Connected thread groove spacer and vacuum pump
10823200 ยท 2020-11-03
Assignee
Inventors
- Yoshiyuki Sakaguchi (Chiba, JP)
- Tooru Miwata (Chiba, JP)
- Kengo Saegusa (Chiba, JP)
- Nahoko Yoshihara (Chiba, JP)
Cpc classification
F04D19/042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/044
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D17/168
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/046
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F04D29/54
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A thread groove pump portion, which is an exhaust element, is structured such that a Siegbahn structure is attached onto a cylindrical thread, and such that respective parts are connected to each other at this attachment section. A flow channel of the Siegbahn portion and a flow channel of the cylindrical thread (the thread groove pump portion) are connected to each other so as to substantially form a right angle when viewed from an axis direction of the vacuum pump, thus, the flow channel of the Siegbahn portion and the flow channel of the thread groove pump portion are connected to each other. the length of a compression flow channel of the thread groove pump portion can be increased in a radial direction due to the connected Siegbahn portion.
Claims
1. A connected thread groove spacer comprising: a spiral groove portion which has a disc shape and in which a spiral groove with a spiral ridge portion and a spiral root portion is engraved; and a thread groove portion which has a cylindrical shape and in which a thread groove with a thread ridge portion and a thread root portion is formed, the thread groove portion being connected to the spiral groove portion, wherein a flow channel of the spiral groove portion is connected to a flow channel of the thread groove portion, a value of a first gradient angle, which is a gradient angle between an axis and a thread depth in the thread groove portion, is smaller than a value of a second gradient angle, which is a gradient angle between an axis perpendicular line perpendicular to the axis and a groove depth in the spiral groove portion, and the value of the first gradient angle is larger than zero.
2. The connected thread groove spacer according to claim 1, wherein, in the spiral groove portion and the thread groove portion, at least one of borderlines between the spiral ridge portion and the spiral root portion, or a first extended line extending from this borderline is connected in a continuous manner to at least one of borderlines between the thread ridge portion and the thread root portion, or a second extended line extending from this borderline, at a connection portion where the spiral groove portion and the thread groove portion are connected to each other.
3. The connected thread groove spacer according to claim 2, further, wherein a top surface of the spiral ridge portion and a top surface of the thread ridge portion are connected to each other at the connection portion in a non-continuous manner.
4. The connected thread groove spacer according to claim 2, further, wherein the spiral ridge portion and the thread ridge portion are connected to each other at the connection portion in a continuous manner.
5. The connected thread groove spacer according to claim 1, wherein, in the spiral groove portion and the thread groove portion, the spiral ridge portion and the thread ridge portion are connected to each other in a continuous manner at a connection portion where the spiral groove portion and the thread groove portion are connected to each other.
6. The connected thread groove spacer according to claim 5, further, wherein the spiral ridge portion and the thread ridge portion intersect with each other by being connected to each other at the connection portion, with a borderline surface between the spiral ridge portion and the spiral root portion and a borderline surface between the thread ridge portion and the thread root portion being disposed in a non-continuous manner.
7. The connected thread groove spacer according to claim 1, wherein a value of a first angle formed by an inner diameter tangent of the spiral groove portion and an inner diameter-side tangent of the spiral ridge portion is equal to or smaller than a value of a second angle formed by an outer diameter tangent of the spiral groove portion and the inner diameter-side tangent of the spiral ridge portion, the first angle being formed to be larger than 15 and the second angle being formed to be smaller than 25.
8. The connected thread groove spacer according to claim 1, wherein the spiral groove portion and the thread groove portion are formed integrally.
9. A vacuum pump comprising: a housing in which an inlet port and an outlet port are formed; a rotating shaft that is enclosed in the housing and supported rotatably; a rotor blade that is provided on the rotating shaft; a stator blade that is disposed concentrically with the rotor blade and axially opposes the rotor blade with a gap therebetween; and a thread groove pump mechanism that has the connected thread groove spacer described in claim 1 that is fixed to the housing.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DESCRIPTION OF THE PREFERRED EMBODIMENT
(15) (i) Overview of Embodiment
(16) A connected thread groove spacer according to an embodiment of the present invention has a structure that connects a Siegbahn pump portion and a thread groove pump portion.
(17) More specifically, the thread groove pump portion, which is an exhaust element, is structured such that a Siegbahn structure is attached onto a cylindrical thread, and such that respective parts are connected to each other at this attachment section. In other words, a flow channel of the Siegbahn portion and a flow channel of the cylindrical thread (the thread groove pump portion) are connected to each other so as to substantially form a right angle (to be expressed as axially perpendicular for example, hereinafter) when viewed from an axis direction of the vacuum pump, thus, the flow channel of the Siegbahn portion and the flow channel of the thread groove pump portion are connected to each other.
(18) Note that this configuration for connecting these portions can be created integrally by means of casting.
(19) According to this configuration, the length of a compression flow channel of the thread groove pump portion can be increased in a radial direction due to the connected Siegbahn portion.
(20) (ii) Details of Embodiment
(21) The vacuum pump according to the embodiment of the present invention has, on at least one of a stator disc to be provided and a rotating disc to be provided, the Siegbahn pump portion in which a spiral groove with ridge portions and root portions is engraved (provided), and a thread groove pump portion, which is a gas transfer mechanism in which a spiral groove is formed on a surface opposing a rotating cylinder, a thread groove spacer opposing an outer circumferential surface of the rotating cylinder with a predetermined clearance therebetween is provided, and gas is sent toward an outlet port by being guided by a thread groove (spiral groove) as the rotating cylinder rotates at high speed.
(22) Preferred embodiments of the present invention are described hereinafter in detail with reference to
(23) (ii-1) Configuration of Vacuum Pump
(24)
(25) In the embodiments of the present invention, a diameter direction of rotor blades is referred to as radial (diametrical) direction, and the direction perpendicular to the diameter direction of the rotor blades is referred to as axis direction (or axial direction).
(26) A casing (outer cylinder) 2 forming a housing of the vacuum pump 1 has a substantially cylindrical shape and configures a casing of the vacuum pump 1 along with a base 3 provided at a lower portion of the casing 2 (outlet port 6 side). The gas transfer mechanism, a structure that exhibits the exhaust performance of the vacuum pump 1, is stored in this casing.
(27) In the present embodiment, this gas transfer mechanism is configured roughly by a rotating portion (rotor portion/Siegbahn portion) that is supported rotatably and a stator portion (thread groove pump portion) fixed to the casing.
(28) Although not shown, a control device for controlling the operation of the vacuum pump 1 is connected to the outside of the housing of the vacuum pump 1 by a dedicated line.
(29) An inlet port 4 for introducing gas to the vacuum pump 1 is formed at an end portion of the casing 2. A flange portion 5 protruding toward an outer circumference is formed on an end surface of the casing 2 on the inlet port 4 side.
(30) The outlet port 6 for exhausting gas from the vacuum pump 1 is formed in the base 3.
(31) The rotating portion has a shaft 7, which is a rotating shaft, a rotor 8 provided in this shaft 7, a plurality of rotor blades 9 provided in the rotor 8, and a rotor cylindrical portion 10 provided on the outlet port 6 side (the thread groove pump portion). Note that the rotor portion is configured by the shaft 7 and the rotor 8.
(32) Each of the rotor blades 9 is configured by a disc-shaped disc member extending radially in a direction perpendicular to the axis of the shaft 7. In the present embodiment, the lowest stage of the rotor blades 9 (the outlet port 6 side) is configured as a disk to perform compression of the Siegbahn portion.
(33) The rotor cylindrical portion 10 is configured by a cylindrical member that is concentric with a rotation axis of the rotor 8.
(34) A motor portion for rotating the shaft 7 at high speed is provided approximately axially in the middle of the shaft 7, the motor portion being enclosed in a stator column 80.
(35) Furthermore, radial magnetic bearing devices for supporting the shaft 7 in the radial direction in a non-contact manner are provided within the stator column 80, at the inlet port 4 side and the outlet port side 6 with respect to the motor portion of the shaft 7. Also, an axial magnetic bearing device for supporting the shaft 7 in the axis direction (axial direction) in a non-contact manner is provided at a lower end of the shaft 7.
(36) A stator portion (stator portion) is formed on the inner circumferential side of the casing (casing 2). This stator portion is configured from stator blades 50 or the like which are inclined at a predetermined angle from a plane surface perpendicular to the axis of the shaft 7 and extend from an inner circumferential surface of the casing 2 toward the shaft 7. The stator blades 50 are separated from each other by cylindrical spacers (stator portions) and fixed.
(37) Note that the rotor blades 9 and the stator blades 50 are disposed alternately in a plurality of stages in the axis direction, but in order to meet the exhaust performance required in the vacuum pump, any number or rotor parts and any number of stator parts can be provided if necessary.
(38) Furthermore, in the present embodiment, the thread groove pump portion with a connected thread groove spacer 20 is provided close to the outlet port 6 from the Siegbahn pump portion mentioned above.
(39) As with a conventional thread groove spacer, in the connected thread groove spacer 20, a thread groove (spiral groove) is formed on a surface opposing the rotor cylindrical portion 10.
(40) The surface of the connected thread groove spacer 20 that opposes the rotor cylindrical portion 10 (i.e., an inner circumferential surface parallel to the axis of the vacuum pump 1) opposes an outer circumferential surface of the rotor cylindrical portion 10, with a predetermined clearance therebetween. When the rotor cylindrical portion 10 rotates at high speed, the gas that is compressed in the vacuum pump 1 is sent toward the outlet port 6 by being guided by the thread groove with the rotation of the rotor cylindrical portion 10. Specifically, the thread groove functions as a flow channel for transporting the gas.
(41) As described above, the surface of the connected thread groove spacer 20 which opposes the rotor cylindrical portion 10 opposes the rotor cylindrical portion 10, with the predetermined clearance therebetween, thereby configuring the gas transfer mechanism for transporting the gas by means of the thread groove formed on the axis direction-side inner circumferential surface of the connected thread groove spacer 20.
(42) The smaller the clearance is the better, in order to reduce the force of the gas flowing back toward the inlet port 4.
(43) The direction of the spiral groove formed in the connected thread groove spacer 20 is a direction toward the outlet port 6 when the gas is transported through the spiral groove in the direction of rotation of the rotor 8.
(44) The depth of the spiral groove becomes shallow toward the outlet port 6; the gas transported through the spiral groove becomes compressed more toward the outlet port 6.
(45) According to the foregoing configuration, in the vacuum pump 1, the gas that is drawn through the inlet port 4 is compressed in the Siegbahn portion, then compressed further in the thread groove pump portion, and discharged from the outlet port 6. Therefore, the vacuum pump 1 can perform a vacuum exhaust treatment in a vacuum chamber (not shown) provided in the vacuum pump 1.
(46) (ii-2) Configuration of Connected Thread Groove Spacer
(47) The connected thread groove spacer 20 is now described in detail.
(48)
(49) As shown in
(50) The thread groove spacer axis perpendicular portion 201 is configured to be substantially perpendicular (horizontal) to the axis direction of the vacuum pump 1. A surface of the thread groove spacer axis perpendicular portion 201 at the inlet port 4 side opposes the rotor blades 9 of the Siegbahn portion, with a predetermined clearance therebetween, and has a spiral groove with ridge portions and root portions engraved. On the other hand, a surface of the thread groove spacer axis perpendicular portion 201 on the side opposite to the inlet port 4 is provided on the base 3 side.
(51) The thread groove spacer axis parallel portion 202 is configured to be substantially parallel to the axis direction of the vacuum pump 1. A thread groove is formed on an inner circumferential surface of the thread groove spacer axis parallel portion 202 that opposes the rotor cylindrical portion 10, with a predetermined clearance therebetween.
(52) (ii-3-1) Type 1 of Basic Structure of Connection Portion
(53)
(54) As described above, a spiral groove with perpendicular portion ridge portions 300 and perpendicular portion root portions 400 is engraved in the thread groove spacer axis perpendicular portion 201, and a thread groove with parallel portion ridge portions 500 and parallel portion root portions 600 is formed in the thread groove spacer axis parallel portion 202.
(55) The connected thread groove spacer 20 of the present embodiment is produced by means of, for example, casting, wherein the thread groove spacer axis perpendicular portion 201 and the thread groove spacer axis parallel portion 202 are integrated to configure the connected thread groove spacer 20, as shown in
(56) Compared to creating the thread groove spacer axis perpendicular portion 201 and the thread groove spacer axis parallel portion 202 as separate parts and then tightening these parts together, integrally configuring the thread groove spacer axis perpendicular portion 201 and the thread groove spacer axis parallel portion 202 can reduce the time it takes for tightening these parts as well as the cost of manufacturing these parts.
(57) As described above, in the vacuum pump 1 according to the present embodiment, due to the connected thread groove spacer 20 provided therein, the gas is compressed by the thread groove spacer axis perpendicular portion 201 and the rotor blades 9 (the Siegbahn portion), in the flow channel perpendicular to the axial direction. Subsequently, the gas is further compressed by the thread groove spacer axis parallel portion 202 and the rotor cylindrical portion 10 (the thread groove pump portion), in the flow channel parallel to the axial direction.
(58) As described above, in the vacuum pump 1 according to the present embodiment, because the connected thread groove spacer 20 serves to extend the gas flow channel from the direction perpendicular to the axial direction to the direction parallel to the axial direction, a long flow channel for compressing the gas can be obtained without increasing the axial length (n) of the casing 2 or the axial length (m) of the base 3 (i.e., while preventing an increase in the entire height of the vacuum pump 1). Note that the flow channel extending from the perpendicular direction to the parallel direction is in the shape of an inverted L when viewed in axial cross section.
(59) In the present embodiment, the thread groove spacer axis perpendicular portion 201 and the thread groove spacer axis parallel portion 202 of the connected thread groove spacer 20 are configured integrally; however, the configuration is not limited thereto. For example, configuring the thread groove spacer axis perpendicular portion 201 and the thread groove spacer axis parallel portion 202 as separate parts shows no problems in terms of performance as long as the thread groove spacer axis perpendicular portion 201 and the thread groove spacer axis parallel portion 202 are formed into an inverted L shape extending from the direction perpendicular to the axial direction to the direction parallel to the axial direction.
(60)
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(62) Note that the details described hereinafter with reference to
(63)
(64) First, as shown in
(65) Moreover, in the perpendicular portion ridge portion 300 of the thread groove spacer axis perpendicular portion 201 and the parallel portion ridge portion 500 of the thread groove spacer axis parallel portion 202, the ridge portions (the perpendicular portion ridge portion 300 and the parallel portion ridge portion 500) of the two portions (the thread groove spacer axis perpendicular portion 201 and the thread groove spacer axis parallel portion 202) are configured to be continuous with each other on the extended lines of the borderlines between the respective ridge portions and the bottom surfaces at the joint (connection portion) between the thread groove spacer axis perpendicular portion 201 and the thread groove spacer axis parallel portion 202, but the ridge portions themselves (the top surfaces or peak surfaces) are not configured to be continuous, and configured in a non-continuous manner. In other words, a circumferential direction of the gas passage (flow channel) is opened.
(66) The joint here represents the whole area in which the thread groove spacer axis perpendicular portion 201 and the thread groove spacer axis parallel portion 202 of the connected thread groove spacer 20 overlap (meet) and that opposes the rotor blades 9 and the rotor cylindrical portion 10, as shown in
(67)
(68) As shown in
(69) Also, the perpendicular portion ridge portion 300 and the perpendicular portion root portion 400 have a predetermined inlet angle (2: defined as a second angle) at the outer diameter side (outer circumference side) of the thread groove spacer axis perpendicular portion 201 that corresponds to the inlet of the Siegbahn portion. This inlet angle 2 is formed by an outer diameter tangent of the thread groove spacer axis perpendicular portion 201 and the inner diameter-side tangent of the perpendicular portion ridge portion 300.
(70) Furthermore, in the connected thread groove spacer 20, the parallel portion ridge portion 500 and the parallel portion root portion 600 have a predetermined lead angle () at the inner diameter side of the outlet (the outlet port 6 side) of the thread groove spacer axis parallel portion 202. In this embodiment, the thread sectional area of the thread groove spacer axis parallel portion 202 in the joint structure becomes larger as the value of this lead angle becomes smaller Therefore, in the present embodiment in which the ridge width (the width of the top surface) of the Siegbahn portion is formed by taking an outer circumferential line of the cross section of the parallel portion ridge portion 500 on an upper surface of the thread groove portion (the thread groove spacer axis parallel portion 202) as a phase angle of the Siegbahn portion (the thread groove spacer axis perpendicular portion 201), the phase angle () of the ridge portion of the Siegbahn portion becomes large as well.
(71) Note that Z1 represents the depth of the outlet of the Siegbahn portion, or more specifically the length of the section between the line of the inner diameter of the thread groove spacer axis perpendicular portion 201 (the Siegbahn portion) and the line of the upper surface of the thread groove spacer axis parallel portion 202 (Holweck). L represents the axial length of the thread groove spacer axis parallel portion 202.
(72) (ii-3-2) Type 2 of Basic Structure of Connection Portion (Modification 1)
(73)
(74) As shown in
(75) However, according to the connected thread groove spacer 21 of Modification 1, unlike the connected thread groove spacer 20, in the perpendicular portion ridge portion 300 of the thread groove spacer axis perpendicular portion 211 and the parallel portion ridge portion 500 of the thread groove spacer axis parallel portion 212, the ridge portions (the perpendicular portion ridge portion 300 and the parallel portion ridge portion 500) of the two portions (the thread groove spacer axis perpendicular portion 211 and the thread groove spacer axis parallel portion 212) are formed to be continuous with each other (
(76) (ii-3-3) Type 3 of Basic Structure of Connection Portion (Modification 2)
(77)
(78) As shown in
(79) In the connected thread groove spacer 22 according to Modification 2, at the joint structure where the thread groove spacer axis perpendicular portion 221 and the thread groove spacer axis parallel portion 222 are connected (joined) to each other, the parallel portion ridge portion 500 of the thread groove spacer axis parallel portion 222 extends to the perpendicular portion ridge portion 300 of the thread groove spacer axis perpendicular portion 221, and the borderline surfaces between the ridge portions and root portions of these portions are connected to each other in a non-continuous manner.
(80) Therefore, the joint structure is a structure with an intersecting surface where the perpendicular portion ridge portion 300 and the parallel portion ridge portion 500 intersect with each other, wherein the circumferential direction of the gas passage is closed.
(81)
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(83)
(84) As shown in
(85) Also, as with the embodiment and Modification 1 described above, the perpendicular portion ridge portion 300 and the perpendicular portion root portion 400 have a predetermined inlet angle (2: defined as a second angle) at the outer diameter side of the thread groove spacer axis perpendicular portion 221 that corresponds to the inlet of the Siegbahn portion. This inlet angle 2 is formed by an outer diameter tangent of the thread groove spacer axis perpendicular portion 221 and the inner diameter-side tangent of the perpendicular portion ridge portion 300.
(86) In addition, the parallel portion ridge portion 500 and the parallel portion root portion 600 have a predetermined lead angle () on the parallel portion root portion 600 side at the inner diameter side of the outlet (the outlet port 6 side) of the thread groove spacer axis parallel portion 222. In Modification 2, as with the embodiment and Modification 1 described above, the thread sectional area of the thread groove spacer axis parallel portion 222 in the joint structure becomes larger as the value of this lead angle becomes smaller. Consequently, the phase angle () of each ridge portion of the Siegbahn portion becomes large as well.
(87) In Modification 2, unlike the embodiment and Modification 1 described above, the phase angle of each ridge portion of the Siegbahn portion is defined by the outer circumferential line of the intersecting surface described above (
(88) As shown in
(89) In Modification 2, therefore, since the intersecting surface is formed in the joint structure, the top surface of the perpendicular portion ridge portion 300 of the thread groove spacer axis perpendicular portion 221 and the top surface of the parallel portion ridge portion 500 of the thread groove spacer axis parallel portion 222 can be connected (joined) smoothly in a continuous manner without breaking. Consequently, the thread groove spacer axis perpendicular portion 221 and the thread groove spacer axis parallel portion 222 can be connected (joined) smoothly.
(90) (ii-4) Angles (Gradient) in Connected Thread Groove Spacer
(91)
(92) Note that the details described hereinafter with reference to
(93) As shown in
(94) This configuration can exhibit high exhaust performance of the connected thread groove spacer 20.
(95)
(96) Note that the details described hereinafter with reference to
(97)
(98) In the embodiment and each of the modifications according to the present invention, the following relation is established between the outlet angle 1 and the inlet angle 2.
12(1)
15<1, and 2<25(2)
(99) This configuration can exhibit high exhaust performance of the connected thread groove spacer 20 (21, 22).
(100)
(101) In
(102) As shown in
(103) According to this configuration, in the connected thread groove spacers 20 (21, 22) according to the embodiment and each modification of the present invention and the vacuum pump 1 in which the connected thread groove spacer 20 (21, 22) is provided, the gas is compressed in a direction perpendicular to the axial direction by the Siegbahn portion, which is configured by putting together (or integrating) the connected thread groove spacer 20 (21, 22) as a single part, and then the gas is compressed by the provided thread groove pump portion (Holweck) in the axial direction. Since the flow channel is made longer by connecting the passage extending in the direction perpendicular to the axial direction and the passage extending in the direction parallel to the axial direction (configuring the shape of an L when viewed in axial cross section), the height of the thread groove pump portion can be reduced while keeping the exhaust performance.
(104) As a result, the size of the entire pump can be reduced while keeping the exhaust performance thereof, resulting in reduction of the manufacturing cost.
(105) Note that the embodiment and modifications of the present invention may be combined as necessary.
(106) Although elements have been shown or described as separate embodiments above, portions of each embodiment may be combined with all or part of other embodiments described above.
(107) Although the subject matter has been described in language specific to structural features and/or methodological acts, 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 described as example forms of implementing the claims.