TWM513933U - Spiral compressor and its seal mechanism thereof - Google Patents

Spiral compressor and its seal mechanism thereof Download PDF

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Publication number
TWM513933U
TWM513933U TW104208565U TW104208565U TWM513933U TW M513933 U TWM513933 U TW M513933U TW 104208565 U TW104208565 U TW 104208565U TW 104208565 U TW104208565 U TW 104208565U TW M513933 U TWM513933 U TW M513933U
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Taiwan
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disposed
sealing mechanism
shaft sealing
slinger
casing
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TW104208565U
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Chinese (zh)
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Yue-Zhi Hong
Yi-Sheng Chen
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Fu Sheng Ind Co Ltd
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Priority to TW104208565U priority Critical patent/TWM513933U/en
Publication of TWM513933U publication Critical patent/TWM513933U/en

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  • Applications Or Details Of Rotary Compressors (AREA)

Description

螺旋壓縮機及其軸封機構Screw compressor and its shaft sealing mechanism

本創作是有關於一種軸封機構,尤指一種能夠有效達到阻隔潤滑油氣汙染壓縮腔室的螺旋壓縮機及其軸封機構。The present invention relates to a shaft sealing mechanism, and more particularly to a screw compressor and a shaft sealing mechanism thereof, which can effectively achieve a lubrication chamber that blocks the lubrication of lubricating oil.

由於螺旋壓縮機已廣泛地運用於流體加壓,使流體形成高壓狀態,再供客戶端設備或各單位使用。尤其現有一種乾式無油螺旋壓縮機,亦即其壓縮腔室內除壓縮氣體外,無任何介質(潤滑油或其混合物)進行冷卻或密封。現有乾式無油式壓縮機的氣缸系統在壓縮過程中不需要潤滑油,因此不會沾有油味,不會有油汙染,更不需時常換油保養,因而可應用於食品、醫療等領域中。Since screw compressors have been widely used for fluid pressurization, the fluid is brought to a high pressure state for use by the client equipment or units. In particular, there is a dry oil-free screw compressor in which no medium (lubricating oil or a mixture thereof) is cooled or sealed except for compressed gas in its compression chamber. The cylinder system of the existing dry oil-free compressor does not need lubricating oil during the compression process, so it does not have oily smell, no oil pollution, and does not need oil change maintenance from time to time, so it can be applied to food, medical and other fields. in.

雖然乾式無油壓縮機內無任何介質,但其軸承內仍含有潤滑油脂。在壓縮機長期且高速的運轉中,恐仍有少部分油脂滲入壓縮腔室內;或者是,由於溫度升高會使油脂蒸發和氧化分解,隨著高壓流體進入壓縮腔室,因此必須配置一軸封機構10。如圖1所示,現有的無油螺旋壓縮機軸封機構10特點在於,設置在螺旋轉子20上的軸封機構10包含油封30組件與氣封組件50。如圖所示,從同步齒輪40向左依序排列為採用滾珠或滾柱軸承32的油封組件30、氣封組件50及壓縮腔室70。複數排列的氣封組件50更包含浮環52、波形彈簧54、 浮環座56與設置於兩浮環座56之間的排氣孔58。此外,在滾珠或滾柱軸承32的一側還會設置一拋油環60,以形成低壓區域,同時配置一迷宮環62以阻隔潤滑油氣,避免汙染螺旋壓縮腔室70。Although there is no medium in the dry oil-free compressor, the bearing still contains lubricating grease. During long-term and high-speed operation of the compressor, there is still a small amount of grease infiltrated into the compression chamber; or, due to the increase in temperature, the grease evaporates and oxidizes and decomposes. As the high-pressure fluid enters the compression chamber, a shaft seal must be disposed. Agency 10. As shown in FIG. 1, the conventional oil-free screw compressor shaft seal mechanism 10 is characterized in that the shaft seal mechanism 10 disposed on the spiral rotor 20 includes an oil seal 30 assembly and a gas seal assembly 50. As shown, the oil seal assembly 30, the gas seal assembly 50, and the compression chamber 70, which are ball or roller bearings 32, are sequentially arranged from the synchronizing gear 40 to the left. The plurality of air seal assemblies 50 further include a floating ring 52, a wave spring 54, The float ring seat 56 and the vent hole 58 disposed between the two float ring seats 56. In addition, a slinger 60 may be provided on one side of the ball or roller bearing 32 to form a low pressure region while a labyrinth ring 62 is disposed to block the lubricating oil gas from contaminating the helical compression chamber 70.

然而現有的軸承機構10配置多組的氣封軸承50,導致螺旋轉子20軸向方向較長,組裝不便等問題,因此針對上述軸封機構存在的問題點乃需有亟待改善之處。However, the conventional bearing mechanism 10 is provided with a plurality of sets of the air-sealed bearings 50, which causes the spiral rotor 20 to have a long axial direction and inconvenient assembly. Therefore, there is a need for improvement in the problems of the above-mentioned shaft sealing mechanism.

本創作目的之一,在於提供一種元件較少(結構精簡)、軸封性能提升,且縮短螺旋轉子軸向密封長度的螺旋壓縮機及其軸封機構。One of the purposes of the present invention is to provide a screw compressor and a shaft sealing mechanism which have fewer components (simplified structure), improved shaft seal performance, and shortened axial seal length of the spiral rotor.

本創作另一目的在於可相對縮小壓縮機體積的螺旋壓縮機及其軸封機構。Another object of the present invention is a screw compressor and a shaft sealing mechanism that can relatively reduce the volume of the compressor.

為達上述目的,本創作提供一種軸封機構,設置在一機殼及相對於機殼的一螺旋轉子之間。軸封機構包括一迷宮環軸封及一O型環。迷宮環軸封包含沿螺旋轉子軸向設置的一本體及徑向貫穿本體的一排氣孔。O型環設置於迷宮環軸封外表面上。To achieve the above object, the present invention provides a shaft sealing mechanism disposed between a casing and a spiral rotor relative to the casing. The shaft sealing mechanism includes a labyrinth ring shaft seal and an O-ring. The labyrinth ring seal includes a body disposed along the axial direction of the spiral rotor and a vent hole extending through the body in a radial direction. The O-ring is placed on the outer surface of the labyrinth ring seal.

本創作另一較廣義的實施態樣還提供一種螺旋壓縮機,包括一機殼、至少一螺旋轉子及前述實施例的軸封機構。機殼形成有一壓縮腔室。螺旋轉子設置於機殼並穿過壓縮腔室,其中螺旋轉子具有至少一肩部及鄰接肩部的一逆向螺旋齒。軸封機構設置於機殼上並相對於螺旋轉子設置。Another broad aspect of the present invention also provides a screw compressor including a casing, at least one helical rotor, and the shaft sealing mechanism of the foregoing embodiment. The casing is formed with a compression chamber. The spiral rotor is disposed in the casing and passes through the compression chamber, wherein the helical rotor has at least one shoulder and a reverse helical tooth abutting the shoulder. The shaft sealing mechanism is disposed on the casing and disposed relative to the spiral rotor.

較佳地,更包含鄰接該迷宮環軸封的一滾動軸承及一拋油環,其中該拋油環設置於該迷宮環軸封及該滾動軸承之間。Preferably, a rolling bearing and a slinger adjacent to the labyrinth ring seal are further included, wherein the slinger is disposed between the labyrinth ring seal and the rolling bearing.

較佳地,本體相對該螺旋轉子的一側面還具有連續的一逆向螺旋齒,該逆向螺旋齒的齒形方向進一步朝該滾動軸承方向設置。Preferably, the body further has a continuous reverse spiral tooth on a side of the spiral rotor, and the toothed direction of the reverse helical tooth is further disposed toward the rolling bearing.

較佳地,迷宮環軸封外表面還形成用以設置該O型環的一凹槽,且該凹槽形成於該本體的中央位置。Preferably, the outer surface of the labyrinth ring shaft seal further forms a groove for arranging the O-ring, and the groove is formed at a central position of the body.

較佳地,排氣孔數量包含一對,該O型環數量包含一對,各該O型環分別對稱地設置於該本體的兩側,各該排氣孔則分別形成於該對O型環之間。Preferably, the number of vent holes includes a pair, the number of the O-rings includes a pair, and each of the O-rings is symmetrically disposed on two sides of the body, and the vent holes are respectively formed on the pair of O-types. Between the rings.

100‧‧‧軸封機構100‧‧‧ shaft sealing mechanism

102‧‧‧機殼102‧‧‧Shell

110‧‧‧螺旋轉子110‧‧‧Spiral rotor

112‧‧‧肩部112‧‧‧ shoulder

120‧‧‧迷宮環軸封120‧‧‧Maze ring shaft seal

122‧‧‧凹槽122‧‧‧ Groove

130‧‧‧本體130‧‧‧ Ontology

140‧‧‧排氣孔140‧‧‧ venting holes

150‧‧‧O型環150‧‧‧O-ring

160‧‧‧滾動軸承160‧‧‧ rolling bearings

170‧‧‧拋油環170‧‧‧Rearring ring

180‧‧‧逆向螺旋齒180‧‧‧Reverse helical teeth

200‧‧‧螺旋壓縮機200‧‧‧Spiral compressor

202‧‧‧拋油孔202‧‧‧Throwing hole

210‧‧‧壓縮腔室210‧‧‧Compression chamber

220‧‧‧逆向螺旋齒220‧‧‧Reverse helical teeth

圖1為繪示習知螺旋壓縮機的軸封機構之剖視圖。1 is a cross-sectional view showing a shaft sealing mechanism of a conventional screw compressor.

圖2為繪示本創作螺旋壓縮機的軸封機構之剖視圖。2 is a cross-sectional view showing the shaft sealing mechanism of the inventive screw compressor.

圖3為圖2之A部分放大圖。Figure 3 is an enlarged view of a portion A of Figure 2.

圖4為繪示本創作軸封機構的第二具體實施圖。4 is a second embodiment of the present invention.

圖5為繪示本創作軸封機構的第三具體實施圖。FIG. 5 is a third embodiment of the present invention.

圖6為繪示本創作軸封機構的第四具體實施圖。FIG. 6 is a fourth embodiment of the present invention.

圖7為繪示本創作逆向螺旋齒的另一具體實施例圖。FIG. 7 is a view showing another specific embodiment of the reverse spiral tooth of the present invention.

有關本創作之詳細說明及技術內容,配合圖式說明如下,然而所附圖式僅提供參考與說明用,並非用來對本創作加以限制者。The detailed description and technical content of the present invention are described below with reference to the drawings, but the drawings are only for reference and explanation, and are not intended to limit the creation.

如圖2及圖3所示,本創作提供一種軸封機構100,設置在一機殼102及相對於機殼102的一螺旋轉子110之間。也就是說,軸封機構100較佳是固定在機殼102上,螺旋轉子110則相對軸封機構100旋轉。如圖所示,本實施例的軸封 機構100包括一迷宮環軸封120及一O型環150。迷宮環軸封120包含沿螺旋轉子110軸向設置的一本體130及徑向貫穿本體130的一排氣孔140。O型環150設置於迷宮環軸封120的外表面上。As shown in FIGS. 2 and 3, the present invention provides a shaft sealing mechanism 100 disposed between a casing 102 and a helical rotor 110 relative to the casing 102. That is, the shaft sealing mechanism 100 is preferably fixed to the casing 102, and the helical rotor 110 is rotated relative to the shaft sealing mechanism 100. As shown, the shaft seal of this embodiment The mechanism 100 includes a labyrinth ring seal 120 and an O-ring 150. The labyrinth ring seal 120 includes a body 130 disposed axially of the spiral rotor 110 and a venting opening 140 extending through the body 130. The O-ring 150 is disposed on the outer surface of the labyrinth ring seal 120.

如圖3所示,迷宮環軸封120外表面還形成用以設置O型環150的一凹槽122,且凹槽122較佳形成於本體130的中央位置,使呈狹長形的迷宮環軸封120不會偏移地相對螺旋轉子110而設置於機殼102上,以確保密封與定位的精度。在此所述的O型環150在於防止油或氣體從迷宮環軸封120和殼體102之間洩漏。排氣孔140可以開設於O型環150任意一側,並不限制。As shown in FIG. 3, the outer surface of the labyrinth ring shaft seal 120 further defines a recess 122 for arranging the O-ring 150, and the recess 122 is preferably formed at a central position of the body 130 to form an elongated labyrinth ring shaft. The seal 120 is disposed on the casing 102 with respect to the spiral rotor 110 without offset to ensure the accuracy of sealing and positioning. The O-ring 150 described herein is to prevent oil or gas from leaking between the labyrinth ring seal 120 and the housing 102. The vent hole 140 can be opened on either side of the O-ring 150 without limitation.

排氣孔140的數量亦可開設一對或以上,在如圖4所示的實施例中,兩排氣孔140可以對稱或非對稱地開設於O型環150的兩側,而使流體能夠快速地排出。除此之外,O型環150數量亦可包含一對或以上,並不限制。在如圖5所示的實施例中,兩O型環150較佳分別對稱地設置於本體130的兩側,使迷宮環軸封120不會偏移地相對螺旋轉子110而設置於機殼102上,其中排氣孔140可以單一地開設於各O型環140之間,也可以成對(或以上)地開設於各該O型環150之間,如圖6所示。The number of the vent holes 140 may also be a pair or more. In the embodiment shown in FIG. 4, the two vent holes 140 may be symmetrically or asymmetrically opened on both sides of the O-ring 150 to enable the fluid to Discharge quickly. In addition, the number of O-rings 150 may also include one or more, and is not limited. In the embodiment shown in FIG. 5, the two O-rings 150 are preferably symmetrically disposed on opposite sides of the body 130, so that the labyrinth ring seal 120 is disposed on the casing 102 with respect to the spiral rotor 110 without being offset. The venting holes 140 may be separately formed between the O-rings 140, or may be opened in pairs (or above) between the O-rings 150, as shown in FIG.

請一併參考圖2至圖6所示,本創作更包含鄰接迷宮環軸封120的一滾動軸承160及一拋油環170,其中拋油環170設置於迷宮環軸封120及滾動軸承160之間。如圖所示,採用油霧方式潤滑與冷卻的滾動軸承160及拋油環170分別固定於螺旋轉子110上。當螺旋轉子110在軸承機構100支撐下高速旋轉時,拋油環170藉由離心力的作用下,強化阻隔油氣進入緊鄰的迷宮環軸封120內,並使拋油環170形成低壓區域。在此所述的滾動軸承160可為一滾珠軸承、一滾柱軸承或其他適合的軸承。Referring to FIG. 2 to FIG. 6 together, the present invention further includes a rolling bearing 160 adjacent to the labyrinth ring shaft seal 120 and a slinger 170, wherein the slinger 170 is disposed between the labyrinth ring shaft seal 120 and the rolling bearing 160 . As shown in the figure, the rolling bearing 160 and the slinger 170 which are lubricated and cooled by the oil mist method are respectively fixed to the spiral rotor 110. When the spiral rotor 110 rotates at a high speed under the support of the bearing mechanism 100, the oil slinger 170 strengthens the barrier oil and gas into the immediately adjacent labyrinth ring shaft seal 120 by the centrifugal force, and causes the slinger 170 to form a low pressure region. The rolling bearing 160 described herein can be a ball bearing, a roller bearing or other suitable bearing.

在本實施例中,本體130相對螺旋轉子110的一側面還具有連續的一逆向螺旋齒180,其中逆向螺旋齒180的齒形方向進一步朝滾動軸承160方向設置,使油氣可以向壓縮腔室210相反方向送出。也就是說,由於螺旋轉子110的旋轉慣性,逆向螺旋齒180的設置可以帶動迷宮環軸封120與螺旋轉子110間間隙(未標示)內的氣體遠離壓縮腔室210,能有效達到阻隔潤滑油氣汙染,進而使本創作的軸封機構100性能提升(較佳)。In the present embodiment, the body 130 further has a continuous reverse helical tooth 180 on a side of the helical rotor 110, wherein the toothed direction of the reverse helical tooth 180 is further disposed toward the rolling bearing 160 so that the oil and gas can be opposite to the compression chamber 210. Send in the direction. That is to say, due to the rotational inertia of the spiral rotor 110, the arrangement of the reverse helical teeth 180 can drive the gas in the gap (not labeled) between the labyrinth ring shaft seal 120 and the helical rotor 110 away from the compression chamber 210, thereby effectively blocking the lubricating oil gas. Contamination, in turn, improves the performance of the shaft seal mechanism 100 of the present invention (better).

此外,迷宮環軸封120上直立地貫穿本體130一或以上的排氣孔140,使壓縮腔室210內之氣體僅可往外側排放,加上層層阻隔滾動軸承160潤滑油氣進入壓縮腔室210的軸封機構100,都能夠確保乾式無油螺旋壓縮機100的壓縮腔室210內無潤滑油氣被汙染的可能性。In addition, the labyrinth ring seal 120 extends upright through one or more exhaust holes 140 of the body 130, so that the gas in the compression chamber 210 can only be discharged to the outside, and the layer of barrier rolling bearing 160 is added to the compression chamber 210. The shaft sealing mechanism 100 can ensure that there is no possibility of contamination of the lubricating oil in the compression chamber 210 of the dry oil-free screw compressor 100.

請一併參考圖2至圖7所示,本創作另一較廣義的實施態樣還提供一種螺旋壓縮機200,包括一機殼102、至少一螺旋轉子110及前述實施例的軸封機構100。機殼102形成有一壓縮腔室210,螺旋轉子110設置於機殼102並穿過壓縮腔室210,其中螺旋轉子210具有至少一肩部112及鄰接肩部112的一逆向螺旋齒220,如圖7所示。在此所述的逆向螺旋齒220較佳是相對迷宮環軸封120的一側面設置。Referring to FIG. 2 to FIG. 7 together, another generalized embodiment of the present invention further provides a screw compressor 200 including a casing 102, at least one spiral rotor 110, and the shaft sealing mechanism 100 of the foregoing embodiment. . The casing 102 is formed with a compression chamber 210. The spiral rotor 110 is disposed in the casing 102 and passes through the compression chamber 210. The spiral rotor 210 has at least one shoulder portion 112 and a reverse spiral tooth 220 adjacent to the shoulder portion 112, as shown in the figure. 7 is shown. The reverse helical teeth 220 described herein are preferably disposed relative to one side of the labyrinth ring seal 120.

本實施例與前述實施例不同處在於逆向螺旋齒220的設置位置,但達成的功效均相同。此外,拋油環170更抵觸在肩部112上,且機殼102還形成有鄰近拋油環170的一拋油孔202,以便於將油氣排出大氣之外。由於螺旋轉子110具有直徑較小的肩部112使滾動軸承160的潤滑油更不容易順延著螺旋轉子110的外表面滲入迷宮環軸封120與螺旋轉子110間的間隙(未標示)內,以阻隔油氣進入鄰接的壓縮腔室210。再者,在所述間隙內的油氣或流體,更可藉由迷宮環軸封 120設置一或以上的排氣孔140往外側排放。因此,本創作利用層層阻隔潤滑油氣的軸封機構100及肩部112設計進入壓縮腔室210,有效增加本創作的可靠性。The difference between this embodiment and the foregoing embodiment lies in the position where the reverse helical teeth 220 are disposed, but the effects achieved are the same. In addition, the slinger 170 is more resistant to the shoulder 112, and the casing 102 is also formed with a slinger 202 adjacent to the slinger 170 to facilitate the discharge of oil and gas out of the atmosphere. Since the spiral rotor 110 has a shoulder portion 112 having a small diameter, the lubricating oil of the rolling bearing 160 is less likely to penetrate into the gap (not shown) between the labyrinth ring shaft seal 120 and the spiral rotor 110 along the outer surface of the spiral rotor 110 to block The oil and gas enters the adjacent compression chamber 210. Furthermore, the oil and gas or fluid in the gap can be sealed by the labyrinth ring 120 is provided to discharge one or more vent holes 140 to the outside. Therefore, the present invention utilizes the shaft sealing mechanism 100 and the shoulder portion 112 which are layered to block the lubricating oil gas, and is designed to enter the compression chamber 210, thereby effectively increasing the reliability of the creation.

因此本創作的軸封機構100元件較少(結構精簡),藉由設置逆向螺旋齒180、210使軸封性能提升,且縮短螺旋轉子軸向密封長度,進而可相對縮小螺旋壓縮機200的體積。Therefore, the shaft sealing mechanism 100 of the present invention has fewer components (simplified structure), and the shaft sealing performance is improved by providing the reverse helical teeth 180, 210, and the axial sealing length of the spiral rotor is shortened, thereby further reducing the volume of the screw compressor 200. .

綜上所述,本文於此所揭示的實施例應被視為用以說明本創作,而非用以限制本創作。本創作的範圍應由後附申請專利範圍所界定,並涵蓋其合法均等物,並不限於先前的描述。In summary, the embodiments disclosed herein are to be considered as illustrative of the present invention and are not intended to limit the present invention. The scope of this creation is defined by the scope of the appended patent application and covers its legal equivalents and is not limited to the foregoing description.

100‧‧‧軸封機構100‧‧‧ shaft sealing mechanism

102‧‧‧機殼102‧‧‧Shell

110‧‧‧螺旋轉子110‧‧‧Spiral rotor

112‧‧‧肩部112‧‧‧ shoulder

120‧‧‧迷宮環軸封120‧‧‧Maze ring shaft seal

122‧‧‧凹槽122‧‧‧ Groove

130‧‧‧本體130‧‧‧ Ontology

140‧‧‧排氣孔140‧‧‧ venting holes

150‧‧‧O型環150‧‧‧O-ring

160‧‧‧滾動軸承160‧‧‧ rolling bearings

170‧‧‧拋油環170‧‧‧Rearring ring

180‧‧‧逆向螺旋齒180‧‧‧Reverse helical teeth

200‧‧‧螺旋壓縮機200‧‧‧Spiral compressor

202‧‧‧拋油孔202‧‧‧Throwing hole

Claims (10)

一種軸封機構,設置在一機殼及相對於該機殼的一螺旋轉子之間,該軸封機構包含:一迷宮環軸封,包含沿該螺旋轉子軸向設置的一本體及徑向貫穿該本體的一排氣孔;以及一O型環,設置於該迷宮環軸封外表面上。 A shaft sealing mechanism is disposed between a casing and a spiral rotor relative to the casing, the shaft sealing mechanism comprising: a labyrinth ring shaft seal, including a body and a radial passage disposed along the axial direction of the spiral rotor An exhaust hole of the body; and an O-ring disposed on the outer surface of the labyrinth ring seal. 如請求項1所述的軸封機構,更包含鄰接該迷宮環軸封的一滾動軸承及一拋油環,其中該拋油環設置於該迷宮環軸封及該滾動軸承之間。 The shaft sealing mechanism of claim 1, further comprising a rolling bearing and a slinger adjacent to the labyrinth ring seal, wherein the slinger is disposed between the labyrinth ring seal and the rolling bearing. 如請求項2所述的軸封機構,其中該滾動軸承為一滾珠軸承或一滾柱軸承。 The shaft sealing mechanism of claim 2, wherein the rolling bearing is a ball bearing or a roller bearing. 如請求項2所述的軸封機構,其中該本體相對該螺旋轉子的一側面還具有連續的一逆向螺旋齒,該逆向螺旋齒的齒形方向進一步朝該滾動軸承方向設置。 The shaft sealing mechanism of claim 2, wherein the body further has a continuous reverse helical tooth with respect to a side of the helical rotor, the toothed direction of the reverse helical tooth being further disposed toward the rolling bearing. 如請求項1所述的軸封機構,其中該迷宮環軸封外表面還形成用以設置該O型環的一凹槽,且該凹槽形成於該本體的中央位置。 The shaft sealing mechanism of claim 1, wherein the outer surface of the labyrinth ring seal further forms a groove for arranging the O-ring, and the groove is formed at a central position of the body. 如請求項1所述的軸封機構,其中該本體橫向地固定於該機殼上,該螺旋轉子相對該本體旋轉,該排氣孔直立地貫穿該本體上。 A shaft sealing mechanism according to claim 1, wherein the body is laterally fixed to the casing, the spiral rotor is rotated relative to the body, and the vent hole extends through the body upright. 如請求項1所述的軸封機構,其中該排氣孔數量包含一對,該O型環數量包含一對,各該O型環分別對稱地設置於該本體的兩側,各該排氣孔則分別形成於該對O型環之間。 The shaft sealing mechanism of claim 1, wherein the number of the vent holes comprises a pair, the number of the O-rings includes a pair, and each of the O-rings is symmetrically disposed on two sides of the body, each of the exhausts Holes are formed between the pair of O-rings, respectively. 一種螺旋壓縮機,包括:一機殼,形成有一壓縮腔室; 至少一螺旋轉子,設置於該機殼並穿過該壓縮腔室,其中該螺旋轉子具有至少一肩部及鄰接該肩部的一逆向螺旋齒;以及一如請求項1至7任一項所述的軸封機構,該軸封機構設置於該機殼上並相對於該螺旋轉子設置。 A screw compressor comprising: a casing, forming a compression chamber; At least one helical rotor disposed in the housing and passing through the compression chamber, wherein the helical rotor has at least one shoulder and a reverse helical tooth adjacent the shoulder; and as claimed in any one of claims 1 to 7 The shaft sealing mechanism is disposed on the casing and disposed relative to the spiral rotor. 如請求項8所述的螺旋壓縮機,更包含鄰接該迷宮環軸封的一滾動軸承及一拋油環,其中該拋油環設置於該迷宮環軸封及該滾動軸承之間,其中該逆向螺旋齒相對該迷宮環軸封的一側面設置。 The screw compressor of claim 8, further comprising a rolling bearing and a slinger adjacent to the labyrinth ring seal, wherein the slinger is disposed between the labyrinth ring seal and the rolling bearing, wherein the reverse spiral The teeth are disposed relative to a side of the labyrinth ring seal. 如請求項9所述的螺旋壓縮機,其中該拋油環抵觸在該肩部上,該機殼還形成有鄰近該拋油環的一拋油孔。 The screw compressor of claim 9, wherein the oil slinger is in contact with the slinger, and the casing is further formed with a slinger adjacent to the slinger.
TW104208565U 2015-05-29 2015-05-29 Spiral compressor and its seal mechanism thereof TWM513933U (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10920784B2 (en) 2018-11-14 2021-02-16 Industrial Technology Research Institute Magnetic bearing centrifugal compressor and controlling method thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10920784B2 (en) 2018-11-14 2021-02-16 Industrial Technology Research Institute Magnetic bearing centrifugal compressor and controlling method thereof

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