Scroll compressor including seal with axial length that is greater than radial width
09938975 ยท 2018-04-10
Assignee
Inventors
Cpc classification
F04C27/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C18/0223
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C18/0284
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F03C2/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F03C4/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C18/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04C2/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A scroll compressor 10 may include an orbiting scroll having an orbiting scroll wall extending axially from an orbiting scroll plate towards a fixed scroll; a fixed scroll having a fixed scroll wall extending axially from a fixed scroll plate towards the orbiting scroll; and an axially extending drive shaft having an eccentric shaft portion so that rotation of the eccentric shaft portion imparts an orbiting motion to the orbiting scroll relative to the fixed scroll. An axial end portion of the orbiting scroll wall has a first seal for sealing between the orbiting scroll wall and the fixed scroll plate, and an axial end portion of the fixed scroll wall has a second seal for sealing between the fixed scroll wall and the orbiting scroll plate; and the first seal or the second seal has an aspect ratio of axial length to radial width which is 1.25:1 or greater.
Claims
1. A pump including a scroll compressor comprising: an orbiting scroll; a fixed scroll having a fixed scroll wall extending in an axial direction from a fixed scroll plate towards the orbiting scroll, wherein the orbiting scroll has an orbiting scroll wall extending in the axial direction from an orbiting scroll plate towards the fixed scroll, wherein a radial direction is substantially orthogonal to the axial direction; and an axially extending drive shaft having an eccentric shaft portion so that rotation of the eccentric shaft portion imparts an orbiting motion to the orbiting scroll relative to the fixed scroll, wherein: an axial end portion of the orbiting scroll wall has a first groove for receiving a first seal for sealing between the orbiting scroll wall and the fixed scroll plate, and an axial end portion of the fixed scroll wall has a second groove for receiving a second seal for sealing between the fixed scroll wall and the orbiting scroll plate; the first seal or the second seal has an aspect ratio of an axial length to a radial width that is at least 1.25:1 or greater and the axial length ranges from 1.8 mm to 4 mm, and the radial width ranges from 1.2 mm to 2.6 mm; and the first seal or the second seal is received in the respective first groove or second groove with a radial clearance such that a first spiral portion of the first seal or the second seal is located at the radially inner side of the first groove or the second groove, a second spiral portion of the first seal or the second seal is located at the radially outer side of the first groove or the second groove, and in between the first spiral portion and the second spiral portion, an intermediate portion of the first seal or the second seal extends between the radially inner side and the radially outer side of the first groove or the second groove.
2. The scroll compressor of claim 1, wherein the first seal comprises the first and second spiral portions, wherein the second seal comprises a third spiral portion having a third aspect ratio of the axial length to the radial width and a fourth spiral portion having a fourth aspect ratio of the axial length to the radial width, and wherein both the third aspect ratio and the fourth aspect ratio are at least 1.25:1.
3. The scroll compressor of claim 2, wherein the axial end portion of the orbiting scroll wall has a channel for locating the first seal, and wherein the axial end portion of the fixed scroll wall has a channel for locating the second seal.
4. The scroll compressor of claim 2, wherein at least one of the third aspect ratio or the fourth aspect ratio is at least 1.5:1 or greater.
5. The scroll compressor of claim 4, wherein at least one of the third aspect ratio or the fourth aspect ratio is at least 2:1 or greater.
6. The scroll compressor of claim 1, wherein the axial end portion of the orbiting scroll wall has a channel for locating the first seal, and wherein the axial end portion of the fixed scroll wall has a channel for locating the second seal.
7. The scroll compressor of claim 1, wherein the first aspect ratio and the second aspect ratio are different.
8. A seal for a pump including a scroll compressor comprising an orbiting scroll; a fixed scroll having a fixed scroll wall extending in an axial direction from a fixed scroll plate towards the orbiting scroll, wherein the orbiting scroll has an orbiting scroll wall extending in the axial direction from an orbiting scroll plate towards the fixed scroll, wherein a radial direction is substantially orthogonal to the axial direction, and wherein the orbiting scroll wall defines a groove; and an axially extending drive shaft having an eccentric shaft portion so that rotation of the eccentric shaft portion imparts an orbiting motion to the orbiting scroll relative to the fixed scroll, wherein the seal comprises: a first portion having a first aspect ratio of an axial length to a radial width and a second portion having a second aspect ratio of the axial length to the radial width, wherein both the first aspect ratio and the second aspect ratio are at least 1.25:1 or greater and the axial length ranges from 1.8 mm to 4 mm, and the radial width ranges from 1.2 mm to 2.6 mm, wherein the seal is configured to extend between the orbiting scroll wall and the fixed scroll plate and form a seal there between, and wherein the radial width of the seal is sized to be received in the groove with a radial clearance such that a first spiral portion of the seal is located at the radially inner side of the groove, a second spiral portion of the seal is located at the radially outer side of the groove, and in between the first spiral portion and the second spiral portion, an intermediate portion of the seal extends between the radially inner side and the radially outer side of the groove.
9. The seal of claim 8, wherein at least one of the first aspect ratio or the second aspect ratio is 1.5:1 or greater.
10. The seal of claim 9, wherein at least one of the first aspect ratio or the second aspect ratio is at least 2:1 or greater.
11. The seal of claim 8, wherein the seal is configured to be located in the groove of an axial end portion of the orbiting scroll wall.
12. The seal of claim 8, wherein the first aspect ratio and the second aspect ratio are different.
13. A seal for a pump including a scroll compressor comprising an orbiting scroll; a fixed scroll having a fixed scroll wall extending in an axial direction from a fixed scroll plate towards the orbiting scroll, wherein the fixed scroll wall defines a groove, wherein the orbiting scroll has an orbiting scroll wall extending in an axial direction from an orbiting scroll plate towards the fixed scroll, wherein a radial direction is substantially orthogonal to the axial direction; and an axially extending drive shaft having an eccentric shaft portion so that rotation of the eccentric shaft portion imparts an orbiting motion to the orbiting scroll relative to the fixed scroll, wherein the seal comprises: a first portion having a first aspect ratio of an axial length to a radial width and a second portion having a second aspect ratio of the axial length to the radial width, wherein both the first aspect ratio and the second aspect ratio are at least 1.25:1 or greater and the axial length ranges from 1.8 mm to 4 mm, and the radial width ranges from 1.2 mm to 2.6 mm, wherein the seal is configured to extend between the fixed scroll wall and the orbiting scroll plate and form a seal there between, and wherein the radial width of the seal is sized to be received in the groove with a radial clearance such that a first spiral portion of the seal is located at the radially inner side of the groove, a second spiral portion of the seal is located at the radially outer side of the groove, and in between the first spiral portion and the second spiral portion, an intermediate portion of the seal extends between the radially inner side and the radially outer side of the groove.
14. The seal of claim 13, wherein at least one of the first aspect ratio or the second aspect ratio is 1.5:1 or greater.
15. The seal of claim 14, wherein at least one of the first aspect ratio or the second aspect ratio is at least 2:1 or greater.
16. The scroll compressor of claim 13, wherein the seal is configured to be located in the groove of an axial end portion of the fixed scroll wall.
17. The seal of claim 13, wherein the first aspect ratio and the second aspect ratio are different.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In order that the present invention may be well understood, an embodiment thereof, which is given by way of example only, will now be described with reference to the accompanying drawings, in which:
(2)
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DETAILED DESCRIPTION
(7) A section through part of a fixed scroll 50 is shown in
(8) The fixed scroll 50 shown in
(9) The description herein refers to the tip seal of the fixed scroll. It will be appreciated however that additionally or alternatively a similar tip seal arrangement may be provided for the orbiting scroll.
(10) When the tip seal is installed, the tip seal 58 has an aspect ratio of axial length, L, to radial width, W, (as shown in
(11) The arrangement shown offers a number of advantages over the prior art. When manufacturing the tip seal 58 from the materials used currently, the wear rate and tip-seal life (pressure-velocity regime) remains generally unchanged. Additionally, tip seal 58 shows shorter bedding-in or stabilization times. The tip seal 58 is thinner, and therefore more flexible, in the radial direction; in addition, its sectional area is smaller, making it also more flexible in the axial direction. Therefore it demonstrates better capability of presenting its full axial end face 62 against the orbiting scroll. Accordingly, most if not all of the axial face becomes bedded in quickly during initial use.
(12) As the axial end face 62 occupies relatively less area than the axial end face of the prior art tip seal, less dust is generated due to abrasion against the orbiting scroll during use. As dust generated during use must be periodically removed, less dust generation decreases the cost of ownership. Further, in the prior art where the tip seal is relatively stiff in the radial direction, only a portion or corner of the axial end face may be presented to the orbiting scroll. It will be appreciated that whilst in the embodiment the axial end face is smaller than the axial end face in the prior art, a more flexible seal is better able to present its entire end face to the orbiting scroll whereas in the prior art only a corner of the scroll end face may be presented to the orbiting scroll.
(13)
(14) In both
(15) In more detail, when considering the full length of the tip seals 36, 58 at any given time during use of the pump, first portions 68, 70 of the tip seals are located at the radially inner side 72 of the groove 74 and second portions 76, 78 of the tip seals are located at the radially outer side 80 of the groove. In between first and second portions, intermediate portions 82, 84 of the tip seals 36, 58 bridge the gap between the radially inner side 72 and the radially outer side 80 of the groove. Fluid can leak across the tip seals at the intermediate portions, since there is a leakage path which extends between the tip seals and the radially inner side 72 of the groove, underneath the tip seals and between the tip seals and the radially outer side 80 of the groove. That is, at the intermediate portions 82, 84 the tip seal does not block the seepage path by pressing against one of the sides of the groove. The prior art tip seal 36 has a larger radial width to axial depth and is therefore relatively stiff in the radial direction. Consequently, the length of the intermediate portions 82 are longer meaning that more leakage occurs. The tip seal 58 has a smaller radial width to axial depth (a greater axial depth to radial width ratio) and is therefore relatively flexible in the radial direction. Consequently, the length of the intermediate portions 84 are shorter meaning that less leakage occurs.
(16) A further advantage of the present embodiment is that the space occupied by the tip seal is smaller in the radial direction and therefore scroll wall thickness is reduced. Accordingly, as shown in
(17)
(18) As described above, at different points along the length of a single tip-seal 58, the seal is located in the position shown in either
(19) As indicated above, one or both of the tip seals may have increased aspect ratio of more than 1.25:1 (axial length to radial width). Preferably, the aspect ratio is approximately the same along the full length of the each tip seals, however one or both of the tips seals may have different aspect ratios along their lengths. As such, in some examples, the first tip seal (the tip seal of the fixed scroll) may include a first aspect ratio of more than 1.25:1 and a second, different aspect ratio of more than 1.25:1, and the second tip seal (the tip seal of the orbiting scroll) may include a third aspect ratio of more than 1.25:1 and a fourth, different aspect ratio of more than 1.25:1. In some examples, each of the first aspect ratio, the second aspect ratio, the third aspect ratio, and the third ratio may be more than 1.5:1, or each may be more than 2:1.
(20) Whilst a scroll compressor is typically operated for pumping fluid, instead it can operated as a generator for generating electrical energy when pressurized fluid is used to rotate the orbiting scroll relative to the fixed scroll. The present invention is intended to cover use of the scroll compressor for pumping and energy generation.