WO2023103872A1

WO2023103872A1 - Fluid machinery, heat exchange apparatus, and operation method for fluid machinery

Info

Publication number: WO2023103872A1
Application number: PCT/CN2022/135932
Authority: WO
Inventors: 胡余生; 魏会军; 徐嘉; 杜忠诚; 任丽萍; 李直
Original assignee: 珠海格力电器股份有限公司
Priority date: 2021-12-07
Filing date: 2022-12-01
Publication date: 2023-06-15
Also published as: CN116241470A

Abstract

Fluid machinery, a heat exchange apparatus, and an operation method for fluid machinery. The fluid machinery comprises a crankshaft (10), a cylinder sleeve (20), a crossed groove structure (30) and sliding blocks (40), wherein a first included angle A is formed between two eccentric portions (11) of the crankshaft (10), and the eccentricities of the two eccentric portions (11) are equal; the crankshaft (10) and the cylinder sleeve (20) are eccentrically arranged and have a fixed eccentric distance therebetween; the crossed groove structure (30) is rotationally arranged in the cylinder sleeve (20), the crossed groove structure (30) is provided with two limiting channels (31), which are sequentially arranged in the axial direction of the crankshaft (10), the extension directions of the limiting channels (31) are perpendicular to the axial direction of the crankshaft (10), and a second included angle B is formed between the extension directions of the two limiting channels (31), the first included angle A being twice the second included angle B; and the sliding blocks (40) are provided with through holes (41), there are two sliding blocks (40), the two eccentric portions (11) correspondingly extend into the two through holes (41) of the two sliding blocks (40), and the two sliding blocks (40) are correspondingly arranged in the two limiting channels (31) in a sliding manner and thus form a volume-variable cavity (311).

Description

Fluid machinery, heat exchange equipment and operating method of fluid machinery

Cross References to Related Applications

This disclosure is based on the application with the Chinese application number 202111489298.3 and the filing date is December 7, 2021, and claims its priority. The disclosure content of the Chinese application is hereby incorporated into this disclosure as a whole.

technical field

The present disclosure relates to the technical field of heat exchange systems, and in particular, to a fluid machine, heat exchange equipment, and an operating method of the fluid machine.

Background technique

Fluid machinery includes compressors and expanders, etc.

Taking compressors as an example, according to energy saving and environmental protection and consumers' requirements for air-conditioning comfort, the air-conditioning industry has been pursuing high efficiency and low noise. As the heart of the air conditioner, the compressor has a direct impact on the energy efficiency and noise level of the air conditioner. As the mainstream household air-conditioning compressor, the rolling rotor compressor has been relatively mature after nearly a hundred years of development. Due to the limitation of structural principles, the optimization space is limited. In order to achieve a major breakthrough, it is necessary to innovate from the structural principle.

Therefore, there is a need for a fluid machine such as a compressor and an expander with high energy efficiency and low noise.

Contents of the invention

In order to achieve the above object, according to one aspect of the present disclosure, a fluid machine is provided, including a crankshaft, a cylinder liner, a cross groove structure and a slider, wherein the crankshaft is provided with two eccentric parts along its axial direction, and the two eccentric parts There is a phase difference of the first angle A between them, and the eccentricity of the two eccentric parts is equal; the crankshaft and the cylinder liner are set eccentrically and the eccentric distance is fixed; the cross groove structure is rotatably set in the cylinder liner, and the cross groove structure has two Limiting channels, two limiting channels are arranged in sequence along the axial direction of the crankshaft, the extending direction of the limiting channels is perpendicular to the axial direction of the crankshaft, and there is a phase of the second angle B between the extending directions of the two limiting channels difference, wherein, the first included angle A is twice the second included angle B; the slider has through holes, and there are two sliders, and the two eccentric parts extend into the two through holes of the two sliders correspondingly. The two sliders are correspondingly slidably arranged in the two limiting channels and form a variable volume cavity. The variable volume cavity is located in the sliding direction of the slider. The function makes the cross groove structure and the slider rotate in the cylinder liner.

In some embodiments, the eccentricity of the eccentric part is equal to the assembly eccentricity of the crankshaft and the cylinder liner.

In some embodiments, the shaft part of the crankshaft is integrally formed, and the shaft part has only one axis.

In some embodiments, the shaft part of the crankshaft and the eccentric part are integrally formed; or, the shaft part of the crankshaft is detachably connected to the eccentric part.

In some embodiments, the shaft part of the crankshaft includes a first section and a second section connected axially, the first section and the second section are arranged coaxially, and two eccentric parts are respectively arranged on the first section and the second section. paragraph.

In some embodiments, the first segment is detachably connected to the second segment.

In some embodiments, both ends of the limiting channel penetrate to the outer peripheral surface of the intersecting groove structure.

In some embodiments, the two sliders are arranged concentrically with the two eccentric parts respectively, and the sliders make circular motions around the axis of the crankshaft. There is a first rotation gap between the wall of the through hole and the eccentric parts, and the first rotation gap The range is 0.005mm ~ 0.05mm.

In some embodiments, the intersecting groove structure is arranged coaxially with the cylinder liner, and there is a second rotation gap between the outer peripheral surface of the intersecting groove structure and the inner wall surface of the cylinder liner, and the size of the second rotation gap is 0.005mm-0.1mm.

In some embodiments, the first included angle A is 160°-200°; the second included angle B is 80°-100°.

In some embodiments, the fluid machine further includes a flange, the flange is arranged at the axial end of the cylinder liner, and the crankshaft is arranged concentrically with the flange.

In some embodiments, there is a first assembly gap between the crankshaft and the flange, and the range of the first assembly gap is 0.005mm˜0.05mm.

In some embodiments, the range of the first assembly gap is 0.01-0.03 mm.

In some embodiments, the eccentric portion has an arc surface, and the central angle of the arc surface is greater than or equal to 180 degrees.

In some embodiments, the eccentric portion is cylindrical.

In some embodiments, the proximal end of the eccentric portion is flush with the outer circle of the shaft portion of the crankshaft; or, the proximal end of the eccentric portion protrudes from the outer circle of the shaft portion of the crankshaft; or, the proximal end of the eccentric portion is located on the crankshaft The inner side of the outer circle of the shaft body part.

In some embodiments, the slider includes a plurality of sub-sliders, and the plurality of sub-sliders are spliced to form a through hole.

In some embodiments, the two eccentric portions are arranged at intervals in the axial direction of the crankshaft.

In some embodiments, the intersecting groove structure has a central hole through which the two limiting passages communicate, and the diameter of the central hole is larger than the diameter of the crankshaft shaft body.

In some embodiments, the diameter of the central hole is larger than the diameter of the eccentric portion.

In some embodiments, the projection of the slider on the axial direction of the through hole has two relatively parallel straight line segments and an arc segment connecting ends of the two straight line segments.

In some embodiments, the position-limiting channel has a set of opposite first sliding surfaces that are in sliding contact with the slider, the slider has a second sliding surface that cooperates with the first sliding surfaces, and the slider has a The extrusion surface at the end of the channel serves as the head of the slider, the two second sliding surfaces are connected through the extrusion surface, and the extrusion surface faces the variable volume cavity.

In some embodiments, the extrusion surface is an arc surface, and the distance between the arc center of the arc surface and the center of the through hole is equal to the eccentricity of the eccentric portion.

In some embodiments, the radius of curvature of the arc surface is equal to the radius of the inner circle of the cylinder liner; or, there is a difference between the radius of curvature of the arc surface and the radius of the inner circle of the cylinder liner, and the difference ranges from -0.05mm to 0.025 mm.

In some embodiments, the difference ranges from -0.02 to 0.02mm.

In some embodiments, the projected area S of the extrusion surface in the sliding direction of the slider between _{the slider} and the area S _row of the compression exhaust port of the cylinder liner satisfies: the value of the S _slider /S _row is 8-25.

In some embodiments, the value of S _slider /S _row is 12-18.

In some embodiments, the cylinder liner has a compression intake port and a compression exhaust port. When any slider is in the intake position, the compression intake port is connected to the corresponding variable volume chamber; In the case of the air position, the corresponding variable volume chamber is connected to the compression exhaust port.

In some embodiments, the inner wall of the cylinder liner has an air suction chamber, and the air suction chamber communicates with the compressed air inlet.

In some embodiments, the suction cavity extends a first preset distance around the inner wall surface of the cylinder liner to form an arc-shaped suction cavity.

In some embodiments, there are two suction cavities, the two suction cavities are arranged at intervals along the axial direction of the cylinder liner, the cylinder liner also has a suction communication cavity, both of the two suction cavities communicate with the suction communication cavity, and The compressed air inlet communicates with the suction cavity through the suction communication cavity.

In some embodiments, the suction communication cavity extends a second preset distance along the axial direction of the cylinder liner, and at least one end of the suction communication cavity passes through the axial end surface of the cylinder liner.

In some embodiments, an exhaust cavity is opened on the outer wall of the cylinder liner, and the compressed exhaust port is connected to the exhaust cavity by the inner wall of the cylinder liner. The fluid machine also includes an exhaust valve assembly, which is arranged on the exhaust The cavity is set correspondingly to the compression exhaust port.

In some embodiments, there are two compression exhaust ports, and the two compression exhaust ports are arranged at intervals along the axial direction of the cylinder liner. There are two sets of exhaust valve assemblies, and the two sets of exhaust valve assemblies correspond to two compression exhaust port settings.

In some embodiments, a communication hole is provided on the axial end surface of the cylinder liner, and the communication hole communicates with the exhaust cavity. The fluid machine also includes a flange, and an exhaust passage is arranged on the flange, and the communication hole communicates with the exhaust passage. .

In some embodiments, the exhaust cavity penetrates to the outer wall of the cylinder liner, and the fluid machine further includes an exhaust cover plate, which is connected with the cylinder liner and seals the exhaust cavity.

In some embodiments, the fluid machine is a compressor.

In some embodiments, the cylinder liner has an expansion exhaust port and an expansion intake port. When any slider is in the intake position, the expansion exhaust port is connected to the corresponding variable volume chamber; In the case of the air position, the corresponding variable volume chamber is connected to the expansion air inlet.

In some embodiments, the inner wall of the cylinder liner has an expansion exhaust cavity, and the expansion exhaust cavity communicates with the expansion exhaust port.

In some embodiments, the expansion exhaust cavity extends a first preset distance around the inner wall surface of the cylinder liner to form an arc-shaped expansion exhaust cavity, and the expansion exhaust cavity extends from the expansion exhaust port to the expansion intake The side where the port is located extends, and the extension direction of the expansion exhaust cavity is in the same direction as the rotation direction of the intersecting groove structure.

In some embodiments, there are two expansion exhaust chambers, and the two expansion exhaust chambers are arranged at intervals along the axial direction of the cylinder liner. The communication cavity communicates, and the expansion exhaust port communicates with the expansion exhaust cavity through the expansion exhaust communication cavity.

In some embodiments, the expansion exhaust communication cavity extends a second preset distance along the axial direction of the cylinder liner, and at least one end of the expansion exhaust communication cavity passes through the axial end surface of the cylinder liner.

In some embodiments, the fluid machine is an expander.

According to another aspect of the present disclosure, a heat exchange device is provided, including a fluid machine, and the fluid machine is the above-mentioned fluid machine.

According to another aspect of _the present disclosure, there is provided a method for operating a fluid machine, _{comprising: the crankshaft rotates around the axis O 0} _of the crankshaft; The axis O ₁ of the structure is set eccentrically and the eccentric distance is fixed; the first slider moves in a circle with the axis O ₀ of the crankshaft as the center, and the center O ₃ of the first slider and the axis O ₀ of the crankshaft The distance is equal to the eccentricity of the first eccentric part corresponding to the crankshaft, and the eccentricity is equal to the eccentric distance between the axis O ₀ of the crankshaft and the axis O ₁ of the cross groove structure, and the crankshaft rotates to drive the first slider to do Circular motion, and the first slider interacts with the intersecting groove structure and slides reciprocally in the limiting channel of the intersecting groove structure; the second slider performs circular motion with the axis O ₀ of the crankshaft as the center, and the second The distance between the center O ₄ of the slider and the axis O ₀ of the crankshaft is equal to the eccentricity of the second eccentric part corresponding to the crankshaft, and the eccentricity is equal to the difference between the axis O ₀ of the crankshaft and the axis O ₁ of the cross groove structure. The crankshaft rotates to drive the second slider to make a circular motion, and the second slider interacts with the intersecting groove structure and slides reciprocally in the limiting channel of the intersecting groove structure.

In some embodiments, the operation method adopts the principle of the cross slider mechanism, wherein the two eccentric parts of the crankshaft are respectively used as the first connecting rod L ₁ and the second connecting rod L ₂ , and the two limiting channels of the cross groove structure are respectively used as The lengths of the third link L ₃ and the fourth link L ₄ , and the first link L ₁ and the second link L ₂ are equal.

In some embodiments, there is a first included angle A between the first link _L1 and the second link _L2 , and there is a second included angle B between the third link _L3 and the fourth link _L4 , Wherein, the first included angle A is twice the second included angle B.

In some embodiments, the connecting line between the axis O ₀ of the crankshaft and the axis O ₁ of the intersecting groove structure is the connecting line O ₀ O ₁ , and there is a connection between the first connecting rod L ₁ and the connecting line O ₀ O ₁ The third included angle C, there is a fourth included angle D between the corresponding third connecting rod L ₃ and the connecting line O ₀ O ₁ , wherein the third included angle C is twice the fourth included angle D; the second link There is a fifth included angle E between the rod L ₂ and the connecting line O ₀ O ₁ , and there is a sixth included angle F between the corresponding fourth connecting rod L ₄ and the connecting line O ₀ O ₁ , wherein the fifth included angle E It is twice the sixth included angle F; the sum of the third included angle C and the fifth included angle E is the first included angle A, and the sum of the fourth included angle D and the sixth included angle F is the second included angle B.

In some embodiments, _{the operation method also includes that the rotational angular velocity of the slider relative to the eccentric part is the same as the revolution angular velocity of the slider around the axis O 0} _of the crankshaft; The rotational angular velocity with respect to the eccentric part is the same.

In some embodiments, during the rotation of the crankshaft, the crankshaft rotates 2 times to complete 4 intake and exhaust processes.

Applying the technical solution of the present disclosure, by setting the intersecting groove structure into a structural form with two limiting channels, and correspondingly setting two sliders, the two eccentric parts of the crankshaft correspondingly extend into the two through holes of the two sliders At the same time, the two sliders are correspondingly slidably arranged in the two limiting passages to form a variable volume cavity. Since the first angle A between the two eccentric parts is the first angle A between the extension directions of the two limiting passages Two times the included angle B, so that when one of the two sliders is at the dead point position, that is, the driving torque of the eccentric part corresponding to the slider at the dead point position is 0, and it is at the dead point position The slider at the position cannot continue to rotate, and at this time the driving torque of the other eccentric part of the two eccentric parts driving the corresponding slider is the maximum value, ensuring that the eccentric part with the largest driving torque can normally drive the corresponding slider Rotate, so that the cross groove structure is driven to rotate through the slider, and then the slider at the dead point is driven to continue to rotate through the cross groove structure, realizing the stable operation of the fluid machine, avoiding the dead point position of the movement mechanism, and lifting The motion reliability of fluid machinery is improved.

Description of drawings

The accompanying drawings constituting a part of the present disclosure are used to provide a further understanding of the present disclosure, and the exemplary embodiments and descriptions of the present disclosure are used to explain the present disclosure, and do not constitute improper limitations to the present disclosure. In the attached picture:

Fig. 1 shows a schematic diagram of a mechanism principle of compressor operation according to an optional embodiment of the present disclosure;

Fig. 2 shows a schematic diagram of the principle of operation of the compressor in Fig. 1;

FIG. 3 shows a schematic diagram of the internal structure of a compressor according to Embodiment 1 of the present disclosure;

Fig. 4 shows a schematic structural view of the pump body assembly of the compressor in Fig. 3;

Figure 5 shows a schematic diagram of the exploded structure of the pump body assembly in Figure 4;

Fig. 6 shows the schematic diagram of the assembly structure of crankshaft, intersecting groove structure, slide block in Fig. 5;

Fig. 7 shows the schematic cross-sectional structure diagram of the crankshaft, the intersecting groove structure and the slide block in Fig. 6;

Fig. 8 shows a structural schematic diagram of the shaft body part of the crankshaft in Fig. 6 and the eccentricity of two eccentric parts;

Fig. 9 shows a schematic cross-sectional structural view of the assembly eccentricity of the crankshaft and cylinder liner in Fig. 5;

Fig. 10 shows a schematic structural view of the cylinder liner and the lower flange in Fig. 5 when they are in an exploded state;

Fig. 11 shows a structural schematic view of the eccentricity between the cylinder liner and the lower flange in Fig. 10;

Fig. 12 shows a schematic view of the structure of the slider in Fig. 5 in the axial direction of the through hole;

Figure 13 shows a schematic structural view of the cylinder liner in Figure 10;

Fig. 14 shows a structural schematic diagram of another viewing angle of the cylinder liner in Fig. 13;

Fig. 15 shows a schematic cross-sectional structural view of the cylinder liner in Fig. 14;

Fig. 16 shows a schematic cross-sectional structural view of another viewing angle of the cylinder liner in Fig. 14;

FIG. 17 shows a schematic structural view of the Y-direction viewing angle in FIG. 16;

Fig. 18 shows a schematic cross-sectional structural view of the upper flange and the cylinder liner in Fig. 9, in which the exhaust path of the pump body assembly is shown;

Fig. 19 shows a schematic cross-sectional structural view of the exhaust path of the pump body assembly in Fig. 9;

Fig. 20 shows a schematic structural view of the cylinder liner and the exhaust cover in Fig. 5 when they are in an exploded state;

Fig. 21 shows a schematic diagram of the state structure of the compressor in Fig. 3 at the beginning of suction;

Fig. 22 shows a schematic diagram of the state structure of the compressor in Fig. 3 in the suction process;

Fig. 23 shows a schematic diagram of the state structure of the compressor in Fig. 3 at the end of suction;

Figure 24 shows a schematic view of the state structure of the compressor in Figure 3 when it is compressing gas;

Fig. 25 shows a schematic diagram of the state structure of the compressor in Fig. 3 in the exhaust process;

Fig. 26 shows a schematic diagram of the state structure of the compressor in Fig. 3 at the end of exhaust;

Fig. 27 shows a schematic diagram of the internal structure of a compressor according to Embodiment 2 of the present disclosure;

Fig. 28 shows a schematic structural view of the pump body assembly of the compressor in Fig. 27;

Figure 29 shows a schematic diagram of the exploded structure of the pump body assembly in Figure 28;

Fig. 30 shows a schematic structural diagram of the comparison between the height H1 of the bearing and the height H2 of the cylinder liner in Fig. 28;

Figure 31 shows a schematic cross-sectional structural view of the assembly eccentricity of the crankshaft and cylinder liner in Figure 28;

Figure 32 shows a schematic structural view of the cylinder liner and the lower flange in Figure 29 when they are in an exploded state;

Figure 33 shows a schematic structural view of the eccentricity between the cylinder liner and the lower flange in Figure 32;

Fig. 34 shows a schematic structural view of the intake passage and exhaust passage of the upper flange in Fig. 31;

Fig. 35 shows a schematic structural view of the intake passage and exhaust passage of the lower flange in Fig. 31;

Figure 36 shows a schematic structural view of the upper flange and the cylinder liner in Figure 31 when they are in an assembled state;

Figure 37 shows a schematic structural view of the I-I perspective in Figure 36;

Figure 38 shows a schematic view of the structure of the II-II perspective in Figure 37, in this figure, the compressor is in the suction state;

Figure 39 shows a schematic view of the structure of the II-II perspective in Figure 37, in this figure, the compressor is in a compressed gas state;

Figure 40 shows a schematic view of the structure of the II-II perspective in Figure 37, in this figure, the compressor is in the exhaust state;

Fig. 41 shows a schematic diagram of the internal structure of a compressor according to Embodiment 3 of the present disclosure;

Figure 42 shows a schematic structural view of the pump body assembly of the compressor in Figure 41;

Fig. 43 shows a structural schematic diagram of bearings at both axial ends of the intersecting groove structure of the pump body assembly in Fig. 42;

Fig. 44 shows the cross-slot structure in Fig. 43 and the cross-sectional schematic diagram of the bearings at both ends;

Figure 45 shows a schematic diagram of the exploded structure of the pump body assembly in Figure 42;

Fig. 46 shows a schematic cross-sectional structural view of the air intake path of the cylinder liner in Fig. 45;

Figure 47 shows a schematic structural view of another embodiment of the cylinder liner of the pump body assembly in Figure 41;

Fig. 48 shows a schematic cross-sectional structural view of the cylinder liner in Fig. 47;

Fig. 49 shows a schematic cross-sectional structural view of the air intake path of the cylinder liner in Fig. 48;

Fig. 50 shows a schematic cross-sectional view of the pump body assembly in Fig. 42 from another perspective;

Figure 51 shows a schematic structural view of the upper flange of the pump body assembly in Figure 50;

Figure 52 shows a schematic structural view of the lower flange of the pump body assembly in Figure 50;

Fig. 53 shows a schematic diagram of the internal structure of a compressor according to Embodiment 4 of the present disclosure;

Figure 54 shows a schematic structural view of the pump body assembly of the compressor in Figure 53;

Fig. 55 shows a schematic diagram of the internal structure of a compressor according to Embodiment 5 of the present disclosure;

Figure 56 shows a schematic structural view of the pump body assembly of the compressor in Figure 55;

Fig. 57 shows a schematic diagram of the internal structure of a compressor according to Embodiment 6 of the present disclosure;

Figure 58 shows a schematic structural view of the pump body assembly of the compressor in Figure 57;

Figure 59 shows a schematic cross-sectional structural view of the J-J perspective in Figure 58;

FIG. 60 shows a schematic diagram of a cross-sectional structure from a T-T perspective in FIG. 58;

Figure 61 shows a schematic cross-sectional structural view of the K-K perspective in Figure 58;

Figure 62 shows a schematic diagram of the exploded structure of the pump body assembly in Figure 58;

Fig. 63 shows a schematic cross-sectional structural view of the cylinder liner in Fig. 62;

Fig. 64 shows a structural schematic diagram of another viewing angle of the cylinder liner in Fig. 63;

Fig. 65 shows a schematic cross-sectional structural diagram of the U-U perspective in Fig. 64;

Fig. 66 shows a schematic cross-sectional structural view of the V-V perspective in Fig. 65;

Fig. 67 shows a schematic diagram of the internal structure of a compressor according to Embodiment 7 of the present disclosure;

Fig. 68 shows a schematic cross-sectional structural view of the pump body assembly in Fig. 67;

Fig. 69 shows a schematic diagram of the internal structure of a compressor according to Embodiment 8 of the present disclosure;

Figure 70 shows a schematic structural view of the pump body assembly of the compressor in Figure 69;

Fig. 71 shows a schematic diagram of the internal structure of a compressor according to Embodiment 9 of the present disclosure;

Fig. 72 shows a partial structural schematic view of the pump body assembly of the compressor in Fig. 71;

Figure 73 shows a schematic diagram of the exploded structure of the pump body assembly in Figure 72;

Figure 74 shows a schematic structural view of the upper sub-cylinder liner in Figure 72;

Fig. 75 shows a schematic cross-sectional structural view of the upper sub-cylinder liner in Fig. 74;

Figure 76 shows a schematic structural view of the lower sub-cylinder liner in Figure 72;

Fig. 77 shows a schematic cross-sectional structural view of the lower sub-cylinder liner in Fig. 76;

Figure 78 shows a schematic structural view of the upper flange in Figure 73;

Fig. 79 shows a schematic diagram of the internal structure of a compressor according to Embodiment 10 of the present disclosure;

Fig. 80 shows a partial structural schematic view of the pump body assembly of the compressor in Fig. 79;

Figure 81 shows a schematic diagram of the exploded structure of the pump body assembly in Figure 80;

Fig. 82 shows a schematic structural view of the crankshaft, the intersecting groove structure and the slider in Fig. 81 when they are in an assembled state;

Fig. 83 shows a schematic cross-sectional structural view of the crankshaft, intersecting groove structure and slider in Fig. 82;

Figure 84 shows a schematic diagram of the exploded structure of the pump body assembly with bearings in Figure 80;

Fig. 85 shows a schematic diagram of the internal structure of the compressor according to the eleventh embodiment of the present disclosure;

Figure 86 shows a schematic structural view of the pump body assembly of the compressor in Figure 85;

Figure 87 shows a schematic diagram of the exploded structure of the pump body assembly in Figure 86;

Fig. 88 shows a schematic structural view of the crankshaft, the intersecting groove structure and the slider in Fig. 87 when they are in an assembled state;

Fig. 89 shows a schematic cross-sectional structural view of the crankshaft, the intersecting groove structure and the slide block in Fig. 88;

FIG. 90 shows a schematic structural diagram of the cross-groove structure in FIG. 88;

Figure 91 shows a schematic structural view of the slider in Figure 88;

Figure 92 shows a schematic cross-sectional structural view of the pump body assembly with bearings in Figure 86, in which the bearing is located at one axial end;

Figure 93 shows a schematic structural view of the intersecting groove structure and the bearing in Figure 92 when they are in an assembled state;

Figure 94 shows a schematic cross-sectional structural view of the pump body assembly with bearings in Figure 86, in which the bearings are located at both axial ends;

Figure 95 shows a structural schematic view of the intersecting groove structure and the bearing in Figure 94 when they are in an assembled state;

Figure 96 shows a schematic cross-sectional structural view of the pump body assembly with bearings in Figure 86, in which the bearing is located at the other end in the axial direction;

Fig. 97 shows a schematic structural view of the intersecting groove structure and the bearing in Fig. 96 when they are in an assembled state;

Fig. 98 shows a schematic cross-sectional structural view of the pump body assembly with bearings in Fig. 86, in which the bearings are located on the circumferential outer peripheral side;

Fig. 99 shows a schematic structural view of the cylinder liner, intersecting groove structure and bearing in Fig. 98 when they are in an assembled state;

Figure 100 shows a schematic cross-sectional structural view of the pump body assembly with bearings in Figure 86, in which the bearings are located between the two sub-cylinder sleeves;

Figure 101 shows a structural schematic view of the intersecting groove structure and the bearing in Figure 100 when they are in an assembled state;

Fig. 102 shows a schematic diagram of the intersecting groove structure in Fig. 86 and the cross section of the slider being elliptical;

Fig. 103 shows a schematic structural diagram of the intersecting groove structure and the cross section of the slider in Fig. 86;

Fig. 104 shows a schematic diagram of the structure of the intersecting groove structure in Fig. 86 and the cross-section of the slider in a trapezoidal shape;

Fig. 105 shows a schematic diagram of the structure of the intersecting groove structure and the cross section of the slider in Fig. 86;

Fig. 106 shows a schematic diagram of the internal structure of a compressor according to Embodiment 12 of the present disclosure;

Figure 107 shows a schematic structural view of the pump body assembly of the compressor in Figure 106;

Figure 108 shows a schematic structural view of the intersecting groove structure of the pump body assembly in Figure 107;

Fig. 109 shows a schematic diagram of the internal structure of a compressor according to Embodiment 13 of the present disclosure;

Figure 110 shows a schematic structural view of the pump body assembly of the compressor in Figure 109;

Figure 111 shows a schematic structural view of the intersecting groove structure of the pump body assembly in Figure 109;

Fig. 112 shows a schematic diagram of the internal structure of a compressor according to Embodiment 14 of the present disclosure;

Figure 113 shows a schematic structural view of the pump body assembly of the compressor in Figure 112;

Figure 114 shows a schematic structural view of an exploded pump body assembly in Figure 113;

Figure 115 shows a schematic structural view of the crankshaft, the intersecting groove structure and the slide block in Figure 114 when they are in an assembled state;

Fig. 116 shows a schematic cross-sectional structural view of the crankshaft, the intersecting groove structure and the slide block in Fig. 115;

Fig. 117 shows a schematic structural view of the intersecting groove structure in Fig. 114;

Figure 118 shows a schematic structural view of the slider in Figure 114;

Figure 119 shows a schematic structural view of the intersecting groove structure in Figure 114 and the two limiting plates in an assembled state;

Fig. 120 shows a schematic cross-sectional view of the pump body assembly in Fig. 113 from another perspective, in which the exhaust path of the pump body assembly is shown;

Figure 121 shows a schematic cross-sectional structure diagram of the upper flange, cylinder liner and two limit plates in Figure 120;

Fig. 122 shows a schematic diagram of the structure of the intersecting groove structure in Fig. 113 and the cross section of the slider being elliptical;

Fig. 123 shows a schematic structural diagram of the intersecting groove structure and the cross section of the slider in Fig. 113;

Fig. 124 shows a schematic diagram of the intersecting groove structure in Fig. 113 and the cross-section of the slider in a trapezoidal shape;

Fig. 125 shows a schematic diagram of the structure of the intersecting groove structure and the cross section of the slider in Fig. 113;

Fig. 126 shows a schematic diagram of the internal structure of a compressor according to Embodiment 15 of the present disclosure;

Figure 127 shows a schematic structural view of the pump body assembly of the compressor in Figure 126;

Figure 128 shows a schematic diagram of the exploded structure of the pump body assembly in Figure 127;

Fig. 129 shows a schematic structural view of the crankshaft, the intersecting groove structure and the slider in Fig. 128 when they are in an assembled state;

Fig. 130 shows a schematic cross-sectional structural view of the crankshaft, the intersecting groove structure and the slide block in Fig. 129;

Figure 131 shows a schematic structural view of the intersecting groove structure of the pump body assembly in Figure 128;

Figure 132 shows a schematic structural view of two sliders of the pump body assembly in Figure 128;

Figure 133 shows a schematic cross-sectional structural view of the exhaust path of the pump body assembly in Figure 127;

Fig. 134 shows a schematic cross-sectional structural view of the pump body assembly in Fig. 133 omitting the crankshaft, the intersecting groove structure, the slider and the lower flange;

Fig. 135 shows a schematic cross-sectional structural view of the pump body assembly in Fig. 133 omitting the crankshaft, slider and lower flange;

Figure 136 shows a schematic cross-sectional structural view of the pump body assembly with bearings in Figure 127, in which the bearings are located at both axial ends;

Figure 137 shows a schematic structural view of the intersecting groove structure and the bearing in Figure 137 when they are in an assembled state;

Figure 138 shows a schematic cross-sectional structural view of the pump body assembly with bearings in Figure 127, in which the bearing is located at one axial end;

Figure 139 shows a schematic cross-sectional structural view of the pump body assembly with bearings in Figure 127, in which the bearing is located at the other end in the axial direction;

Figure 140 shows a schematic cross-sectional structural view of the pump body assembly with bearings in Figure 127, in which the bearings are located on the outer circumferential side;

Figure 141 shows a schematic cross-sectional structural view of the cylinder liner, intersecting groove structure and bearing in Figure 140 when they are in an assembled state;

Fig. 142 shows a schematic diagram of the internal structure of a compressor according to Embodiment 16 of the present disclosure;

Fig. 143 shows a partial cross-sectional structural schematic diagram of the pump body assembly of the compressor in Fig. 142;

Figure 144 shows a schematic structural view of the intersecting groove structure of the pump body assembly in Figure 143;

Fig. 145 shows a schematic diagram of the internal structure of a compressor according to Embodiment 17 of the present disclosure;

Figure 146 shows a schematic structural view of the pump body assembly of the compressor in Figure 145;

Figure 147 shows a schematic structural view of the intersecting groove structure of the pump body assembly in Figure 146;

Fig. 148 shows a schematic diagram of the internal structure of a compressor according to Embodiment 18 of the present disclosure;

Figure 149 shows a schematic structural view of the pump body assembly of the compressor in Figure 148;

Figure 150 shows a schematic structural view of the intersecting groove structure of the pump body assembly in Figure 149;

Fig. 151 shows a schematic structural diagram of a cross groove structure and a slider according to an optional embodiment of the present disclosure;

Fig. 152 shows a schematic structural diagram of a cross groove structure and a slider according to an optional embodiment of the present disclosure;

Fig. 153 shows a schematic structural diagram of a cross groove structure and a slider according to an optional embodiment of the present disclosure;

Fig. 154 shows a structural schematic diagram of a cross groove structure and a slider according to an optional embodiment of the present disclosure;

Figure 155 shows a schematic diagram of the mechanism principle of the operation of the compressor in the technology known to the inventor;

Figure 156 shows a schematic diagram of the mechanism principle of the improved compressor operation in the technology known to the inventor;

Fig. 157 shows a schematic diagram of the operating mechanism of the compressor in Fig. 156. In this figure, the force arm of the drive shaft driving the slider to rotate is shown;

Fig. 158 shows a schematic diagram of the operating mechanism of the compressor in Fig. 156, in which the center of the limiting groove structure coincides with the center of the eccentric part.

Wherein, the above-mentioned accompanying drawings include the following reference signs:

10. Crankshaft; 11. Eccentric part; 12. Shaft part;

20. Cylinder liner; 21. Compression air inlet; 22. Compression exhaust port; 23. Suction cavity; 24. Suction connection cavity; 25. Exhaust cavity; 26. Communication hole; 27. Sub cylinder liner; 271 , the first radial suction hole; 272, the diversion hole; 273, the suction transition hole; 274, the second radial suction hole; 275, the first exhaust communication port; 276, the exhaust drainage hole; 277, the first Two exhaust connecting ports; 28, circumferential convex ring; 281, elongated hole; 210, annular sinking groove; 220, radial suction hole; 230, axial distribution hole;

30. Cross groove structure; 31. Limiting channel; 311. Variable volume cavity; 32. Center hole; 36. Supporting convex ring; 361. Thrust surface; 37. Supporting ring surface; 38. Opening hole; 39. Channel;

40. slider; 41. through hole; 42. extrusion surface;

50, flange; 51, exhaust channel; 52, upper flange; 53, lower flange; 54, air intake channel; 541, first air intake channel section; 542, second air intake channel section; 55, row Air groove; 551, exhaust communication port; 56, suction channel; 57, flange exhaust port;

60. Exhaust valve assembly; 61. Exhaust valve plate; 62. Valve plate baffle;

70. Exhaust cover;

80. Dispenser component; 81. Housing assembly; 82. Motor assembly; 83. Pump body assembly; 84. Upper cover assembly; 85. Lower cover assembly;

90. Fasteners;

100, end cover; 110, limit plate; 1101, via hole; 1102, avoidance channel;

200, bearing; 201, suction through hole; 202, exhaust through hole.

Detailed ways

The following will clearly and completely describe the technical solutions in the embodiments of the present disclosure with reference to the accompanying drawings in the embodiments of the present disclosure. Obviously, the described embodiments are only some of the embodiments of the present disclosure, not all of them. The following description of at least one exemplary embodiment is merely illustrative in nature and in no way intended as any limitation of the disclosure, its application or uses. Based on the embodiments in the present disclosure, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present disclosure.

As shown in Figure 155, a principle of compressor operating mechanism is proposed based on the cross slider mechanism, that is, with point _O1 as the center of the cylinder, point _O2 as the center of the drive shaft, and point _O3 as the center of the slider, the cylinder and drive The shaft is set eccentrically, wherein the slider center O ₃ makes a circular motion on a circle with a diameter of O ₁ O ₂ .

In the above operating mechanism principle, the cylinder center O ₁ and the drive shaft center O ₂ are used as the two rotation centers of the motion mechanism, and at the same time, the midpoint O ₀ of the line segment O ₁ O ₂ is used as the virtual center of the slider center O ₃ , so that the slider While the block reciprocates relative to the cylinder, the slider also reciprocates relative to the drive shaft.

Since the midpoint O ₀ of the line segment O ₁ O ₂ is the virtual center, it is impossible to set up a balance system, resulting in the deterioration of the high-frequency vibration characteristics of the compressor. Based on the principle of the above-mentioned operating mechanism, as shown in Figure 156, a The motion mechanism with O ₀ as the drive shaft center, that is, the cylinder center O ₁ and the drive shaft center O ₀ as the two rotation centers of the motion mechanism, the drive shaft has an eccentric portion, the slider and the eccentric portion are coaxially arranged, and the drive shaft and The assembly eccentricity of the cylinder is equal to the eccentricity of the eccentric part, so that the slider center _O3 makes a circular motion with the drive shaft center _O0 as the center and _O1O0 as the radius _.

Correspondingly, a set of operating mechanisms is proposed, including a cylinder, a limit groove structure, a slider and a drive shaft, wherein the limit groove structure is rotatably arranged in the cylinder, and the cylinder and the limit groove structure are coaxially arranged, that is, The center _O1 of the cylinder is also the center of the limit groove structure, the slider reciprocates relative to the limit groove structure, the slider is coaxially assembled with the eccentric portion of the drive shaft, and the slider moves circularly around the shaft part of the drive shaft, specifically The movement process is: the drive shaft rotates, driving the slider to revolve around the center of the shaft part of the drive shaft, the slider rotates relative to the eccentric part at the same time, and the slider reciprocates in the limit groove of the limit groove structure, and pushes the limit Bitslot structure rotation.

However, as shown in Figure 157, the length of the force arm L that the drive shaft drives the slider to rotate is L=2e×cosθ×cosθ, where e is the eccentricity of the eccentric part, and θ is the line connecting O ₁ O ₀ and the slider The angle between the sliding directions in the limit slot.

As shown in Figure 158, when the center _O1 of the cylinder (that is, the center of the limit groove structure) coincides with the center of the eccentric part, the resultant force of the driving force of the drive shaft passes through the center of the limit groove structure, that is, it is applied on the limit groove structure. The torque on the groove structure is zero, and the limit groove structure cannot rotate. At this time, the motion mechanism is at the dead point and cannot drive the slider to rotate.

Based on this, the present disclosure proposes a mechanism principle of a cross groove structure with two limiting channels and double sliders, and builds a fluid machine such as a compressor and an expander based on this principle, and the fluid machine has high energy efficiency , low noise, the following will take the compressor as an example to introduce the compressor based on the cross-groove structure with two limiting channels and double sliders.

In order to improve the problems of low energy efficiency and high noise of fluid machines such as compressors and expanders in the prior art, the present disclosure provides a fluid machine, a heat exchange device and a method for operating a fluid machine, wherein the heat exchange device The following fluid machines are included, and the fluid machines are operated by the following operating methods.

The fluid machine in the present disclosure includes a crankshaft 10, a cylinder liner 20, a cross groove structure 30 and a slider 40, wherein the crankshaft 10 is provided with two eccentric parts 11 along its axial direction, and a first clip is provided between the two eccentric parts 11. The phase difference of the angle A, the eccentricity of the two eccentric parts 11 are equal; the crankshaft 10 and the cylinder liner 20 are set eccentrically and the eccentric distance is fixed; the cross groove structure 30 is rotatably arranged in the cylinder liner 20, and the cross groove structure 30 has two Limiting channels 31, two limiting channels 31 are arranged in sequence along the axial direction of the crankshaft 10, the extending direction of the limiting channels 31 is perpendicular to the axial direction of the crankshaft 10, and there is a second gap between the extending directions of the two limiting channels 31 The phase difference between the two included angles B, wherein the first included angle A is twice the second included angle B; the slider 40 has a through hole 41, and there are two sliders 40, and the two eccentric parts 11 extend into two corresponding In the two through holes 41 of the slider 40, the two sliders 40 are correspondingly slidably arranged in the two limiting passages 31 and form a variable volume cavity 311. The variable volume cavity 311 is located in the sliding direction of the slider 40, and the crankshaft 10 rotates. The sliding block 40 is driven to reciprocate and slide in the limiting channel 31 while interacting with the intersecting groove structure 30 , so that the intersecting groove structure 30 and the sliding block 40 rotate in the cylinder sleeve 20 .

By setting the intersecting groove structure 30 into a structural form with two limiting channels 31 and correspondingly setting up two sliders 40, the two eccentric parts 11 of the crankshaft extend into the two through holes 41 of the two sliders 40 correspondingly. , at the same time, the two sliders 40 are correspondingly slidably arranged in the two limiting passages 31 to form a variable volume cavity 311, since the first angle A between the two eccentric parts 11 is the extension direction of the two limiting passages 31 Twice the second included angle B between them, so that when one of the two sliders 40 is at the dead point position, that is, the driving torque of the eccentric portion 11 corresponding to the slider 40 at the dead point position is 0, the slider 40 at the dead point cannot continue to rotate, and at this time, the driving torque of the other eccentric part 11 driving the corresponding slider 40 in the two eccentric parts 11 is the maximum value, ensuring the maximum driving torque. The eccentric portion 11 of the moment can normally drive the corresponding slider 40 to rotate, thereby driving the cross groove structure 30 to rotate through the slider 40, and then driving the slider 40 at the dead point to continue to rotate through the cross groove structure 30, realizing The stable operation of the fluid machinery avoids the dead point position of the motion mechanism, improves the movement reliability of the fluid machinery, and ensures the working reliability of the heat exchange equipment.

In addition, since the fluid machine provided by the present disclosure can run stably, that is, it ensures high energy efficiency and low noise of the fluid machine such as a compressor and an expander, thereby ensuring the working reliability of the heat exchange equipment.

It should be noted that, in the present disclosure, neither the first included angle A nor the second included angle B is zero.

As shown in Figures 1 and 2, when the above-mentioned fluid machine is in operation, the crankshaft 10 rotates around the axis O ₀ of the crankshaft 10; the intersecting groove structure 30 revolves around the axis O ₀ of the crankshaft 10, and the axis O ₀ Set eccentrically with the axis O ₁ of the intersecting groove structure 30 and the eccentric distance is fixed; the first slider 40 makes a circular motion with the axis O ₀ of the crankshaft 10 as the center of a circle, and the center O ₃ of the first slider 40 is aligned with the crankshaft The distance between the axis O0 of ₁₀ is equal to the eccentricity of the first eccentric part 11 corresponding to the crankshaft 10, and the eccentricity is equal to the eccentricity between the axis O0 of the crankshaft ₁₀ and the axis O1 of the intersecting groove structure ₃₀ distance, the crankshaft 10 rotates to drive the first slider 40 to make a circular motion, and the first slider 40 interacts with the intersecting groove structure 30 and slides reciprocally in the limiting channel 31 of the intersecting groove structure 30; The block 40 moves in a circle with the axis O0 of the crankshaft ₁₀ as the center, and the distance between the center _O4 of the second slider 40 and the axis _O0 of the crankshaft 10 is equal to the second eccentric part 11 corresponding to the crankshaft 10 The amount of eccentricity, and the amount of eccentricity is equal to the eccentric distance between the axis O ₀ of the crankshaft 10 and the axis O ₁ of the cross groove structure 30, the crankshaft 10 rotates to drive the second slider 40 to do circular motion, and the second The slider 40 interacts with the intersecting groove structure 30 and slides reciprocally in the limiting channel 31 of the intersecting groove structure 30 .

The fluid machine operated in the above method constitutes an Oldham slider mechanism, and the operating method adopts the principle of the Oldham slider mechanism, wherein the two eccentric parts 11 of the crankshaft 10 serve as the first connecting rod _L1 and the second connecting rod _L2 respectively. , the two limiting channels 31 of the intersecting groove structure 30 are respectively used as the third link L ₃ and the fourth link L ₄ , and the lengths of the first link L ₁ and the second link L ₂ are equal (please refer to FIG. 1 ).

As shown in Figure 1, there is a first included angle A between the first link _L1 and the second link _L2 , and there is a second included angle B between the third link _L3 and the fourth link _L4 , Wherein, the first included angle A is twice the second included angle B.

As shown in Figure 2, the line connecting the axis O ₀ of the crankshaft 10 and the axis O ₁ of the intersecting groove structure 30 is the line O ₀ O ₁ , and the line between the first connecting rod L ₁ and the line O ₀ O ₁ There is a third included angle C between them, and there is a fourth included angle D between the corresponding third link L ₃ and the connecting line O ₀ O ₁ , wherein the third included angle C is twice the fourth included angle D; There is a fifth included angle E between the second connecting rod L ₂ and the connecting line O ₀ O ₁ , and there is a sixth included angle F between the corresponding fourth connecting rod L ₄ and the connecting line O ₀ O ₁ , wherein the fifth included angle The angle E is twice the sixth angle F; the sum of the third angle C and the fifth angle E is the first angle A, and the sum of the fourth angle D and the sixth angle F is the second angle b.

In some embodiments, the operation method further includes that the rotational angular velocity of the slider 40 relative to the eccentric portion 11 is the same as the revolution angular velocity of the slider 40 around the axis O ₀ of the crankshaft ₁₀ ; The revolution angular velocity is the same as the rotation angular velocity of the slider 40 relative to the eccentric portion 11 .

Specifically, the axis _O0 of the crankshaft 10 corresponds to the rotation center of the first connecting rod _L1 and the second connecting rod _L2 , and the axis O1 of the intersecting groove structure ₃₀ corresponds to the third connecting rod L3 and the fourth connecting rod _L3 . The rotation center of the connecting rod _L4 ; the two eccentric parts 11 of the crankshaft 10 are respectively used as the first connecting rod _L1 and the second connecting rod _L2 , and the two limiting channels 31 of the intersecting groove structure 30 are respectively used as the third connecting rod L ₃ and the fourth connecting rod L ₄ , and the lengths of the first connecting rod L ₁ and the second connecting rod L ₂ are equal, so that when the crankshaft 10 rotates, the eccentric part 11 on the crankshaft 10 drives the corresponding slider 40 around the crankshaft The axis O0 of ₁₀ revolves, and the slider 40 can rotate relative to the eccentric part 11 at the same time, and the relative rotation speed of the two is the same, because the first slider 40 and the second slider 40 are respectively in two corresponding limits Reciprocating movement in the position channel 31, and drives the intersecting groove structure 30 to make a circular motion, limited by the two limiting channels 31 of the intersecting groove structure 30, the moving direction of the two sliders 40 always has the phase of the second included angle B difference, when one of the two sliders 40 is at the dead center position, the eccentric portion 11 for driving the other of the two sliders 40 has the largest driving torque, and the eccentric portion 11 with the largest driving torque can The corresponding slider 40 is normally driven to rotate, so that the cross groove structure 30 is driven to rotate by the slider 40, and then the slider 40 at the dead point is driven by the cross groove structure 30 to continue to rotate, realizing the stable operation of the fluid machine. The dead point position of the motion mechanism is avoided, and the motion reliability of the fluid machinery is improved, thereby ensuring the working reliability of the heat exchange equipment.

It should be noted that, in the present disclosure, the maximum moment arm of the driving torque of the eccentric portion 11 is 2e.

Under this movement method, the running track of the slider 40 is a circle, and the circle takes the axis O ₀ of the crankshaft 10 as the center and the connecting line O ₀ O ₁ as the radius.

It should be noted that, in the present disclosure, during the rotation of the crankshaft 10 , the crankshaft 10 rotates 2 times to complete 4 intake and exhaust processes.

Eighteen optional implementations will be given below to introduce the structure of the fluid machine in detail, so as to better explain the operation method of the fluid machine through structural features.

Embodiment one

As shown in Fig. 3 to Fig. 26, the fluid machine also includes a flange 50, the flange 50 is arranged on the axial end of the cylinder liner 20, the crankshaft 10 is concentrically arranged with the flange 50, and the cross groove structure 30 is concentric with the cylinder liner 20. shaft setting, the assembly eccentricity of the crankshaft 10 and the intersecting groove structure 30 is determined by the relative positional relationship between the flange 50 and the cylinder liner 20, wherein the flange 50 is fixed on the cylinder liner 20 by a fastener 90, and the axis center of the flange 50 The relative position of the axis of the inner ring of the cylinder liner 20 is controlled by the alignment of the flange 50, and the relative position of the axis of the flange 50 and the axis of the inner ring of the cylinder liner 20 determines the axis of the crankshaft 10 and the cross groove structure 30 The relative position of the shaft center, the essence of adjusting the center through the flange 50 is to make the eccentricity of the eccentric part 11 equal to the assembly eccentricity of the crankshaft 10 and the cylinder liner 20 .

Specifically, as shown in FIG. 8, the eccentricity of the two eccentric parts 11 is equal to e, and as shown in FIG. 20 are coaxially arranged, the assembly eccentricity between the crankshaft 10 and the intersecting groove structure 30 is the assembly eccentricity between the crankshaft 10 and the cylinder liner 20), and the flange 50 includes an upper flange 52 and a lower flange 53, as shown in Figure 11 As shown, the distance between the axis of the inner ring of the cylinder liner 20 and the axis of the inner ring of the lower flange 53 is e, which is equal to the eccentricity of the eccentric portion 11 .

In some embodiments, there is a first assembly gap between the crankshaft 10 and the flange 50, and the range of the first assembly gap is 0.005mm˜0.05mm.

In some embodiments, the range of the first assembly gap is 0.01-0.03 mm.

In some embodiments, the two sliders 40 are arranged concentrically with the two eccentric parts 11 respectively, the sliders 40 make a circular motion around the axis of the crankshaft 10, and there is a first rotation between the wall of the through hole 41 and the eccentric parts 11. The gap, the range of the first rotation gap is 0.005mm-0.05mm.

In some embodiments, there is a second rotation gap between the outer peripheral surface of the intersecting groove structure 30 and the inner wall surface of the cylinder liner 20 , and the size of the second rotation gap is 0.005 mm˜0.1 mm.

As shown in FIGS. 4 to 9 , the shaft part 12 of the crankshaft 10 is integrally formed, and the shaft part 12 has only one axis. In this way, the one-time molding of the shaft part 12 is facilitated, thereby reducing the difficulty of manufacturing the shaft part 12 .

It should be noted that, in an unillustrated embodiment of the present disclosure, the shaft portion 12 of the crankshaft 10 includes a first section and a second section connected along its axial direction, the first section and the second section are arranged coaxially, Two eccentric portions 11 are respectively arranged on the first segment and the second segment.

In some embodiments, the first segment is detachably connected to the second segment. In this way, ease of assembly and disassembly of the crankshaft 10 is ensured.

As shown in FIGS. 4 to 9 , the shaft portion 12 of the crankshaft 10 and the eccentric portion 11 are integrally formed. In this way, one-shot forming of the crankshaft 10 is facilitated, thereby reducing the difficulty of manufacturing the crankshaft 10 .

It should be noted that, in an unillustrated embodiment of the present disclosure, the shaft portion 12 of the crankshaft 10 is detachably connected to the eccentric portion 11 . In this way, the installation and removal of the eccentric portion 11 is facilitated.

As shown in FIGS. 5 to 7 , both ends of the limiting channel 31 penetrate to the outer peripheral surface of the intersecting groove structure 30 . In this way, it is beneficial to reduce the manufacturing difficulty of the intersecting groove structure 30 .

It should be noted that, in the present disclosure, the first included angle A is 160°-200°; the second included angle B is 80°-100°. In this way, it only needs to satisfy the relationship that the first included angle A is twice the second included angle B.

In some embodiments, the first included angle A is 160 degrees, and the second included angle B is 80 degrees.

In some embodiments, the first included angle A is 165 degrees, and the second included angle B is 82.5 degrees.

In some embodiments, the first included angle A is 170 degrees, and the second included angle B is 85 degrees.

In some embodiments, the first included angle A is 175 degrees, and the second included angle B is 87.5 degrees.

In some embodiments, the first included angle A is 180 degrees, and the second included angle B is 90 degrees.

In some embodiments, the first included angle A is 185 degrees, and the second included angle B is 92.5 degrees.

In some embodiments, the first included angle A is 190 degrees, and the second included angle B is 95 degrees.

In some embodiments, the first included angle A is 195 degrees, and the second included angle B is 97.5 degrees.

It should be noted that, in the present disclosure, the eccentric portion 11 has an arc surface, and the central angle of the arc surface is greater than or equal to 180 degrees. In this way, it is ensured that the arc surface of the eccentric portion 11 can exert an effective driving force on the slider 40 , thereby ensuring the reliability of the movement of the slider 40 .

As shown in FIGS. 4 to 9 , the eccentric portion 11 is cylindrical.

In some embodiments, the proximal end of the eccentric portion 11 is flush with the outer circle of the shaft portion 12 of the crankshaft 10 .

In some embodiments, the proximal end of the eccentric portion 11 protrudes beyond the outer circle of the shaft portion 12 of the crankshaft 10 .

In some embodiments, the proximal end of the eccentric portion 11 is located inside the outer circle of the shaft portion 12 of the crankshaft 10 .

It should be noted that, in an unillustrated embodiment of the present disclosure, the slider 40 includes a plurality of sub-sliders, and the plurality of sub-sliders are assembled to form a through hole 41 .

As shown in FIGS. 4 to 9 , two eccentric portions 11 are arranged at intervals in the axial direction of the crankshaft 10 . In this way, during the process of assembling the crankshaft 10 , the cylinder liner 20 and the two sliders 40 , ensuring the distance between the two eccentric parts 11 can provide an assembly space for the cylinder liner 20 to ensure the convenience of assembly.

As shown in FIG. 5 , the intersecting groove structure 30 has a central hole 32 through which the two limiting passages 31 communicate. The diameter of the central hole 32 is larger than the diameter of the shaft portion 12 of the crankshaft 10 . In this way, it is ensured that the crankshaft 10 can pass through the central hole 32 smoothly.

In some embodiments, the diameter of the central hole 32 is larger than the diameter of the eccentric portion 11 . In this way, it is ensured that the eccentric portion 11 of the crankshaft 10 can smoothly pass through the central hole 32 .

As shown in FIG. 12 , the axial projection of the slider 40 on the through hole 41 has two relatively parallel straight line segments and an arc segment connecting ends of the two straight line segments. The limiting channel 31 has a set of first sliding surfaces oppositely disposed in sliding contact with the slider 40 , the sliding block 40 has a second sliding surface cooperating with the first sliding surfaces, and the sliding block 40 has a The extrusion surface 42 at the end of the slider 40 is used as the head of the slider 40, and the two second sliding surfaces are connected by the extrusion surface 42, and the extrusion surface 42 faces the variable volume chamber 311. In this way, the projection of the second sliding surface of the slider 40 in the axial direction of the through hole 41 is a straight line segment, and at the same time, the projection of the extrusion surface 42 of the slider 40 in the axial direction of the through hole 41 is an arc segment.

Specifically, the extrusion surface 42 is an arc surface, and the distance between the arc center of the arc surface and the center of the through hole 41 is equal to the eccentricity of the eccentric portion 11 . In Fig. 12, the center of the through hole 41 of the slider 40 is the O _slider , and the distance between the arc centers of the two arc surfaces and the center of the through hole 41 is e, that is, the eccentricity of the eccentric portion 11, as shown in Fig. 12 The dotted line of X indicates the circle where the arc centers of the two arc surfaces are located.

In some embodiments, the radius of curvature of the arc surface is equal to the radius of the inner circle of the cylinder liner 20 .

In some embodiments, there is a difference between the radius of curvature of the arc surface and the radius of the inner circle of the cylinder liner 20 , and the range of the difference is -0.05mm˜0.025mm.

In some embodiments, the difference ranges from -0.02 to 0.02 mm.

It should be noted that, in the present disclosure, the projected area S of the extrusion surface 42 in the sliding direction of the slider 40 between _{the slider} and the _area S of the compression exhaust port 22 of the cylinder liner 20 satisfies: S _slider /S _{The row} value is 8-25.

In some embodiments, the value of S _slider /S _row is 12-18.

It should be noted that the fluid machine shown in this embodiment is a compressor. As shown in FIG. The lower cover assembly 85, wherein the liquid separator part 80 is arranged on the outside of the housing assembly 81, the upper cover assembly 84 is assembled on the upper end of the housing assembly 81, the lower cover assembly 85 is assembled on the lower end of the housing assembly 81, and the motor assembly 82 Both the motor assembly 82 and the pump body assembly 83 are located inside the housing assembly 81 , wherein the motor assembly 82 is located above the pump body assembly 83 , or the motor assembly 82 is located below the pump body assembly 83 . The pump body assembly 83 of the compressor includes the crankshaft 10 , the cylinder liner 20 , the intersecting groove structure 30 , the slider 40 , the upper flange 52 and the lower flange 53 .

In some embodiments, the above components are connected by means of welding, shrink fitting, or cold pressing.

The assembly process of the entire pump body assembly 83 is as follows: the lower flange 53 is fixed on the cylinder liner 20, the two sliders 40 are respectively placed in the corresponding two limiting passages 31, and the two eccentric parts 11 of the crankshaft 10 respectively extend into the In the two through holes 41 of the corresponding two sliders 40, the assembled crankshaft 10, the cross groove structure 30 and the two sliders 40 are placed in the cylinder liner 20, and one end of the crankshaft 10 is installed on the lower flange 53 , the other end of the crankshaft 10 is set through the upper flange 52 , see FIG. 4 and FIG. 5 for details.

It should be noted that, in this embodiment, the closed space surrounded by the slider 40, the limiting channel 31, the cylinder liner 20 and the upper flange 52 (or the lower flange 53) is the variable volume chamber 311, and the pump body assembly 83 has four variable volume chambers 311 in total. During the rotation of the crankshaft 10, the crankshaft 10 rotates 2 revolutions, and a single variable volume chamber 311 completes one intake and exhaust process. For the compressor, the crankshaft 10 rotates 2 revolutions, totaling Complete 4 suction and exhaust processes.

As shown in Figures 21 to 26, the sliding block 40 rotates relative to the cylinder liner 20 during the reciprocating movement in the limiting channel 31. In Figures 21 to 23, the sliding block 40 is clockwise from 0° to 180° During the rotation process, the variable volume chamber 311 increases. During the process of increasing the variable volume chamber 311, the variable volume chamber 311 communicates with the suction chamber 23 of the cylinder liner 20. When the slider 40 rotates to 180 degrees, the variable volume chamber The volume of 311 reaches the maximum value, and at this time, the variable volume chamber 311 is separated from the suction chamber 23, thereby completing the suction operation. In Fig. 24 to Fig. 26, the slider 40 continues to rotate clockwise from 180° to 360° During the process, the variable volume chamber 311 decreases, and the slider 40 compresses the gas in the variable volume chamber 311. When the slider 40 rotates until the variable volume chamber 311 communicates with the compression exhaust port 22, and when the variable volume chamber 311 When the gas inside reaches the exhaust pressure, the exhaust valve plate 61 of the exhaust valve assembly 60 opens, and the exhaust operation starts until the compression ends and enters the next cycle.

As shown in Figures 21 to 26, the point marked with M is used as the reference point for the relative movement of the slider 40 and the crankshaft 10, and Figure 22 shows the process of the slider 40 rotating clockwise from 0° to 180°, the rotation of the slider 40 The angle is θ1, and the corresponding rotation angle of the crankshaft 10 is 2θ1. Fig. 24 shows that the slider 40 continues to rotate clockwise from 180° to 360°, and the rotation angle of the slider 40 is 180°+θ2. The crankshaft 10 rotates at an angle of 360°+2θ2. Figure 25 shows that the slider 40 continues to rotate clockwise from 180° to 360°, and the variable volume cavity 311 communicates with the compression exhaust port 22, and the slider 40 rotates The angle is 180°+θ3, and the corresponding rotation angle of the crankshaft 10 is 360°+2θ3, that is, the slider 40 rotates once, and the corresponding crankshaft 10 rotates twice, wherein, θ1<θ2<θ3.

Specifically, as shown in Fig. 10, Fig. 13 to Fig. 26, the cylinder liner 20 has a compression intake port 21 and a compression exhaust port 22. When any slider 40 is at the intake position, the compression intake port 21 and the The corresponding variable volume cavity 311 is in conduction; when any slider 40 is in the exhaust position, the corresponding variable volume cavity 311 is in conduction with the compression exhaust port 22 .

As shown in FIGS. 10 to 16 and 20 to 26 , the inner wall surface of the cylinder liner 20 has an air suction chamber 23 , and the air suction chamber 23 communicates with the compressed air inlet 21 . In this way, it is ensured that the suction chamber 23 can store a large amount of gas, so that the variable volume chamber 311 can be fully suctioned, so that the compressor can take in enough air, and when the suction is insufficient, the stored gas can be supplied in time Give the variable volume chamber 311 to ensure the compression efficiency of the compressor.

In some embodiments, the suction cavity 23 is a cavity formed by radially hollowing out the inner wall of the cylinder liner 20 , and there may be one suction cavity 23 or two upper and lower ones.

Specifically, the suction cavity 23 extends a first preset distance around the inner wall surface of the cylinder liner 20 to form an arc-shaped suction cavity 23 . In this way, it is ensured that the volume of the suction chamber 23 is large enough to store a large amount of gas.

As shown in Figure 10, Figure 13 and Figure 15, there are two suction chambers 23, and the two suction chambers 23 are arranged at intervals along the axial direction of the cylinder liner 20. The cylinder liner 20 also has a suction communication chamber 24, and the two suction chambers The air cavities 23 communicate with the suction communication cavity 24 , and the compressed air inlet 21 communicates with the suction cavity 23 through the suction communication cavity 24 . In this way, it is beneficial to increase the volume of the suction cavity 23, thereby reducing the suction pressure pulsation.

As shown in FIG. 13 to FIG. 15 , the suction communication cavity 24 extends a second preset distance along the axial direction of the cylinder liner 20 , and at least one end of the suction communication cavity 24 passes through the axial end surface of the cylinder liner 20 . In this way, it is convenient to open the suction communication cavity 24 from the end surface of the cylinder liner 20 , ensuring the convenience of processing the suction communication cavity 24 .

As shown in Fig. 10, Fig. 13 to Fig. 26, an exhaust cavity 25 is opened on the outer wall of the cylinder liner 20, and the compression exhaust port 22 is connected to the exhaust cavity 25 by the inner wall of the cylinder liner 20. The fluid machine also includes an exhaust The valve assembly 60 , the exhaust valve assembly 60 is arranged in the exhaust cavity 25 and is arranged corresponding to the compression exhaust port 22 . In this way, the exhaust cavity 25 is used to accommodate the exhaust valve assembly 60 , which effectively reduces the occupied space of the exhaust valve assembly 60 , makes the components reasonably arranged, and improves the space utilization rate of the cylinder liner 20 .

As shown in Figures 15 to 19, there are two compression exhaust ports 22, and the two compression exhaust ports 22 are arranged at intervals along the axial direction of the cylinder liner 20, and the exhaust valve assembly 60 is divided into two groups, and the two sets of exhaust valve assemblies 60 are set corresponding to the two compression exhaust ports 22 respectively. In this way, since the two compression exhaust ports 22 are respectively provided with two sets of exhaust valve assemblies 60, a large amount of gas leakage in the variable volume chamber 311 is effectively avoided, and the compression efficiency of the variable volume chamber 311 is ensured.

As shown in Figure 16, the exhaust valve assembly 60 is connected to the cylinder liner 20 through a fastener 90, the exhaust valve assembly 60 includes an exhaust valve plate 61 and a valve plate baffle 62, and the exhaust valve plate 61 is arranged in the exhaust cavity 25 and cover the corresponding compression exhaust port 22, the valve plate baffle 62 is overlapped on the exhaust valve plate 61. In this way, the setting of the valve plate baffle 62 effectively prevents the excessive opening of the exhaust valve plate 61 , thereby ensuring the exhaust performance of the cylinder liner 20 .

In some embodiments, fasteners 90 are screws.

As shown in Figure 10, Figure 13, Figure 18 to Figure 20, a communication hole 26 is also provided on the axial end surface of the cylinder liner 20, and the communication hole 26 communicates with the exhaust chamber 25, and the fluid machine also includes a flange 50, the flange An exhaust channel 51 is provided on the 50 , and the communication hole 26 communicates with the exhaust channel 51 . In this way, the exhaust reliability of the cylinder liner 20 is ensured.

As shown in FIG. 20 , the exhaust cavity 25 penetrates to the outer wall of the cylinder liner 20 , and the fluid machine further includes an exhaust cover 70 , which is connected to the cylinder liner 20 and seals the exhaust cavity 25 . In this way, the exhaust cover plate 70 plays a role of isolating the variable volume chamber 311 from the external space of the pump body assembly 83 .

As shown in Figure 18 and Figure 19, when the variable volume cavity 311 is connected with the compression exhaust port 22, when the pressure of the variable volume cavity 311 reaches the exhaust pressure, the exhaust valve plate 61 opens, and the compressed gas passes through the compression exhaust port 22 enters the exhaust cavity 25, and passes through the communication hole 26 on the cylinder liner 20, then is discharged through the exhaust passage 51 and enters the external space of the pump body assembly 83 (that is, the cavity of the compressor), thereby completing the exhaust process .

In some embodiments, exhaust cover plate 70 is secured to cylinder liner 20 by fasteners 90 .

In some embodiments, fasteners 90 are screws.

In some embodiments, the outer contour of the exhaust cover 70 matches the outer contour of the exhaust cavity 25 .

The following is a detailed introduction to the operation of the compressor:

As shown in Figure 3, the motor assembly 82 drives the crankshaft 10 to rotate, and the two eccentric parts 11 of the crankshaft 10 respectively drive the corresponding two sliders 40 to move. When the slider 40 revolves around the axis of the crankshaft 10, the slider 40 Relative to the eccentric part 11, the slider 40 reciprocates along the limiting channel 31, and drives the cross groove structure 30 to rotate in the cylinder liner 20. The slider 40 reciprocates along the limiting channel 31 while revolving to form a cross slide Movement mode of the block mechanism.

Other usage occasions: the compressor can be used as an expander by exchanging the positions of the suction port and the exhaust port. That is, the exhaust port of the compressor is used as the suction port of the expander, and high-pressure gas is passed in, and other pushing mechanisms rotate, and the gas is discharged through the suction port of the compressor (exhaust port of the expander) after expansion.

When the fluid machine is an expander, the cylinder liner 20 has an expansion exhaust port and an expansion intake port. When any slider 40 is in the intake position, the expansion exhaust port is in communication with the corresponding variable volume chamber 311; When a slider 40 is in the exhaust position, the corresponding variable volume cavity 311 is in communication with the expansion inlet. In this way, when the high-pressure gas enters the variable volume chamber 311 through the expansion air inlet, the high-pressure gas pushes the intersecting groove structure 30 to rotate, and the intersecting groove structure 30 rotates to drive the slider 40 to rotate, and at the same time, the slider 40 is relatively opposite to the intersecting groove structure. 30 slides linearly, so that the slider 40 drives the eccentric part 11 to rotate, that is, drives the crankshaft 10 to rotate. By connecting the crankshaft 10 with other power-consuming devices, the crankshaft 10 can be made to output work.

In some embodiments, the inner wall of the cylinder liner 20 has an expansion exhaust cavity, and the expansion exhaust cavity communicates with the expansion exhaust port.

In some embodiments, the expansion exhaust cavity extends a first preset distance around the inner wall surface of the cylinder liner 20 to form an arc-shaped expansion exhaust cavity, and the expansion exhaust cavity expands from the expansion exhaust port to the expansion inlet. The side where the air port is located extends, and the extension direction of the expansion exhaust chamber is the same as the rotation direction of the intersecting groove structure 30 .

In some embodiments, there are two expansion exhaust chambers, and the two expansion exhaust chambers are arranged at intervals along the axial direction of the cylinder liner 20. The cylinder liner 20 also has an expansion exhaust communication chamber, and the two expansion exhaust chambers are connected to the expansion The exhaust communication cavity communicates, and the expansion exhaust port communicates with the expansion exhaust cavity through the expansion exhaust communication cavity.

In some embodiments, the expansion exhaust communication cavity extends a second preset distance along the axial direction of the cylinder liner 20 , and at least one end of the expansion exhaust communication cavity passes through the axial end surface of the cylinder liner 20 .

Embodiment two

As shown in Figures 27 to 40, a fluid machine with bearings includes a crankshaft 10, a cylinder liner 20, a bearing 200, an intersecting groove structure 30 and a slider 40, wherein the crankshaft 10 is provided with two eccentric parts 11 along its axial direction; The crankshaft 10 and the cylinder liner 20 are arranged eccentrically and the eccentric distance is fixed; the bearing 200 is arranged in the cylinder liner 20 and the outer ring of the bearing 200 is attached to the inner wall of the cylinder liner 20; the intersecting groove structure 30 is rotatably arranged in the cylinder liner 20, The outer peripheral surface of the intersecting groove structure 30 fits the inner ring of the bearing 200, and the ratio between the height H1 of the bearing 200 and the height H2 of the cylinder liner 20 is greater than 0.9 and less than 1, and the intersecting groove structure 30 has two limiting channels 31 , two limiting passages 31 are arranged in sequence along the axial direction of the crankshaft 10, and the extending direction of the limiting passages 31 is perpendicular to the axial direction of the crankshaft 10; the slider 40 has a through hole 41, and there are two sliders 40, two of which are eccentric The part 11 correspondingly extends into the two through holes 41 of the two sliders 40, and the two sliders 40 are correspondingly slidably arranged in the two limiting passages 31 to form a variable volume chamber 311, which is located at the side of the slider 40. In the sliding direction, the crankshaft 10 rotates to drive the slider 40 to slide back and forth in the limiting channel 31 and interact with the intersecting groove structure 30 , so that the intersecting groove structure 30 and the slider 40 rotate in the cylinder liner 20 .

By setting the bearing 200 in the cylinder liner 20 and the outer ring of the bearing 200 is attached to the inner wall of the cylinder liner 20, the ratio between the height H1 of the bearing 200 and the height H2 of the cylinder liner 20 is greater than 0.9 and less than 1, so that , the entire outer circle of the intersecting groove structure 30 in the axial direction is supported by the bearing 200 to reduce friction, so that the sliding friction between the circumferential outer surface of the intersecting groove structure 30 and the inner wall of the cylinder liner 20 changes to the circumferential direction of the intersecting groove structure 30 The rolling friction between the outer surface and the bearing 200 reduces mechanical friction power consumption. The inner ring of the bearing 200 cooperates with the intersecting groove structure 30 , and the inner ring of the bearing 200 cooperates with the inner wall of the cylinder liner 20 .

In some embodiments, the bearing 200 is a cage needle roller + inner ring bearing, or a ball bearing, or other bearings capable of realizing this function.

As shown in FIG. 30 , the height H1 of the bearing 200 and the height H2 of the cylinder liner 20 satisfy: 0.003mm≤H2-H1≤0.1mm. In this way, by optimizing the difference between the height H1 of the bearing 200 and the height H2 of the cylinder liner 20, the inclination phenomenon of the intersecting groove structure 30 is effectively prevented, ensuring good lubrication between the intersecting groove structure 30 and the cylinder liner 20 , thereby reducing the mechanical friction power consumption between the intersecting groove structure 30 and the cylinder liner 20, which is beneficial to improving the performance of the compressor, thereby improving the operation reliability of the compressor.

It should be noted that, in this embodiment, since the height H1 of the bearing 200 is similar to the height H2 of the cylinder liner 20, and in order to ensure the reliability of the support of the bearing 200 to the intersecting groove structure 30, no suction and discharge are provided in the radial direction of the bearing 200. The air port, specifically, as shown in Figure 31, Figure 37 to 40, the fluid machine includes two flanges 50, the two flanges 50 are respectively assembled on the axial ends of the cylinder liner 20, and the two flanges 50 are respectively An air intake passage 54 is provided, and the two air intake passages 54 communicate with the two limiting passages 31 respectively, and an exhaust passage 51 is respectively provided on the two flanges 50, and the air intake passage 54 on the same flange 50 and the There is a phase difference between the exhaust passages 51 . In this way, while the integrity of the bearing 200 is ensured, the reliability of the intake and exhaust of the cylinder liner 20 is ensured.

As shown in Figures 31 and 37, the intake passage 54 includes a first intake passage segment 541 and a second intake passage segment 542 connected in sequence, the first intake passage segment 541 extends radially along the flange 50, and the second intake passage segment 541 extends radially along the flange 50. The two intake channel segments 542 extend axially along the flange 50 . In this way, the communication reliability between the intake passage 54 and the variable volume cavity 311 is ensured.

As shown in Figure 37, an exhaust groove 55 is provided on the end surface of the flange 50 facing away from the cylinder liner 20, and the bottom of the exhaust groove 55 is provided with an exhaust communication port 551, which communicates with the limiting passage 31, and the exhaust communication The port 551 extends in the axial direction of the flange 50 . In this way, the exhaust reliability of the cylinder liner 20 is ensured.

As shown in Figure 37, the end of the intake passage 54 is the intake communication port, and the initial end of the exhaust passage 51 is the exhaust communication port 551. When any slider 40 is at the intake position, the intake communication port and the corresponding The variable volume chamber 311 is in conduction; when any slider 40 is in the exhaust position, the corresponding variable volume chamber 311 is in conduction with the exhaust communication port 551 .

When the fluid machine is an expander, the end of the intake passage 54 is the intake communication port, and the initial end of the exhaust passage 51 is the exhaust communication port 551. When any slider 40 is at the intake position, the exhaust communication port 551 is in communication with the corresponding variable volume cavity 311; when any slider 40 is in the exhaust position, the corresponding variable volume cavity 311 is in communication with the intake port.

As shown in FIGS. 36 and 37 , the cylinder liner 20 has a circumferential protruding ring 28 , and the circumferential protruding ring 28 is provided with elongated holes 281 .

Embodiment Three

As shown in Figures 41 to 52, a fluid machine with bearings includes a crankshaft 10, a cylinder liner 20, a bearing 200, an intersecting groove structure 30 and a slider 40, wherein the crankshaft 10 is provided with two eccentric parts 11 along its axial direction; The crankshaft 10 and the cylinder liner 20 are eccentrically arranged and the eccentric distance is fixed; there is at least one bearing 200, the bearing 200 is arranged in the cylinder liner 20 and is located at the axial end of the cylinder liner 20, and the outer ring of the bearing 200 is in contact with the cylinder liner 20 The inner wall of the cross groove structure 30 is rotatably arranged in the cylinder liner 20, and the outer peripheral surface of the cross groove structure 30 is attached to the inner ring of the bearing 200. The cross groove structure 30 has two limiting channels 31, two limiting channels The positioning channel 31 is arranged in sequence along the axial direction of the crankshaft 10, and the extension direction of the limiting channel 31 is perpendicular to the axial direction of the crankshaft 10; the sliding block 40 has a through hole 41, and there are two sliding blocks 40, and the two eccentric parts 11 extend correspondingly. into the two through holes 41 of the two sliders 40, the two sliders 40 are correspondingly slidably arranged in the two limiting passages 31 and form a variable volume cavity 311, which is located in the sliding direction of the slider 40, The crankshaft 10 rotates to drive the slider 40 to reciprocate and slide in the limiting channel 31 while interacting with the intersecting groove structure 30 , so that the intersecting groove structure 30 and the slider 40 rotate in the cylinder liner 20 .

At least one bearing 200 is arranged in the cylinder liner 20 and at the axial end of the cylinder liner 20, and the outer ring of the bearing 200 is attached to the inner wall of the cylinder liner 20, so that the outer peripheral surface of the intersecting groove structure 30 passes through the bearing 200 supports wear reduction, so that the sliding friction between the circumferential outer surface of the intersecting groove structure 30 and the inner wall of the cylinder liner 20 becomes rolling friction between the circumferential outer surface of the intersecting groove structure 30 and the bearing 200, reducing mechanical friction power consumption , wherein, the inner ring of the bearing 200 cooperates with the intersecting groove structure 30 , and the inner ring of the bearing 200 cooperates with the inner wall of the cylinder liner 20 .

In some embodiments, the bearing 200 is a rolling bearing, or a cylindrical roller bearing, or a cage needle roller + inner ring bearing, or other bearings capable of realizing this function.

As shown in Figure 45 and Figure 50, the axial end surface of the cylinder liner 20 is provided with an annular sinking groove 210. The distance between them is equal, and the bearing 200 is installed at the annular sinker 210. In this way, the bearing 200 is installed in the cylinder liner 20 in an embedded manner, which not only can effectively prevent the cross groove structure 30 from tilting, but also reduce mechanical friction, and can also keep the height of each component of the pump body assembly 83 constant, which is convenient for scale chemical production.

As shown in FIGS. 41 to 45 , 49 and 52 , bearings 200 are provided at both ends of the axial end of the cylinder liner 20 . In this way, the rotation stability of the intersecting groove structure 30 in the cylinder liner 20 is ensured.

As shown in FIG. 44 , the relationship between the diameter Q of the outer peripheral surface of the intersecting groove structure 30 and the height N of the bearing 200 satisfies: 3≤Q/N≤7. The diameter R of the outer peripheral surface of the intersecting groove structure 30 and the height N of the bearing 200 satisfy: 1.5≦R/N≦3.5. In this way, the inclination phenomenon of the intersecting groove structure 30 is effectively prevented, and good lubrication between the intersecting groove structure 30 and the cylinder liner 20 is ensured, thereby reducing the mechanical friction power consumption between the intersecting groove structure 30 and the cylinder liner 20. It is beneficial to improve the performance of the compressor, thereby improving the operation reliability of the compressor.

It should be noted that, in this embodiment, since the two bearings 200 are respectively located at the two ends of the axial end of the cylinder liner 20, the suction and exhaust of the cylinder liner 20 in the first embodiment are still applicable, and will not be repeated here. .

As shown in Figure 46, there are two suction chambers 23, and the two suction chambers 23 are arranged at intervals along the axial direction of the cylinder liner 20. The cylinder liner 20 also has a suction communication chamber 24, and the two suction chambers 23 are connected to the suction The gas communication cavity 24 communicates, and the compressed air inlet 21 communicates with the suction cavity 23 through the suction communication cavity 24 .

Certainly, in this embodiment, as shown in Fig. 47 to Fig. 49, there are two suction cavities 23, the two suction cavities 23 are arranged at intervals along the axial direction of the cylinder liner 20, and there are two compressed air inlets 21, The two compressed air inlets 21 are provided in one-to-one correspondence with the two suction chambers 23 and communicate with each other. That is, in this embodiment, the two air suction chambers 23 may also be independent from each other, and not communicated through the air suction communication chamber 24 .

Embodiment Four

As shown in FIG. 53 and FIG. 54 , the difference between this embodiment and the third embodiment is that only one end of the axial end of the cylinder liner 20 is provided with a bearing 200 .

It should be noted that, in this embodiment, since the bearing 200 is located at one end of the axial end of the cylinder liner 20 , the suction and exhaust of the cylinder liner 20 in the first embodiment are still applicable.

Embodiment five

As shown in FIG. 55 and FIG. 56 , the difference between this embodiment and the third embodiment is that only one end of the axial end of the cylinder liner 20 is provided with a bearing 200 .

Embodiment six

As shown in Figures 57 to 66, a fluid machine with bearings includes a crankshaft 10, a cylinder liner 20, a bearing 200, an intersecting groove structure 30 and a slider 40, wherein the crankshaft 10 is provided with two eccentric parts 11 along its axial direction; The crankshaft 10 and the cylinder liner 20 are arranged eccentrically and the eccentric distance is fixed; there is at least one bearing 200, and the bearing 200 is arranged on the axial end surface of the cylinder liner 20 and is located outside the cylinder liner 20; the cross groove structure 30 is rotatably arranged on the cylinder liner 20 sleeve 20, and the axial part of the outer peripheral surface of the intersecting groove structure 30 fits the inner ring of the bearing 200, the intersecting groove structure 30 has two limiting channels 31, and the two limiting channels 31 are along the axial direction of the crankshaft 10. Second setting, the extension direction of the limiting channel 31 is perpendicular to the axial direction of the crankshaft 10; the slider 40 has a through hole 41, and there are two sliders 40, and the two eccentric parts 11 extend into the two through holes of the two sliders 40 correspondingly. In the hole 41, two sliders 40 are correspondingly slidably arranged in the two limiting passages 31 to form a variable volume cavity 311. The variable volume cavity 311 is located in the sliding direction of the slider 40, and the crankshaft 10 rotates to drive the slider 40 within the limit. While reciprocating sliding in the channel 31 , it interacts with the intersecting groove structure 30 , so that the intersecting groove structure 30 and the slider 40 rotate in the cylinder liner 20 .

By arranging the bearing 200 at the axial end surface of the cylinder liner 20 and outside the cylinder liner 20, the axial part of the outer peripheral surface of the intersecting groove structure 30 is attached to the inner ring of the bearing 200, so that the intersecting groove structure 30 The outer circumferential surface of the cross groove structure 30 is supported by the bearing 200 to reduce friction, so that the sliding friction between the circumferential outer surface of the intersecting groove structure 30 and the inner wall of the cylinder liner 20 changes to the rolling friction between the circumferential outer surface of the intersecting groove structure 30 and the bearing 200, reducing Mechanical friction power consumption is obtained, wherein, the inner ring of the bearing 200 cooperates with the intersecting groove structure 30, and the inner ring of the bearing 200 cooperates with the inner wall of the cylinder liner 20.

In some embodiments, only one end of the axial end of the cylinder liner 20 is provided with a bearing 200; It is set above one end of the axial end as an example.

In some embodiments, the diameter D1 of the inner ring of the bearing 200 and the diameter D3 of the outer peripheral surface of the cylinder liner 20 satisfy: D1-D3 is 0.003-0.02 mm.

In some embodiments, the diameter D2 of the outer peripheral surface of the intersecting groove structure 30 and the diameter D3 of the inner wall surface of the cylinder liner 20 satisfy: D2-D3 is 0.02-0.05 mm.

It should be noted that, in this embodiment, the bearing 200 is arranged above one of the axial ends of the cylinder liner 20 as an example.

As shown in Figure 59, Figure 60, Figure 63 to Figure 66, when only one end of the axial end of the cylinder liner 20 is provided with a bearing 200, the fluid machine includes two flanges 50, and the two flanges 50 are respectively assembled on The axial end of the cylinder liner 20 and the axial end of the bearing 200, the cylinder liner 20 is provided with a radial suction hole 220 and an axial split hole 230 communicating with the radial suction hole 220; wherein, the radial suction The hole 220 communicates with the radially corresponding limiting channel 31 of the cylinder liner 20, the bearing 200 is provided with a suction through hole 201 for communicating with the axial distribution hole 230, and the flange 50 on the side of the bearing 200 has a suction channel 56. One end of the air passage 56 communicates with the air suction through hole 201 , and the other end of the air suction passage 56 communicates with the corresponding limiting passage 31 at the bearing 200 . In this way, the air intake reliability of the upper and lower limiting passages 31 is ensured.

As shown in FIG. 59 , FIG. 60 , and FIG. 63 to FIG. 66 , the inner wall surface of the cylinder liner 20 has an air suction cavity 23 , and the air suction cavity 23 communicates with the radial air suction holes 220 .

In some embodiments, the suction cavity 23 extends a first preset distance around the inner wall surface of the cylinder liner 20 to form an arc-shaped suction cavity 23 .

As shown in Figure 60, Figure 61, Figure 63, Figure 64, and Figure 66, the cylinder liner 20 has a compression exhaust port 22, and there is a phase difference between the compression exhaust port 22 and the radial suction hole 220, the cylinder liner 20 An exhaust cavity 25 is opened on the outer wall of the cylinder liner 20, and the compression exhaust port 22 is connected to the exhaust cavity 25 by the inner wall of the cylinder liner 20. The fluid machine also includes an exhaust valve assembly 60, which is arranged in the exhaust cavity 25 Inside and corresponding to the compression exhaust port 22.

As shown in Figure 61, the flange 50 on the side of the bearing 200 is provided with a flange exhaust port 57, the flange exhaust port 57 communicates with the limiting channel 31 located at the bearing 200, and the flange exhaust port 57 is located at the bearing 200 within the inner ring side of the In this way, the reliability of exhausting the variable volume chamber 311 located on the side of the bearing 200 is ensured.

When the fluid machine is a compressor, the end of the radial suction hole 220 is the first intake communication port, and the end of the suction passage 56 is the second intake communication port. When the slider 40 at the cylinder liner 20 is in the intake port position, the first intake port communicates with the corresponding variable volume chamber 311, and when the slider 40 at the cylinder liner 20 is at the exhaust position, the corresponding variable volume chamber 311 communicates with the compression exhaust port 22; When the slider 40 at the bearing 200 is at the air intake position, the second air intake communication port is in communication with the corresponding variable volume cavity 311; when the slider 40 at the bearing 200 is at the exhaust position, the corresponding variable volume cavity 311 is connected to the The flange exhaust port 57 is connected.

When the fluid machine is an expander, the end of the radial suction hole 220 is the first intake communication port, and the end of the suction passage 56 is the second intake communication port. When the slider 40 at the cylinder liner 20 is in the intake port position, the compression exhaust port 22 is in communication with the corresponding variable volume chamber 311, and when the slider 40 at the cylinder liner 20 is in the exhaust position, the corresponding variable volume chamber 311 is in communication with the first intake port; When the slider 40 at the bearing 200 is at the intake position, the flange exhaust port 57 is in communication with the corresponding variable volume cavity 311, and when the slider 40 at the bearing 200 is at the exhaust position, the corresponding variable volume cavity 311 is connected to the exhaust position. The second air intake communication port is conducted.

Embodiment seven

As shown in Figure 67 and Figure 68, when both ends of the axial end of the cylinder liner 20 are provided with bearings 200, the cylinder liner 20 is provided with a radial suction hole 220 and communicates with the radial suction hole 220 The axial distribution hole 230; wherein, one end of the axial distribution hole 230 communicates with one of the two limiting passages 31, and the other end of the axial distribution hole 230 communicates with the other of the two limiting passages 31.

As shown in FIG. 68 , the inner wall of the cylinder liner 20 has an air suction chamber 23 , and the air suction chamber 23 communicates with the axial distribution hole 230 .

As shown in FIG. 68 , there are two suction chambers 23 , and the two suction chambers 23 are arranged at intervals along the axial direction of the cylinder liner 20 . The two suction chambers 23 correspond to and communicate with the two limiting passages 31 one by one.

It should be noted that, in this embodiment, the cylinder liner 20 has a compression exhaust port 22, and there is a phase difference between the compression exhaust port 22 and the radial suction hole 220 (the compression exhaust port on the cylinder liner 20 of this embodiment The air port 22 is consistent with the position and opening method of the compression exhaust port 22 in Fig. 17 in Embodiment 1, and will not be repeated here).

In some embodiments, there are two compression exhaust ports 22, and the two compression exhaust ports 22 are arranged at intervals along the axial direction of the cylinder liner 20, and the two compression exhaust ports 22 are connected to the two two limiting passages 31 Corresponding and connected.

It should be noted that, when the fluid machine is a compressor, the end of the suction chamber 23 is an air intake communication port, and when any slider 40 is in the intake position, the intake communication port is in communication with the corresponding variable volume chamber 311 ; When any slider 40 is in the exhaust position, the corresponding variable volume cavity 311 is in communication with the compression exhaust port 22 .

It should be noted that, when the fluid machine is an expander, the end of the suction chamber 23 is an intake communication port, and when any slider 40 is at the intake position, the compression exhaust port 22 is connected to the corresponding variable volume chamber 311. When any slider 40 is in the exhaust position, the corresponding variable volume cavity 311 is in communication with the intake port.

Embodiment eight

As shown in FIGS. 69 and 70 , the difference between this embodiment and Embodiment 6 is that the bearing 200 in this embodiment is arranged below one of the axial ends.

It should be noted that the bearing 200 in this embodiment is located at one end of the axial end, and similarly, the suction and exhaust method in Embodiment 6 is still applicable to this embodiment.

Embodiment nine

As shown in Figures 71 to 78, a fluid machine with bearings includes a crankshaft 10, a cylinder liner 20, a bearing 200, a cross groove structure 30 and a slider 40, wherein the crankshaft 10 is provided with two eccentric parts 11 along its axial direction The crankshaft 10 and the cylinder liner 20 are eccentrically arranged and the eccentric distance is fixed, and the cylinder liner 20 includes two sub-cylinder liners 27 arranged separately along its axial direction; the bearing 200 is arranged between the two sub-cylinder liners 27, and the axial direction of the bearing 200 is two The end faces of the two sub-cylinder sleeves 27 are respectively attached to the end faces of the side of the bearing 200. The bearing 200 is concentrically arranged with the two sub-cylinder sleeves 27; the cross groove structure 30 is rotatably arranged in the cylinder sleeve 20, and the cross groove structure 30 axial Part of the outer peripheral surface of the crankshaft fits the inner ring of the bearing 200. The intersecting groove structure 30 has two limiting channels 31. The two limiting channels 31 are arranged in sequence along the axial direction of the crankshaft 10. The extending direction of the limiting channels 31 is vertical. In the axial direction of the crankshaft 10; the slider 40 has a through hole 41, and there are two sliders 40, the two eccentric parts 11 correspondingly extend into the two through holes 41 of the two sliders 40, and the two sliders 40 slide correspondingly It is arranged in two limiting passages 31 and forms a variable volume chamber 311. The variable volume chamber 311 is located in the sliding direction of the slider 40, and the crankshaft 10 rotates to drive the slider 40 to reciprocate in the limiting passage 31 while sliding with the intersecting groove. The structure 30 interacts so that the intersecting groove structure 30 and the slider 40 rotate in the cylinder sleeve 20 .

By setting the cylinder liner 20 into a structural form including two sub-cylinder liners 27, at the same time, the bearing 200 is arranged between the two sub-cylinder liners 27, and the end faces of the two axial ends of the bearing 200 are respectively aligned with the two sub-cylinder liners 27 toward the bearing 200. The end face of one side is attached, and the bearing 200 is arranged concentrically with the two sub-cylinder sleeves 27, so that part of the outer peripheral surface of the intersecting groove structure 30 in the axial direction is attached to the inner ring of the bearing 200, so that the outer peripheral surface of the intersecting groove structure 30 passes through the bearing 200 supports wear reduction, so that the sliding friction between the circumferential outer surface of the intersecting groove structure 30 and the inner wall of the cylinder liner 20 becomes rolling friction between the circumferential outer surface of the intersecting groove structure 30 and the bearing 200, reducing mechanical friction power consumption , wherein, the inner ring of the bearing 200 cooperates with the intersecting groove structure 30 , and the inner ring of the bearing 200 cooperates with the inner wall of the cylinder liner 20 .

In some embodiments, the diameter D1 of the inner ring of the bearing 200 and the diameter D3 of the inner wall of the cylinder liner 20 satisfy: D1-D3 is -0.1-0.06 mm.

In some embodiments, the diameter D2 of the outer peripheral surface of the intersecting groove structure 30 and the diameter D3 of the inner wall surface of the cylinder liner 20 satisfy: D2-D3 is 0-0.1 mm.

As shown in Fig. 72, Fig. 74 to Fig. 77, the upper sub-cylinder liner 27 of the two sub-cylinder sleeves 27 is provided with a first radial air suction hole 271 and a split hole 272 communicating with the first radial air suction hole 271 , the diversion hole 272 extends along the axial direction of the sub-cylinder liner 27 and penetrates to the lower end surface of the sub-cylinder liner 27. The position where the bearing 200 is opposite to the diversion hole 272 is provided with a suction through hole 201, and the two sub-cylinder liners 27 are located below The sub cylinder sleeve 27 is provided with an air intake transition hole 273 and a second radial air intake hole 274 communicating with the air intake transition hole 273 . In this way, the suction reliability of the pump body assembly 83 is ensured.

As shown in Figure 72 and Figure 74, the fluid machine also includes two flanges 50, the two flanges 50 are respectively assembled on the axial ends of the cylinder liner 20, and the upper one of the two sub-cylinder liners 27 The inner wall surface has a first exhaust communication port 275 , the first exhaust communication port 275 penetrates to the upper end surface of the sub cylinder liner 27 and communicates with the flange exhaust port 57 on the flange 50 . In this way, the exhaust reliability of the pump body assembly 83 is ensured.

As shown in Fig. 72, Fig. 76 to Fig. 78, the bearing 200 also has an exhaust through-hole 202, and the two sub-cylinder sleeves 27 are respectively provided with exhaust drainage holes 276 at positions opposite to the exhaust through-hole 202, and the two exhaust The drainage holes 276 are all communicated with the exhaust through hole 202 and communicated with the flange exhaust port 57. The inner wall surface of the lower sub-cylinder sleeve 27 of the two sub-cylinder sleeves 27 has a second exhaust communication port 277. The communication port 277 communicates with the flange exhaust port 57 sequentially through the lower exhaust flow hole 276 , the exhaust through hole 202 , and the upper exhaust flow hole 276 . In this way, the exhaust reliability of the pump body assembly 83 is ensured.

When the fluid machine is a compressor, the end of the first radial air suction hole 271 is the first air intake communication port, and the end of the second radial air suction hole 274 is the second air intake communication port. When the slider 40 is at the intake position, the first intake port communicates with the corresponding variable volume chamber 311, and when the upper slider 40 is at the exhaust position, the corresponding variable volume chamber 311 communicates with the first exhaust port 275. conduction; when the lower slider 40 is at the air intake position, the second air intake communication port is in communication with the corresponding variable volume cavity 311, and when the lower slider 40 is at the exhaust position, the corresponding variable volume cavity 311 It communicates with the second exhaust communication port 277 .

When the fluid machine is an expander, the end of the first radial air suction hole 271 is the first air intake communication port, and the end of the second radial air suction hole 274 is the second air intake communication port. 40 is at the intake position, the first exhaust communication port 275 is in communication with the corresponding variable volume cavity 311, and when the upper slider 40 is at the exhaust position, the corresponding variable volume cavity 311 is connected to the first intake communication port. conduction; when the lower slider 40 is at the air intake position, the second exhaust communication port 277 is connected to the corresponding variable volume cavity 311, and when the lower slider 40 is at the exhaust position, the corresponding variable volume cavity 311 communicates with the second air intake port.

Embodiment ten

As shown in Figures 79 to 84, the difference between this embodiment and Embodiment 1 is that the cross section of the limiting channel 31 of the intersecting groove structure 30 in this embodiment in the sliding direction of the slider 40 is a square, wherein, Fig. In 82, the bearing 200 is arranged in the cylinder liner 20 and the outer ring of the bearing 200 is attached to the inner wall of the cylinder liner 20, and the ratio between the height H1 of the bearing 200 and the height H2 of the cylinder liner 20 is greater than 0.9 and less than 1.

Embodiment Eleven

As shown in Figures 85 to 105, the fluid machine includes two flanges 50, a crankshaft 10, a cylinder liner 20, a cross groove structure 30 and a slider 40, wherein the crankshaft 10 is provided with two eccentric parts 11 along its axial direction, and the two There is a phase difference of the first angle A between the two eccentric parts 11; the crankshaft 10 and the cylinder liner 20 are arranged eccentrically and the eccentric distance is fixed; the intersecting groove structure 30 is rotatably arranged in the cylinder liner 20, and the intersecting groove structure 30 has two Limiting channels 31, two limiting channels 31 are arranged in sequence along the axial direction of the crankshaft 10, the extending direction of the limiting channels 31 is perpendicular to the axial direction of the crankshaft 10, and there is a second gap between the extending directions of the two limiting channels 31 The phase difference between the two included angles B, wherein the first included angle A is twice the second included angle B; the slider 40 has a through hole 41, and there are two sliders 40, and the crankshaft 10 passes through two flanges 50 and The cylinder liner 20, and the two eccentric parts 11 extend into the two through holes 41 of the two sliders 40 correspondingly, and the two sliders 40 are correspondingly slidably arranged in the two limiting passages 31 to form a variable volume cavity 311, The variable volume cavity 311 is located in the sliding direction of the slider 40. The crankshaft 10 rotates to drive the slider 40 to reciprocate and slide in the limiting channel 31 while interacting with the intersecting groove structure 30, so that the intersecting groove structure 30 and the slider 40 are in the cylinder. Turn in cover 20.

By arranging the two flanges 50 on the axial ends of the cylinder liner 20 respectively, at the same time, the crankshaft 10 passes through the two flanges 50 and the cylinder liner 20 to ensure that the two flanges 50 can limit the cylinder liner 20 function, thereby ensuring the installation reliability of the cylinder liner 20.

As shown in FIG. 90 , openings 38 for crankshaft 10 are reserved on both ends of the intersecting groove structure 30 . The openings 38 are arranged concentrically with the intersecting groove structure 30 . In this way, it is ensured that the crankshaft 10 can smoothly pass through the intersecting groove structure 30 , and when the intersecting groove structure 30 is located in the cylinder liner 20 , the cylinder liner 20 can be well sealed.

As shown in FIG. 90 and FIG. 91 , the shape of the slider 40 on the section of the limiting channel 31 is adapted to the shape of the section of the limiting channel 31 . In this way, the sliding stability of the slider 40 in the limiting channel 31 is ensured.

In some embodiments, the projection of the slider 40 in the sliding direction of the slider 40 is a square, and the width B of the square and the height H of the square satisfy: 0.5˜3.

In some embodiments, the width B of the square and the height H of the square satisfy: 1.5˜2.5.

In some embodiments, the cross section of the limiting channel 31 is a part of a semicircle, the projection of the slider 40 on the sliding direction of the slider 40 is composed of an arc segment and a straight line segment, and the radius of curvature of the arc is twice the is D1, the length of the straight line is d1, and the distance between D1 and d1 satisfies: d1/D1 is 0.3-1.

In some embodiments, the relationship between D1 and d1 satisfies: d1/D1 is 0.5˜0.7.

As shown in FIGS. 92 and 93 , the axial end of the intersecting groove structure 30 is sleeved with a bearing 200 , and is located above the axial end of the intersecting groove structure 30 .

As shown in FIG. 94 and FIG. 95 , bearings 200 are sheathed on both axial ends of the intersecting groove structure 30 .

As shown in FIG. 96 and FIG. 97 , the other axial end of the intersecting groove structure 30 is sleeved with a bearing 200 , and is located below one axial end of the intersecting groove structure 30 .

As shown in Figure 98 and Figure 99, the bearing 200 is arranged in the cylinder liner 20 and the outer ring of the bearing 200 is attached to the inner wall of the cylinder liner 20, and at the same time the ratio between the height H1 of the bearing 200 and the height H2 of the cylinder liner 20 is defined Greater than 0.9 and less than 1.

As shown in Figures 100 and 101, the cylinder liner 20 includes two sub-cylinder liners 27, the bearing 200 is arranged between the two sub-cylinder liners 27, and the end faces of the two axial ends of the bearing 200 are respectively aligned with the two sub-cylinder liners 27 toward the bearing 200. The end face of the side is fitted, and the bearing 200 is concentrically arranged with the two sub-cylinder sleeves 27.

As shown in FIG. 102 to FIG. 105 , the section of the limiting channel 31 is one of semicircle, circle, rectangle, ellipse, square and trapezoid.

Embodiment 12

As shown in Figures 106 to 108, the end surface of at least one end of the intersecting groove structure 30 is open, and the limiting channel 31 on one side of the open shape directly penetrates to the end surface along the axial direction of the intersecting groove structure 30, and the intersecting groove structure An opening 38 is reserved on the end surface of the non-open end of 30 for the crankshaft 10 to protrude from.

It should be noted that, in this embodiment, one end of the intersecting groove structure 30 is open, and the open end is located above.

Embodiment Thirteen

As shown in FIGS. 109 to 111 , the difference between this embodiment and Embodiment 12 is that one end of the intersecting groove structure 30 is open, and the open end is located below.

Embodiment Fourteen

As shown in Figures 112 to 125, the fluid machine includes a crankshaft 10, a cylinder liner 20, at least one end cover 100, a cross groove structure 30 and a slider 40, wherein the crankshaft 10 is provided with two eccentric parts 11 along its axial direction, There is a phase difference of the first angle A between the two eccentric parts 11; the crankshaft 10 and the cylinder liner 20 are set eccentrically and the eccentric distance is fixed; the crankshaft 10 is set through the end cover 100 and the cylinder liner 20; the cross groove structure 30 is rotatable Set in the cylinder liner 20, the intersecting groove structure 30 has two limiting passages 31, the two limiting passages 31 are arranged in sequence along the axial direction of the crankshaft 10, the extending direction of the limiting passages 31 is perpendicular to the axial direction of the crankshaft 10, And there is a phase difference of the second included angle B between the extension directions of the two limiting channels 31, wherein the first included angle A is twice the second included angle B, and the axial direction of the intersecting groove structure 30 has at least one support Protruding ring 36, and the outer circle diameter of supporting protruding ring 36 is smaller than the outer circle diameter of intersecting groove structure 30, and supporting protruding ring 36 protrudes toward end cover 100; Slide block 40 has through hole 41, and slide block 40 is two, two The two eccentric parts 11 correspondingly extend into the two through holes 41 of the two sliders 40, and the two sliders 40 are correspondingly slidably arranged in the two limiting passages 31 and form a variable volume cavity 311, which is located on the slider In the sliding direction of 40, the crankshaft 10 rotates to drive the slider 40 to reciprocally slide in the limiting channel 31 and interact with the intersecting groove structure 30, so that the intersecting groove structure 30 and the slider 40 rotate in the cylinder liner 20.

According to the calculation formula of the friction power consumption of the outer circle of the intersecting groove structure 30 , the friction power consumption of the friction pair is proportional to the third power of the radius. Therefore, the smaller the radius of the friction pair, the smaller the friction power consumption.

Specifically, the intersecting groove structure 30 of this embodiment has at least one supporting protrusion ring 36 in the axial direction, and at the same time, the outer diameter of the supporting protrusion ring 36 is smaller than the outer diameter of the intersecting groove structure 30, and the supporting protrusion ring 36 faces the end cap 100 In this way, since the outer diameter of the supporting convex ring 36 is significantly smaller than the outer diameter of the intersecting groove structure 30, during the operation of the compressor, the outer circle of the supporting convex ring 36 serves as a bearing surface, so that the frictional power consumption is significantly smaller than that of the intersecting groove structure. The outer circle of the structure 30 serves as a bearing surface.

In this embodiment, both ends of the intersecting groove structure 30 have supporting convex rings 36. Along the axial direction of the intersecting groove structure 30, the inner rings of the supporting convex rings 36 face the middle of the intersecting groove structure 30 and are formed to allow the crankshaft 10 to pass through. The channel 39 is arranged concentrically with the supporting convex ring 36, and the channel 39 communicates with the limiting channel 31.

As shown in Figure 113, Figure 114, Figure 117, and Figure 119, the end cover 100 includes a flange 50 and a limiting plate 110, the flange 50 is arranged at the end of the cylinder liner 20, and the limiting plate 110 is arranged between the flange 50 and the limiting plate 110. Between the cylinder liners 20, the limiting plate 110 has a through hole 1101 for avoiding the crankshaft 10, the height of the supporting convex ring 36 is greater than the thickness of the limiting plate 110, and the end surface of the supporting convex ring 36 facing the side of the flange 50 serves as a thrust On the surface 361 , the supporting convex ring 36 passes through the through hole 1101 and makes thrust contact with the flange 50 . In this way, only the thrust surface 361 of the support collar 36 is brought into thrust contact with the flange 50 .

In some embodiments, the height of the supporting protruding ring 36 and the thickness of the limiting plate 110 meet: the optimal height difference between the two is in the range of 0.05 mm˜1 mm.

As shown in Figure 113, Figure 114, Figure 117, and Figure 119, the end cover 100 includes a flange 50 and a limiting plate 110, the flange 50 is arranged at the end of the cylinder liner 20, and the limiting plate 110 is arranged between the flange 50 and the limiting plate 110. Between the cylinder liners 20, the limiting plate 110 has a through hole 1101 for avoiding the crankshaft 10, and the supporting convex ring 36 is inserted into the through hole 1101. The height of the supporting convex ring 36 is smaller than the thickness of the limiting plate 110, and the cross groove structure The supporting ring surface 37 located outside the supporting protruding ring 36 is in thrust contact with the limiting plate 110 . In this way, the end surface of the supporting convex ring 36 is suspended in the air, and at the same time, the supporting ring surface 37 outside the supporting convex ring 36 is in thrust contact with the limiting plate 110 .

As shown in FIG. 120 and FIG. 121 , an avoidance channel 1102 is opened at the position where the limit plate 110 is opposite to the communication hole 26 , and the communication hole 26 communicates with the exhaust channel 51 through the avoidance channel 1102 .

It should be noted that, in this disclosure, the limiting plate 110 is arranged concentrically with the intersecting groove structure 30 , and the through hole 1101 is the central hole of the limiting plate 110 .

As shown in FIGS. 122 to 125 , the section of the limiting channel 31 is one of semicircle, circle, rectangle, ellipse, square and trapezoid.

The air intake and exhaust mode of this embodiment is consistent with that of the first embodiment.

Embodiment 15

As shown in Figures 126 to 141, only one end of the intersecting groove structure 30 has a supporting protruding ring 36, and the end face of the end of the intersecting groove structure 30 not provided with the supporting protruding ring 36 is open, and the limiting channel 31 is along the intersecting groove structure. The axial direction of 30 directly penetrates to the end face.

In this embodiment, one end with an open end face is located below the intersecting groove structure 30 .

As shown in FIG. 131 and FIG. 132 , in this embodiment, the cross sections of the two sliders 40 are determined according to the two limiting channels 31 of the intersecting groove structure 30 .

As shown in FIG. 136 and FIG. 137 , bearings 200 are sleeved on both axial ends of the intersecting groove structure 30 .

As shown in FIG. 138 , the axial end of the intersecting groove structure 30 is sleeved with a bearing 200 , and is located above the axial end of the intersecting groove structure 30 .

As shown in FIG. 139 , the other axial end of the intersecting groove structure 30 is sleeved with a bearing 200 , and is located below one axial end of the intersecting groove structure 30 .

As shown in Figure 140 and Figure 141, the bearing 200 is arranged in the cylinder liner 20 and the outer ring of the bearing 200 is attached to the inner wall of the cylinder liner 20, and the ratio between the height H1 of the bearing 200 and the height H2 of the cylinder liner 20 is defined at the same time Greater than 0.9 and less than 1.

Embodiment sixteen

As shown in Figures 142 to 144, only one end of the intersecting groove structure 30 has a supporting protruding ring 36, and the end face of the end of the intersecting groove structure 30 not provided with a supporting protruding ring 36 is open, and the limiting channel 31 is along the intersecting groove structure. The axial direction of 30 directly penetrates to the end face.

In this embodiment, one end with an open end face is located above the intersecting groove structure 30 .

Embodiment 17

As shown in Figures 145 to 147, only one end of the intersecting groove structure 30 has a supporting convex ring 36, and the end surface of the end of the intersecting groove structure 30 not provided with the supporting convex ring 36 is only reserved with an opening 38 for the crankshaft 10 to protrude from. , the opening 38 is set concentrically with the supporting convex ring 36 , and the opening 38 communicates with the limiting channel 31 .

In this embodiment, the end surface of the lower end of the intersecting groove structure 30 only reserves an opening 38 for the crankshaft 10 to protrude from.

Embodiment eighteen

As shown in FIGS. 148 to 150 , only the opening 38 for the crankshaft 10 is reserved on the end surface of the upper end of the intersecting groove structure 30 .

As shown in Figures 151 to 154, the projection of the slider 40 in its sliding direction is adapted to the section of the limiting channel 31, wherein Figure 149 shows the chamfering of the direction slider and the corresponding cross groove structure 30, Figure 150 It is a trapezoidal slider and the corresponding intersecting groove structure 30, FIG. 151 shows the chamfering of the trapezoidal slider and the corresponding intersecting groove structure 30, and FIG. 152 shows a semicircle+straight edge slider and the corresponding intersecting groove structure 30.

It should be noted that the terminology used herein is only for describing specific embodiments, and is not intended to limit the exemplary embodiments according to the present disclosure. As used herein, unless the context clearly dictates otherwise, the singular is intended to include the plural, and it should also be understood that when the terms "comprising" and/or "comprising" are used in this specification, they mean There are features, steps, operations, means, components and/or combinations thereof.

Relative arrangements of components and steps, numerical expressions and numerical values set forth in these embodiments do not limit the scope of the present disclosure unless specifically stated otherwise. At the same time, it should be understood that, for the convenience of description, the sizes of the various parts shown in the drawings are not drawn according to the actual proportional relationship. Techniques, methods and devices known to those of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, such techniques, methods and devices should be considered part of the Authorized Specification. In all examples shown and discussed herein, any specific values should be construed as illustrative only, and not as limiting. Therefore, other examples of the exemplary embodiment may have different values. It should be noted that like numerals and letters denote like items in the following figures, therefore, once an item is defined in one figure, it does not require further discussion in subsequent figures.

For the convenience of description, spatially relative terms may be used here, such as "on ...", "over ...", "on the surface of ...", "above", etc., to describe The spatial positional relationship between one device or feature shown and other devices or features. It will be understood that the spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is turned over, devices described as "above" or "above" other devices or configurations would then be oriented "beneath" or "above" the other devices or configurations. under other devices or configurations”. Thus, the exemplary term "above" can encompass both an orientation of "above" and "beneath". The device may be otherwise oriented (rotated 80 degrees or at other orientations) and the spatially relative descriptions used herein interpreted accordingly.

It should be noted that the terms "first" and "second" in the specification and claims of the present disclosure and the above drawings are used to distinguish similar objects, but not necessarily used to describe a specific sequence or sequence. It is to be understood that the data so used are interchangeable under appropriate circumstances such that the embodiments of the disclosure described herein can be practiced in sequences other than those illustrated or described herein.

The above descriptions are only preferred embodiments of the present disclosure, and are not intended to limit the present disclosure. For those skilled in the art, the present disclosure may have various modifications and changes. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present disclosure shall be included within the protection scope of the present disclosure.

Claims

A fluid machine comprising:

A crankshaft (10), the crankshaft (10) is provided with two eccentric parts (11) along its axial direction, there is a phase difference of a first angle A between the two eccentric parts (11), and the two eccentric parts (11) have a phase difference of a first angle A, and the two The eccentricity of the eccentric part (11) is equal;

A cylinder liner (20), the crankshaft (10) and the cylinder liner (20) are arranged eccentrically and the eccentric distance is fixed;

A cross groove structure (30), the cross groove structure (30) is rotatably arranged in the cylinder liner (20), the cross groove structure (30) has two limiting passages (31), the two The limiting channels (31) are sequentially arranged along the axial direction of the crankshaft (10), the extending direction of the limiting channels (31) is perpendicular to the axial direction of the crankshaft (10), and the two limiting channels There is a phase difference of a second angle B between the extension directions of the bit channels (31), wherein the first angle A is twice the second angle B;

Two sliders (40), each slider (40) has a through hole (41), and the two eccentric parts (11) extend into the two sliders (40) correspondingly. In the through hole (41), the two sliders (40) are correspondingly slidably arranged in the two limiting passages (31) to form a variable volume cavity (311), and the variable volume cavity (311) is located at the In the sliding direction of the slider (40), the crankshaft (10) rotates to drive the slider (40) to slide back and forth in the limiting channel (31) The interaction makes the intersecting groove structure (30) and the slider (40) rotate in the cylinder sleeve (20).
The fluid machine according to claim 1, wherein the eccentricity of the eccentric part (11) is equal to the eccentricity between the crankshaft (10) and the cylinder liner (20).
The fluid machine according to claim 1 or 2, wherein the shaft part (12) of the crankshaft (10) is integrally formed, and the shaft part (12) has only one axis.
A fluid machine according to any one of claims 1-3, wherein,

The shaft part (12) of the crankshaft (10) is integrally formed with the eccentric part (11); or

The shaft part (12) of the crankshaft (10) is detachably connected with the eccentric part (11).
The fluid machine according to any one of claims 1-4, wherein the shaft part (12) of the crankshaft (10) comprises a first segment and a second segment connected along its axial direction, the first segment It is arranged coaxially with the second section, and the two eccentric parts (11) are respectively arranged on the first section and the second section.
A fluid machine according to claim 5, wherein said first segment is detachably connected to said second segment.
The fluid machine according to any one of claims 1-6, wherein both ends of the limiting channel (31) penetrate to the outer peripheral surface of the intersecting groove structure (30).
The fluid machine according to any one of claims 1-7, wherein the two sliders (40) are arranged concentrically with the two eccentric parts (11) respectively, and the sliders (40) surround the The axis of the crankshaft (10) makes a circular motion, and there is a first rotation gap between the wall of the through hole (41) and the eccentric part (11), and the range of the first rotation gap is 0.005 mm to 0.05 mm. mm.
The fluid machine according to any one of claims 1-8, wherein the intersecting groove structure (30) is arranged coaxially with the cylinder liner (20), and the outer peripheral surface of the intersecting groove structure (30) and the There is a second rotation gap between the inner wall surfaces of the cylinder liner (20), and the range of the second rotation gap is 0.005mm-0.1mm.
The fluid machine according to any one of claims 1-9, wherein the range of the first included angle A is 160°-200°; the range of the second included angle B is 80°-100°.
The fluid machine according to any one of claims 1-10, further comprising a flange (50), the flange (50) is arranged at the axial end of the cylinder liner (20), and the crankshaft ( 10) Set concentrically with the flange (50).
The fluid machine according to claim 11, wherein there is a first assembly gap between the crankshaft (10) and the flange (50), and the range of the first assembly gap is 0.005mm-0.05mm.
The fluid machine according to claim 12, wherein the first assembly gap ranges from 0.01 to 0.03 mm.
The fluid machine according to any one of claims 1-13, wherein the eccentric portion (11) has an arc surface, and the central angle of the arc surface is greater than or equal to 180 degrees.
The fluid machine according to any one of claims 1-14, wherein the eccentric portion (11) is cylindrical.
The fluid machine according to claim 15, wherein the proximal end of the eccentric portion (11) is arranged as one of the following:

The proximal end of the eccentric portion (11) is flush with the outer circle of the shaft portion (12) of the crankshaft (10);

The proximal end of the eccentric portion (11) protrudes from the outer circle of the shaft portion (12) of the crankshaft (10);

The proximal end of the eccentric portion (11) is located inside the outer circle of the shaft portion (12) of the crankshaft (10).
The fluid machine according to any one of claims 1-16, wherein the slider (40) comprises a plurality of sub-sliders, and the plurality of sub-sliders form the through hole (41) after splicing.
The fluid machine according to any one of claims 1-17-, wherein the two eccentric portions (11) are arranged at intervals in the axial direction of the crankshaft (10).
The fluid machine according to any one of claims 1-18, wherein the intersecting groove structure (30) has a central hole (32), and the two limiting passages (31) pass through the central hole (32) In communication, the diameter of the central hole (32) is greater than the diameter of the shaft portion (12) of the crankshaft (10).
The fluid machine according to claim 19, wherein the diameter of the central hole (32) is larger than the diameter of the eccentric portion (11).
The fluid machine according to any one of claims 1-20, wherein the axial projection of the slider (40) on the through hole (41) has two relatively parallel straight line segments and connecting the two The arc segment at the end of the straight line segment.
The fluid machine according to any one of claims 1-21, wherein the limiting passage (31) has a set of oppositely disposed first sliding surfaces in sliding contact with the slider (40), the The slider (40) has a second sliding surface matched with the first sliding surface, the slider (40) has a pressing surface (42) facing the end of the limiting channel (31), The extrusion surface (42) serves as the head of the slider (40), the two second sliding surfaces are connected through the extrusion surface (42), and the extrusion surface (42) faces the Describe variable volume cavity (311).
The fluid machine according to claim 22, wherein the extrusion surface (42) is an arc surface, and the distance between the arc center of the arc surface and the center of the through hole (41) is equal to the eccentric portion ( 11) The amount of eccentricity.
The fluid machine according to claim 23, wherein:

The radius of curvature of the arc surface is equal to the radius of the inner circle of the cylinder liner (20); or

There is a difference between the radius of curvature of the arc surface and the radius of the inner circle of the cylinder liner (20), and the range of the difference is -0.05mm˜0.025mm.
The fluid machine according to claim 24, wherein said difference ranges from -0.02 to 0.02mm.
The fluid machine according to any one of claims 22-25, wherein the projected area S of the extrusion surface (42) in the sliding direction of the slider (40) and the cylinder liner (20) The range of the ratio S slide block /S row between the area S rows of the compression exhaust ports (22) is 8-25.
The fluid machine according to claim 26, wherein the ratio S slider /S row ranges from 12 to 18.
The fluid machine according to any one of claims 1-27, wherein the cylinder liner (20) has a compressed air inlet (21) and a compressed air outlet (22);

When any one of the sliders (40) is at the air intake position, the compression air inlet (21) is connected to the corresponding variable volume chamber (311);

When any one of the sliders (40) is in the exhaust position, the corresponding variable volume cavity (311) is in communication with the compression exhaust port (22).
The fluid machine according to claim 28, wherein the inner wall of the cylinder liner (20) has an air suction chamber (23), and the air suction chamber (23) communicates with the compressed air inlet (21).
The fluid machine according to claim 29, wherein the suction cavity (23) extends a first preset distance around the inner wall surface of the cylinder liner (20) to form an arc-shaped suction cavity (23) .
The fluid machine according to claim 29 or 30, wherein two said suction cavities (23) are arranged at intervals along the axial direction of said cylinder liner (20), and said cylinder liner (20) also has a suction communication cavity (24), both of the suction chambers (23) communicate with the suction communication chamber (24), and the compressed air inlet (21) communicates with the suction communication chamber (24) The suction cavity (23) is connected.
The fluid machine according to claim 31, wherein the suction communication cavity (24) extends a second preset distance along the axial direction of the cylinder liner (20), and at least one end of the suction communication cavity (24) Through the axial end surface of the cylinder liner (20).
The fluid machine according to any one of claims 28-32, wherein an exhaust chamber (25) is opened on the outer wall of the cylinder liner (20), and the compression exhaust port (22) is controlled by the cylinder liner The inner wall of (20) communicates with the exhaust cavity (25), the fluid machine also includes an exhaust valve assembly (60), and the exhaust valve assembly (60) is arranged in the exhaust cavity (25) Inside and set corresponding to the compression exhaust port (22).
The fluid machine according to claim 33, wherein the two compression exhaust ports (22) are arranged at intervals along the axial direction of the cylinder liner (20), and the exhaust valve assemblies (60) are in two groups, two A set of exhaust valve assemblies (60) is set corresponding to the two compression exhaust ports (22).
The fluid machine according to claim 34, wherein a communication hole (26) is further provided on the axial end surface of the cylinder liner (20), and the communication hole (26) communicates with the exhaust chamber (25), The fluid machine also includes a flange (50), an exhaust passage (51) is arranged on the flange (50), and the communication hole (26) communicates with the exhaust passage (51).
The fluid machine according to any one of claims 33-35, wherein the exhaust cavity (25) penetrates to the outer wall surface of the cylinder liner (20), and the fluid machine further includes an exhaust cover plate (70 ), the exhaust cover plate (70) is connected with the cylinder liner (20) and seals the exhaust chamber (25).
The fluid machine according to any one of claims 28 to 36, wherein the fluid machine is a compressor.
The fluid machine according to any one of claims 1-27, wherein the cylinder liner (20) has an expansion exhaust port and an expansion intake port;

When any of the sliders (40) is at the intake position, the expansion exhaust port is connected to the corresponding variable volume cavity (311);

When any one of the sliders (40) is in the exhaust position, the corresponding variable volume chamber (311) communicates with the expansion inlet.
The fluid machine according to claim 38, wherein the inner wall of the cylinder liner (20) has an expansion exhaust cavity, and the expansion exhaust cavity communicates with the expansion exhaust port.
The fluid machine according to claim 38 or 39, wherein the expansion exhaust cavity extends a first preset distance around the inner wall surface of the cylinder liner (20) to form an arc-shaped expansion exhaust cavity, and The expansion exhaust cavity extends from the expansion exhaust port to the side where the expansion air intake is located, and the extension direction of the expansion exhaust cavity is in the same direction as the rotation direction of the intersecting groove structure (30).
The fluid machine according to claim 40, wherein two expansion exhaust chambers are arranged at intervals along the axial direction of the cylinder liner (20), and the cylinder liner (20) also has an expansion exhaust communication cavity, two The inflation and exhaust chambers are all in communication with the inflation and exhaust communication chambers, and the expansion and exhaust ports are in communication with the inflation and exhaust chambers through the inflation and exhaust communication chambers.
The fluid machine according to claim 41, wherein the expansion exhaust communication cavity extends a second preset distance in the axial direction of the cylinder liner (20), and at least one end of the expansion exhaust communication cavity passes through the cylinder The axial end face of the sleeve (20).
A fluid machine according to any one of claims 38 to 42, wherein the fluid machine is an expander.
A heat exchange device, including a fluid machine, wherein the fluid machine is the fluid machine according to any one of claims 1-43.
A method for operating a fluid machine, comprising:

Crankshaft (10) rotates around the axis O of said crankshaft (10);

The intersecting groove structure (30) revolves around the axis O 0 of the crankshaft (10), the axis O 0 of the crankshaft (10) is eccentrically arranged with the axis O 1 of the intersecting groove structure (30), and the eccentric distance fixed;

The first slide block (40) moves in a circle with the shaft center O0 of the crankshaft (10), and the center O3 of the first slide block (40) is aligned with the axis of the crankshaft (10) The distance between the center O 0 is equal to the eccentricity of the first eccentric portion (11) corresponding to the crankshaft (10), and the eccentricity is equal to the axis O 0 of the crankshaft (10) and the intersecting groove The eccentric distance between the axis O1 of the structure (30), the crankshaft (10) rotates to drive the first slider (40) to do circular motion, and the first slider (40) and The intersecting groove structure (30) interacts and slides reciprocally in the limiting channel (31) of the intersecting groove structure (30);

The second slide block (40) takes the axis O of the crankshaft (10) as the center to do circular motion, and the center O of the second slide block ( 40 ) is aligned with the axis of the crankshaft (10). The distance between the center O 0 is equal to the eccentricity of the second eccentric portion (11) corresponding to the crankshaft (10), and the eccentricity is equal to the axis O 0 of the crankshaft (10) and the intersecting groove The eccentric distance between the axis O1 of the structure (30), the crankshaft (10) rotates to drive the second slider (40) to do circular motion, and the second slider (40) and The intersecting groove structure (30) interacts and slides reciprocally in the limiting channel (31) of the intersecting groove structure (30).
The operation method according to claim 45, wherein the two eccentric parts (11) of the crankshaft (10) serve as the first connecting rod L 1 and the second connecting rod L 2 respectively, and the cross groove structure (30) The two limiting passages (31) serve as the third link L 3 and the fourth link L 4 respectively, and the lengths of the first link L 1 and the second link L 2 are equal.
The operation method according to claim 46, wherein there is a first angle A between the first link L1 and the second link L2 , and the third link L3 and the fourth There is a second included angle B between the connecting rods L 4 , wherein the first included angle A is twice the second included angle B.
The operating method according to claim 47, wherein the line connecting the axis O 0 of the crankshaft (10) and the axis O 1 of the intersecting groove structure (30) is the line O 0 O 1 ,

There is a third included angle C between the first connecting rod L 1 and the connecting line O 0 O 1 , and a fourth angle C between the corresponding third connecting rod L 3 and the connecting line O 0 O 1 An included angle D, wherein the third included angle C is twice the fourth included angle D;

There is a fifth included angle E between the second connecting rod L 2 and the connecting line O 0 O 1 , and a sixth included angle E between the corresponding fourth connecting rod L 4 and the connecting line O 0 O 1 An included angle F, wherein the fifth included angle E is twice the sixth included angle F;

The sum of the third included angle C and the fifth included angle E is the first included angle A, and the sum of the fourth included angle D and the sixth included angle F is the second included angle b.
The operating method according to any one of claims 45-48, further comprising:

The angular velocity of rotation of the slider (40) relative to the eccentric portion (11) is the same as the angular velocity of revolution of the slider (40) around the axis O of the crankshaft ( 10 );

The revolution angular velocity of the intersecting groove structure (30) around the axis O0 of the crankshaft (10) is the same as the rotation angular velocity of the slider (40) relative to the eccentric portion (11).
The operating method according to any one of claims 45-49, wherein during the rotation of the crankshaft (10), the crankshaft (10) rotates 2 times to complete 4 suction and exhaust processes.