CN104265630B - A spherical ball compressor - Google Patents
A spherical ball compressor Download PDFInfo
- Publication number
- CN104265630B CN104265630B CN201410489893.0A CN201410489893A CN104265630B CN 104265630 B CN104265630 B CN 104265630B CN 201410489893 A CN201410489893 A CN 201410489893A CN 104265630 B CN104265630 B CN 104265630B
- Authority
- CN
- China
- Prior art keywords
- spherical shell
- sphere
- ring
- spherical
- groove
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/02—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
- F04C18/04—Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents of internal-axis type
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Compressor (AREA)
Abstract
Description
技术领域technical field
本发明涉及一种球形滚珠压缩机,具有回转式压缩机的工作特征,用于对各种气体进行压缩,提高气体压力。The invention relates to a spherical ball compressor, which has the working characteristics of a rotary compressor and is used for compressing various gases and increasing the gas pressure.
背景技术Background technique
压缩机是一种用来压缩气体以提高气体压力或输送气体的机械,广泛应用于动力、制冷、冶金、石油化工等行业。按作用原理分类,压缩机主要可分为容积型和速度型。容积型压缩机分为往复式和回转式,速度型压缩机分为离心式和轴流式。往复式压缩机通过活塞在气缸内的往复运动,周期性地吸气、压缩和排气,完成气体的压缩过程。回转式压缩机是通过活塞的旋转动作使气体体积缩小以提高气体压力的,其工作效率通常高于往复式压缩机。回转式压缩机的种类很多,采用的具体压缩方法各不相同,各有自己的特点。Compressor is a kind of machinery used to compress gas to increase gas pressure or transport gas. It is widely used in power, refrigeration, metallurgy, petrochemical and other industries. According to the principle of action, compressors can be mainly divided into volume type and speed type. Volumetric compressors are divided into reciprocating and rotary, and speed compressors are divided into centrifugal and axial. The reciprocating compressor periodically inhales, compresses and exhausts air through the reciprocating movement of the piston in the cylinder to complete the gas compression process. The rotary compressor reduces the volume of the gas through the rotation of the piston to increase the gas pressure, and its working efficiency is usually higher than that of the reciprocating compressor. There are many types of rotary compressors, and the specific compression methods used are different, each with its own characteristics.
目前,回转式压缩机按结构特点可分为滚动转子式、滑片式、螺杆式、涡旋式等,各有其优缺点。滚动转子式压缩机一旦在其轴承、主轴、滚轮或是滑片处发生磨损,间隙增大,将会对其性能产生较明显的不良影响。滑片式压缩机由于滑片与转子及气缸间存在较大的机械摩擦损失,导致其效率相对较低,从而限制了它的使用范围。螺杆式压缩机不适合小的气体流量场合,气体周期性地高速通过吸、排气孔口以及通过缝隙的泄漏等因素会造成很大的噪声,因而需要采取消音减噪措施;另外,螺旋形转子的空间曲面的加工精度要求高,需用专用设备和刀具来加工;由于间隙密封和转子刚度等的限制,目前螺杆式压缩机还不能像往复式压缩机那样达到较高的终了压力。涡旋式制冷压缩机在较小的气体流量的工况下,效率相对比较低,制造成本比较高,需要高精度的加工设备及精确的调心装配技术。At present, rotary compressors can be divided into rolling rotor type, sliding vane type, screw type, scroll type, etc. according to their structural characteristics, each with its own advantages and disadvantages. Once the bearings, main shaft, rollers or slides of the rolling rotor compressor are worn and the gap increases, it will have a more obvious adverse effect on its performance. Due to the large mechanical friction loss between the sliding vane and the rotor and the cylinder, the sliding vane compressor has a relatively low efficiency, which limits its application range. Screw compressors are not suitable for small gas flow occasions. Factors such as the periodic high-speed passage of gas through suction and exhaust holes and leakage through gaps will cause a lot of noise, so noise reduction and noise reduction measures need to be taken; in addition, the spiral The machining accuracy of the space curved surface of the rotor is high, and special equipment and tools are needed to process it; due to the limitations of gap seals and rotor stiffness, screw compressors cannot achieve higher end pressures like reciprocating compressors at present. Scroll refrigeration compressors have relatively low efficiency and high manufacturing costs under the condition of small gas flow, and require high-precision processing equipment and precise self-aligning assembly technology.
综上所述,已有的回转式压缩机均存在各种缺陷或局限性。To sum up, the existing rotary compressors have various defects or limitations.
发明内容Contents of the invention
本发明公开了一种球形滚珠压缩机,目的是消除或减轻目前应用的回转式压缩机的缺陷或不足,结构简单、易损件少,且部件加工简单、无需精密的装配技术,同时压缩效率高。The invention discloses a spherical ball compressor, which aims at eliminating or alleviating the defects or deficiencies of the currently used rotary compressors. high.
本发明的技术方案如下:Technical scheme of the present invention is as follows:
一种球形滚珠压缩机,包括同心的球体和球壳,所述球体的外径略小于所述球壳的内径使所述球体可以在球壳内转动;所述球体的外表面设有一条凸起的球体凸环和两条内凹的球体弧槽,所述两条球体弧槽对称地设于所述球体的两端,分别与所述球体凸环呈90°夹角相交,在两个相交处所述球体凸环开有两处凸环缺口,所述球体弧槽的横截面为半圆形;所述球壳的内表面设有一条凹下的球壳凹环和一条凹下的球壳环槽,所述球壳环槽与所述球壳凹环以5~85°夹角相交,形成两个球壳环槽和球壳凹环之间相通的球壳槽交汇处,所述球壳凹环与所述球体凸环相嵌在一起,所述球壳环槽的横截面为与所述球体弧槽的横截面相同尺寸的半圆形;在所述球体上设有两根球体轴,所述球体轴与所述球体凸环垂直,球体绕所述球体轴旋转;在所述球壳上设有轴孔,所述轴孔的轴线与所述球壳凹环垂直,所述球体轴穿过所述轴孔与驱动机械连接;所述球体弧槽和球壳环槽之间有两个弧环槽交汇处,每个所述弧环槽交汇处均设有一个滚珠,所述滚珠的半径与所述球体弧槽的横截面半径一致;在每个所述球壳槽交汇处的两侧,均分别开设有吸气口和排气口,所述吸气口和排气口均与所述球壳环槽相通,所述排气口上设有排气阀。A spherical ball compressor, comprising a concentric sphere and a spherical shell, the outer diameter of the sphere is slightly smaller than the inner diameter of the spherical shell so that the sphere can rotate in the spherical shell; the outer surface of the sphere is provided with a convex The raised sphere convex ring and two concave sphere arc grooves, the two sphere arc grooves are symmetrically arranged at both ends of the sphere, and intersect with the sphere convex ring at an angle of 90° respectively. The convex ring of the sphere at the intersection has two convex ring gaps, and the cross section of the arc groove of the sphere is semicircular; the inner surface of the spherical shell is provided with a concave spherical shell concave ring and a concave concave ring. Spherical shell ring groove, the spherical shell ring groove and the spherical shell concave ring intersect at an angle of 5 to 85° to form a spherical shell groove intersection between two spherical shell ring grooves and the spherical shell concave ring. The concave ring of the spherical shell is embedded with the convex ring of the sphere, and the cross section of the annular groove of the spherical shell is a semicircle with the same size as the cross section of the arc groove of the sphere; root sphere axis, the sphere axis is perpendicular to the sphere convex ring, and the sphere rotates around the sphere axis; a shaft hole is arranged on the spherical shell, the axis of the shaft hole is perpendicular to the concave ring of the spherical shell, The sphere shaft passes through the shaft hole and is connected to the driving machine; there are two arc ring groove intersections between the sphere arc groove and the spherical shell ring groove, and each arc ring groove intersection is provided with a ball , the radius of the ball is consistent with the cross-sectional radius of the arc groove of the sphere; on both sides of the intersection of each spherical shell groove, there are respectively provided with an air inlet and an exhaust port, and the air inlet and the air outlet The exhaust ports communicate with the annular groove of the spherical shell, and the exhaust ports are provided with exhaust valves.
本发明其压缩原理在于:随着球体在球壳内的转动,在球体弧槽和球壳环槽的约束下,滚珠在球体弧槽内作往复运动,在球壳环槽内作回转运动;大部分时间所述球壳槽交汇处被所述球体凸环占据,所述球壳环槽内在滚珠前进方向和球体凸环之间形成压缩空间(这时排气阀在弹簧力作用下关闭),进行气体压缩;所述球壳环槽内在滚珠后方空间与所述吸气口连通,进行吸气过程;当滚珠移动到接近所述球壳槽交汇处时,被压缩的气体大于排气阀弹簧力顶开所述排气阀阀门,实现排气;排气后滚珠将进入球壳槽交汇处,这时所述球体凸环上的凸环缺口正好转入球壳槽交汇处,使得通道打开,滚珠通过。滚珠通过所述球壳槽交汇处后再次产生吸气、压缩、排气效果。球体旋转一周,两个滚珠各产生两次压缩、排气过程。The compression principle of the present invention is: as the ball rotates in the spherical shell, under the constraints of the spherical arc groove and the spherical shell ring groove, the ball reciprocates in the spherical arc groove and rotates in the spherical shell ring groove; Most of the time, the intersection of the spherical shell groove is occupied by the spherical convex ring, and a compression space is formed in the spherical shell annular groove between the forward direction of the ball and the spherical convex ring (at this time, the exhaust valve is closed under the spring force. ), to perform gas compression; the space behind the ball in the spherical shell ring groove communicates with the air suction port to carry out the air suction process; when the ball moves close to the junction of the spherical shell groove, the compressed gas is greater than the exhaust gas The spring force of the air valve opens the exhaust valve valve to realize exhaust; after the exhaust, the ball will enter the intersection of the spherical shell groove, and at this time, the convex ring gap on the convex ring of the ball just turns into the intersection of the spherical shell groove, This opens the channel and allows the ball to pass through. After the balls pass through the intersection of the spherical shell grooves, the effects of air suction, compression and exhaust are generated again. The ball rotates once, and the two balls each generate two compression and exhaust processes.
其中,所述球体凸环的横截面为矩形,所述球壳凹环的横截面为与所述球体凸环的横截面相同尺寸的矩形。Wherein, the cross section of the spherical convex ring is rectangular, and the cross section of the spherical shell concave ring is rectangular with the same size as the cross section of the spherical convex ring.
其中,所述球壳环槽与所述球壳凹环之间的夹角为5~85°;所述球壳环槽与所述球壳凹环之间的夹角越大,所述球体弧槽的弧长越长。Wherein, the angle between the spherical shell ring groove and the spherical shell concave ring is 5-85°; the larger the angle between the spherical shell ring groove and the spherical shell concave ring, the more the sphere The arc length of the arc groove is longer.
优选地,所述球壳环槽与所述球壳凹环之间的夹角为45°。Preferably, the included angle between the spherical shell ring groove and the spherical shell concave ring is 45°.
优选地,所述凸环缺口的宽度略大于所述球体弧槽的直径,以便于球体弧槽中的滚珠通过。Preferably, the width of the notch of the convex ring is slightly larger than the diameter of the arc groove of the sphere, so as to facilitate the passage of the balls in the arc groove of the sphere.
进一步地,为装配方便,所述球壳为两个关于凹环中心对称的部件对接构成。Further, for the convenience of assembly, the spherical shell is formed by butting of two symmetrical parts about the center of the concave ring.
由于滚珠在球体弧槽内的往复运动可能会造成弧槽内气体的有害压缩或膨胀,进一步地,在所述球体弧槽的底部开有一条细槽,让滚珠两侧气体导通。Since the reciprocating motion of the ball in the arc groove of the ball may cause harmful compression or expansion of the gas in the arc groove, further, a thin groove is opened at the bottom of the arc groove of the ball to allow the gas on both sides of the ball to conduct.
由于采用了上述技术方案,本发明的优点和积极效果:本发明所述的一种球形滚珠压缩机结构简单、部件加工简单、无吸气阀,易损件少、无需精密的装配技术、制作成本低、适用于各种气体压缩,压缩效率高。Due to the adoption of the above technical solution, the advantages and positive effects of the present invention: a spherical ball compressor described in the present invention has simple structure, simple parts processing, no suction valve, less wearing parts, no need for precise assembly technology, production Low cost, suitable for various gas compression, high compression efficiency.
附图说明Description of drawings
图1是本发明一种球形滚珠压缩机的一个较优实施例的球体的正面视图。Fig. 1 is a front view of a ball in a preferred embodiment of a spherical ball compressor of the present invention.
图2是图1所示球体的侧面视图。Figure 2 is a side view of the sphere shown in Figure 1 .
图3是图1所示球体的正面剖视图。Fig. 3 is a front cross-sectional view of the sphere shown in Fig. 1 .
图4是本发明一种球形滚珠压缩机的一个较优实施例的球壳的正面剖视图。Fig. 4 is a front sectional view of a spherical shell of a preferred embodiment of a spherical ball compressor of the present invention.
图5是图4所示球壳的F-F位置侧面剖视图。Fig. 5 is a side cross-sectional view at position F-F of the spherical shell shown in Fig. 4 .
图6是本发明一种球形滚珠压缩机的一个较优实施例的正剖面视图;此图中,滚珠在球体弧槽的左止点位置,在球壳环槽的一端吸气口和另一端排气口的中间位置。Fig. 6 is a front sectional view of a preferred embodiment of a spherical ball compressor of the present invention; Middle position of the exhaust port.
图7是图6所示球形滚珠压缩机的A-A位置的剖视图,该剖面沿着球壳环槽剖开,与图6所示的剖面相垂直;此图中,滚珠的位置与图6相同,滚珠移动前方压缩气体,后方吸气。Fig. 7 is a sectional view of the A-A position of the spherical ball compressor shown in Fig. 6, the section is cut along the ring groove of the spherical shell, and is perpendicular to the section shown in Fig. 6; in this figure, the position of the ball is the same as that of Fig. 6, The balls move the front to compress the gas and the rear to inhale it.
图8是球体从图6位置旋转一定角度后,沿着球体弧槽位置的剖视图。Fig. 8 is a cross-sectional view along the position of the arc groove of the sphere after the sphere is rotated by a certain angle from the position in Fig. 6 .
图9是图8所示球形滚珠压缩机的B-B位置的剖视图,该剖面沿着球壳环槽剖开,与图8所示的剖面成一定角度;此图中,滚珠移动前方排气,后方吸气。Fig. 9 is a cross-sectional view of the B-B position of the spherical ball compressor shown in Fig. 8. The cross-section is cut along the ring groove of the spherical shell and forms a certain angle with the cross-section shown in Fig. 8; inhale.
图10是球体从图6位置旋转90°后,沿着球体弧槽位置的剖视图;此图中,滚珠的位置处于球体弧槽中间位置,也即处于凸环缺口位置,同时滚珠也处于球壳的球壳槽交汇处。Figure 10 is a sectional view along the arc groove of the ball after the ball is rotated 90° from the position in Figure 6; in this figure, the position of the ball is in the middle of the arc groove of the ball, that is, at the notch of the convex ring, and the ball is also in the spherical shell The intersection of spherical shell and groove.
图11是图10所示球形滚珠压缩机的C-C位置的剖视图,该剖面沿着球壳环槽剖开,与图10所示的剖面成45°;此图中,滚珠的位置与图10相同,此时,既不排气、也不吸气。Figure 11 is a cross-sectional view of the C-C position of the spherical ball compressor shown in Figure 10, the section is cut along the ring groove of the spherical shell, and is 45° from the section shown in Figure 10; in this figure, the position of the ball is the same as that in Figure 10 , at this time, neither exhaust nor inhale.
图12是球体从图10位置继续旋转若干角度后,沿着球体弧槽位置的剖视图;此图中,滚珠的位置处于球体弧槽偏右一些的位置。Figure 12 is a cross-sectional view of the ball along the arc groove after the ball continues to rotate for several angles from the position in Figure 10; in this figure, the position of the ball is slightly to the right of the arc groove of the ball.
图13是图12所示球形滚珠压缩机的D-D位置的剖视图,该剖面沿着球壳环槽剖开,与图12所示的剖面成一定角度;此图中,滚珠移动前方压缩气体,后方吸气。Fig. 13 is a cross-sectional view of the D-D position of the spherical ball compressor shown in Fig. 12. The cross-section is cut along the ring groove of the spherical shell and forms a certain angle with the cross-section shown in Fig. 12; in this figure, the ball moves forward to compress the gas, and the rear inhale.
图14是球体从图10位置旋转90°后,也即是球体从图6位置旋转180°后,沿着球体弧槽位置的剖视图;此图中,滚珠在球体弧槽的右止点位置,在球壳环槽一端吸气口和另一端排气口的中间位置。由于两个滚珠及两处吸气口和排气口的对称性,此图的效果与图6等同。Figure 14 is a sectional view along the arc groove of the ball after the ball rotates 90° from the position in Figure 10, that is, after the ball rotates 180° from the position in Figure 6; in this figure, the ball is at the right dead center of the arc groove of the ball, In the middle of the suction port at one end of the ring groove of the spherical shell and the exhaust port at the other end. Due to the symmetry of the two balls and the two air inlets and exhaust ports, the effect of this figure is equivalent to that of Figure 6.
图15是图14所示球形滚珠压缩机的E-E位置的剖视图,该剖面沿着球壳环槽剖开,与图14所示的剖面相垂直;此图中,滚珠的位置与图14相同,滚珠移动前方压缩气体,后方吸气。由于两个滚珠及两处吸气口和排气口的对称性,此图的效果与图7等同。Figure 15 is a sectional view of the E-E position of the spherical ball compressor shown in Figure 14, the section is cut along the ring groove of the spherical shell, and is perpendicular to the section shown in Figure 14; in this figure, the position of the ball is the same as that of Figure 14, The balls move the front to compress the gas and the rear to inhale it. Due to the symmetry of the two balls and the two air inlets and exhaust ports, the effect of this figure is equivalent to that of Figure 7.
其中:1.球体轴,2.球体,3.球体凸环,4.球体弧槽,5.轴孔,6.球壳,7.球壳环槽,8.球壳凹环,9.滚珠,10.吸气口,11.排气阀,12.排气口,13.凸环缺口,14.球壳槽交汇处。Among them: 1. sphere shaft, 2. sphere, 3. sphere convex ring, 4. sphere arc groove, 5. shaft hole, 6. spherical shell, 7. spherical shell ring groove, 8. spherical shell concave ring, 9. ball , 10. Suction port, 11. Exhaust valve, 12. Exhaust port, 13. Convex notch, 14. Spherical shell groove intersection.
具体实施方式detailed description
以下结合附图和实施例对本发明作进一步描述,但本实施例并不用于限制本发明,凡是采用本发明的相似结构及其相似变化,均应列入本发明的保护范围。The present invention will be further described below in conjunction with accompanying drawing and embodiment, but present embodiment is not intended to limit the present invention, and all adopt similar structures of the present invention and similar changes thereof, all should be included in the scope of protection of the present invention.
一种球形滚珠压缩机,如图1~15所示,包括同心的球体2和球壳6,球体2的外径略小于球壳6的内径使球体2可以在球壳6内转动。A spherical ball compressor, as shown in Figures 1-15, includes a concentric sphere 2 and a spherical shell 6. The outer diameter of the sphere 2 is slightly smaller than the inner diameter of the spherical shell 6 so that the sphere 2 can rotate in the spherical shell 6.
结合图1~3所示,球体2的外表面设有一条凸起的球体凸环3和两条内凹的球体弧槽4,两条球体弧槽4对称地设于球体2的两端,分别与球体凸环3呈90°夹角相交,在两个相交处球体凸环3开有两处凸环缺口13。其中球体凸环3的横截面为矩形,球体弧槽4的横截面为半圆形。结合图4~5所示,球壳6的内表面设有一条凹下的球壳凹环8和一条凹下的球壳环槽7,球壳环槽7与球壳凹环8可以以5~85°夹角相交形成两个球壳环槽7和球壳凹环8之间相通的球壳槽交汇处14,其中该夹角优选是45°,本实施例中,采用45°夹角。在每个球壳槽交汇处14的两侧,均分别开设有吸气口10和排气口12,吸气口10和排气口12均与球壳环槽4相通,排气口12上设有排气阀11。其中,球壳凹环8的横截面尺寸与球体凸环3的横截面尺寸相匹配,球壳凹环8与球体凸环3相嵌在一起,球体2可沿相嵌的环道在球壳6内回转。球壳环槽7的横截面为与球体弧槽4的横截面相同尺寸的半圆形。As shown in Figures 1-3, the outer surface of the sphere 2 is provided with a raised sphere convex ring 3 and two concave sphere arc grooves 4, and the two sphere arc grooves 4 are symmetrically arranged at both ends of the sphere 2, They respectively intersect with the spherical convex ring 3 at an angle of 90°, and there are two convex ring gaps 13 in the spherical convex ring 3 at the two intersections. The cross section of the spherical convex ring 3 is rectangular, and the cross section of the spherical arc groove 4 is semicircular. As shown in Figures 4-5, the inner surface of the spherical shell 6 is provided with a concave spherical shell ring 8 and a concave spherical shell ring groove 7, the spherical shell ring groove 7 and the spherical shell concave ring 8 can be formed in 5 ~85° included angle intersects to form the spherical shell groove intersection 14 between the two spherical shell ring grooves 7 and the spherical shell concave ring 8, wherein the included angle is preferably 45°. In this embodiment, the included angle of 45° is used . On both sides of the intersection 14 of each spherical shell groove, an air inlet 10 and an exhaust port 12 are respectively provided. An exhaust valve 11 is provided. Wherein, the cross-sectional size of the concave ring 8 of the spherical shell matches the cross-sectional size of the convex ring 3 of the spherical shell, the concave ring 8 of the spherical shell is embedded with the convex ring 3 of the spherical body, and the sphere 2 can be placed on the spherical shell along the embedded ring road. 6 internal turns. The cross section of the spherical shell ring groove 7 is a semicircle with the same size as the cross section of the spherical arc groove 4 .
在球体2上设有两根球体轴1,球体轴1与球体凸环3垂直,球体2绕球体轴1旋转,在球壳6上设有轴孔5,轴孔5的轴线与球壳凹环8垂直,球体轴1穿过轴孔5与驱动机械连接,带动球体2转动。Two ball shafts 1 are arranged on the ball 2. The ball shaft 1 is perpendicular to the ball convex ring 3. The ball 2 rotates around the ball shaft 1. The ball shell 6 is provided with a shaft hole 5. The axis of the shaft hole 5 is concave with the ball shell. The ring 8 is vertical, and the sphere shaft 1 passes through the shaft hole 5 and is connected with the driving machine to drive the sphere 2 to rotate.
球体弧槽4和球壳环槽7之间有两个弧环槽交汇处,每个弧环槽交汇处均设有一个滚珠9,滚珠9的半径与球体弧槽4的横截面半径一致,这样滚珠9的一半在球体弧槽4内,另一半在球壳环槽7内。凸环缺口13的宽度略大于滚珠9的直径,以便于球体弧槽4中的滚珠9从凸环缺口13处通过。球壳槽交汇处14的大小可以让滚珠9通过,也可以让球体凸环3通过。There are two arc ring groove intersections between the spherical arc groove 4 and the spherical shell ring groove 7, each arc ring groove intersection is provided with a ball 9, the radius of the ball 9 is consistent with the cross-sectional radius of the spherical arc groove 4, Half of the ball 9 is in the arc groove 4 of the ball like this, and the other half is in the ring groove 7 of the spherical shell. The width of the notch 13 of the convex ring is slightly larger than the diameter of the ball 9 so that the ball 9 in the arc groove 4 of the ball passes through the notch 13 of the convex ring. The size of the spherical shell groove intersection 14 can allow the ball 9 to pass through, and also can allow the spheroid convex ring 3 to pass through.
其中,为装配方便,球壳6可以为两个关于凹环中心对称的部件对接构成。Wherein, for the convenience of assembly, the spherical shell 6 can be formed by butting two components symmetrical to the center of the concave ring.
由于滚珠9在球体弧槽4内的往复运动可能会造成球体弧槽4内气体的有害压缩或膨胀,进一步地可以在球体弧槽4的底部开一条细槽(图中未示出),让球体弧槽4内滚珠9两侧气体导通。Since the reciprocating motion of the ball 9 in the arc groove 4 of the ball may cause harmful compression or expansion of the gas in the arc groove 4 of the ball, further a thin groove (not shown) can be opened at the bottom of the arc groove 4 of the ball to allow The two sides of the ball 9 in the spherical arc groove 4 are connected with gas.
结合图6和7所示,滚珠9在球体弧槽4的左止点位置,球壳槽交汇处14被球体凸环3占据,排气阀11在弹簧力的作用下关闭;在球壳环槽7中,滚珠9在前进方向与球体凸环3之间形成了压缩空间,气体被压缩;同时,通过吸气孔,滚珠9后方空间吸气。As shown in Figures 6 and 7, the ball 9 is at the left dead center position of the ball arc groove 4, the intersection 14 of the spherical shell groove is occupied by the spherical convex ring 3, and the exhaust valve 11 is closed under the action of the spring force; In the groove 7, a compression space is formed between the ball 9 and the spherical convex ring 3 in the forward direction, and the gas is compressed; at the same time, through the suction hole, the space behind the ball 9 sucks air.
球体2从图6中位置继续旋转一定角度至图8中位置,此时滚珠9在球体弧槽4的位置接近凸环缺口13;结合图9所示,滚珠9在球壳环槽7中的位置接近球壳槽交汇处14。球壳槽交汇处14被球体凸环3继续占据,排气阀11在压缩气体的压力下(大于弹簧力)打开,滚珠9移动前方排气,后方吸气。The ball 2 continues to rotate at a certain angle from the position in Figure 6 to the position in Figure 8, at this time the position of the ball 9 in the arc groove 4 of the ball is close to the notch 13 of the convex ring; as shown in Figure 9, the ball 9 in the ring groove 7 of the spherical shell The location is close to the spherical shell groove intersection 14. The spherical shell groove intersection 14 is continued to be occupied by the spheroid convex ring 3, and the exhaust valve 11 is opened under the pressure of the compressed gas (greater than the spring force), and the ball 9 moves to exhaust in the front and inhale in the rear.
球体2从图6中位置旋转90°后至图10中位置,此时滚珠9的位置处于球体弧槽4的中间位置,也即处于凸环缺口13的位置;结合图11所示,凸环缺口13到达球壳槽交汇处14,也就是球壳槽交汇处14不再被球体凸环3占据,通道处于开通状态,滚珠9也正好处于球壳6的球壳槽交汇处14,可以通过。此时压缩机排气结束,排气阀11关闭,压缩机既不压缩也不吸气。After the ball 2 rotates 90° from the position in Figure 6 to the position in Figure 10, the position of the ball 9 is at the middle of the arc groove 4 of the ball, that is, at the position of the notch 13 of the convex ring; as shown in Figure 11, the convex ring The notch 13 reaches the intersection 14 of the spherical shell groove, that is, the intersection 14 of the spherical shell groove is no longer occupied by the spherical convex ring 3, the passage is in an open state, and the ball 9 is also just at the intersection 14 of the spherical shell groove of the spherical shell 6, and can pass through . At this moment, the exhaust of the compressor ends, the exhaust valve 11 is closed, and the compressor neither compresses nor sucks air.
球体2从图10中位置继续旋转若干角度后至图12中位置,此时滚珠9的位置处于球体弧槽4偏右一些的位置;结合图13所示,此时球壳槽交汇处14被球体凸环3重新占据,在球壳环槽7中,滚珠9靠近吸气口10,滚珠9移动前方压缩气体,后方开始吸气。The ball 2 continues to rotate several angles from the position in Figure 10 to the position in Figure 12. At this time, the position of the ball 9 is at a position slightly to the right of the arc groove 4 of the ball; The spheroid convex ring 3 occupies again, and in the spherical shell ring groove 7, the ball 9 is close to the suction port 10, and the ball 9 moves the front to compress the gas, and the rear starts to inhale.
球体2从图10中位置旋转90°后至图14中位置,此时滚珠9在球体弧槽4的右止点位置;结合图15所示,此时球壳槽交汇处14被球体凸环3继续占据,排气阀11在弹簧力的作用下关闭;在球壳环槽7中,滚珠9在前进方向与球体凸环3之间形成了压缩空间,气体被压缩;同时,通过吸气孔,滚珠9后方空间吸气。The ball 2 rotates 90° from the position shown in Figure 10 to the position shown in Figure 14. At this time, the ball 9 is at the right dead center of the arc groove 4 of the ball; 3 continues to occupy, the exhaust valve 11 is closed under the action of the spring force; in the spherical shell ring groove 7, the ball 9 forms a compression space between the forward direction and the ball convex ring 3, and the gas is compressed; at the same time, through the suction Hole, ball 9 rear space suction.
如上所述,从图6~图15,展示了球体2在球壳6内旋转180°后,两个滚珠9分别实现一次压缩、吸气、排气过程。在这个过程中,滚珠9在球体弧槽4内从左止点到达右止点,同时在球壳环槽7内旋转180°。由于结构的对称性,球体2继续旋转180°后的结果与前述情形基本相同,只是滚珠9在球体弧槽4内从右止点回到左止点,同时在球壳环槽7内继续旋转180°回到图7所示原点。球体2在球壳6内旋转一周360°后,压缩机实现两次压缩、吸气、排气过程。As mentioned above, from Fig. 6 to Fig. 15, it shows that after the ball 2 rotates 180° in the spherical shell 6, the two balls 9 respectively realize a process of compression, air intake and exhaust. During this process, the ball 9 moves from the left dead center to the right dead center in the arc groove 4 of the ball, and at the same time rotates 180° in the ring groove 7 of the spherical shell. Due to the symmetry of the structure, the result after the sphere 2 continues to rotate 180° is basically the same as the previous situation, except that the ball 9 returns from the right dead center to the left dead center in the arc groove 4 of the ball, and continues to rotate in the ring groove 7 of the spherical shell at the same time 180° back to the origin shown in Figure 7. After the sphere 2 rotates 360° once in the spherical shell 6, the compressor realizes two compression, suction and exhaust processes.
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410489893.0A CN104265630B (en) | 2014-09-23 | 2014-09-23 | A spherical ball compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410489893.0A CN104265630B (en) | 2014-09-23 | 2014-09-23 | A spherical ball compressor |
Publications (2)
Publication Number | Publication Date |
---|---|
CN104265630A CN104265630A (en) | 2015-01-07 |
CN104265630B true CN104265630B (en) | 2016-08-17 |
Family
ID=52157186
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410489893.0A Expired - Fee Related CN104265630B (en) | 2014-09-23 | 2014-09-23 | A spherical ball compressor |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN104265630B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109162762A (en) * | 2018-09-05 | 2019-01-08 | 上海理工大学 | Spherical Ball Expander |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109162779A (en) * | 2018-09-05 | 2019-01-08 | 上海理工大学 | A kind of organic Rankine cycle power generation system |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1898457A (en) * | 2004-04-06 | 2007-01-17 | 帕拉维斯股份公司 | Rotary-piston engine and vehicle comprising an engine of this type |
CN101929463A (en) * | 2010-08-26 | 2010-12-29 | 马丽莉 | Automatical compensation mechanism for sealing clearance of hinges used for spherical compressor |
CN102116294A (en) * | 2011-01-31 | 2011-07-06 | 程涛 | Spherical cylinder for constant torque compressors and gas engines |
CN102822448A (en) * | 2010-03-16 | 2012-12-12 | 亚历山大·弗拉基米罗维奇·迪定 | Volumetric Rotary Mechanism |
-
2014
- 2014-09-23 CN CN201410489893.0A patent/CN104265630B/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1898457A (en) * | 2004-04-06 | 2007-01-17 | 帕拉维斯股份公司 | Rotary-piston engine and vehicle comprising an engine of this type |
CN102822448A (en) * | 2010-03-16 | 2012-12-12 | 亚历山大·弗拉基米罗维奇·迪定 | Volumetric Rotary Mechanism |
CN101929463A (en) * | 2010-08-26 | 2010-12-29 | 马丽莉 | Automatical compensation mechanism for sealing clearance of hinges used for spherical compressor |
CN102116294A (en) * | 2011-01-31 | 2011-07-06 | 程涛 | Spherical cylinder for constant torque compressors and gas engines |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109162762A (en) * | 2018-09-05 | 2019-01-08 | 上海理工大学 | Spherical Ball Expander |
Also Published As
Publication number | Publication date |
---|---|
CN104265630A (en) | 2015-01-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN109209819B (en) | A piston transmission mechanism and a two-dimensional compressor | |
CN103899510B (en) | Super-pressure air compressor | |
WO2017024863A1 (en) | Fluid machinery, heat exchanging apparatus, and operating method for fluid machinery | |
WO2017024864A1 (en) | Fluid machinery, heat exchange device, and method for operating fluid machinery | |
WO2017024868A1 (en) | Fluid machinery, heat exchange device, and method for operating fluid machinery | |
CN201621068U (en) | Novel translation rotary type compressor | |
CN104265630B (en) | A spherical ball compressor | |
CN104285052A (en) | pump or rotary compressor | |
CN105485007B (en) | The rotary compressor of unit two-stage compression | |
CN105201829A (en) | Multi-sliding-vane compressor and sectional compression method | |
CN103821715B (en) | Translation revolving compressor mechanical | |
CN203796562U (en) | Rotating piston type compressor | |
CN105649983A (en) | Air compressor pump | |
CN200971862Y (en) | Synchronous rotary compressor | |
CN103267005B (en) | A kind of back and forth radial compressor | |
CN106762638A (en) | A kind of translation piston compressor | |
CN203201742U (en) | Magnetic force type same-plane multi-cylinder and multistage combined compressor | |
CN201757060U (en) | Rotary compressor | |
CN112983819B (en) | Compression assembly of rotary compressor and compressor | |
WO2020015284A1 (en) | Pump body assembly, fluid machinery and heat exchange device | |
CN101328891B (en) | Dual rotors translation type rotary compressing device | |
CN103591023B (en) | A kind of eccentric block type radial flexible compensating mechanism of rolling piston class fluid machinery | |
CN110966188A (en) | Pump body structure of rotary cylinder piston compressor and rotary cylinder piston compressor | |
CN201420676Y (en) | Double Ring Rotary Compressor Cylinder | |
CN203835721U (en) | Translation rotary type compression machine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160817 Termination date: 20180923 |