Screw-rotor machine with straight flank sections

Claim 2

A pair of intermeshing rotors having helical lands and intervening grooves and adapted for rotation about parallel axes within a working space of a screw rotor machine, one of the rotors being of female rotor type and shaped such that each groove flank circle of the rotor and a minor portion located outside thereof, said minor portion following a curve approaching the adjacent groove when moving from the pitch circle outwardly, and the other of said rotors being of male rotor type and shaped such that each land flank thereof has a major portion located outside the pitch circle of the rotor and a minor portion located inside thereof, characterized in that in a plane perpendicular to the rotor axes said minor flank portion of at least one flank of each male rotor land comprises a first generally straight section located adjacent to the related pitch circle, and a second concavely curved section extending from said first section to the dedendum circle of the rotor, said first flank section forming at its point of intersection with the pitch circle an angle of less than 30° with a radial line drawn through said point of intersection from the center of the rotor.

Claim 3

A pair of rotors as defined in claim 1 wherein said first section forms an angle of about 0° with said radial line drawn through said point of intersection with the pitch circle.

Claim 4

A pair of rotors as defined in claim 1, in which said angle between said first section and said radial line is about 20°.

Claim 5

A pair of rotors as defined in claim 1, in which the flanks of one rotor only deviate from the theoretical shape, whereas the flanks of the other rotor follow the theoretical shape as close as the manufacturing tolerances allow.

Claim 6

A pair of rotors as defined in claim 4, in which said deviations have a minimum extent within an area extending a short distance on each side of the pitch circle of the related rotor.

Claim 7

A pair of rotors as defined in claim 5, in which said deviations are disposed in the female rotor.

Claim 8

A pair of rotors as defined in claim 1 wherein the second section is generated by the tip portion of the corresponding female rotor groove flank.

Claim 9

A pair of rotors as defined in claim 7, wherein said minor portion of the female rotor groove flank substantially follows a curve generated by the first section of the minor portion of the trailing flank of the male rotor and has a tangent at its point of intersection with the pitch circle of the female rotor forming an angle with a radial line through said point from the center of the female rotor, said angle having the same value as that of the angle between the first section of the cooperating male rotor land flank and the related radial line.

Claim 10

A pair of rotors as defined in claim 8, in which said major and minor flank portions of the female rotor groove have a common tangent and form the trailing flank of the groove, when the rotors are disposed in a compressor.

Claim 11

A pair of rotors as defined in claim 9, in which said common tangent passes through the center of the female rotor.

Claim 12

A pair of the rotors as defined in claim 9, in which a section of said major portion of the female rotor flank located adjacent to the pitch circle comprises a straight line.

Claim 13

A pair of rotors as defined in claim 8, in which said major and minor flank portionsof the female rotor groove have a common tangent and form the leading flank of the groove when the rotors are disposed in a compressor.

Claim 14

A pair of rotors as defined in claim 12, in which the trailing flank of the female rotor groove further has major and minor flank portions having a common tangent at their common point on the pitch circle which forms an angle of about 0° with a radial line drawn through said common point of tangency from the center of the rotor.

Claim 15

A pair of the rotors as defined in claim 13, in which a section of said major portion of the female rotor flank located adjacent to the pitch circle comprises a straight line.

Claim 16

A pair of rotors as defined in claim 8, wherein the major portion of the leading flank of the female rotor comprises three sections, the first section being shaped as a circular arc extending over an angle of about 20° with its center located on the pitch circle, a second section being shaped as a circular arc having its center located outside the pitch circle, and the third section comprises a straight line which forms a tangent to the circular arc of said second section and at a point on the pitch circle and which forms an angle of less than 30° with a radial line drawn through said common point of tangency.

Claim 17

A pair of rotors as defined in claim 15, wherein the major portion of the trailing flank of said female rotor comprises three sections, the first section of said trailing flank being a mirror image of the first section of the leading flank, the second section of said trailing flank having at its inner end point a tangent common to that of the first section of said trailing flank and comprises a curve of generally epicycloidal type, and a third section extending from the end of said second section of said trailing flank and comprises a straight radial line drawn from the center of the rotor.

Claim 18

A pair of rotors as defined in claim 16, wherein the leading flank of the male rotor comprises a major portion having three sections, the first section of the male rotor leading flank being substantially shaped as a circular arc conforming with the first section of the leading flank of the female rotor, the second section of the leading flank of the male rotor being generated by the second section of the leading flank of the female rotor, and the third section of the male rotor leading flank being generated by the third section of the leading flank of the female rotor.

Claim 19

A pair of rotors as defined in claim 17, wherein the major portion of the trailing flank of the male rotor comprises a major portion having three sections, the first section of the male rotor trailing flank being a mirror image of the first section of the male rotor leading flank, the end point of the first section of the male rotor trailing flank further generating the generally epicycloidal second section of the female rotor trailing flank, the second section of the male rotor trailing flank being generated by a point on the trailing flank of the female rotor, and the third section of the male rotor trailing flank being generated by the third section of the trailing flank of the female rotor.

Claim 20

Screw rotor machine apparatus for selectively compressing an expanding an elastic working fluid and having a casing with a working space providing with spaced apart high pressure and low pressure ports and including at least two intersecting bores with coplanar axes, a pair of cooperating intermeshing rotors disposed in said bores and having helical lands and intervening grooves, the rotors being adapted for rotation about parallel axes within the working space of the machine, one of the rotors being of female type and shaped such that each groove flank thereof has a major portion located inside the pitch circle of the rotor and a minor portion located outside thereof, said minor portion following a curve approaching the adjacent groove when moving from the pitch circle outwardly, and the other of said rotors being of male rotor type and shaped such that each land flank thereof has a major portion located outside the pitch circle of the rotor and a minor portion located inside thereof, characterized in that in a plane perpendicular to the rotor axes said minor flank portion of at least one flank of each male rotor land comprises a first generally straight section located adjacent to the related pitch circle, and a second concavely curved section extending from said first section to the dedendum circle of the rotor, said first flank section forming at its point of intersection with the pitch circle an angle of less than 30° with a radial line drawn through said point of intersection from the center of the rotor.

Claim 21

Screw rotor machine apparatus for selectively compressing an expanding an elastic working fluid and having a casing with a working space providing with spaced apart high pressure and low pressure ports and including at least two intersecting bores with coplanar axes, a pair of cooperating intermeshing rotors disposed in said bores and having helical lands and intervening grooves, the rotors being adapted for rotation about parallel axes within the working space of the machine, one of the rotors being of female type and shaped such that each groove flank thereof has a major portion located inside the pitch circle of the rotor and a minor portion located outside thereof, said minor portion following a curve approaching the adjacent groove when moving from the pitch circle outwardly, and the other of said rotors being of male rotor type and shaped such that each land flank thereof has a major portion located outside the pitch circle of the rotor and a minor portion located inside thereof, characterized in that in a plane perpendicular to the rotor axes said minor flank portion of at least one flank of each male rotor land comprises a first generally straight section located adjacent to the related pitch circle, and a second concavely curved section extending from said first section to the dedendum circle of the rotor, said first flank section forming at its point of intersection with the pitch circle an angle of less than 30° with a radial line drawn through said point of intersection from the center of the rotor.

Claim 22

Apparatus as defined in claim 19, wherein said first section forms an angle of about 0° with said radial line drawn through said point of intersection with the pitch circle.

Claim 23

Apparatus as defined in claim 19, in which said angle between said first section and said radial line is about 20°.

Claim 24

Apparatus as defined in claim 19, in which said second section is generated by the tip portion of the corresponding female rotor groove flank.

Claim 25

Apparatus as defined in claim 19, in which the flanks of one rotor only deviate from the theoretical shape, whereas the flanks of the other rotor follow the theoretical shape as close as the manufacturing tolerances allow.

Claim 26

Apparatus as defined in claim 23, in which said deviations have a minimum extent within an area extending a short distance on each side of the pitch circle of the related rotor.

Claim 27

Apparatus as defined in claim 24, in which said deviations are disposed in the female rotor.

Claim 28

Apparatus as defined in claim 19, in which said minor portion of the female rotor groove flank substantially comprises a curve generated by the first section of the minor portion of the trailing flank of the male rotor and has a tangent at its point of intersection with the pitch circle of the female forming an angle with a radial line through said point from the center of the female rotor, said angle having the same value as that of the angle between the first section of the cooperating male rotor land flank and the related radial line.

Claim 29

Apparatus as defined in claim 26, in which said major flank portions of the female rotor groove have a common tangent and form the trailing flank of the groove, when the rotors are disposed in a compressor.

Claim 30

Apparatus as defined in claim 27, in which said common tangent passes through the center of the female rotor.

Claim 31

Apparatus as defined in claim 27, in which a section of said major portion of the female rotor flank located adjacent to the pitch circle comprises a straight line.

Claim 32

Apparatus as defined in claim 26, in which said major and minor flank portions of the female rotor groove have a common tangent and form the leading flank of the groove, when the rotors are disposed in a compressor.

Claim 33

Apparatus as defined in claim 30, in which the trailing flank of the female rotor groove further has major and minor flank portions having a common tangent at their common point on the pitch circle which forms an angle of about 0° with a radial line drawn through said common point of tangency from the center of the rotor.