point of the groove.
Claims
1. A pair of co-operating screw rotors, comprising: a male rotor having helically extending lobes and intermediate grooves; and a female rotor having: helically extending lobes and intermediate grooves which are configured to intermesh with the helically extending lobes and intermediate grooves of said male rotor; a pitch radius (R.sub.FP) defining a pitch circle (CFP), each groove of the female rotor having a first flank comprising at least three concave sections, and a first section comprises the radially innermost point of said groove, a second section is shaped as a circular arc with a radius (R2) having its center located outside the pitch circle, and a third section is shaped as a circular arc with a radius (R3) having its center located outside the pitch circle, said radius (R3) of the third section being greater than said radius (R2) of the second section which is greater than the radial distance (R) between the pitch circle and said radially innermost point of said groove.
2. The pair of co-operating screw rotors according to claim 1, wherein said first section is shaped as a circular arc with a radius (R1) having its center located on the pitch circle.
3. The pair of co-operating screw rotors according to claim 1, wherein each lobe of the male rotor has a first lobe flank comprising a convex section which is shaped as a circular arc with a radius having its center located on or inside the pitch circle of the male rotor, and wherein said first section of said female rotor is generated by said convex section of said male rotor.
4. The pair of co-operating screw rotors according to claim 1, wherein the second section is shaped as a circular arc with a radius (R2) having its center located on a straight line extending radially from an end point of said first section along the normal direction of said first section.
5. The pair of co-operating screw rotors according to claim 1, wherein the third section is shaped as a circular arc with a radius (R3) having its center located on a straight line extending radially from an end point of said second section along the normal direction of said second section.
6. The pair of co-operating screw rotors according to claim 2, wherein said center of said first section is defined by the crossing of the pitch circle and a straight line traversing the center of the rotor and the radially innermost point of said groove.
7. The pair of co-operating screw rotors according to claim 6, wherein said radius of said first section corresponds to the radial distance between the pitch circle and said radially innermost point of said groove.
8. A pair of co-operating screw rotors according to claim 1, wherein said sections are formed immediately adjacent to each other.
9. The pair of co-operating screw rotors according to claim 1, wherein said sections are consecutively disposed.
10. The pair of co-operating screw rotors according to claim 1, wherein said radius (R2) of the second section is 1.25 to 1.75 times the radial distance (R) between the pitch circle and said radially innermost point of said groove, and wherein said radius (R3) of the third section is 2 to 3 times the radial distance (R) between the pitch circle and said radially innermost point of said groove.
11. The pair of co-operating screw rotors according to claim 2, wherein each lobe of the male rotor has a first lobe flank comprising a substantially convex section which is generated at least partly by said at least three concave sections of said female rotor.
12. The pair of co-operating screw rotors according to, wherein each lobe of the male rotor has a first lobe flank comprising a substantially convex section which is generated at least partly by said second and third sections of said female rotor.
13. The pair of co-operating screw rotors according to claim 1, wherein each groove of the female rotor has a second flank comprising a substantially concave section, each lobe of the male rotor has a second lobe flank comprising a substantially convex section which is generated by said concave section of said female rotor.
14. The pair of co-operating screw rotors according to claim 2, wherein the second section is shaped as a circular arc with a radius (R2) having its center located on a straight line extending radially from an end point of said first section along the normal direction of said first section.
15. The pair of co-operating screw rotors according to claim 3, wherein the second section is shaped as a circular arc with a radius (R2) having its center located on a straight line extending radially from an end point of said first section along the normal direction of said first section.
16. The pair of co-operating screw rotors according to claim 2, wherein said radius (R2) of the second section is 1.25 to 1.75 times the radial distance (R) between the pitch circle and said radially innermost point of said groove, and wherein said radius (R3) of the third section is 2 to 3 times the radial distance (R) between the pitch circle and said radially innermost point of said groove.
17. The pair of co-operating screw rotors according to claim 3, wherein said radius (R2) of the second section is 1.25 to 1.75 times the radial distance (R) between the pitch circle and said radially innermost point of said groove, and wherein said radius (R3) of the third section is 2 to 3 times the radial distance (R) between the pitch circle and said radially innermost point of said groove.
18. The pair of co-operating screw rotors according to claim 17, wherein each groove of the female rotor has a second flank comprising a substantially concave section, each lobe of the male rotor has a second lobe flank comprising a substantially convex section which is generated by said concave section of said female rotor.
19. The pair of co-operating screw rotors according to claim 3, wherein each groove of the female rotor has a second flank comprising a substantially concave section, each lobe of the male rotor has a second lobe flank comprising a substantially convex section which is generated by said concave section of said female rotor.
20. The pair of co-operating screw rotors according to claim 4, wherein each groove of the female rotor has a second flank comprising a substantially concave section, each lobe of the male rotor has a second lobe flank comprising a substantially convex section which is generated by said concave section of said female rotor.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0027] These and other aspects of the present invention will now be described in more detail, with reference to the appended drawings showing currently preferred embodiment(s) of the invention, wherein
[0028]
[0029]
[0030]
[0031]
DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
[0032] In the following description, known screw rotors according to the prior art and also embodiments of the present invention are described.
[0033]
[0034] Each rotor 1, 2 has a plurality of lobes, and intermediate grooves extending helically along the entire rotor. One rotor 1 is of the male rotor type with the major part of each lobe located outside the pitch circle and the other rotor is of the female rotor type with the major part of each lobe located inside the pitch circle. The female rotor normally has more lobes than the male rotor 1, and a common lobe combination is 4+6. Low pressure air or gas is admitted into the working space of the compressor through an inlet port 8, is then compressed in the chevron-shaped working chambers formed between the rotors and the walls of the working space. Each chamber travels to the right in
[0035] The compression cycle is schematically illustrated in
[0036] In
[0037]
[0038]
[0039] The female rotor has a pitch radius R.sub.FP defining a pitch circle C.sub.FP. The illustrated groove has a first or leading flank comprising at least three concave sections 112, 113, 114. The sections 112, 113, 114 are formed immediately adjacent to each other and consecutively. A first section 112 comprises the radially innermost point 116 of the groove. A second section 113 is shaped as a circular arc with a radius R.sub.2 having its center O.sub.2 located outside the pitch circle. The center O.sub.2 is located on a straight line extending from the end point 117 of the first section along the normal direction of the first section, at a distance R.sub.2 from the groove. A third section 114 is shaped as a circular arc with a radius R.sub.3 having its center O.sub.3 located outside the pitch circle. The center O.sub.3 is located on a straight line extending from the end point 118 of the second section through O.sub.2, at a distance R.sub.3 from the groove. As can be seen in the figure, the radius of the third section is greater than the radius of the second section, which is greater than the radial distance R between the pitch circle and the radially innermost point 116 of said groove. Advantageously, R.sub.2 is 1.25 to 1.75 times R, and R.sub.3 is 2 to 3 times R.
[0040]
[0041] Although exemplary embodiments of the present invention have been shown and described, it will be apparent to the person skilled in the art that a number of changes and modifications may be made. It is understood that the above description of the invention and the drawings are to be regarded as non-limiting examples thereof and that the scope of the invention is defined by the patent claims.