TWM651447U - Compressor - Google Patents

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Publication number
TWM651447U
TWM651447U TW112208508U TW112208508U TWM651447U TW M651447 U TWM651447 U TW M651447U TW 112208508 U TW112208508 U TW 112208508U TW 112208508 U TW112208508 U TW 112208508U TW M651447 U TWM651447 U TW M651447U
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Taiwan
Prior art keywords
bushing
compressor
positioning protrusion
main axis
angle
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TW112208508U
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Chinese (zh)
Inventor
李訓安
李宣甫
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復盛股份有限公司
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Application filed by 復盛股份有限公司 filed Critical 復盛股份有限公司
Publication of TWM651447U publication Critical patent/TWM651447U/en

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Abstract

A compressor including a housing, a motor disposed in the housing, a driving shaft connected to the motor, a first compression mechanism connected to the driving shaft and a second compression mechanism is provided. The driving shaft passes through a first compression chamber of the housing and extends into a second compression chamber of the housing. The first compression mechanism and the second compression mechanism are respectively disposed in the first compression chamber and the second compression chamber. The second compression mechanism includes a stationary scroll, a movable scroll engaged with the stationary scroll, a bushing seat positioned at an end portion of the driving shaft, a bushing and a bearing. A main axis of the driving shaft passes through a positioning protrusion of the bushing seat, and the positioning protrusion deviates from a straight line formed by a plurality of contact points between the movable scroll and the stationary scroll in an angle. The bushing is sleeved on the positioning protrusion, and a center line of the bushing is eccentric to the main axis. The bearing is sleeved on the bushing, and the movable scroll is sleeved on the bearing.

Description

壓縮機compressor

本新型創作是有關於一種壓縮機。 The new invention relates to a compressor.

在蒸發器的低壓氣態流體送入二級壓縮機後,先後在第一壓縮腔與第二壓縮腔內分別經第一壓縮機構與第二壓縮機構壓縮形成高壓氣態流體,以提高製冷循環效率。舉例來說,第一壓縮機構可為螺桿壓縮機構,且第二壓縮機構可為渦卷壓縮機構。 After the low-pressure gaseous fluid from the evaporator is sent to the two-stage compressor, it is compressed in the first compression chamber and the second compression chamber respectively by the first compression mechanism and the second compression mechanism to form a high-pressure gaseous fluid to improve the refrigeration cycle efficiency. For example, the first compression mechanism may be a screw compression mechanism, and the second compression mechanism may be a scroll compression mechanism.

詳細而言,渦卷壓縮機構包括動渦卷與靜渦卷,且馬達透過驅動軸帶動動渦卷相對於靜渦卷繞動。隨著動渦卷的繞動,動渦卷與靜渦卷在徑向上產生多個接觸點,以形成容積由外圍向中心逐漸縮減的多個壓縮空間,使得氣態流體不斷地被加壓,以轉變成高壓氣態流體,並由靜渦卷的中心排出第二壓縮腔。 Specifically, the scroll compression mechanism includes an movable scroll and a fixed scroll, and the motor drives the movable scroll to orbit relative to the fixed scroll through the drive shaft. As the movable scroll revolves, the movable scroll and the stationary scroll generate multiple contact points in the radial direction to form multiple compression spaces whose volumes gradually decrease from the periphery to the center, so that the gaseous fluid is continuously pressurized to It is converted into high-pressure gaseous fluid and discharged from the second compression chamber through the center of the static scroll.

一般而言,驅動軸的端部為偏心軸部,其中襯套套接於偏心軸部,且動渦卷透過軸承套接於襯套。因此,繞動時的動渦卷所產生的慣性力會傳至偏心軸部上,不僅加大了軸承的負荷,也導致軸承受力不均,使得軸承的特定區域產生嚴重的磨損,影響到了壓縮機的運轉效率及使用壽命。 Generally speaking, the end of the driving shaft is an eccentric shaft part, wherein the bushing is sleeved on the eccentric shaft part, and the orbiting scroll is sleeved on the bushing through the bearing. Therefore, the inertial force generated by the orbiting scroll will be transmitted to the eccentric shaft, which not only increases the load on the bearing, but also causes uneven force on the bearing, causing severe wear in specific areas of the bearing, affecting the The operating efficiency and service life of the compressor.

另一方面,襯套在徑向上可滑動地套接於偏心軸部,且動渦卷可隨襯套在徑向上同步滑動。因動渦卷與靜渦卷之間的多個接觸點在徑向上連成一直線,並與襯套的徑向滑動路徑及退讓路徑重合,當多個壓縮空間的產生異常高壓時,動渦卷與襯套不易在徑向上滑動,即動渦卷與襯套不易產生徑向退讓,導致動渦卷無法順暢地相對於靜渦卷繞動。 On the other hand, the bushing is slidably sleeved on the eccentric shaft portion in the radial direction, and the movable scroll can slide synchronously with the bushing in the radial direction. Because the multiple contact points between the movable scroll and the stationary scroll are connected in a straight line in the radial direction and coincide with the radial sliding path and retreat path of the bushing, when abnormal high pressure is generated in multiple compression spaces, the movable scroll It is not easy for the movable scroll and the bushing to slide in the radial direction, that is, the movable scroll and the bushing are not easy to retreat in the radial direction, resulting in the movable scroll unable to smoothly rotate relative to the fixed scroll.

本新型提供一種壓縮機,有助於提升運轉效率及使用壽命。 The new model provides a compressor that helps improve operating efficiency and service life.

本新型創作提出一種壓縮機,包括殼體、馬達、驅動軸、第一壓縮機構以及第二壓縮機構。殼體具有相連通的第一壓縮腔與第二壓縮腔。馬達設置於殼體內。驅動軸連接於馬達。驅動軸穿過第一壓縮腔,且延伸至第二壓縮腔。第一壓縮機構設置於第一壓縮腔內,且連接於驅動軸。第二壓縮機構設置於第二壓縮腔內,且包括靜渦卷、動渦卷、襯套座、襯套以及軸承。動渦卷嚙合於靜渦卷,並與靜渦卷之間具有多個接觸點,以形成多個壓縮空間。襯套座定位於驅動軸的端部,且具有定位凸部。驅動軸的主軸線通過定位凸部,且定位凸部相對於多個接觸點所連成的直線偏擺一角度。襯套套接於定位凸部,且襯套的中心線偏心於主軸線。軸承套接於襯套,且動渦卷套接於軸承。 This new invention proposes a compressor, which includes a housing, a motor, a drive shaft, a first compression mechanism and a second compression mechanism. The housing has a first compression chamber and a second compression chamber that are connected. The motor is arranged in the housing. The drive shaft is connected to the motor. The drive shaft passes through the first compression chamber and extends to the second compression chamber. The first compression mechanism is disposed in the first compression chamber and connected to the drive shaft. The second compression mechanism is disposed in the second compression chamber and includes a fixed scroll, a movable scroll, a bushing seat, a bushing and a bearing. The movable scroll meshes with the fixed scroll and has multiple contact points with the fixed scroll to form multiple compression spaces. The bushing seat is positioned at the end of the drive shaft and has a positioning protrusion. The main axis of the drive shaft passes through the positioning protrusion, and the positioning protrusion is deflected at an angle relative to a straight line connected by multiple contact points. The bushing is sleeved on the positioning protrusion, and the center line of the bushing is eccentric to the main axis. The bearing is sleeved on the bushing, and the movable scroll is sleeved on the bearing.

本新型創作提出另一種壓縮機,包括殼體、馬達、驅動 軸以及壓縮機構。殼體具有壓縮腔。馬達設置於殼體內。驅動軸連接於馬達。驅動軸延伸至壓縮腔。壓縮機構設置於壓縮腔內,且包括靜渦卷、動渦卷、襯套座、襯套以及軸承。動渦卷嚙合於靜渦卷,並與靜渦卷之間具有多個接觸點,以形成多個壓縮空間。襯套座定位於驅動軸的端部,且具有定位凸部。驅動軸的主軸線通過定位凸部,且定位凸部相對於多個接觸點所連成的直線偏擺一角度。襯套套接於定位凸部,且襯套的中心線偏心於主軸線。軸承套接於襯套,且動渦卷套接於軸承。 This new creation proposes another compressor, including a casing, a motor, a drive shaft and compression mechanism. The housing has a compression chamber. The motor is arranged in the housing. The drive shaft is connected to the motor. The drive shaft extends into the compression chamber. The compression mechanism is arranged in the compression chamber and includes a fixed scroll, a moving scroll, a bushing seat, a bushing and a bearing. The movable scroll meshes with the fixed scroll and has multiple contact points with the fixed scroll to form multiple compression spaces. The bushing seat is positioned at the end of the drive shaft and has a positioning protrusion. The main axis of the drive shaft passes through the positioning protrusion, and the positioning protrusion is deflected at an angle relative to a straight line connected by multiple contact points. The bushing is sleeved on the positioning protrusion, and the center line of the bushing is eccentric to the main axis. The bearing is sleeved on the bushing, and the movable scroll is sleeved on the bearing.

基於上述,在本新型創作的壓縮機中,襯套座定位於驅動軸的端部,其中動渦卷透過軸承與襯套連接於襯套座的定位凸部,且襯套的中心線偏心於驅動軸的主軸線。詳細而言,動渦卷與靜渦卷之間的多個接觸點,以形成多個密閉空間,且定位凸部相對於多個接觸點所連成的直線偏擺一角度,使得軸承可在動渦卷繞動時平均受力,防止軸承的特定區域因受力過大而產生嚴重的磨損,據以提升壓縮機的運轉效率及使用壽命。 Based on the above, in the compressor created by the present invention, the bushing seat is positioned at the end of the drive shaft, in which the movable scroll is connected to the positioning protrusion of the bushing seat through the bearing and the bushing, and the center line of the bushing is eccentric to The main axis of the drive shaft. Specifically, multiple contact points between the movable scroll and the fixed scroll form multiple closed spaces, and the positioning convex portion is deflected at an angle relative to the straight line connected by the multiple contact points, so that the bearing can When the movable scroll rotates, the force is evenly applied to prevent specific areas of the bearing from being severely worn due to excessive force, thereby improving the operating efficiency and service life of the compressor.

為讓本新型創作的上述特徵和優點能更明顯易懂,下文特舉實施例,並配合所附圖式作詳細說明如下。 In order to make the above-mentioned features and advantages of the present invention more obvious and easy to understand, examples are given below and explained in detail with the accompanying drawings.

10、20:壓縮機 10, 20: Compressor

11、21:殼體 11, 21: Shell

11a:第一壓縮腔 11a: First compression chamber

11b:第二壓縮腔 11b: Second compression chamber

12、22:馬達 12, 22: Motor

13、23:驅動軸 13, 23: Drive shaft

13a:端部 13a: end

13b:主軸線 13b: Main axis

14:第一壓縮機構 14:First compression mechanism

21a:壓縮腔 21a:Compression chamber

100:第二壓縮機構 100: Second compression mechanism

100a:壓縮機構 100a: Compression mechanism

101:接觸點 101:Contact point

102:壓縮空間 102: Compressed space

103:直線 103: straight line

110:靜渦卷 110:Static Uzumaki

120:動渦卷 120: Moving scroll

130、130a、130b:襯套座 130, 130a, 130b: bushing seat

131:定位凸部 131: Positioning convex part

131a:定位基準線 131a: Positioning baseline

131b:第一穿孔 131b: First perforation

131c:第二穿孔 131c: Second perforation

1311、1421:長邊 1311, 1421: long side

1312、1422:短邊 1312, 1422: short side

132:第一承靠面 132:First supporting surface

133:第二承靠面 133:Second supporting surface

134:承靠斜面 134: Supporting slope

140:襯套 140: Bushing

141:中心線 141: Center line

142:穿槽 142:Through groove

150:軸承 150:Bearing

160:固定塊 160: fixed block

170:鎖定件 170: Locking piece

A、B:部位 A, B: parts

α、β:角度 α, β: angle

I-I、J-J:線段 I-I, J-J: line segments

圖1A是本新型創作一實施例的壓縮機的示意圖。 Figure 1A is a schematic diagram of a compressor according to an embodiment of the present invention.

圖1B是圖1A的壓縮機的側視示意圖。 Figure 1B is a schematic side view of the compressor of Figure 1A.

圖1C是圖1A的壓縮機沿線段I-I的剖面示意圖。 FIG. 1C is a schematic cross-sectional view of the compressor of FIG. 1A along line section I-I.

圖1D是圖1C中的部位A的局部放大示意圖。 Figure 1D is a partially enlarged schematic view of part A in Figure 1C.

圖1E是圖1A的壓縮機沿線段J-J的剖面示意。 FIG. 1E is a cross-sectional view of the compressor of FIG. 1A along line section J-J.

圖1F是圖1E中的部位B的局部放大示意圖。 Figure 1F is a partially enlarged schematic view of part B in Figure 1E.

圖2A是本新型創作一實施例的動渦卷與襯套座的組合示意圖。 Figure 2A is a schematic diagram of the combination of the movable scroll and the bushing seat according to an embodiment of the present invention.

圖2B是圖2A的爆炸示意圖。 Figure 2B is an exploded diagram of Figure 2A.

圖2C是圖2B的軸承、襯套及襯套座的正視示意圖。 Figure 2C is a schematic front view of the bearing, bushing and bushing seat of Figure 2B.

圖2D與圖2E是圖2C的襯套座在二個不同視角的示意圖。 FIG. 2D and FIG. 2E are schematic views of the bushing seat in FIG. 2C from two different viewing angles.

圖3A與圖3B是本新型創作另一實施例的襯套座在二個不同視角的示意圖。 3A and 3B are schematic views of the bushing seat from two different angles according to another embodiment of the present invention.

圖4A是本新型創作又一實施例的軸承、襯套及襯套座的正視示意圖。 Figure 4A is a schematic front view of a bearing, bushing and bushing seat according to another embodiment of the present invention.

圖4B是圖4A的襯套座的示意圖。 Figure 4B is a schematic view of the bushing seat of Figure 4A.

圖5是本新型創作另一實施例的壓縮機的剖面示意圖。 Figure 5 is a schematic cross-sectional view of a compressor according to another embodiment of the present invention.

圖1A是本新型創作一實施例的壓縮機的示意圖。圖1B是圖1A的壓縮機的側視示意圖。圖1C是圖1A的壓縮機沿線段I-I的剖面示意圖。圖1D是圖1C中的部位A的局部放大示意圖。請參考圖1A至圖1C,在本實施例中,壓縮機10可為二級壓縮機,且包括殼體11、馬達12、驅動軸13、第一壓縮機構14以及第二 壓縮機構100。詳細而言,殼體11具有相連通的第一壓縮腔11a與第二壓縮腔11b,其中馬達12設置於殼體11內,且驅動軸13連接於馬達12。第一壓縮機構14與第二壓縮機構100分別設置於第一壓縮腔11a與第二壓縮腔11b內,其中驅動軸13穿過第一壓縮腔11a,且延伸至第二壓縮腔11b。 Figure 1A is a schematic diagram of a compressor according to an embodiment of the present invention. Figure 1B is a schematic side view of the compressor of Figure 1A. FIG. 1C is a schematic cross-sectional view of the compressor of FIG. 1A along line section I-I. Figure 1D is a partially enlarged schematic view of part A in Figure 1C. Please refer to FIGS. 1A to 1C . In this embodiment, the compressor 10 may be a two-stage compressor and includes a housing 11 , a motor 12 , a drive shaft 13 , a first compression mechanism 14 and a second compressor. Compression mechanism 100. In detail, the housing 11 has a first compression chamber 11 a and a second compression chamber 11 b that communicate with each other. The motor 12 is disposed in the housing 11 , and the drive shaft 13 is connected to the motor 12 . The first compression mechanism 14 and the second compression mechanism 100 are respectively disposed in the first compression chamber 11a and the second compression chamber 11b, wherein the drive shaft 13 passes through the first compression chamber 11a and extends to the second compression chamber 11b.

請參考圖1C與圖1D,第一壓縮機構14可螺桿壓縮機構,且第二壓縮機構100可為渦卷壓縮機構。第一壓縮機構14連接於驅動軸13,且第二壓縮機構100連接於驅動軸13中位於第二壓縮腔11b內的端部13a。馬達12可透過驅動軸13帶動第一壓縮機構14與第二壓縮機構100同步運轉,使得低壓氣態流體先後在第一壓縮腔11a與第二壓縮腔11b內分別經第一壓縮機構14與第二壓縮機構100壓縮形成高壓氣態流體,然後自第二壓縮腔11b排出。 Please refer to FIG. 1C and FIG. 1D. The first compression mechanism 14 can be a screw compression mechanism, and the second compression mechanism 100 can be a scroll compression mechanism. The first compression mechanism 14 is connected to the drive shaft 13, and the second compression mechanism 100 is connected to the end 13a of the drive shaft 13 located in the second compression chamber 11b. The motor 12 can drive the first compression mechanism 14 and the second compression mechanism 100 to operate synchronously through the drive shaft 13, so that the low-pressure gaseous fluid passes through the first compression mechanism 14 and the second compression chamber 11b respectively in the first compression chamber 11a and the second compression chamber 11b. The compression mechanism 100 compresses the high-pressure gaseous fluid and then discharges it from the second compression chamber 11b.

圖1E是圖1A的壓縮機沿線段J-J的剖面示意。圖1F是圖1E中的部位B的局部放大示意圖。請參考圖1C至圖1F,在本實施例中,第二壓縮機構100包括靜渦卷110、動渦卷120、襯套座130、襯套140以及軸承150。靜渦卷110在第二壓縮腔11b內固定不動,且動渦卷120嚙合於靜渦卷110。動渦卷120可被驅動軸13帶動而相對於靜渦卷110繞動,在動渦卷120相對於靜渦卷110繞動的過程中,動渦卷120與靜渦卷110之間產生多個接觸點101,並形成容積由外圍向中心逐漸縮減的多個壓縮空間102,使得氣態流體不斷地被加壓,以轉變成高壓氣態流體,然後由靜渦 卷110的中心排出第二壓縮腔11b。 FIG. 1E is a cross-sectional view of the compressor of FIG. 1A along line section J-J. Figure 1F is a partially enlarged schematic view of part B in Figure 1E. Please refer to FIGS. 1C to 1F . In this embodiment, the second compression mechanism 100 includes a fixed scroll 110 , an orbiting scroll 120 , a bushing seat 130 , a bushing 140 and a bearing 150 . The fixed scroll 110 is fixed in the second compression chamber 11b, and the movable scroll 120 is meshed with the fixed scroll 110. The orbiting scroll 120 can be driven by the driving shaft 13 to orbit relative to the stationary scroll 110. During the orbiting process of the orbiting scroll 120 relative to the stationary scroll 110, multiple scrolls are generated between the orbiting scroll 120 and the stationary scroll 110. contact points 101, and form multiple compression spaces 102 whose volumes gradually decrease from the periphery to the center, so that the gaseous fluid is continuously pressurized to transform into a high-pressure gaseous fluid, and then is transformed into a high-pressure gaseous fluid by a static vortex. The center of the roll 110 discharges the second compression chamber 11b.

請參考圖1D至圖1F,襯套座130定位於驅動軸13的端部13a,且具有向靜渦卷110凸伸的定位凸部131。驅動軸13的主軸線13b通過定位凸部131,且定位凸部131相對於多個接觸點101所連成的直線103偏擺角度α。另一方面,動渦卷120透過軸承150與襯套140連接於襯套座130的定位凸部131,其中動渦卷120套接於軸承150,且軸承150套接於襯套140。襯套140套接於定位凸部131,且襯套140的中心線141偏心於主軸線13b。 Referring to FIGS. 1D to 1F , the bushing seat 130 is positioned at the end 13 a of the drive shaft 13 and has a positioning protrusion 131 protruding toward the stationary scroll 110 . The main axis 13b of the driving shaft 13 passes through the positioning protrusion 131, and the positioning protrusion 131 is deflected by an angle α relative to the straight line 103 connected by the plurality of contact points 101. On the other hand, the orbiting scroll 120 is connected to the positioning protrusion 131 of the bushing seat 130 through the bearing 150 and the bushing 140 . The orbiting scroll 120 is sleeved on the bearing 150 , and the bearing 150 is sleeved on the bushing 140 . The bushing 140 is sleeved on the positioning protrusion 131, and the center line 141 of the bushing 140 is eccentric to the main axis 13b.

因此,當驅動軸13帶動襯套座130旋轉時,動渦卷120、軸承150以及襯套140可繞主軸線13b偏心繞動。在定位凸部131相對於直線103偏擺角度α的設計下,軸承150可在動渦卷120繞動時平均受力,防止軸承150的特定區域因受力過大而產生嚴重的磨損,據以提升壓縮機10的運轉效率及使用壽命。 Therefore, when the driving shaft 13 drives the bushing seat 130 to rotate, the movable scroll 120, the bearing 150 and the bushing 140 can revolve eccentrically around the main axis 13b. Under the design of the deflection angle α of the positioning protrusion 131 relative to the straight line 103, the bearing 150 can receive the force evenly when the movable scroll 120 revolves, preventing a specific area of the bearing 150 from being severely worn due to excessive force. Accordingly, The operating efficiency and service life of the compressor 10 are improved.

舉例來說,定位凸部131相對於多個接觸點101所連成的直線103偏擺角度α可為銳角,較佳地,角度α可以是介於5度至45度,優選地,角度α可以是等於15度。 For example, the deflection angle α of the positioning protrusion 131 relative to the straight line 103 connected by the plurality of contact points 101 may be an acute angle. Preferably, the angle α may be between 5 degrees and 45 degrees. Preferably, the angle α It can be equal to 15 degrees.

請參考圖1D至圖1F,在本實施例中,襯套140具有穿槽142,其中定位凸部131設置於穿槽142內,且定位凸部131的高度小於穿槽142的深度。藉由定位凸部131與穿槽142的配合,襯套140可在設定的行程內相對於襯套座130往復或徑向滑動,且無法相對於襯套座130旋轉。依穿槽142的主延伸方向而論,穿槽142相對於多個接觸點101所連成的直線103偏擺角度 α。進一步來說,定位凸部131具有通過主軸線13b且平行於穿槽142的定位基準線131a,且定位基準線131a與多個接觸點101所連成的直線103之間夾有角度α。 Please refer to FIGS. 1D to 1F . In this embodiment, the bushing 140 has a through groove 142 , in which the positioning protrusion 131 is disposed in the through groove 142 , and the height of the positioning protrusion 131 is less than the depth of the through groove 142 . Through the cooperation of the positioning protrusion 131 and the through groove 142, the bushing 140 can reciprocate or slide radially relative to the bushing seat 130 within a set stroke, and cannot rotate relative to the bushing seat 130. According to the main extension direction of the through groove 142, the through groove 142 is deflected relative to the straight line 103 formed by the plurality of contact points 101. α. Furthermore, the positioning protrusion 131 has a positioning reference line 131 a passing through the main axis 13 b and parallel to the through groove 142 , and there is an angle α between the positioning reference line 131 a and the straight line 103 connecting the plurality of contact points 101 .

換句話說,定位凸部131與穿槽142的配合決定了襯套140與動渦卷120的滑動路徑及退讓路徑,且襯套140的滑動路徑及退讓路徑與定位基準線131a重合。因此,襯套140的滑動路徑及退讓路徑與多個接觸點101所連成的直線103之間夾有角度α。 In other words, the cooperation between the positioning protrusion 131 and the through groove 142 determines the sliding path and retreat path of the bushing 140 and the movable scroll 120, and the sliding path and retreat path of the bushing 140 coincide with the positioning reference line 131a. Therefore, there is an angle α between the sliding path and the retreat path of the bushing 140 and the straight line 103 connecting the plurality of contact points 101 .

請參考圖1F,定位凸部131還具有相對的二個長邊1311與相對的二個短邊1312,且二個短邊1312連接於二個長邊1311之間。具體而言,由於二個長邊1311平行於定位基準線131a,因此二個長邊1311可以是分別繞順時針和逆時針方向相對於多個接觸點101所連成的直線103偏擺角度α。另外,定位基準線131a延伸通過二個短邊1312。 Please refer to FIG. 1F , the positioning protrusion 131 also has two opposite long sides 1311 and two opposite short sides 1312 , and the two short sides 1312 are connected between the two long sides 1311 . Specifically, since the two long sides 1311 are parallel to the positioning reference line 131a, the two long sides 1311 can be deflected by the angle α of the straight line 103 connected in the clockwise and counterclockwise directions relative to the plurality of contact points 101. . In addition, the positioning reference line 131a extends through the two short sides 1312.

相應地,穿槽142具有分別面對於二個長邊1311的二個長邊1421與分別面對於二個短邊1312的二個短邊1422,其中二個長邊1421平行於定位基準線131a,且定位基準線131a延伸通過二個短邊1422。由於二個長邊1421平行於定位基準線131a,因此二個長邊1421可以是分別繞順時針和逆時針方向相對於多個接觸點101所連成的直線103偏擺角度α。 Correspondingly, the through groove 142 has two long sides 1421 respectively facing the two long sides 1311 and two short sides 1422 respectively facing the two short sides 1312, wherein the two long sides 1421 are parallel to the positioning reference line 131a, And the positioning reference line 131a extends through the two short sides 1422. Since the two long sides 1421 are parallel to the positioning reference line 131a, the two long sides 1421 may be deflected by an angle α relative to the straight line 103 formed by the plurality of contact points 101 in clockwise and counterclockwise directions respectively.

請參考圖1D至圖1F,在動渦卷120相對於靜渦卷110繞動的過程中,動渦卷120、軸承150及襯套140可在徑向上同步地相對於襯套座130及靜渦卷110滑動,且襯套140的徑向滑動 路徑及退讓路徑相對於多個接觸點101所連成的直線103偏擺角度α(即襯套140的徑向滑動路徑及退讓路徑未與多個接觸點101所連成的直線103重合),由於直線103方向與退讓方向(平行於定位基準線131a)不同,因此即便多個壓縮空間102產生異常高壓,動渦卷120、軸承150及襯套140仍可在徑向上滑動或產生徑向退讓,以維持動渦卷120的繞動順暢度,有助於提升壓縮機10的運轉效率。 Please refer to FIGS. 1D to 1F . During the orbiting process of the orbiting scroll 120 relative to the stationary scroll 110 , the orbiting scroll 120 , the bearing 150 and the bushing 140 can be synchronously radially rotated relative to the bushing seat 130 and the stationary scroll 110 . Scroll 110 slides and bushing 140 slides radially The path and the retreat path are deflected by an angle α relative to the straight line 103 connected by the multiple contact points 101 (that is, the radial sliding path and the retreat path of the bushing 140 do not coincide with the straight line 103 connected by the multiple contact points 101), Since the direction of the straight line 103 is different from the retreat direction (parallel to the positioning reference line 131a), even if abnormal high pressure is generated in the multiple compression spaces 102, the movable scroll 120, the bearing 150 and the bushing 140 can still slide in the radial direction or produce radial retreat. , to maintain the smoothness of the orbiting scroll 120 and help improve the operating efficiency of the compressor 10 .

請參考圖1C與圖1D,在本實施例中,第二壓縮機構100還包括固定塊160與鎖定件170。固定塊160設置於襯套140內,並抵接定位凸部131。另一方面,鎖定件170穿過固定塊160與定位凸部131並鎖入驅動軸13的端部13a,以將襯套座130定位於驅動軸13的端部13a。舉例來說,鎖定件170可為螺栓。 Please refer to FIG. 1C and FIG. 1D. In this embodiment, the second compression mechanism 100 further includes a fixing block 160 and a locking piece 170. The fixing block 160 is disposed in the bushing 140 and contacts the positioning protrusion 131 . On the other hand, the locking piece 170 passes through the fixing block 160 and the positioning protrusion 131 and is locked into the end 13 a of the drive shaft 13 to position the bushing seat 130 at the end 13 a of the drive shaft 13 . For example, the locking member 170 may be a bolt.

如圖1D與圖1F所示,定位凸部131還具有第一穿孔131b,且驅動軸13的主軸線13b通過第一穿孔131b。鎖定件170先穿過固定塊160再穿過第一穿孔131b,然後鎖入驅動軸13的端部13a,以將動渦卷120、軸承150、襯套140及襯套座130定位於入驅動軸13的端部13a。 As shown in FIG. 1D and FIG. 1F , the positioning protrusion 131 also has a first through hole 131 b, and the main axis 13 b of the driving shaft 13 passes through the first through hole 131 b. The locking piece 170 first passes through the fixed block 160 and then through the first through hole 131b, and then is locked into the end 13a of the drive shaft 13 to position the movable scroll 120, the bearing 150, the bushing 140 and the bushing seat 130 in the drive shaft. End 13a of shaft 13.

另一方面,定位凸部131還具有第二穿孔131c,其中第一穿孔131b與第二穿孔131c之間的連線重合於定位基準線131a,且相對於多個接觸點101所連成的直線103偏擺角度α。也就是說,第一穿孔131b是用於調整定位凸部131使其產生偏擺角度α,且第一穿孔131b與第二穿孔131c之間的連線固定住了 定位凸部131所偏擺的角度α,使得動渦卷120、軸承150及襯套140的退讓方向(平行於定位基準線131a)避開動渦卷120與靜渦卷110之間的多個接觸點101或直線103,因此能透過較小的作用力(可稱為退讓力)即可產生退讓,防止軸承150的特定區域因受力過大而產生嚴重的磨損。 On the other hand, the positioning protrusion 131 also has a second through hole 131c, wherein the connection line between the first through hole 131b and the second through hole 131c coincides with the positioning reference line 131a, and is relative to the straight line connected by the plurality of contact points 101. 103 Yaw angle α. That is to say, the first through hole 131b is used to adjust the positioning protrusion 131 to produce a deflection angle α, and the connection line between the first through hole 131b and the second through hole 131c is fixed. The positioning protrusion 131 is deflected by an angle α such that the retreat direction of the movable scroll 120 , the bearing 150 and the bushing 140 (parallel to the positioning reference line 131 a ) avoids multiple gaps between the movable scroll 120 and the fixed scroll 110 The contact point 101 or the straight line 103 can yield through a small force (which can be called a yield force), thereby preventing a specific area of the bearing 150 from being severely worn due to excessive force.

圖2A是本新型創作一實施例的動渦卷與襯套座的組合示意圖。圖2B是圖2A的爆炸示意圖。圖2C是圖2B的軸承、襯套及襯套座的正視示意圖。請參考圖2A至圖2C,在本實施例中,襯套140承靠於襯套座130,且襯套140的中心線141相對於主軸線13b傾斜一角度β,且角度β可以是介於0.5至5度。 Figure 2A is a schematic diagram of the combination of the movable scroll and the bushing seat according to an embodiment of the present invention. Figure 2B is an exploded diagram of Figure 2A. Figure 2C is a schematic front view of the bearing, bushing and bushing seat of Figure 2B. Please refer to FIGS. 2A to 2C . In this embodiment, the bushing 140 is supported on the bushing seat 130 , and the centerline 141 of the bushing 140 is inclined at an angle β relative to the main axis 13 b , and the angle β may be between 0.5 to 5 degrees.

如圖1F、圖2A與圖2C所示,軸承150隨襯套140相對於主軸線13b傾斜,但動渦卷120未相對於主軸線13b傾斜,因此,軸承150可在動渦卷120繞動時平均受力,防止軸承150的特定區域因受力過大而產生嚴重的磨損,據以提升壓縮機10的運轉效率及使用壽命。另外,當動渦卷120相對於靜渦卷110繞動時,動渦卷120的退讓方向平行於定位凸部131的長邊1311或定位基準線131a,且避開了動渦卷120與靜渦卷110之間的多個接觸點101或直線103。因此,繞動時的動渦卷120的向心分力較小,以透過較小的作用力(可稱為退讓力)在徑向上產生退讓,防止軸承150的特定區域因受力過大而產生嚴重的磨損。 As shown in FIGS. 1F, 2A and 2C, the bearing 150 and the bushing 140 are tilted relative to the main axis 13b, but the movable scroll 120 is not tilted relative to the main axis 13b. Therefore, the bearing 150 can revolve around the movable scroll 120. The force is evenly applied at all times to prevent a specific area of the bearing 150 from being severely worn due to excessive force, thereby improving the operating efficiency and service life of the compressor 10 . In addition, when the orbiting scroll 120 orbits relative to the stationary scroll 110, the retreat direction of the orbiting scroll 120 is parallel to the long side 1311 of the positioning protrusion 131 or the positioning reference line 131a, and avoids the orbiting scroll 120 and the stationary scroll 110. Multiple contact points 101 or straight lines 103 between scrolls 110 . Therefore, the centripetal force of the movable scroll 120 when orbiting is small, so that a small force (which can be called a concession force) is used to generate concessions in the radial direction, thereby preventing a specific area of the bearing 150 from being overly stressed and causing damage. Severe wear and tear.

圖2D與圖2E是圖2C的襯套座在二個不同視角的示意圖。請參考圖2C至圖2E,襯套座130還具有第一承靠面132與 連接第一承靠面132的第二承靠面133,且定位凸部131凸出於第一承靠面132與第二承靠面133。詳細而言,第一承靠面132高於第二承靠面133,接觸第一承靠面132與第二承靠面133的襯套140可因第一承靠面132與第二承靠面133之間的高低差而產生傾斜,使得襯套140的中心線141相對於主軸線13b傾斜。另一方面,為確保接觸第一承靠面132與第二承靠面133的襯套140在襯套座130上產生傾斜,高度較高的第一承靠面132的面積小於高度較低的第二承靠面133的面積。 FIG. 2D and FIG. 2E are schematic views of the bushing seat in FIG. 2C from two different viewing angles. Please refer to FIGS. 2C to 2E , the bushing seat 130 also has a first bearing surface 132 and a The second supporting surface 133 is connected to the first supporting surface 132 , and the positioning protrusion 131 protrudes from the first supporting surface 132 and the second supporting surface 133 . Specifically, the first bearing surface 132 is higher than the second bearing surface 133 , and the bushing 140 contacting the first bearing surface 132 and the second bearing surface 133 can be caused by the first bearing surface 132 and the second bearing surface 133 . The height difference between the surfaces 133 causes an inclination, so that the center line 141 of the bushing 140 is inclined relative to the main axis 13b. On the other hand, in order to ensure that the bushing 140 contacting the first bearing surface 132 and the second bearing surface 133 is tilted on the bushing seat 130, the area of the higher first bearing surface 132 is smaller than that of the lower one. The area of the second supporting surface 133.

如圖2D與圖2E所示,第一承靠面132與第二承靠面133之間的高低差介於0.5毫米至5毫米之間。另外,第二承靠面133的分布範圍沿其中一個長邊1311往二個短邊1312延伸,並擴及各個短邊1312的至少一半,也就是分布介於短邊1312的邊長的1/2至整個邊長之間。 As shown in FIG. 2D and FIG. 2E , the height difference between the first supporting surface 132 and the second supporting surface 133 is between 0.5 mm and 5 mm. In addition, the distribution range of the second supporting surface 133 extends along one of the long sides 1311 to the two short sides 1312, and extends to at least half of each short side 1312, that is, the distribution range is between 1/1 of the length of the short side 1312. 2 to the entire side length.

圖3A與圖3B是本新型創作另一實施例的襯套座在二個不同視角的示意圖。請參考圖3A與圖3B,不同於圖2D與圖2E所示的襯套座130,本實施例的襯套座130a的第二承靠面133高於第一承靠面132,且高度較高的第二承靠面133的面積小於高度較低的第一承靠面132的面積。詳細而言,第一承靠面132的分布範圍沿其中一個長邊1311往二個短邊1312延伸,並擴及各個短邊1312的至少一半,也就是分布介於短邊1312的邊長的1/2至整個邊長之間,如圖3B所示。 3A and 3B are schematic views of the bushing seat from two different angles according to another embodiment of the present invention. Please refer to Figures 3A and 3B. Different from the bushing seat 130 shown in Figures 2D and 2E, the second supporting surface 133 of the bushing seat 130a of this embodiment is higher than the first supporting surface 132, and the height is relatively high. The area of the tall second supporting surface 133 is smaller than the area of the lower first supporting surface 132 . Specifically, the distribution range of the first supporting surface 132 extends along one of the long sides 1311 to the two short sides 1312, and extends to at least half of each short side 1312, that is, the distribution range is between the length of the short sides 1312. Between 1/2 and the entire side length, as shown in Figure 3B.

襯套座的二個承靠面的高低設計是以動渦卷的繞動方向 來決定,舉例來說,圖2D與圖2E所示的襯套座130適用於順時針繞轉的動渦卷,使得開始繞動的動渦卷先繞經低面(即第二承靠面133)。相對地,圖3A與圖3B所示的襯套座130a適用於逆時針繞轉的動渦卷,使得開始繞動的動渦卷先繞經低面(即第一承靠面132),在動渦卷120發生退讓時,襯套座130底部承靠的第二承靠面133為低面而非高面,使得退讓阻力較小,動渦卷120可透過較小的作用力(可稱為退讓力)即可產生退讓,防止軸承150的特定區域因受力過大而產生嚴重的磨損。 The height design of the two supporting surfaces of the bushing seat is based on the orbiting direction of the movable scroll. To determine, for example, the bushing seat 130 shown in FIG. 2D and FIG. 2E is suitable for the movable scroll that rotates clockwise, so that the movable scroll that starts to revolve first passes through the lower surface (ie, the second supporting surface). 133). In contrast, the bushing seat 130a shown in FIGS. 3A and 3B is suitable for the movable scroll that rotates counterclockwise, so that the movable scroll that starts to revolve first winds through the lower surface (ie, the first supporting surface 132), and then When the movable scroll 120 retreats, the second supporting surface 133 that the bottom of the bushing seat 130 rests on is a low surface instead of a high surface, so that the resistance to retreat is smaller, and the movable scroll 120 can pass through a smaller force (which can be called The setback force) can produce a setback to prevent a specific area of the bearing 150 from being severely worn due to excessive force.

圖4A是本新型創作又一實施例的軸承、襯套及襯套座的正視示意圖。圖4B是圖4A的襯套座的示意圖。請參考圖4A與圖4B,不同於前述實施例的襯套座130或襯套座130a,本實施例的襯套座130b的承靠面為一承靠斜面134。詳細而言,襯套140接觸承靠斜面134,使得襯套140的中心線141相對於主軸線13b傾斜一角度β,且角度β可以是介於0.5度至5度。 Figure 4A is a schematic front view of a bearing, bushing and bushing seat according to another embodiment of the present invention. Figure 4B is a schematic view of the bushing seat of Figure 4A. Please refer to FIG. 4A and FIG. 4B. Different from the bushing seat 130 or the bushing seat 130a in the previous embodiment, the bearing surface of the bushing seat 130b in this embodiment is a bearing inclined surface 134. In detail, the bushing 140 contacts the supporting slope 134 so that the centerline 141 of the bushing 140 is inclined at an angle β relative to the main axis 13b, and the angle β may be between 0.5 degrees and 5 degrees.

襯套座的承靠斜面的高低設計是以動渦卷的繞動方向來決定,舉例來說,具有左高右低的承靠斜面的襯套座適用於順時針繞轉的動渦卷,使得開始繞動的動渦卷先繞經低面。相對地,具有右高左低的承靠斜面的襯套座適用於逆時針繞轉的動渦卷,使得開始繞動的動渦卷先繞經低面。 The height design of the supporting slope of the bushing seat is determined by the orbiting direction of the movable scroll. For example, a bushing seat with a supporting slope that is high on the left and low on the right is suitable for a clockwise rotating scroll. Make the movable scroll that starts to revolve around the lower surface first. Correspondingly, a bushing seat with a supporting inclined surface that is higher on the right and lower on the left is suitable for the movable scroll that rotates counterclockwise, so that the movable scroll that starts to rotate first winds through the lower surface.

圖5是本新型創作另一實施例的壓縮機的剖面示意圖。前一實施例的壓縮機10為二級壓縮機,其於相連通的二個壓縮腔分別設有螺桿壓縮機構與渦卷壓縮機構,相較於此,圖5所示的 壓縮機20為單級壓縮機,其殼體21具有單一個壓縮腔21a,且在壓縮腔21a內配置單一個壓縮機構100a,例如渦卷壓縮機構。 Figure 5 is a schematic cross-sectional view of a compressor according to another embodiment of the present invention. The compressor 10 of the previous embodiment is a two-stage compressor, and its two connected compression chambers are respectively provided with a screw compression mechanism and a scroll compression mechanism. In comparison, the compressor 10 shown in Figure 5 The compressor 20 is a single-stage compressor, and its casing 21 has a single compression chamber 21a, and a single compression mechanism 100a, such as a scroll compression mechanism, is configured in the compression chamber 21a.

如圖5所示,馬達22與驅動軸23設置於殼體21內,其中驅動軸23連接於馬達22,且延伸至壓縮腔21a以連接於壓縮機構100a。詳細而言,馬達22可透過驅動軸23帶動壓縮機構100a運轉,使得低壓氣態流體壓縮腔21a內經壓縮機構100a壓縮形成高壓氣態流體,然後自壓縮腔21a排出。 As shown in FIG. 5 , the motor 22 and the drive shaft 23 are disposed in the housing 21 , where the drive shaft 23 is connected to the motor 22 and extends to the compression chamber 21 a to be connected to the compression mechanism 100 a. Specifically, the motor 22 can drive the compression mechanism 100a to operate through the drive shaft 23, so that the low-pressure gaseous fluid in the compression chamber 21a is compressed by the compression mechanism 100a to form a high-pressure gaseous fluid, which is then discharged from the compression chamber 21a.

本實施例的壓縮機構100a與前一實施例的第二壓縮機構100同為渦卷壓縮機構,且具有相同的結構設計,例如在靜渦卷與動渦卷的配合、襯套座的結構設計、襯套座與驅動軸的配合、襯套的結構設計、襯套與襯套座的配合、襯套的中心線與驅動軸的主軸線的相對關係(例如偏心關係與傾斜關係)以及襯套、軸承及動渦卷的配合等方面均相同,於此不贅述。 The compression mechanism 100a of this embodiment is the same scroll compression mechanism as the second compression mechanism 100 of the previous embodiment, and has the same structural design, such as the cooperation between the fixed scroll and the movable scroll and the structural design of the bushing seat. , the fit of the bushing seat and the drive shaft, the structural design of the bushing, the fit of the bushing and the bushing seat, the relative relationship between the centerline of the bushing and the main axis of the drive shaft (such as eccentricity and inclination), and the relationship between the bushing and the bushing , bearings and the coordination of the movable scroll are all the same, and will not be repeated here.

綜上所述,在本新型創作的壓縮機中,襯套座定位於驅動軸的端部,其中動渦卷透過軸承與襯套連接於襯套座的定位凸部,且襯套可因第一承靠面與第二承靠面(或承靠斜面)之間的高低差,而使襯套的中心線偏心於驅動軸的主軸線。詳細而言,動渦卷與靜渦卷之間的多個接觸點,以形成多個密閉空間,且定位凸部相對於多個接觸點所連成的直線偏擺一角度,使得退讓方向與直線的方向不同,且動渦卷退讓時承靠面(或承靠斜面)為低面,動渦卷的退讓阻力小,因此可透過較小的作用力即可產生退讓,達到軸承可在動渦卷繞動時平均受力,防止軸承的特定區域因受力 過大而產生嚴重的磨損,據以提升壓縮機的運轉效率及使用壽命。 To sum up, in the compressor of the present invention, the bushing seat is positioned at the end of the drive shaft, and the movable scroll is connected to the positioning protrusion of the bushing seat through the bearing and the bushing, and the bushing can be The height difference between the first bearing surface and the second bearing surface (or bearing slope) causes the center line of the bushing to be eccentric to the main axis of the drive shaft. Specifically, multiple contact points between the movable scroll and the stationary scroll form multiple closed spaces, and the positioning convex portion is deflected at an angle relative to the straight line connected by the multiple contact points, so that the retreat direction is consistent with the straight line formed by the multiple contact points. The directions of the straight lines are different, and the supporting surface (or supporting slope) is a low surface when the movable scroll retreats. The retreat resistance of the movable scroll is small, so the retreat can be caused by a small force, so that the bearing can move in the The scrolls are evenly stressed when they rotate, preventing specific areas of the bearing from being stressed. If it is too large, it will cause serious wear and tear, thereby improving the operating efficiency and service life of the compressor.

另一方面,在動渦卷相對於靜渦卷繞動的過程中,動渦卷、軸承及襯套可在徑向上同步地相對於靜渦卷滑動,因襯套的徑向滑動路徑或退讓路徑相對於多個接觸點所連成的直線偏擺一角度(即襯套的徑向滑動路徑或退讓路徑未與多個接觸點所連成的直線重合),即便多個壓縮空間產生異常高壓,動渦卷、軸承及襯套仍可在徑向上滑動或產生徑向退讓,以維持動渦卷的繞動順暢度,有助於提升壓縮機的運轉效率。 On the other hand, during the orbiting process of the movable scroll relative to the fixed scroll, the movable scroll, bearings and bushings can slide synchronously relative to the fixed scroll in the radial direction. Due to the radial sliding path or retreat of the bushing, The path deviates at an angle relative to the straight line connected by multiple contact points (that is, the radial sliding path or retreat path of the bushing does not coincide with the straight line connected by multiple contact points), even if multiple compression spaces generate abnormally high pressure , the movable scroll, bearings and bushings can still slide in the radial direction or yield radially to maintain the smoothness of the movable scroll and help improve the operating efficiency of the compressor.

雖然本新型創作已以實施例揭露如上,然其並非用以限定本新型創作,任何所屬技術領域中具有通常知識者,在不脫離本新型創作的精神和範圍內,當可作些許的更動與潤飾,故本新型創作的保護範圍當視後附的申請專利範圍所界定者為準。 Although the embodiments of the present invention have been disclosed above, they are not intended to limit the invention. Anyone with ordinary knowledge in the technical field can make some modifications and changes without departing from the spirit and scope of the invention. Therefore, the scope of protection of this new creation shall be determined by the appended patent application scope.

10:壓縮機 10:Compressor

11:殼體 11: Shell

11a:第一壓縮腔 11a: First compression chamber

11b:第二壓縮腔 11b: Second compression chamber

12:馬達 12: Motor

13:驅動軸 13: Drive shaft

14:第一壓縮機構 14:First compression mechanism

100:第二壓縮機構 100: Second compression mechanism

A:部位 A: Part

Claims (30)

一種壓縮機,包括: 一殼體,具有相連通的一第一壓縮腔與一第二壓縮腔; 一馬達,設置於該殼體內; 一驅動軸,連接於該馬達,其中該驅動軸穿過該第一壓縮腔,且延伸至該第二壓縮腔; 一第一壓縮機構,設置於該第一壓縮腔內,且連接於該驅動軸;以及 一第二壓縮機構,設置於該第二壓縮腔內,且包括: 一靜渦卷; 一動渦卷,嚙合於該靜渦卷,並與該靜渦卷之間具有多個接觸點,以形成多個壓縮空間; 一襯套座,定位於該驅動軸的一端部,且具有一定位凸部,其中該驅動軸的一主軸線通過該定位凸部,且該定位凸部相對於該些接觸點所連成的一直線偏擺一角度; 一襯套,套接於該定位凸部,且該襯套的一中心線偏心於該主軸線;以及 一軸承,套接於該襯套,且該動渦卷套接於該軸承。 A compressor including: A shell having a first compression chamber and a second compression chamber that are connected; A motor is provided in the housing; a drive shaft connected to the motor, wherein the drive shaft passes through the first compression chamber and extends to the second compression chamber; a first compression mechanism, disposed in the first compression chamber and connected to the drive shaft; and A second compression mechanism is provided in the second compression chamber and includes: A still scroll; A moving scroll is engaged with the stationary scroll and has multiple contact points with the stationary scroll to form multiple compression spaces; A bushing seat is positioned at one end of the drive shaft and has a positioning protrusion, wherein a main axis of the drive shaft passes through the positioning protrusion, and the positioning protrusion is relative to the contact points connected to each other. A straight line deflects by an angle; A bushing is sleeved on the positioning protrusion, and a center line of the bushing is eccentric to the main axis; and A bearing is sleeved on the bushing, and the orbiting scroll is sleeved on the bearing. 如請求項1所述的壓縮機,其中該襯套具有一穿槽,且該定位凸部設置於該穿槽內,該穿槽相對於該些接觸點所連成的該直線偏擺該角度。The compressor of claim 1, wherein the bushing has a through groove, and the positioning protrusion is disposed in the through groove, and the through groove is deflected by the angle relative to the straight line connected by the contact points. . 如請求項2所述的壓縮機,其中該定位凸部具有通過該主軸線且平行於該穿槽的一定位基準線,且該定位基準線與該些接觸點所連成的該直線之間夾有該角度。The compressor according to claim 2, wherein the positioning protrusion has a positioning reference line passing through the main axis and parallel to the through groove, and between the positioning reference line and the straight line connecting the contact points This angle is included. 如請求項1所述的壓縮機,其中該襯套適於沿一滑動路徑相對於該襯套座往復滑動,且該滑動路徑與該些接觸點所連成的該直線之間夾有該角度。The compressor of claim 1, wherein the bushing is adapted to slide back and forth relative to the bushing seat along a sliding path, and the sliding path and the straight line connected by the contact points include the angle. . 如請求項4所述的壓縮機,其中該定位凸部具有通過該主軸線的一定位基準線,且該定位基準線重合於該滑動路徑,該定位基準線與該些接觸點所連成的該直線之間夾有該角度。The compressor of claim 4, wherein the positioning convex portion has a positioning reference line passing through the main axis, and the positioning reference line coincides with the sliding path, and the positioning reference line is connected with the contact points. The angle is between the straight lines. 如請求項1所述的壓縮機,其中該角度為一銳角。The compressor of claim 1, wherein the angle is an acute angle. 如請求項6所述的壓縮機,其中該角度介於5度至45度。The compressor of claim 6, wherein the angle is between 5 degrees and 45 degrees. 如請求項7所述的壓縮機,其中該角度等於15度。The compressor of claim 7, wherein the angle is equal to 15 degrees. 如請求項1所述的壓縮機,其中該定位凸部具有一長邊與連接該長邊的一短邊,且該長邊相對於該些接觸點所連成的該直線偏擺該角度。The compressor of claim 1, wherein the positioning protrusion has a long side and a short side connected to the long side, and the long side is deflected at the angle relative to the straight line connected by the contact points. 如請求項1所述的壓縮機,其中該第二壓縮機構還包括: 一固定塊,設置於該襯套內,並抵接該定位凸部;以及 一鎖定件,穿過該固定塊與該定位凸部並鎖入該驅動軸的該端部。 The compressor according to claim 1, wherein the second compression mechanism further includes: A fixed block is disposed in the bushing and contacts the positioning protrusion; and A locking piece passes through the fixing block and the positioning protrusion and locks into the end of the driving shaft. 如請求項10所述的壓縮機,其中該定位凸部具有一第一穿孔,且該驅動軸的該主軸線通過該第一穿孔,該鎖定件穿過該第一穿孔並鎖入該驅動軸的該端部。The compressor of claim 10, wherein the positioning protrusion has a first through hole, and the main axis of the drive shaft passes through the first through hole, and the locking piece passes through the first through hole and is locked into the drive shaft. of that end. 如請求項11所述的壓縮機,其中該定位凸部還具有一第二穿孔,且該第一穿孔與該第二穿孔之間的一連線相對於該些接觸點所連成的該直線偏擺該角度。The compressor of claim 11, wherein the positioning protrusion further has a second through hole, and a connecting line between the first through hole and the second through hole is relative to the straight line connecting the contact points. deflect this angle. 如請求項1所述的壓縮機,其中該襯套座還具有一第一承靠面與連接該第一承靠面的一第二承靠面,且該定位凸部凸出於該第一承靠面與該第二承靠面,該第一承靠面與該第二承靠面之間具有一高低差,該襯套接觸該第一承靠面與該第二承靠面,且該襯套的該中心線相對於該主軸線傾斜。The compressor of claim 1, wherein the bushing seat further has a first bearing surface and a second bearing surface connected to the first bearing surface, and the positioning protrusion protrudes from the first bearing surface. There is a height difference between the supporting surface and the second supporting surface, the first supporting surface and the second supporting surface, the bushing contacts the first supporting surface and the second supporting surface, and The centerline of the bushing is inclined relative to the main axis. 如請求項13所述的壓縮機,其中該襯套的該中心線相對於該主軸線傾斜0.5度至5度。The compressor of claim 13, wherein the center line of the bushing is inclined from 0.5 to 5 degrees relative to the main axis. 如請求項13所述的壓縮機,其中該第一承靠面與該第二承靠面中的一者高於該第一承靠面與該第二承靠面中的另一者,該第一承靠面與該第二承靠面中較高者的面積小於該第一承靠面與該第二承靠面中較低者的面積。The compressor of claim 13, wherein one of the first bearing surface and the second bearing surface is higher than the other of the first bearing surface and the second bearing surface, and the The area of the higher one of the first supporting surface and the second supporting surface is smaller than the area of the lower one of the first supporting surface and the second supporting surface. 如請求項13所述的壓縮機,其中該第一承靠面與該第二承靠面之間的該高低差介於0.05毫米至0.5毫米之間。The compressor of claim 13, wherein the height difference between the first bearing surface and the second bearing surface is between 0.05 mm and 0.5 mm. 如請求項13所述的壓縮機,其中該定位凸部具有相對的二個長邊與相對的二個短邊,且該二個短邊連接於該二個長邊之間,該第一承靠面的分布範圍沿一該長邊往該二個短邊延伸,並擴及各該短邊的至少一半。The compressor of claim 13, wherein the positioning protrusion has two opposite long sides and two opposite short sides, and the two short sides are connected between the two long sides, and the first bearing The distribution range of the back surface extends from one long side to the two short sides, and extends to at least half of each short side. 如請求項1所述的壓縮機,其中該襯套座還具有一承靠斜面,且該定位凸部凸出於該承靠斜面,該襯套接觸該承靠斜面,且該襯套的該中心線相對於該主軸線傾斜。The compressor of claim 1, wherein the bushing seat also has a supporting slope, and the positioning protrusion protrudes from the supporting slope, the bushing contacts the supporting slope, and the bushing The centerline is tilted relative to this main axis. 如請求項18所述的壓縮機,其中該襯套的該中心線相對於該主軸線傾斜0.5度至5度。The compressor of claim 18, wherein the center line of the bushing is inclined from 0.5 to 5 degrees relative to the main axis. 如請求項1所述的壓縮機,其中該第一壓縮機構為一螺桿壓縮機構。The compressor of claim 1, wherein the first compression mechanism is a screw compression mechanism. 一種壓縮機,包括: 一殼體,具有一壓縮腔; 一馬達,設置於該殼體內; 一驅動軸,連接於該馬達,其中該驅動軸延伸至該壓縮腔;以及 一壓縮機構,設置於該壓縮腔內,且包括: 一靜渦卷; 一動渦卷,嚙合於該靜渦卷,並與該靜渦卷之間具有多個接觸點,以形成多個壓縮空間; 一襯套座,定位於該驅動軸的一端部,且具有一定位凸部,其中該驅動軸的一主軸線通過該定位凸部,且該定位凸部相對於該些接觸點所連成的一直線偏擺一角度; 一襯套,套接於該定位凸部,且該襯套的一中心線偏心於該主軸線;以及 一軸承,套接於該襯套,且該動渦卷套接於該軸承。 A compressor including: A shell with a compression chamber; A motor is provided in the housing; a drive shaft connected to the motor, wherein the drive shaft extends to the compression chamber; and A compression mechanism is provided in the compression chamber and includes: A still scroll; A moving scroll is engaged with the stationary scroll and has multiple contact points with the stationary scroll to form multiple compression spaces; A bushing seat is positioned at one end of the drive shaft and has a positioning protrusion, wherein a main axis of the drive shaft passes through the positioning protrusion, and the positioning protrusion is relative to the contact points connected to each other. A straight line deflects by an angle; A bushing is sleeved on the positioning protrusion, and a center line of the bushing is eccentric to the main axis; and A bearing is sleeved on the bushing, and the orbiting scroll is sleeved on the bearing. 如請求項21所述的壓縮機,其中該襯套具有一穿槽,且該定位凸部設置於該穿槽內,該穿槽相對於該些接觸點所連成的該直線偏擺該角度,該定位凸部具有通過該主軸線且平行於該穿槽的一定位基準線,且該定位基準線與該些接觸點所連成的該直線之間夾有該角度。The compressor of claim 21, wherein the bushing has a through groove, and the positioning protrusion is disposed in the through groove, and the through groove is deflected by the angle relative to the straight line connected by the contact points. , the positioning protrusion has a positioning reference line passing through the main axis and parallel to the through groove, and the angle is sandwiched between the positioning reference line and the straight line connecting the contact points. 如請求項21所述的壓縮機,其中該襯套適於沿一滑動路徑相對於該襯套座往復滑動,且該滑動路徑與該些接觸點所連成的該直線之間夾有該角度,該定位凸部具有通過該主軸線的一定位基準線,且該定位基準線重合於該滑動路徑,該定位基準線與該些接觸點所連成的該直線之間夾有該角度。The compressor of claim 21, wherein the bushing is adapted to slide back and forth relative to the bushing seat along a sliding path, and the sliding path and the straight line connected by the contact points include the angle. , the positioning convex portion has a positioning reference line passing through the main axis, and the positioning reference line coincides with the sliding path, and the angle is sandwiched between the positioning reference line and the straight line connected by the contact points. 如請求項21所述的壓縮機,其中該角度介於5度至45度。The compressor of claim 21, wherein the angle is between 5 degrees and 45 degrees. 如請求項21所述的壓縮機,其中該襯套座還具有一第一承靠面與連接該第一承靠面的一第二承靠面,且該定位凸部凸出於該第一承靠面與該第二承靠面,該第一承靠面與該第二承靠面之間具有一高低差,該襯套接觸該第一承靠面與該第二承靠面,且該襯套的該中心線相對於該主軸線傾斜。The compressor according to claim 21, wherein the bushing seat further has a first bearing surface and a second bearing surface connected to the first bearing surface, and the positioning protrusion protrudes from the first bearing surface. There is a height difference between the supporting surface and the second supporting surface, the first supporting surface and the second supporting surface, the bushing contacts the first supporting surface and the second supporting surface, and The centerline of the bushing is inclined relative to the main axis. 如請求項25所述的壓縮機,其中該襯套的該中心線相對於該主軸線傾斜0.5度至5度。The compressor of claim 25, wherein the center line of the bushing is inclined from 0.5 to 5 degrees relative to the main axis. 如請求項25所述的壓縮機,其中該第一承靠面與該第二承靠面中的一者高於該第一承靠面與該第二承靠面中的另一者,該第一承靠面與該第二承靠面中較高者的面積小於該第一承靠面與該第二承靠面中較低者的面積。The compressor of claim 25, wherein one of the first bearing surface and the second bearing surface is higher than the other of the first bearing surface and the second bearing surface, and the The area of the higher one of the first supporting surface and the second supporting surface is smaller than the area of the lower one of the first supporting surface and the second supporting surface. 如請求項25所述的壓縮機,其中該第一承靠面與該第二承靠面之間的該高低差介於0.05毫米至0.5毫米之間。The compressor of claim 25, wherein the height difference between the first bearing surface and the second bearing surface is between 0.05 mm and 0.5 mm. 如請求項21所述的壓縮機,其中該襯套座還具有一承靠斜面,且該定位凸部凸出於該承靠斜面,該襯套接觸該承靠斜面,且該襯套的該中心線相對於該主軸線傾斜。The compressor according to claim 21, wherein the bushing seat also has a supporting slope, and the positioning protrusion protrudes from the supporting slope, the bushing contacts the supporting slope, and the bushing The centerline is tilted relative to this main axis. 如請求項29所述的壓縮機,其中該襯套的該中心線相對於該主軸線傾斜0.5度至5度。The compressor of claim 29, wherein the centerline of the bushing is inclined from 0.5 to 5 degrees relative to the main axis.
TW112208508U 2023-08-11 Compressor TWM651447U (en)

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