TWM270266U - Concave structure of compressor thrust bearing - Google Patents

Concave structure of compressor thrust bearing Download PDF

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Publication number
TWM270266U
TWM270266U TW93217277U TW93217277U TWM270266U TW M270266 U TWM270266 U TW M270266U TW 93217277 U TW93217277 U TW 93217277U TW 93217277 U TW93217277 U TW 93217277U TW M270266 U TWM270266 U TW M270266U
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TW
Taiwan
Prior art keywords
thrust surface
concave
scroll
compressor
thrust
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TW93217277U
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Chinese (zh)
Inventor
Guang-De Tang
Jin-Dung Chen
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Chyn Tec Internat Co Ltd
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Application filed by Chyn Tec Internat Co Ltd filed Critical Chyn Tec Internat Co Ltd
Priority to TW93217277U priority Critical patent/TWM270266U/en
Publication of TWM270266U publication Critical patent/TWM270266U/en

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Description

M270266 八、新型說明: 【新型所屬之技術領域】 本創作係關於一種壓縮機止推面凹面結構,其特別係在支撐 下渦卷之止推面中形成凹面,用以促進潤滑油膜之建立者。 【先前技術】 習知的渦卷壓縮機中,由於其具有許多動件,以及其動件之 間會發生摩擦,其中,支撐其下渦卷之支撐座頂端面具有一止推 面,用以提供該下渦卷之底端面依附於該止推面上。一般這類的 渦卷壓縮機中,其支撐下渦卷之止推面,雖然具有溝槽,然而, 這些溝槽之只係設計作為導引潤滑油進入止推面,其未考慮平面 尺寸與深度對潤滑油液體動力之影響,導致引入止推面之潤滑油 無法形成良好的油膜分佈,因而造成潤滑效果不佳,使得其容易 因為磨損過度而造成使用壽命縮短。因此,本創作基於習用渦卷 壓縮機止推面之缺失而進行改良。 【新型内容】 本創作係一種壓縮機止推面凹面結構,其主要係應用於一渦 卷壓縮機中,該渦卷壓縮機係具有一上渦卷以及一下渦卷,且下 渦卷設置於一支撐座之止推面上,且下渦卷設置於一支撐座之止 推面上,一曲柄軸樞接於該支撐座中而一端動力連結至一轉動動 力,該曲柄轴頂端形成一曲柄,且透過該曲柄樞接該下满卷底端 面,使得下渦卷與上渦卷形成偏心的相對繞動運動,用以形成高 壓流體生成裝置。 M270266 本創作的壓縮機止推面凹面結構之一目的,係在其支撐座頂 端之止推面中,形成具有特定平面尺寸與深度之凹面,並透過凹 面之配置,而達到建立較佳的油膜分佈,因而可提供良好的潤滑 效果,以減缓元件之摩擦損耗,並延長其使用壽命者。 本創作的壓縮機止推面凹面結構之另一目的,係透過止推面 之凹面,可促進潤滑油引入止推面中,用以提供油膜建立所需之 潤滑油者。 為使熟悉該項技藝人士瞭解本創作之目的、特徵及功效,茲 藉由下述具體實施例,並配合所附之圖式,詳加說明如后。 【實施方式】 第1圖係顯示本創作壓縮機止推面凹面結構的一種具體實施 例之剖面示意圖,第2圖係顯示本創作壓縮機止推面凹面結構的 局部元件俯視平面示意圖,第3圖係顯示本創作壓縮機止推面凹 面結構的局部元件俯視示意圖,第4圖係顯示本創作第3圖I-Ι斷 面之剖面示意圖。 請參考第1圖所顯示,其主要係於一渦卷壓縮機(丨),透過在 一密閉殼體(11)的結構中,裝設一上渦卷(12)、一下渦卷(13)以及 一支撐座(14),所形成之高壓流體生成裝置。 前述之上渦卷(12)以及下渦卷(Π)係設置於該支撐座(14)所構 成,且下渦卷設置於一支撐座(14)上,一曲柄軸(13a)樞接於該支 撐座(14)中而一端動力連結至一轉動動力,該曲柄軸(13a)頂端形 成一曲柄(13b),且透過該曲柄(13b)樞接該下渦卷(13)端面,使得 下渦卷(13)與上渦卷(12)形成偏心的相對繞動運動,用以產生並輪 M270266 出高壓之工作氣體。 ^月 > 考第2、第3以及第4圖所顯示,前述之支撐座(1句頂端 面形成-止推面(15),該止推面(15)形成數個凹面(i5a)以及導油槽 (15d)其中該凹面(15a)具有適當深度以及平面尺寸,並配合該 止推面(15)與A下渴卷(13)之相對運動,而形成適當的配置,用以 建立該止推面(15)與該下渦卷(13)之_油膜⑽; 以及,該導油 槽⑽)具有適當深度,用卩將潤滑油導引入該止推面⑽與該下 渦卷(1,3)之間。以第2、第3以及第4圖所顯示為例,該止推面 士係形成數個凹面⑽),且各個凹面⑽)形成輻射狀分佈,使得 *下渴卷(13)在運作過程中與止推面(15)相對繞動時,觀察其單一 位置點所產生之路彳軌跡㈤所示 ,而各個凹面(15a)之平面 尺寸與/木度’係配合該止推面(15)與該下渦卷(13)繞動執跡(M)之 相對運動速度及方向,而造成下渦卷(13)與止推面(1〇之間的潤滑 油足以建立適當厚度之油膜(16), 以形成適當的油膜壓力分佈 ()並促使油膜(16)能趨向分佈均勻,用以分散下渦卷(13)與止推 面(15)之間的接觸應力,且提供其潤滑作用。 、第5圖係顯示為本創作壓縮機止推面溝槽結構另一實施例的 俯視平面示意圖。 ^ /明參考第5圖所顯示,前述之支撐座(14)頂端之止推面(15), ^系化成數個溝槽(l5b),各個溝槽⑽)形成同心圓分佈,且因為下 屑卷(13)在運作過程中係與止推面(15)形成相對繞動,因此下渦卷 (13)表面任—位置點不會沿著溝槽(15b)延伸方向運動,故能產生 液體動力潤滑之效果,而建立潤滑油膜。 、第6圖係顯示為本創作壓縮機止推面溝槽結構再一實施例的 俯視平面示意圖。 M270266 請參考第6圖所顯示,基於相同理由,前述之支撐座(14)頂端 之止推面(15),亦可形成數個溝槽(15c),且各個溝槽(15c)形成離 散的區塊分佈’其區塊係可以係圓形、矩形或其它任意的幾何造 型’並同時此在下渦卷(13)與止推面(15)形成相對繞動的過程中, 產生液體動力潤滑之效果,而建立潤滑油膜。 透過前述止推面(15)中所形成的凹面(15a)或(15b)或(15c),其 具有特定平面尺寸與深度,並經過適當的配置,因而可建立較佳 的油膜分佈,同時提供良好的潤滑效果,以減緩元件之摩擦損耗, 並延長其使用壽命者。再者,透過前述止推面(1乃之凹面(l5a)或M270266 8. Description of the new type: [Technical field to which the new type belongs] This creation relates to a concave structure of the thrust surface of a compressor, which is formed in particular by forming a concave surface in the thrust surface of a scroll under support to promote the establishment of a lubricant film . [Prior art] In the conventional scroll compressor, since it has many moving parts, and friction occurs between the moving parts, the top mask of the support seat supporting the lower scroll has a thrust surface for A bottom end surface provided with the lower scroll is attached to the thrust surface. Generally, in this type of scroll compressor, the thrust surface of the scroll under its support has grooves. However, these grooves are only designed to guide the lubricating oil into the thrust surface. It does not consider the plane size and The effect of depth on the fluid power of the lubricating oil leads to the inability of the lubricating oil introduced into the thrust surface to form a good oil film distribution, which results in poor lubricating effect and makes it easy to shorten its service life due to excessive wear. Therefore, this creation is based on the lack of thrust surfaces of conventional scroll compressors. [New content] This creation is a concave structure of the thrust surface of a compressor, which is mainly used in a scroll compressor. The scroll compressor has an upper scroll and a lower scroll, and the lower scroll is provided in A thrust surface of a support base, and a lower scroll is disposed on the thrust surface of a support base, a crank shaft is pivotally connected in the support base and one end is connected to a rotational power, and a crank is formed at the top end of the crank shaft And, the bottom end surface of the lower full roll is pivotally connected through the crank, so that the lower scroll and the upper scroll form an eccentric relative orbiting movement to form a high-pressure fluid generating device. M270266 One of the objectives of the concave structure of the thrust surface of the compressor is to form a concave surface with a specific plane size and depth in the thrust surface at the top of its support base, and to achieve a better oil film through the configuration of the concave surface. Distribution, which can provide good lubricating effect, to reduce the friction loss of components, and extend its service life. Another purpose of the concave structure of the thrust surface of the compressor created by this invention is to promote the introduction of lubricating oil into the thrust surface through the concave surface of the thrust surface to provide the lubricant required for the oil film establishment. In order to make those skilled in the art understand the purpose, characteristics and effects of this creation, the following specific examples are given in conjunction with the accompanying drawings, which will be described in detail later. [Embodiment] FIG. 1 is a schematic cross-sectional view showing a specific embodiment of the concave structure of the thrust surface of the compressor of the present invention, and FIG. 2 is a schematic plan view of the partial elements of the concave structure of the thrust surface of the compressor of the present invention, and The figure is a schematic plan view showing some components of the concave structure of the thrust surface of the compressor of the present invention, and the fourth diagram is a schematic cross-sectional view of the section I-I of the third diagram of the present invention. Please refer to Figure 1. It is mainly connected to a scroll compressor (丨). Through a structure of a closed casing (11), an upper scroll (12) and a lower scroll (13) are installed. And a support base (14), which forms a high-pressure fluid generating device. The upper scroll (12) and the lower scroll (Π) are arranged on the supporting base (14), and the lower scroll is arranged on a supporting base (14), and a crank shaft (13a) is pivotally connected to the supporting base (14). In the support base (14), one end of the power is connected to a rotational power. The top of the crank shaft (13a) forms a crank (13b), and the end of the lower scroll (13) is pivotally connected through the crank (13b), so that the lower The scroll (13) and the upper scroll (12) form an eccentric relative orbiting motion, which is used to generate and rotate the M270266 high-pressure working gas. ^ Months> As shown in Figs. 2, 3 and 4, the aforementioned support seat (the top surface of a sentence forms a thrust surface (15), and the thrust surface (15) forms several concave surfaces (i5a) and The oil guide groove (15d), wherein the concave surface (15a) has an appropriate depth and a planar size, and cooperates with the relative movement of the thrust surface (15) and the A thirst roll (13) to form an appropriate configuration for establishing the stop _Oil film ⑽ of the thrust surface (15) and the lower scroll (13); and, the oil guide groove ⑽) has an appropriate depth, and the lubricant is guided into the thrust surface 卩 and the lower scroll (1, 3) Between. Taking Figures 2, 3, and 4 as examples, the thrust surface is formed with several concave surfaces ⑽), and each concave surface ⑽) forms a radial distribution, so that the lower thirst roll (13) is in the operation process. When orbiting relative to the thrust surface (15), observe the path trajectory ㈤ generated by its single position point, and the plane size and / woodiness of each concave surface (15a) are matched with the thrust surface (15) The relative movement speed and direction of the orbit (M) with the lower scroll (13), so that the lubricating oil between the lower scroll (13) and the thrust surface (10) is sufficient to establish an oil film of an appropriate thickness (16 ) To form an appropriate oil film pressure distribution () and promote the oil film (16) to be evenly distributed to disperse the contact stress between the lower scroll (13) and the thrust surface (15) and provide its lubrication. Fig. 5 is a schematic plan view showing the top surface of another embodiment of the thrust groove structure of the compressor. ^ / Referring to Fig. 5 shows the thrust surface (15) at the top of the support base (14). ), Is formed into several grooves (l5b), each groove ⑽) forms a concentric circle distribution, and because the lower chip roll (13) is in the operation process It is relatively orbiting with the thrust surface (15). Therefore, the position of the surface of the lower scroll (13) will not move along the extending direction of the groove (15b), so it can produce the effect of hydrodynamic lubrication and establish lubrication. Oil film. Fig. 6 is a schematic top plan view showing another embodiment of the groove structure of the thrust surface of the compressor. M270266 Please refer to Figure 6. For the same reason, the thrust surface (15) at the top of the aforementioned support base (14) can also form several grooves (15c), and each groove (15c) forms a discrete Block distribution 'The block system can be circular, rectangular or other arbitrary geometric shapes', and at the same time, during the process of the relative scroll of the lower scroll (13) and the thrust surface (15), hydrodynamic lubrication is generated. Effect while building a lubricant film. Through the concave surface (15a) or (15b) or (15c) formed in the aforementioned thrust surface (15), which has a specific plane size and depth, and is properly configured, a better oil film distribution can be established, while providing Good lubricating effect to reduce friction loss of components and prolong their service life. Moreover, through the aforementioned thrust surface (1 is the concave surface (l5a) or

(15b)或(15c),可促進潤滑油引入止推面中,用以提供油膜建立所 需之潤滑油者。 N 另外,請參考第2、第5以及第6圖所顯示,各導油槽(15d) 一端開口於該止推面(15)之側邊緣,另一端則開口於該下渦卷(13) 曲柄軸(13a)與支撐座(14)之樞接處。使得該止推面(15)與該下渦卷 (13)之間產生相對運動時,可形成壓力差而將潤滑油吸入各導油槽 (15d)中,並提供形成油膜(16)所需。 彳曰 綜上所述,本創作之壓縮機止推面溝槽結構能夠達到以下效 果: / 1·本創作的壓縮機止推面凹面結構中,其支撐座頂端之止推面开> 成凹面,可於止推面與下渦卷之間有效地建立潤滑油膜,用= 減缓元件之摩擦損耗者。 2·本創作的壓縮機止推面凹面結構中,其支撐座頂端之止推面# 成導油槽,同時可將潤滑油導引入止推面中,用以提供建立= 膜所需之潤滑油者。 ' 3.透過本創作的壓縮機止推面凹面結構中,透過該止推面之凹 M270266 面,可提供建立潤滑油膜,並適當分配油膜之分佈,而達到接 觸壓力分佈變化較為和緩者。 雖然本創作已以具體實施例揭露如上,然其並非用以限定本 創作,任何熟悉此技藝者,在不脫離本創作之精神和範圍内,當 可作各種之更動與潤飾,其所作之更動與潤飾皆屬於本創作之範 疇,本創作之保護範圍當視後附之申請專利範圍所界定者為準。 【圖式簡單說明】 第1圖係顯示本創作壓縮機止推面凹面結構的一種具體實施例之 剖面示意圖。 第2圖係顯示本創作壓縮機止推面凹面結構的局部元件俯視平面 不意圖。 第3圖係顯示本創作壓縮機止推面凹面結構的局部元件俯視示意 圖。 第4圖係顯示本創作第3圖I-Ι斷面之剖面示意圖。 第5圖係顯示為本創作壓縮機止推面凹面結構另一實施例的俯視 平面示意圖。 第6圖係顯示為本創作壓縮機止推面凹面結構再一實施例的俯視 平面示意圖。 【主要元件符號說明】 渦卷壓縮機(1) 殼體(11) M270266 上渦卷(12) 下渦卷(13) 曲柄軸(13a) 曲柄(13b) 支撐座(14) 止推面(15) 溝槽凹面(15a) (15b) (15c) 導油槽(15d) 油膜(16) 壓力分佈(P) 繞動執跡(Μ)(15b) or (15c) can promote the introduction of lubricating oil into the thrust surface to provide the lubricant required for oil film establishment. N In addition, please refer to Figures 2, 5 and 6, as shown in the figure, one end of each oil guide groove (15d) is open at the side edge of the thrust surface (15), and the other end is open at the lower scroll (13) crank. The pivot joint of the shaft (13a) and the support seat (14). When a relative movement occurs between the thrust surface (15) and the lower scroll (13), a pressure difference can be formed to suck the lubricating oil into each of the oil guide grooves (15d), and to provide the oil film (16). In summary, the groove structure of the thrust surface of the compressor of this creation can achieve the following effects: / 1 · In the concave structure of the thrust surface of the compressor of this creation, the thrust surface at the top of the support seat is opened > Concave surface can effectively establish a lubricant film between the thrust surface and the lower scroll. Use = to reduce the friction loss of the component. 2. In the concave structure of the thrust surface of the compressor of this creation, the thrust surface # on the top of the support seat forms an oil guide groove, and at the same time, the lubricant can be introduced into the thrust surface to provide the lubrication required to establish the membrane. Oiler. '3. Through the concave structure of the thrust surface of the compressor created by this creation, through the concave M270266 surface of the thrust surface, it is possible to provide the establishment of a lubricating oil film, and the distribution of the oil film is appropriately distributed, so that the change of the contact pressure distribution is relatively gentle. Although this creation has been disclosed as above with specific embodiments, it is not intended to limit this creation. Anyone who is familiar with this skill can make various changes and decorations without departing from the spirit and scope of this creation. And retouching both belong to the scope of this creation, and the scope of protection of this creation shall be determined by the scope of the attached patent application. [Brief description of the drawings] Fig. 1 is a schematic cross-sectional view showing a specific embodiment of the concave structure of the thrust surface of the compressor of the present invention. Fig. 2 shows the plan view of the partial elements of the concave surface structure of the thrust surface of the compressor of this creation. Fig. 3 is a schematic plan view showing some components of the concave structure of the thrust surface of the compressor of the present invention. Figure 4 is a schematic cross-sectional view showing the section I-I in Figure 3 of this creation. Fig. 5 is a schematic top plan view showing another embodiment of the concave structure of the thrust surface of the creative compressor. Fig. 6 is a schematic top plan view showing another embodiment of the concave structure of the thrust surface of the creative compressor. [Description of main component symbols] Scroll compressor (1) Housing (11) M270266 Upper scroll (12) Lower scroll (13) Crank shaft (13a) Crank (13b) Support seat (14) Thrust surface (15 ) Groove concave surface (15a) (15b) (15c) Oil guide groove (15d) Oil film (16) Pressure distribution (P) Orbit (M)

Claims (1)

M270266 九、申請專利範圍: 1. 一種壓縮機止推面凹面結構,其主要係於一渦卷壓縮機中,具 有一上渦卷以及一下渦卷,且下渦卷設置於一支撐座上,一曲 柄軸樞接於該支撐座中而一端動力連結至一轉動動力,該曲柄 軸頂端形成一曲柄,且透過該曲柄樞接該下渦卷底端面,使得 下渦卷與上渦卷形成偏心的相對繞動運動,用以形成一高壓流 · 體生成裝置;其特徵在於: 前述之支撐座頂端面形成一止推面,該止推面形成凹入表面的 凹面,該凹面具有適當深度以及平面尺寸,並配合該止推面與馨 該下渦卷之相對運動,用以建立該止推面與該下渦卷之間的油 膜。 2. 如申請專利範圍第1項所述之壓縮機止推面凹面結構,其中, 該止推面上增設一或數個導油槽具有適當深度,用以將潤滑油 導引入該止推面與該下渦卷之間。 3. 如申請專利範圍第2項所述之壓縮機止推面凹面結構,其中, 該導油槽一端開口於該止推面之側邊緣,另一端則開口於該下 渦卷曲柄軸與支撐座之樞接處。 · 4. 如申請專利範圍第1項所述之壓縮機止推面凹面結構,其中, 該止推面上之各個凹面之平面尺寸與深度,係配合該止推面與 該下渦卷之相對運動速度及方向,而造成下渦卷與止推面之間 的潤滑油足以建立適當厚度之油膜,而形成適當的油膜壓力分 佈。 5. 如申請專利範圍第1項所述之壓縮機止推面凹面結構,其中, 該止推面上係形成數個凹面,且各個凹面形成輻射狀分佈。 ^ 11 M270266 6·如申請專利範圍第1項所述之壓縮機止推面凹面結構,其中, 該支撐座頂端之止推面,係形成數個凹面,且各個凹面形成同 心圓分佈。 7·如申請專利範圍第1項所述之壓縮機止推面凹面結構,其中, 該支撐座頂端之止推面,亦可形成數個凹面,且各個凹面形成 離散的區塊分佈。 12M270266 9. Scope of patent application: 1. A compressor thrust surface concave structure, which is mainly connected to a scroll compressor, has an upper scroll and a lower scroll, and the lower scroll is arranged on a support base. A crank shaft is pivoted in the support seat and one end is connected to a rotating power. A crank is formed at the top end of the crank shaft, and the bottom end surface of the lower scroll is pivoted through the crank, so that the lower scroll and the upper scroll form an eccentricity. The relative orbiting motion is used to form a high-pressure flow and volume generating device; it is characterized in that: the front end surface of the support seat forms a thrust surface, the thrust surface forms a concave surface with a concave surface, and the concave surface has an appropriate depth and The plane size and the relative movement of the thrust surface and the lower scroll are used to establish an oil film between the thrust surface and the lower scroll. 2. The concave structure of the thrust surface of the compressor as described in item 1 of the scope of the patent application, wherein one or more oil guide grooves are added to the thrust surface to have an appropriate depth for introducing the lubricant into the thrust surface. And the lower scroll. 3. The concave structure of the thrust surface of the compressor according to item 2 of the scope of the patent application, wherein one end of the oil guide groove is opened at a side edge of the thrust surface, and the other end is opened at the lower vortex curling shaft and the support seat. Of the pivot. · 4. The concave structure of the thrust surface of the compressor as described in item 1 of the scope of patent application, wherein the plane size and depth of each concave surface of the thrust surface are matched with the relative of the thrust surface and the lower scroll. The speed and direction of the movement, so that the lubricating oil between the lower scroll and the thrust surface is sufficient to establish an oil film of an appropriate thickness and form an appropriate oil film pressure distribution. 5. The concave structure of the thrust surface of the compressor according to item 1 of the scope of the patent application, wherein the thrust surface is formed with several concave surfaces, and each concave surface forms a radial distribution. ^ 11 M270266 6. The concave structure of the thrust surface of the compressor according to item 1 of the scope of patent application, wherein the thrust surface at the top of the support base forms a plurality of concave surfaces, and each concave surface forms a concentric circle distribution. 7. The concave structure of the thrust surface of the compressor according to item 1 of the scope of patent application, wherein the thrust surface at the top of the support base can also form several concave surfaces, and each concave surface forms a discrete block distribution. 12
TW93217277U 2004-10-29 2004-10-29 Concave structure of compressor thrust bearing TWM270266U (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114562454A (en) * 2022-04-01 2022-05-31 广东美的环境科技有限公司 Movable disc structure, compressor and temperature control equipment
WO2024022505A1 (en) * 2022-07-29 2024-02-01 丹佛斯(天津)有限公司 Scroll compressor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114562454A (en) * 2022-04-01 2022-05-31 广东美的环境科技有限公司 Movable disc structure, compressor and temperature control equipment
CN114562454B (en) * 2022-04-01 2023-12-22 广东美的环境科技有限公司 Movable plate structure, compressor and temperature control equipment
WO2024022505A1 (en) * 2022-07-29 2024-02-01 丹佛斯(天津)有限公司 Scroll compressor

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