WO2023207934A1 - Vortex compression mechanism, and vortex compressor comprising same - Google Patents

Vortex compression mechanism, and vortex compressor comprising same Download PDF

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Publication number
WO2023207934A1
WO2023207934A1 PCT/CN2023/090467 CN2023090467W WO2023207934A1 WO 2023207934 A1 WO2023207934 A1 WO 2023207934A1 CN 2023090467 W CN2023090467 W CN 2023090467W WO 2023207934 A1 WO2023207934 A1 WO 2023207934A1
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WO
WIPO (PCT)
Prior art keywords
scroll
head section
exhaust
orbiting scroll
compression mechanism
Prior art date
Application number
PCT/CN2023/090467
Other languages
French (fr)
Chinese (zh)
Inventor
梁计
钱源
Original Assignee
谷轮环境科技(苏州)有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from CN202220969524.1U external-priority patent/CN217152298U/en
Priority claimed from CN202210439484.4A external-priority patent/CN116988971A/en
Application filed by 谷轮环境科技(苏州)有限公司 filed Critical 谷轮环境科技(苏州)有限公司
Publication of WO2023207934A1 publication Critical patent/WO2023207934A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00

Definitions

  • the present disclosure relates to the field of scroll compressors, and more specifically, to a scroll compression mechanism and a scroll compressor including the same.
  • a scroll compressor can be used in refrigeration systems, air conditioning systems and heat pump systems, for example.
  • a scroll compressor includes a scroll compression mechanism (also simply referred to as a "compression mechanism") for compressing a working fluid.
  • the compression mechanism includes fixed scroll and orbiting scroll.
  • the fixed scroll and the orbiting scroll are engaged to define a series of cavities that move from the radially outer side to the radially inner side and gradually become smaller in volume, including a suction chamber for sucking fluid, a compression chamber, and a cavity connected to the exhaust port for discharge. Exhaust chamber for compressed fluid.
  • An object of the present disclosure is to provide an improved scroll compression mechanism and scroll compressor that can reduce power loss and improve exhaust efficiency.
  • Another object of the present disclosure is to provide an improved scroll compression mechanism and scroll compressor that can avoid power loss due to excessive compression and can simultaneously Reduce or eliminate pressure sudden changes during the exhaust process.
  • Another object of the present disclosure is to provide an improved scroll compression mechanism and scroll compressor that can ensure the strength of the scroll and improve the scroll.
  • the scroll compression mechanism and the scroll compressor have a simple structure, are easy to implement, and are highly cost-effective.
  • a scroll compression mechanism including:
  • the fixed scroll including a fixed scroll end plate and a fixed scroll wrap extending from one side of the fixed scroll end plate;
  • An orbiting scroll the orbiting scroll includes an orbiting scroll end plate and an orbiting scroll wrap extending from one side of the orbiting scroll end plate,
  • the fixed scroll is engaged with the orbiting scroll to define therebetween an open suction chamber, at least one closed compression chamber, and a discharge chamber at the center, arranged in sequence from radially outward to radially inward,
  • the fixed scroll end plate includes an exhaust port in fluid communication with the exhaust chamber and at least one exhaust valve port in fluid communication with the compression chamber for early exhaust,
  • the orbiting scroll wrap includes an orbiting scroll head section
  • the fixed scroll wrap includes a fixed scroll head section
  • the orbiting scroll head section and the fixed scroll head section define The exhaust chamber in the following state: the exhaust chamber is about to be in fluid communication with the compression chamber but is not yet in fluid communication with the compression chamber, and is provided on the inner wall of the orbiting scroll head section
  • the orbiting scroll head section is configured to prevent passage through the at least one exhaust valve port by covering at least a portion of the at least one exhaust valve port with a top surface of the orbiting scroll head section during operation.
  • the compression chamber is in fluid communication with the exhaust chamber.
  • the scroll compression mechanism and the scroll compressor can reduce power loss and improve exhaust efficiency. Moreover, the scroll compression mechanism and scroll compressor can avoid power loss caused by excessive compression and can simultaneously alleviate or eliminate pressure sudden changes during the exhaust process.
  • At least a portion of the guide groove extends to a top surface of the orbiting scroll head section.
  • the guide groove is positioned at a predetermined distance from a top surface of the orbiting scroll head section.
  • the flow guide groove is arranged to be smaller than the distance from the moving vortex vortex.
  • the distance between the wrap and the root of the orbiting scroll end plate is closer to the top surface of the orbiting scroll head section. This will help improve the strength of the scroll root.
  • the guide groove is arranged to extend a predetermined distance toward the inner end of the orbiting scroll head section from a starting point: the starting point is the orbiting scroll head section The position of the segment that is engaged with the fixed scroll head section and is about to begin to disengage from the fixed scroll head section.
  • the guide groove is configured to have different recessed depths at different positions and has a maximum recessed depth at the starting point.
  • the extension height of the guide groove in the axial direction of the scroll compression mechanism is less than or equal to 2/3 of the axial height of the orbiting scroll wrap to ensure that the wrap is strength.
  • the recessed depth of the guide groove is less than or equal to 7/8 of the thickness of the corresponding section of the movable scroll head section to ensure the strength of the scroll.
  • the thickness of the portion of the orbiting scroll head section where the guide groove is provided is greater than or equal to 0.5 mm.
  • the flow channel is configured to include at least one section. In order to avoid undesirable early mixing of the compressed fluid while improving the exhaust gas flow efficiency.
  • a scroll compressor including the scroll compression mechanism as described above.
  • the scroll compression mechanism and scroll compressor according to the present disclosure at least provide the following beneficial effects: the scroll compression mechanism and scroll compressor according to the present disclosure can reduce power loss and improve exhaust efficiency, and can avoid The power loss caused by excessive compression can simultaneously alleviate or eliminate the pressure sudden change during the exhaust process, while ensuring the strength of the scroll, improving the scroll, and has a simple structure, easy to implement, and high cost. benefit.
  • FIG. 1 shows a schematic longitudinal cross-sectional view of a scroll compressor according to a first embodiment of the present disclosure
  • Figure 2a shows an exploded view of the scroll compression mechanism of the scroll compressor in Figure 1;
  • Figure 2b shows a perspective view of the fixed scroll in Figure 2a
  • Figure 2c shows a perspective view of the orbiting scroll in Figure 2a
  • Figure 2d shows a side view of the assembled state of the scroll compression mechanism in Figure 2a and its corresponding K-K cross-sectional view
  • Figure 2e shows a schematic diagram of the change process of the exhaust chamber defined by the orbiting scroll wrap and the fixed scroll wrap during the exhaust period of the scroll compressor;
  • FIG. 3 a shows a perspective view of an orbiting scroll in a scroll compression mechanism according to a second embodiment of the present disclosure, showing a first side of the orbiting scroll;
  • Figure 3b shows a side view of the assembled state of the scroll compression mechanism according to the second embodiment of the present disclosure and its corresponding M-M cross-sectional view
  • Figure 3c shows a side view of the assembled state of the scroll compression mechanism according to the second embodiment of the present disclosure and its corresponding L-L cross-sectional view.
  • a vertical scroll compressor is taken as an example for convenience of description.
  • the scroll compressor according to the present disclosure may also be any other suitable type of scroll compressor, such as a horizontal scroll compressor.
  • Figures 1 to 2e illustrate a first embodiment according to the present disclosure. The first embodiment will be described in detail below with reference to Figures 1 to 2e.
  • the scroll compressor 100 may include a casing 10 , an electric motor (including a stator 14 and a rotor 15 ), a drive shaft 16 , a main bearing seat 18 , an orbiting scroll 24 , and a fixed scroll 22 .
  • the orbiting scroll 24 and the fixed scroll 22 constitute a scroll compression mechanism (hereinafter also referred to as "compression mechanism") CM suitable for compressing a working fluid (eg refrigerant), as better shown in Figures 2a and 2b , wherein the fixed scroll 22 includes the fixed scroll end plate 221, the fixed scroll wrap 222 and the exhaust port V located at the center of the fixed scroll end plate 221; the movable scroll 24 includes the movable scroll end plate 241, the movable scroll end plate 241 and the movable scroll end plate 241.
  • a working fluid eg refrigerant
  • the scroll wrap 242 and the hub 240 are joined by the fixed scroll wrap 222 and the movable scroll wrap 242 to define an air inlet to the compression mechanism CM in sequence from the radially outer side to the radially inner side in the compression mechanism CM (in the figure) (not shown) an open suction chamber in fluid communication for use in At least one closed compression chamber for fluid compression and an open exhaust chamber E in fluid communication with the exhaust port V (see Figure 2d and Figure 2e).
  • the pressure of the radially inner compression chamber is higher than that of the radially outer compression chamber.
  • the compression chamber adjacent to the exhaust chamber E is called the high-pressure chamber H.
  • the exhaust chamber E in this article refers to the area defined by the fixed scroll wrap 222 and the orbiting scroll wrap 242 that is about to be fluidly connected to the high-pressure chamber H—that is, currently A cavity that is only fluidly connected to the exhaust port V is formed at the critical moment when the exhaust is finished and the next exhaust is about to occur but is not yet in fluid communication with the high-pressure chamber H.
  • the exhaust chamber E will be described in detail below in conjunction with the "starting point A".
  • the electric motor includes a stator 14 and a rotor 15 .
  • the rotor 15 is used to drive the drive shaft 16 to rotate about its rotation axis relative to the housing 10 .
  • the fixed scroll 22 is fixed to the main bearing seat 18 and held in place, and the movable scroll 24 is driven by an electric motor via the drive shaft 16 so as to be able to perform translational rotation relative to the fixed scroll 22 by means of an Oldham slip ring 17 - —that is, orbiting (that is, the axis of the orbiting scroll 24 revolves relative to the axis of the fixed scroll 22, but both the orbiting scroll 24 and the fixed scroll 22 themselves do not rotate around their respective axes).
  • the air inlet of the compression mechanism CM sucks in low-pressure fluid and compresses the fluid through a series of closed compression chambers, and then enters the exhaust chamber E and discharges the high-pressure fluid through the exhaust port V.
  • a pair of high-pressure chambers H are defined in the compression mechanism CM, and the two high-pressure chambers H are adjacent to the radially central exhaust chamber E.
  • the exhaust chamber E The current exhaust process in the chamber is over, and it will be fluidly connected to the two high-pressure chambers H for the next exhaust process.
  • the fluid can flow from the two high-pressure chambers H into the exhaust chamber E, the fluid is discharged through the exhaust port V as the orbiting scroll 24 rotates. After the fluid in the high-pressure chamber H is discharged, the compression chamber radially outside the high-pressure chamber H will be connected to the exhaust chamber E for the next exhaust process.
  • the inventor of the present application has studied the entire flow process of fluid in the scroll compression mechanism and found significant pressure changes of the fluid. For example, under certain working conditions, the fluid is compressed to a pressure higher than the required pressure. In addition, , a sudden change in pressure will occur when transitioning from one exhaust process to another. Based on these findings, the inventor of the present application proposed a solution that can simultaneously solve the power loss caused by these pressure changes.
  • the required discharge gas pressure may be less than the designed discharge pressure (ie, the designed fluid pressure discharged through the exhaust port V).
  • the designed discharge pressure ie, the designed fluid pressure discharged through the exhaust port V.
  • the fixed scroll end plate 221 may include at least one located near the exhaust chamber E, preferably but not limited to, in fluid communication with the high-pressure chamber H (see FIG. 2d ).
  • An exhaust valve port P (see Figure 2b).
  • the exhaust valve port P can preferably be closed by a valve such as an electronic valve and opened under certain conditions (such as a predetermined pressure) to discharge the fluid in the high-pressure chamber H to the exhaust port in advance before entering the exhaust chamber E. V, thus avoiding unnecessary further compression of the fluid.
  • Multiple exhaust valve ports P may preferably be provided to communicate the two high-pressure chambers H to the exhaust chamber respectively. For example, as shown in FIG. 2b, four exhaust valve ports P are provided on radially opposite sides of the exhaust port V respectively.
  • the orbiting scroll wrap 242 includes an orbiting scroll head section 246
  • the fixed scroll wrap 222 includes a fixed scroll head section 226
  • the orbiting scroll head section 246 and The fixed scroll head section 226 jointly defines the above-mentioned exhaust chamber E - that is, the critical moment when the current exhaust is over and the next exhaust is about to start but is not yet in fluid communication with the high-pressure chamber H and is only connected to the exhaust port V. Fluidically connected cavities.
  • the movable scroll head section 246 is joined to the fixed scroll head section 226 at the starting point A
  • the fixed scroll head section 226 is joined to the movable scroll head section 246 at point B.
  • the orbiting scroll head section 246 is defined as the section from the starting point A to the terminal end (ie, the radially inner end), and the fixed scroll head section 226 is defined as the section from B point to the terminal end (i.e., the radially inner end), and both define the exhaust chamber E.
  • FIG. 2e shows a schematic diagram of the changing stages of the exhaust chamber E defined by the movable scroll head section 246 and the fixed scroll head section 226 during the discharge of the scroll compressor 100, in which the movable scroll head section 246 and the fixed scroll head section 226 are shown.
  • the scroll head section 246 has a second configuration with guide grooves 2460 and a first configuration without guide grooves. It should be noted that the guide grooves 2460 in Figure 2e are only schematic. The actual shape and size of the guide groove 2460 are not specifically depicted.
  • the orbiting scroll head section 246 and the fixed scroll head section 226 are engaged with each other to define the exhaust chamber E, at which time the "first stage”"stage” refers to the critical stage before starting exhaust.
  • the movable scroll head section 246 is in contact with the fixed scroll head section at the starting point A.
  • Section 226 is engaged, and then enters the "second stage” - that is, the exhaust stage begins.
  • the movable scroll head section 246 begins to disengage from the fixed scroll head section 226 at the starting point A, As a result, the fluid starts to flow from the high-pressure chamber H into the exhaust chamber E (as shown by the arrow in the figure), and exhaust begins.
  • the inner wall of the orbiting scroll head section 246 facing the exhaust chamber E can be A guide groove 2460 is provided on 2466 to accelerate the flow of fluid from the high-pressure chamber H into the exhaust chamber E, thereby improving the exhaust efficiency and the working efficiency of the scroll compressor 100 .
  • the guide groove 2460 by providing the guide groove 2460, the gap between the movable scroll head section 246 and the fixed scroll head section 226 can be significantly expanded, thereby improving the Exhaust efficiency.
  • the scroll compression mechanism takes into account the technical problems of over-compression and sudden pressure changes during fluid travel, thereby significantly reducing power loss and thereby improving the efficiency of the scroll compressor.
  • the setting of the exhaust valve port P will limit the structural improvement of the scroll wrap (especially the orbiting scroll wrap), because it often causes fluid leakage between adjacent cavities or a reduction in the strength of the scroll, etc.
  • the inventor of the present application has proposed a solution that combines the exhaust valve port P with the improvement of the scroll. While optimizing the exhaust passage, the communication between the scroll compression chamber (especially the high-pressure chamber) and the exhaust chamber is eliminated.
  • the guide groove 2460 is arranged to extend from the above-mentioned starting point A—that is, the starting point A is between the tip section 2260 of the fixed scroll head section 226 and the movable scroll head section 246
  • the position on the orbiting scroll head section 246 that is in contact with the tip section 2260 is therefore in the stage where exhaust is just beginning—that is, the above-mentioned second stage, and the third stage—that is, , the exhaust stage when the gap is further expanded, can effectively accelerate the flow of fluid from the high-pressure chamber H into the exhaust chamber E.
  • the slight section 2260 of the fixed scroll head section 226 only refers to a section of the fixed scroll head section 226 close to the terminal end in this article, and is not intended to specifically refer to the terminal end, that is, , the tip section 2260 that joins point A of the orbiting scroll head section 246 may preferably be its terminal end point, or it may be a certain position in the section at a certain distance from the terminal end point, although in this article
  • the portion that engages the starting point A of the orbiting scroll head section 246 is preferably the fixed scroll head section. 226 terminal endpoint, but it should be understood that there is no particular restriction on this.
  • the orbiting scroll head section 246 includes the guide groove 2460, the orbiting scroll
  • the axial top surface 247 of the head section 246 is narrowed, so there may be the following technical problems when the movable scroll 24 and the fixed scroll 22 abut each other to perform a compression operation: the movable scroll head section 246 At a certain moment, the top surface 247 cannot properly cover the exhaust valve port P and the exhaust valve port P spans both sides of the movable scroll head section 246 to fluidly communicate the spaces on both sides, thereby making it possible This results in a reduction in compression efficiency, which is undesirable.
  • the present disclosure improves the configuration of the guide groove 2460.
  • the guide groove 2460 according to the present disclosure is configured to enable the top surface 247 of the orbiting scroll head section 246 to operate During this period, the exhaust valve ports P are covered so that each exhaust valve port P does not, for example, span both sides of the movable scroll head section 246 and fluidly communicate the spaces on both sides.
  • the guide groove 2460 is preferably provided to extend to the top surface 247 of the orbiting scroll head section 246, and is preferably provided in two sections, That is, the guide groove 2460 includes a first groove section 2461 and a second groove section 2462 that are spaced apart from each other. That is, there is unremoved material included between the first groove section 2461 and the second groove section 2462. spacer section 2463.
  • the guide groove 2460 still preferably extends from the above-mentioned starting point A, that is, the first groove section 2461 starts from the starting point A, so as to better accelerate the exhaust, and more preferably, the first groove section 2461 extends from the starting point A.
  • a groove section 2461 has a relatively larger recessed depth at the starting point A - that is, a depth recessed into the orbiting scroll head section 246 along the normal direction of the tangent plane of the inner wall 2466, so that it can be formed at the starting point A.
  • Starting point A that is, when exhaust is just beginning, the fluid is accelerated into the exhaust chamber E more quickly.
  • the guide groove 2460 is preferably configured to have different recessed depths at different locations, preferably with a maximum recessed depth near the starting point A.
  • the recessed depth of the guide groove 2460 is less than or equal to 7/8 of the thickness of the orbiting scroll head section 246, that is, the portion of the orbiting scroll head section 246 including the guide groove 2460 - That is, the thickness of the remaining portion after the material is removed should be no less than 1/8 of its original thickness, and more preferably, the portion of the orbiting scroll head section 246 including the guide groove 2460 - that is, The thickness of the remaining part after the material is removed is greater than or equal to 0.5mm, thereby ensuring that the part has the required strength.
  • the extension height of the guide groove 2460 in the axial direction of the scroll compression mechanism CM is less than or equal to 2/3 of the total axial height of the orbiting scroll wrap 246 to ensure required strength.
  • the guide groove 2460 is disposed closer to the top surface 247 of the orbiting scroll head section 246 as a whole.
  • the root of the orbiting scroll end plate 241 is connected to the root of the orbiting scroll head section 246 away from the orbiting scroll head section 246 to ensure the strength of the orbiting scroll head section 246 .
  • the second groove section 2462 preferably extends to the terminal end of the orbiting scroll head section 246 to better accelerate the fluid throughout the exhaust process. flows into the exhaust chamber E.
  • the present disclosure is not limited thereto. That is to say, the length (radius) of the guide groove 2460 extending along the profile direction of the orbiting scroll head section 246 can be set according to actual needs in order to achieve optimized exhaust gas. This effect ensures good coverage of the exhaust valve port P and ensures the strength of the scroll.
  • the spacing section 2463 its position and size can be set according to the actual situation - for example, the position and size of the exhaust valve port P, the strength requirements of the scroll part including the guide groove 2460, etc.
  • the purpose is to: First, by providing the spacer section 2463, the exhaust valve port P can be better covered to improve compression efficiency; at the same time, the spacer section 2463 is conducive to further improving the strength of the scroll part including the guide groove 2460, especially It is beneficial to reduce the stress concentration at the connection root between the guide groove 2460 and the remaining scroll parts and the stress concentration at the connection root between the orbiting scroll head section 246 and the orbiting scroll end plate 241 .
  • the recessed depth at various positions of the guide groove 2460 can be flexibly set according to the position and size of the exhaust valve port P, for example, Figure 2d
  • the first groove section 2461 and the second groove section 2462 each have different recessed depths at different locations; similarly, although the guide groove 2460 has a consistent axial height in this embodiment,
  • the present disclosure is not limited thereto.
  • the guide groove 2460 can be flexibly arranged to have different axial heights at different positions, and it is understood that the guide groove 2460 can also be arranged on the axis. It is upwardly multi-segmented, ie it includes a plurality of groove sections spaced apart in the axial direction.
  • the guide groove 2460 is provided in two sections in the above embodiment, that is, including a first groove section 2461 and a second groove section 2462 spaced apart from each other, the present disclosure is not limited thereto, and it should be understood that Yes, in some cases, the guide groove 2460 can also be configured to include more sections—for example, three sections, four sections, etc., or it can be configured as a continuous single section at different locations. It has different recessed depths, as long as it can ensure good coverage of the exhaust valve port P. Moreover, according to actual conditions, the guide groove 2460 may have any suitable shape, and there is no particular limitation on this.
  • FIG. 3a shows a perspective view of the orbiting scroll 24 in the scroll compression mechanism CM according to the second embodiment of the present disclosure
  • FIG. 3b shows the assembled state of the scroll compression mechanism CM according to the second embodiment of the present disclosure
  • 3c shows a side view of the scroll compression mechanism CM and its corresponding LL cross-sectional view in an assembled state according to the second embodiment of the present disclosure.
  • the guide groove 2460 is provided in the form of a continuous single groove section, and as previously mentioned, the guide groove 2460 also preferably extends from the starting point A in this embodiment. , the difference is that the guide groove 2460 is configured not to extend to the top surface 247 of the orbiting scroll head section 246, so as not to occupy the area of the top surface 247.
  • FIG. 3b shows a cross-sectional view taken at the MM section closer to the orbiting scroll end plate 241, which shows the guide groove 2460;
  • FIG. 3c shows a cross-section closer to the orbiting scroll wrap 242.
  • the guide groove 2460 in this embodiment can also be configured in a two-section or more-section configuration similar to that in the first embodiment. The only difference lies in the guide groove 2460 in this embodiment.
  • the flow channels 2460 do not extend to the top surface 247 of the orbiting scroll head section 246 .
  • the present disclosure also provides a scroll compressor 100.
  • the scroll compressor 100 includes a scroll compression mechanism CM according to the present disclosure.
  • the scroll compression mechanism CM may be, for example, the scroll compression mechanism CM in the above embodiment. Or there could be other possible variations.

Abstract

A vortex compression mechanism and a vortex compressor comprising same. The vortex compression mechanism comprises a fixed vortex (22) and a moving vortex (24). A moving vortex head section (246) and a fixed vortex head section (226) define an exhaust cavity (E) in the following state: the exhaust cavity (E) is in a state of being about to be in fluid communication with a compression cavity but is not in fluid communication with the compression cavity. Concave flow guide grooves (2460) are provided on the inner wall of the moving vortex head section (246), so as to increase the flow of fluid from the compression cavity into the exhaust cavity (E) when the moving vortex head section (246) and the fixed vortex head section (226) are separated. The moving vortex head section (246) is configured to cover at least a portion of the at least one exhaust valve port (P) by the top surface (247) of the moving vortex head section (246) during operation, so as to prevent fluid communication between the compression cavity and the exhaust cavity (E) via the at least one exhaust valve port (P). The compression mechanism and the vortex compressor can reduce the power loss, improve the exhaust efficiency, prevent excessive compression, relieve or eliminate sudden pressure changes in the exhaust process, and improve the vortex strength, and the structure is simple and the cost benefit is high.

Description

涡旋压缩机构和包括其的涡旋压缩机Scroll compression mechanism and scroll compressor including same
本申请要求以下中国专利申请的优先权:于2022年4月25日提交中国专利局的申请号为202210439484.4、发明创造名称为“涡旋压缩机构和包括其的涡旋压缩机”的中国专利申请;于2022年4月25日提交中国专利局的申请号为202220969524.1、发明创造名称为“涡旋压缩机构和包括其的涡旋压缩机”的中国专利申请。这些专利申请的全部内容通过引用结合在本申请中。This application claims priority to the following Chinese patent applications: a Chinese patent application with the application number 202210439484.4 and the invention name "Scroll compression mechanism and scroll compressor including the same" submitted to the China Patent Office on April 25, 2022. ; The Chinese patent application with the application number 202220969524.1 and the invention title "Scroll compression mechanism and scroll compressor including the same" was submitted to the China Patent Office on April 25, 2022. The entire contents of these patent applications are incorporated by reference into this application.
技术领域Technical field
本公开涉及涡旋压缩机领域,更具体地,涉及一种涡旋压缩机构和包括其的涡旋压缩机。The present disclosure relates to the field of scroll compressors, and more specifically, to a scroll compression mechanism and a scroll compressor including the same.
背景技术Background technique
本部分提供了与本公开相关的背景信息,这些信息并不必然构成现有技术。This section provides background information related to the present disclosure that may not necessarily constitute prior art.
涡旋压缩机可以应用于例如制冷系统、空调系统和热泵系统中。涡旋压缩机包括用于压缩工作流体的涡旋压缩机构(也简称为“压缩机构”)。压缩机构包括定涡旋和动涡旋。定涡旋和动涡旋接合以在其间限定从径向外侧向径向内侧运动且体积逐渐变小的一系列腔体,包括吸入流体的吸气腔、压缩腔和与排气口连通以便排出经压缩的流体的排气腔。Scroll compressors can be used in refrigeration systems, air conditioning systems and heat pump systems, for example. A scroll compressor includes a scroll compression mechanism (also simply referred to as a "compression mechanism") for compressing a working fluid. The compression mechanism includes fixed scroll and orbiting scroll. The fixed scroll and the orbiting scroll are engaged to define a series of cavities that move from the radially outer side to the radially inner side and gradually become smaller in volume, including a suction chamber for sucking fluid, a compression chamber, and a cavity connected to the exhaust port for discharge. Exhaust chamber for compressed fluid.
本领域技术人员一直致力于减小涡旋压缩机的功率损耗和/或提高排气效率的研究。Those skilled in the art have been committed to research on reducing the power loss of scroll compressors and/or improving exhaust efficiency.
发明内容Contents of the invention
在本部分中提供本公开的总体概要,而不是本公开完全范围或本公开所有特征的全面公开。This section provides a general summary of the disclosure and is not intended to be a comprehensive disclosure of the disclosure's full scope or all features of the disclosure.
本公开的一个目的是提供一种改进的涡旋压缩机构和涡旋压缩机,该涡旋压缩机构和涡旋压缩机能够减小功率损耗并且能够提高排气效率。An object of the present disclosure is to provide an improved scroll compression mechanism and scroll compressor that can reduce power loss and improve exhaust efficiency.
本公开的另一个目的是提供一种改进的涡旋压缩机构和涡旋压缩机,该涡旋压缩机构和涡旋压缩机能够避免因过度压缩而造成的功率损耗并且能够同时 缓解或消除排气过程中的压力突变的情况。Another object of the present disclosure is to provide an improved scroll compression mechanism and scroll compressor that can avoid power loss due to excessive compression and can simultaneously Reduce or eliminate pressure sudden changes during the exhaust process.
本公开的另一个目的是提供一种改进的涡旋压缩机构和涡旋压缩机,该涡旋压缩机构和涡旋压缩机能够确保涡卷的强度、改善涡卷。该涡旋压缩机构和涡旋压缩机具有简单的结构,易于实现,并且具有较高的成本效益。Another object of the present disclosure is to provide an improved scroll compression mechanism and scroll compressor that can ensure the strength of the scroll and improve the scroll. The scroll compression mechanism and the scroll compressor have a simple structure, are easy to implement, and are highly cost-effective.
根据本公开的一个方面,提供了一种涡旋压缩机构,包括:According to one aspect of the present disclosure, a scroll compression mechanism is provided, including:
定涡旋,所述定涡旋包括定涡旋端板和从所述定涡旋端板的一侧延伸的定涡旋涡卷;以及a fixed scroll, the fixed scroll including a fixed scroll end plate and a fixed scroll wrap extending from one side of the fixed scroll end plate; and
动涡旋,所述动涡旋包括动涡旋端板和从所述动涡旋端板的一侧延伸的动涡旋涡卷,An orbiting scroll, the orbiting scroll includes an orbiting scroll end plate and an orbiting scroll wrap extending from one side of the orbiting scroll end plate,
所述定涡旋与所述动涡旋接合以在其之间限定从径向外侧至径向内侧依次排列的开放的吸气腔、至少一个封闭的压缩腔以及中心处的排气腔,the fixed scroll is engaged with the orbiting scroll to define therebetween an open suction chamber, at least one closed compression chamber, and a discharge chamber at the center, arranged in sequence from radially outward to radially inward,
所述定涡旋端板包括与所述排气腔流体联通的排气口以及与所述压缩腔流体联通以提前排气的至少一个排气阀口,The fixed scroll end plate includes an exhaust port in fluid communication with the exhaust chamber and at least one exhaust valve port in fluid communication with the compression chamber for early exhaust,
所述动涡旋涡卷包括动涡卷头部部段,所述定涡旋涡卷包括定涡卷头部部段,所述动涡卷头部部段和所述定涡卷头部部段限定如下状态的所述排气腔:所述排气腔处于即将与所述压缩腔流体连通但仍未与所述压缩腔流体连通的状态,在所述动涡卷头部部段的内壁上设置有内凹的导流槽以在所述动涡卷头部部段和所述定涡卷头部部段分离时增加流体从所述压缩腔流入所述排气腔内的流量,The orbiting scroll wrap includes an orbiting scroll head section, the fixed scroll wrap includes a fixed scroll head section, and the orbiting scroll head section and the fixed scroll head section define The exhaust chamber in the following state: the exhaust chamber is about to be in fluid communication with the compression chamber but is not yet in fluid communication with the compression chamber, and is provided on the inner wall of the orbiting scroll head section There is a concave guide groove to increase the flow of fluid from the compression chamber into the exhaust chamber when the movable scroll head section and the fixed scroll head section are separated,
所述动涡卷头部部段构造成在操作期间通过所述动涡卷头部部段的顶表面覆盖所述至少一个排气阀口的至少一部分而防止经由所述至少一个排气阀口将所述压缩腔与所述排气腔流体连通。The orbiting scroll head section is configured to prevent passage through the at least one exhaust valve port by covering at least a portion of the at least one exhaust valve port with a top surface of the orbiting scroll head section during operation. The compression chamber is in fluid communication with the exhaust chamber.
由此,该涡旋压缩机构和涡旋压缩机能够减小功率损耗并且能够提高排气效率。并且该涡旋压缩机构和涡旋压缩机能够避免因过度压缩而造成的功率损耗并且能够同时缓解或消除排气过程中的压力突变的情况。Therefore, the scroll compression mechanism and the scroll compressor can reduce power loss and improve exhaust efficiency. Moreover, the scroll compression mechanism and scroll compressor can avoid power loss caused by excessive compression and can simultaneously alleviate or eliminate pressure sudden changes during the exhaust process.
根据本公开的一个实施方式,所述导流槽的至少一部分延伸至所述动涡卷头部部段的顶表面。According to one embodiment of the present disclosure, at least a portion of the guide groove extends to a top surface of the orbiting scroll head section.
根据本公开的一个实施方式,所述导流槽定位成与所述动涡卷头部部段的顶表面相距预定距离处。According to one embodiment of the present disclosure, the guide groove is positioned at a predetermined distance from a top surface of the orbiting scroll head section.
根据本公开的一个实施方式,所述导流槽设置为相比于距离所述动涡旋涡 卷的连接至所述动涡旋端板的根部的距离而更靠近所述动涡卷头部部段的顶表面。从而利于提高涡卷根部的强度。According to an embodiment of the present disclosure, the flow guide groove is arranged to be smaller than the distance from the moving vortex vortex. The distance between the wrap and the root of the orbiting scroll end plate is closer to the top surface of the orbiting scroll head section. This will help improve the strength of the scroll root.
根据本公开的一个实施方式,所述导流槽设置成从如下起始点开始朝向所述动涡卷头部部段的内端延伸预定距离:所述起始点是所述动涡卷头部部段的与所述定涡卷头部部段接合并且即将与所述定涡卷头部部段开始脱离接合的位置。According to an embodiment of the present disclosure, the guide groove is arranged to extend a predetermined distance toward the inner end of the orbiting scroll head section from a starting point: the starting point is the orbiting scroll head section The position of the segment that is engaged with the fixed scroll head section and is about to begin to disengage from the fixed scroll head section.
根据本公开的一个实施方式,所述导流槽构造成在不同位置处具有不同的凹入深度,并且在所述起始点处具有最大凹入深度。According to an embodiment of the present disclosure, the guide groove is configured to have different recessed depths at different positions and has a maximum recessed depth at the starting point.
根据本公开的一个实施方式,所述导流槽在所述涡旋压缩机构的轴向方向上的延伸高度小于等于所述动涡旋涡卷的轴向高度的2/3,以确保涡卷的强度。According to an embodiment of the present disclosure, the extension height of the guide groove in the axial direction of the scroll compression mechanism is less than or equal to 2/3 of the axial height of the orbiting scroll wrap to ensure that the wrap is strength.
根据本公开的一个实施方式,所述导流槽的凹入深度小于等于所述动涡卷头部部段的相应部段的厚度的7/8,以确保涡卷的强度。According to an embodiment of the present disclosure, the recessed depth of the guide groove is less than or equal to 7/8 of the thickness of the corresponding section of the movable scroll head section to ensure the strength of the scroll.
根据本公开的一个实施方式,所述动涡卷头部部段的设置有所述导流槽的部分的厚度大于等于0.5mm。According to an embodiment of the present disclosure, the thickness of the portion of the orbiting scroll head section where the guide groove is provided is greater than or equal to 0.5 mm.
根据本公开的一个实施方式,所述导流槽构造为包括至少一个部段。以便在提高排气流通效率的同时避免压缩流体的不期望的提前混合。According to one embodiment of the present disclosure, the flow channel is configured to include at least one section. In order to avoid undesirable early mixing of the compressed fluid while improving the exhaust gas flow efficiency.
根据本公开的另一方面,提供了一种涡旋压缩机,所述涡旋压缩机包括如前所述的涡旋压缩机构。According to another aspect of the present disclosure, a scroll compressor is provided, the scroll compressor including the scroll compression mechanism as described above.
综上可知,根据本公开的涡旋压缩机构和涡旋压缩机至少提供以下有益效果:根据本公开的涡旋压缩机构和涡旋压缩机能够减小功率损耗并且能够提高排气效率、能够避免因过度压缩而造成的功率损耗并且能够同时缓解或消除排气过程中的压力突变的情况,同时能够确保涡卷的强度、改善涡卷,并且具有简单的结构、易于实现,具有较高的成本效益。In summary, it can be seen that the scroll compression mechanism and scroll compressor according to the present disclosure at least provide the following beneficial effects: the scroll compression mechanism and scroll compressor according to the present disclosure can reduce power loss and improve exhaust efficiency, and can avoid The power loss caused by excessive compression can simultaneously alleviate or eliminate the pressure sudden change during the exhaust process, while ensuring the strength of the scroll, improving the scroll, and has a simple structure, easy to implement, and high cost. benefit.
附图说明Description of the drawings
根据以下参照附图的详细描述,本公开的前述及另外的特征和特点将变得更加清楚,这些附图仅作为示例并且不一定是按比例绘制。在附图中采用相同的附图标记指示相同的部件,在附图中:The foregoing and additional features and characteristics of the present disclosure will become more apparent from the following detailed description with reference to the accompanying drawings, which are by way of example only and are not necessarily drawn to scale. In the drawings, the same reference numbers refer to the same parts:
图1示出根据本公开的第一实施例的涡旋压缩机的示意性纵向截面图;1 shows a schematic longitudinal cross-sectional view of a scroll compressor according to a first embodiment of the present disclosure;
图2a示出图1中的涡旋压缩机的涡旋压缩机构的分解图; Figure 2a shows an exploded view of the scroll compression mechanism of the scroll compressor in Figure 1;
图2b示出图2a中的定涡旋的立体图;Figure 2b shows a perspective view of the fixed scroll in Figure 2a;
图2c示出图2a中的动涡旋的立体图;Figure 2c shows a perspective view of the orbiting scroll in Figure 2a;
图2d示出图2a中的涡旋压缩机构的组装状态的侧视图及其相应的K-K截面图;Figure 2d shows a side view of the assembled state of the scroll compression mechanism in Figure 2a and its corresponding K-K cross-sectional view;
图2e示出涡旋压缩机排气期间动涡旋涡卷与定涡旋涡卷限定的排气腔的变化过程示意图;Figure 2e shows a schematic diagram of the change process of the exhaust chamber defined by the orbiting scroll wrap and the fixed scroll wrap during the exhaust period of the scroll compressor;
图3a示出根据本公开的第二实施例的涡旋压缩机构中的动涡旋的立体图,其示出了动涡旋的第一侧面;3 a shows a perspective view of an orbiting scroll in a scroll compression mechanism according to a second embodiment of the present disclosure, showing a first side of the orbiting scroll;
图3b示出根据本公开的第二实施例的涡旋压缩机构的组装状态的侧视图及其相应的M-M截面图;以及Figure 3b shows a side view of the assembled state of the scroll compression mechanism according to the second embodiment of the present disclosure and its corresponding M-M cross-sectional view; and
图3c示出根据本公开的第二实施例的涡旋压缩机构的组装状态的侧视图及其相应的L-L截面图。Figure 3c shows a side view of the assembled state of the scroll compression mechanism according to the second embodiment of the present disclosure and its corresponding L-L cross-sectional view.
具体实施方式Detailed ways
现在将结合附图1-3c来对本公开的优选实施方式进行详细描述。以下的描述在本质上只是示例性的而非意在限制本公开及其应用或用途。Preferred embodiments of the present disclosure will now be described in detail with reference to Figures 1-3c. The following description is merely exemplary in nature and is not intended to limit the disclosure, its application or uses.
在下述示例性实施方式中,为了便于描述而以立式涡旋压缩机为示例。然而根据本公开的涡旋压缩机也可以是例如卧式涡旋压缩机等任何其他合适类型的涡旋压缩机。In the following exemplary embodiments, a vertical scroll compressor is taken as an example for convenience of description. However, the scroll compressor according to the present disclosure may also be any other suitable type of scroll compressor, such as a horizontal scroll compressor.
图1至图2e示出根据本公开的第一实施例。下面参照图1至图2e对第一实施例进行详细描述。Figures 1 to 2e illustrate a first embodiment according to the present disclosure. The first embodiment will be described in detail below with reference to Figures 1 to 2e.
如图1所示,涡旋压缩机100可以包括壳体10、电动马达(包括定子14和转子15)、驱动轴16、主轴承座18、动涡旋24、定涡旋22。动涡旋24和定涡旋22构成适于压缩工作流体(例如制冷剂)的涡旋压缩机构(下文也简称为“压缩机构”)CM,如图2a和图2b中更好地示出的,其中,定涡旋22包括定涡旋端板221、定涡旋涡卷222和位于定涡旋端板221的中心处的排气口V;动涡旋24包括动涡旋端板241、动涡旋涡卷242和毂部240,由定涡旋涡卷222与动涡旋涡卷242接合以在压缩机构CM内从径向外侧到径向内侧依次限定有与压缩机构CM的进气口(图中未示出)流体连通的开放的吸气腔、用于对工 作流体进行压缩的至少一个封闭的压缩腔、与排气口V流体连通的开放的排气腔E(参见图2d和图2e)。封闭的压缩腔可以为两个或更多个。径向内侧的压缩腔的压力高于径向外侧的压缩腔。本文中,为了便于描述,将邻近排气腔E的压缩腔称为高压腔H。特别地,关于排气腔E,需要说明的是,排气腔E在本文中是指由定涡旋涡卷222和动涡旋涡卷242限定的在即将与高压腔H流体连通——即,当前排气结束且即将下一次排气——但仍未与高压腔H流体连通的临界时刻形成的仅与排气口V流体连通的腔体。下文将结合“起始点A”来对排气腔E进行详细的描述。As shown in FIG. 1 , the scroll compressor 100 may include a casing 10 , an electric motor (including a stator 14 and a rotor 15 ), a drive shaft 16 , a main bearing seat 18 , an orbiting scroll 24 , and a fixed scroll 22 . The orbiting scroll 24 and the fixed scroll 22 constitute a scroll compression mechanism (hereinafter also referred to as "compression mechanism") CM suitable for compressing a working fluid (eg refrigerant), as better shown in Figures 2a and 2b , wherein the fixed scroll 22 includes the fixed scroll end plate 221, the fixed scroll wrap 222 and the exhaust port V located at the center of the fixed scroll end plate 221; the movable scroll 24 includes the movable scroll end plate 241, the movable scroll end plate 241 and the movable scroll end plate 241. The scroll wrap 242 and the hub 240 are joined by the fixed scroll wrap 222 and the movable scroll wrap 242 to define an air inlet to the compression mechanism CM in sequence from the radially outer side to the radially inner side in the compression mechanism CM (in the figure) (not shown) an open suction chamber in fluid communication for use in At least one closed compression chamber for fluid compression and an open exhaust chamber E in fluid communication with the exhaust port V (see Figure 2d and Figure 2e). There can be two or more closed compression chambers. The pressure of the radially inner compression chamber is higher than that of the radially outer compression chamber. In this article, for convenience of description, the compression chamber adjacent to the exhaust chamber E is called the high-pressure chamber H. In particular, regarding the exhaust chamber E, it should be noted that the exhaust chamber E in this article refers to the area defined by the fixed scroll wrap 222 and the orbiting scroll wrap 242 that is about to be fluidly connected to the high-pressure chamber H—that is, currently A cavity that is only fluidly connected to the exhaust port V is formed at the critical moment when the exhaust is finished and the next exhaust is about to occur but is not yet in fluid communication with the high-pressure chamber H. The exhaust chamber E will be described in detail below in conjunction with the "starting point A".
电动马达包括定子14和转子15。转子15用于对驱动轴16进行驱动以使驱动轴16绕其旋转轴线相对于壳体10旋转。定涡旋22固定至主轴承座18而被保持就位,动涡旋24经由驱动轴16通过电动马达而被驱动,从而借助十字滑环17而能够相对于定涡旋22进行平动转动——即绕动(亦即,动涡旋24的轴线相对于定涡旋22的轴线公转,但是动涡旋24和定涡旋22二者本身并未绕它们各自的轴线旋转)。由此,压缩机构CM的进气口吸入低压流体并通过一系列封闭的压缩腔对流体进行压缩,然后进入排气腔E并经由排气口V排出高压流体。The electric motor includes a stator 14 and a rotor 15 . The rotor 15 is used to drive the drive shaft 16 to rotate about its rotation axis relative to the housing 10 . The fixed scroll 22 is fixed to the main bearing seat 18 and held in place, and the movable scroll 24 is driven by an electric motor via the drive shaft 16 so as to be able to perform translational rotation relative to the fixed scroll 22 by means of an Oldham slip ring 17 - —that is, orbiting (that is, the axis of the orbiting scroll 24 revolves relative to the axis of the fixed scroll 22, but both the orbiting scroll 24 and the fixed scroll 22 themselves do not rotate around their respective axes). As a result, the air inlet of the compression mechanism CM sucks in low-pressure fluid and compresses the fluid through a series of closed compression chambers, and then enters the exhaust chamber E and discharges the high-pressure fluid through the exhaust port V.
如图2d中所示,在压缩机构CM的操作期间,在压缩机构CM中限定成对的高压腔H,两个高压腔H邻接径向中心的排气腔E,此时,排气腔E中的当前排气过程结束,即将与两个高压腔H流体连通以便下一次排气过程。当流体能够从两个高压腔H流入排气腔E时,随着动涡旋24的转动将流体经由排气口V排出。在高压腔H内的流体排出之后,在高压腔H径向外侧的压缩腔又即将与排气腔E连通以进行下一次排气过程。As shown in Figure 2d, during operation of the compression mechanism CM, a pair of high-pressure chambers H are defined in the compression mechanism CM, and the two high-pressure chambers H are adjacent to the radially central exhaust chamber E. At this time, the exhaust chamber E The current exhaust process in the chamber is over, and it will be fluidly connected to the two high-pressure chambers H for the next exhaust process. When the fluid can flow from the two high-pressure chambers H into the exhaust chamber E, the fluid is discharged through the exhaust port V as the orbiting scroll 24 rotates. After the fluid in the high-pressure chamber H is discharged, the compression chamber radially outside the high-pressure chamber H will be connected to the exhaust chamber E for the next exhaust process.
本申请的发明人对流体在涡旋压缩机构内的整个流动过程进行了研究,发现了流体的显著压力变化情况,例如,某些工况下,流体被压缩至高于所需压力的压力,此外,在从一个排气过程过渡到另一个排气过程时,会产生压力突变。基于这些发现,本申请的发明人提出了能够同时解决这些压力变化而导致的功率损耗的方案。The inventor of the present application has studied the entire flow process of fluid in the scroll compression mechanism and found significant pressure changes of the fluid. For example, under certain working conditions, the fluid is compressed to a pressure higher than the required pressure. In addition, , a sudden change in pressure will occur when transitioning from one exhaust process to another. Based on these findings, the inventor of the present application proposed a solution that can simultaneously solve the power loss caused by these pressure changes.
在涡旋压缩机的某些工况下,可能需要的排出气体的压力小于设计的排出压力(即,设计的经由排气口V排出的流体压力)。在这些工况下,如果将流体压缩至排气腔E并且经由排气口V排出,则产生过度压缩流体的现象。过度 压缩流体使得涡旋压缩机构CM多做了不必要的功,导致过多的功率耗损。为了避免压缩机构CM对流体的过度压缩而损耗功率,定涡旋端板221可以包括位于临近排气腔E的位置处、优选地但不限于与高压腔H(参见图2d)流体联通的至少一个排气阀口P(参见图2b)。排气阀口P优选地可以由诸如电子阀等的阀闭合并在一定的条件(例如预定的压力)下打开以在进入排气腔E之前将高压腔H中的流体提前排出至排气口V,从而避免不必要地进一步压缩流体。可以优选地设置多个排气阀口P分别将两个高压腔H联通至排气室。例如,如图2b中所示的,分别在排气口V的径向相对的两侧设置4个排气阀口P。通过设置排气阀口P可以避免因过度压缩而造成的功率损耗,因此可以显示降低涡旋压缩机100的功率消耗。Under certain operating conditions of the scroll compressor, the required discharge gas pressure may be less than the designed discharge pressure (ie, the designed fluid pressure discharged through the exhaust port V). Under these operating conditions, if the fluid is compressed into the exhaust chamber E and discharged through the exhaust port V, the phenomenon of over-compression of the fluid will occur. over The compressed fluid causes the scroll compression mechanism CM to do more unnecessary work, resulting in excessive power loss. In order to avoid over-compression of the fluid by the compression mechanism CM and loss of power, the fixed scroll end plate 221 may include at least one located near the exhaust chamber E, preferably but not limited to, in fluid communication with the high-pressure chamber H (see FIG. 2d ). An exhaust valve port P (see Figure 2b). The exhaust valve port P can preferably be closed by a valve such as an electronic valve and opened under certain conditions (such as a predetermined pressure) to discharge the fluid in the high-pressure chamber H to the exhaust port in advance before entering the exhaust chamber E. V, thus avoiding unnecessary further compression of the fluid. Multiple exhaust valve ports P may preferably be provided to communicate the two high-pressure chambers H to the exhaust chamber respectively. For example, as shown in FIG. 2b, four exhaust valve ports P are provided on radially opposite sides of the exhaust port V respectively. By providing the exhaust valve port P, power loss due to excessive compression can be avoided, and therefore the power consumption of the scroll compressor 100 can be reduced.
此外,如图2d和图2e所示,动涡旋涡卷242包括动涡卷头部部段246,定涡旋涡卷222包括定涡卷头部部段226,动涡卷头部部段246和定涡卷头部部段226共同限定上述排气腔E——即,当前排气结束而即将开始下一次排气但仍未与高压腔H流体连通的临界时刻形成的仅与排气口V流体连通的腔体。此时,动涡卷头部部段246在起始点A处与定涡卷头部部段226接合,定涡卷头部部段226于B点处与动涡卷头部部段246接合,也就是说,在本文中,将动涡卷头部部段246限定为从起始点A至终端(即,径向内端)的部段,将定涡卷头部部段226限定为从B点至终端(即,径向内端)的部段,并且二者限定排气腔E。In addition, as shown in FIGS. 2d and 2e , the orbiting scroll wrap 242 includes an orbiting scroll head section 246 , the fixed scroll wrap 222 includes a fixed scroll head section 226 , the orbiting scroll head section 246 and The fixed scroll head section 226 jointly defines the above-mentioned exhaust chamber E - that is, the critical moment when the current exhaust is over and the next exhaust is about to start but is not yet in fluid communication with the high-pressure chamber H and is only connected to the exhaust port V. Fluidically connected cavities. At this time, the movable scroll head section 246 is joined to the fixed scroll head section 226 at the starting point A, and the fixed scroll head section 226 is joined to the movable scroll head section 246 at point B. That is, herein, the orbiting scroll head section 246 is defined as the section from the starting point A to the terminal end (ie, the radially inner end), and the fixed scroll head section 226 is defined as the section from B point to the terminal end (i.e., the radially inner end), and both define the exhaust chamber E.
另外,需要说明的是,为了便于本文的描述,在不同排气过程过渡前后,排气腔E和高压腔H的术语名称将不发生变化,以免混淆或误解,如图2d、图2e、图3b、图3c中所示。本领域普通技术人员将理解,实际工作中,各个腔体是变化的而不存在固定不变的分界点。In addition, it should be noted that, in order to facilitate the description of this article, the term names of the exhaust chamber E and the high-pressure chamber H will not change before and after the transition of different exhaust processes to avoid confusion or misunderstanding, as shown in Figure 2d, Figure 2e, Figure 3b, as shown in Figure 3c. Persons of ordinary skill in the art will understand that in actual work, each cavity changes and there is no fixed demarcation point.
如图2e示出在涡旋压缩机100的排气期间,动涡卷头部部段246和定涡卷头部部段226限定的排气腔E的变化阶段示意图,其中,示出了动涡卷头部部段246带有导流槽2460的第二构型和不带有导流槽的第一构型,需注意的是,图2e中的导流槽2460仅为示意性的,而未具体描绘出导流槽2460的实际形状和尺寸。具体地,如第一构型中的“第一阶段”所示,动涡卷头部部段246和定涡卷头部部段226彼此接合以限定排气腔E,此时的“第一阶段”意指开始排气前的临界阶段,此时,动涡卷头部部段246于起始点A处与定涡卷头部部 段226接合,接下来进入“第二阶段”——即,开始排气阶段,此时,动涡卷头部部段246于起始点A处与定涡卷头部部段226开始脱离接合,从而使得流体从高压腔H开始流入排气腔E(如图中箭头所示),由此开始排气,但此时,由于动涡卷头部部段246和定涡卷头部部段226之间的间隙非常小,排气效率很低,并且可能会导致高压腔H内的瞬时压力突增。如前所述的,为了改善压缩机构CM的排气腔E的排气效率、缓解高压腔H内的瞬时压力突增,可以在动涡卷头部部段246的朝向排气腔E的内壁2466上设置导流槽2460,从而加速流体从高压腔H流入排气腔E,以提高排气效率以及涡旋压缩机100的工作效率。如图2e的第二构型中的各阶段的示意图所示,通过设置导流槽2460能够显著扩大动涡卷头部部段246和定涡卷头部部段226之间的间隙,从而提高排气效率。2e shows a schematic diagram of the changing stages of the exhaust chamber E defined by the movable scroll head section 246 and the fixed scroll head section 226 during the discharge of the scroll compressor 100, in which the movable scroll head section 246 and the fixed scroll head section 226 are shown. The scroll head section 246 has a second configuration with guide grooves 2460 and a first configuration without guide grooves. It should be noted that the guide grooves 2460 in Figure 2e are only schematic. The actual shape and size of the guide groove 2460 are not specifically depicted. Specifically, as shown in the "first stage" in the first configuration, the orbiting scroll head section 246 and the fixed scroll head section 226 are engaged with each other to define the exhaust chamber E, at which time the "first stage""stage" refers to the critical stage before starting exhaust. At this time, the movable scroll head section 246 is in contact with the fixed scroll head section at the starting point A. Section 226 is engaged, and then enters the "second stage" - that is, the exhaust stage begins. At this time, the movable scroll head section 246 begins to disengage from the fixed scroll head section 226 at the starting point A, As a result, the fluid starts to flow from the high-pressure chamber H into the exhaust chamber E (as shown by the arrow in the figure), and exhaust begins. However, at this time, due to the movable scroll head section 246 and the fixed scroll head section 226 The gap between them is very small, the exhaust efficiency is very low, and may cause an instantaneous pressure increase in the high-pressure chamber H. As mentioned above, in order to improve the exhaust efficiency of the exhaust chamber E of the compression mechanism CM and alleviate the instantaneous pressure increase in the high-pressure chamber H, the inner wall of the orbiting scroll head section 246 facing the exhaust chamber E can be A guide groove 2460 is provided on 2466 to accelerate the flow of fluid from the high-pressure chamber H into the exhaust chamber E, thereby improving the exhaust efficiency and the working efficiency of the scroll compressor 100 . As shown in the schematic diagram of each stage in the second configuration of Figure 2e, by providing the guide groove 2460, the gap between the movable scroll head section 246 and the fixed scroll head section 226 can be significantly expanded, thereby improving the Exhaust efficiency.
根据本申请的涡旋压缩机构兼顾了过度压缩与流体行进过程中压力突变的技术问题,由此能够显著降低功率耗损,从而提高涡旋压缩机的效率。通常,排气阀口P的设置会限制涡旋涡卷(特别是,动涡旋涡卷)的结构改进,因为往往会造成相邻腔体之间的流体泄露或者涡卷强度降低等等。然而,本申请的发明人提出了将排气阀口P与涡卷改进相结合的方案,在优化排气通道的同时,消除了涡旋压缩腔(特别地,高压腔)与排气腔联通而在开始排气前出现提前混合的情况(即,在未达到预期压力水平的情况下,不同腔室中的压缩流体经由排气阀口P而提前混合),进一步提高了涡旋压缩机的效率;同时通过涡卷结构设计的改进减小了涡卷的根部应力。The scroll compression mechanism according to the present application takes into account the technical problems of over-compression and sudden pressure changes during fluid travel, thereby significantly reducing power loss and thereby improving the efficiency of the scroll compressor. Generally, the setting of the exhaust valve port P will limit the structural improvement of the scroll wrap (especially the orbiting scroll wrap), because it often causes fluid leakage between adjacent cavities or a reduction in the strength of the scroll, etc. However, the inventor of the present application has proposed a solution that combines the exhaust valve port P with the improvement of the scroll. While optimizing the exhaust passage, the communication between the scroll compression chamber (especially the high-pressure chamber) and the exhaust chamber is eliminated. However, there is advance mixing before starting the exhaust (that is, when the expected pressure level is not reached, the compressed fluids in different chambers are mixed in advance through the exhaust valve port P), which further improves the performance of the scroll compressor. efficiency; at the same time, the root stress of the scroll is reduced through the improvement of the scroll structure design.
并且,优选地,导流槽2460设置成从上述起始点A开始延伸——即,起始点A是在定涡卷头部部段226的稍部部段2260与动涡卷头部部段246即将开始脱离接合时、动涡卷头部部段246上的与稍部部段2260接触的位置,从而在刚开始排气的阶段——即,上述第二阶段、以及第三阶段——即,间隙进一步扩大的排气阶段,均能够有效地加速流体从高压腔H流入排气腔E。And, preferably, the guide groove 2460 is arranged to extend from the above-mentioned starting point A—that is, the starting point A is between the tip section 2260 of the fixed scroll head section 226 and the movable scroll head section 246 When disengagement is about to begin, the position on the orbiting scroll head section 246 that is in contact with the tip section 2260 is therefore in the stage where exhaust is just beginning—that is, the above-mentioned second stage, and the third stage—that is, , the exhaust stage when the gap is further expanded, can effectively accelerate the flow of fluid from the high-pressure chamber H into the exhaust chamber E.
在此需要说明的是,定涡卷头部部段226的稍部部段2260在本文中仅表示定涡卷头部部段226的靠近终端的一个部段,而不意在特指终端,即,与动涡卷头部部段246的A点接合的稍部部段2260可以优选地是其终端端点、也可以是距离该终端端点一定距离处的部段中的某一位置,尽管在本公开的实施例中,与动涡卷头部部段246的起始点A接合的部分优选地是定涡卷头部部段 226的终端端点,但应当理解的是,对此没有特别限制。It should be noted here that the slight section 2260 of the fixed scroll head section 226 only refers to a section of the fixed scroll head section 226 close to the terminal end in this article, and is not intended to specifically refer to the terminal end, that is, , the tip section 2260 that joins point A of the orbiting scroll head section 246 may preferably be its terminal end point, or it may be a certain position in the section at a certain distance from the terminal end point, although in this article In the disclosed embodiment, the portion that engages the starting point A of the orbiting scroll head section 246 is preferably the fixed scroll head section. 226 terminal endpoint, but it should be understood that there is no particular restriction on this.
如前所述,对于同时具有排气阀口P和导流槽2460的涡旋压缩机构CM和涡旋压缩机100,由于动涡卷头部部段246包括导流槽2460而使得动涡卷头部部段246的轴向的顶表面247变窄,因而在动涡旋24与定涡旋22彼此抵接以进行压缩操作的过程中可能存在如下技术问题:动涡卷头部部段246的顶表面247在某一瞬时无法适当地覆盖排气阀口P而使排气阀口P跨越在动涡卷头部部段246的两侧而将所述两侧的空间流体联通,从而可能导致压缩效率降低,这是不期望的。为了解决该技术问题,本公开对导流槽2460的构型进行了改进,总体来说,根据本公开的导流槽2460设置成使得动涡卷头部部段246的顶表面247能够在操作期间将排气阀口P覆盖成使得:每个排气阀口P不会例如跨越在动涡卷头部部段246的两侧而将两侧的空间流体联通。As mentioned above, for the scroll compression mechanism CM and the scroll compressor 100 having both the exhaust valve port P and the guide groove 2460, since the orbiting scroll head section 246 includes the guide groove 2460, the orbiting scroll The axial top surface 247 of the head section 246 is narrowed, so there may be the following technical problems when the movable scroll 24 and the fixed scroll 22 abut each other to perform a compression operation: the movable scroll head section 246 At a certain moment, the top surface 247 cannot properly cover the exhaust valve port P and the exhaust valve port P spans both sides of the movable scroll head section 246 to fluidly communicate the spaces on both sides, thereby making it possible This results in a reduction in compression efficiency, which is undesirable. In order to solve this technical problem, the present disclosure improves the configuration of the guide groove 2460. Generally speaking, the guide groove 2460 according to the present disclosure is configured to enable the top surface 247 of the orbiting scroll head section 246 to operate During this period, the exhaust valve ports P are covered so that each exhaust valve port P does not, for example, span both sides of the movable scroll head section 246 and fluidly communicate the spaces on both sides.
下面将参照图2c和图2d来详细描述导流槽2460的构型。The configuration of the guide groove 2460 will be described in detail below with reference to FIGS. 2c and 2d.
如在图2c和图2d中所示的,本实施例中优选地将导流槽2460设置成延伸至动涡卷头部部段246的顶表面247,并且优选地设置成两段式的,即,导流槽2460包括彼此间隔开的第一槽部段2461和第二槽部段2462,也就是说,第一槽部段2461和第二槽部段2462之间包括有未被去除材料的间隔部段2463。如前所述的,导流槽2460仍然优选地从上述起始点A开始延伸,即,第一槽部段2461从起始点A开始延伸,从而更好地加速排气,并且更优选地,第一槽部段2461在起始点A处具有相对更大的凹入深度——即,沿着内壁2466的切面的法向方向凹入动涡卷头部部段246中的深度,从而能够在起始点A、即刚开始排气时更快速地加速流体进入排气腔E。总体来说,导流槽2460优选地设置成在不同位置处具有不同的凹入深度、优选地在起始点A附近具有最大凹入深度。更优选地,导流槽2460的凹入深度小于等于动涡卷头部部段246的厚度的7/8,即,动涡卷头部部段246的包括有导流槽2460的部分——即,被去除材料后的剩余部分——的厚度应当不小于其原始厚度的1/8,且更优选地,动涡卷头部部段246的包括有导流槽2460的部分——即,被去除材料后的剩余部分——的厚度大于等于0.5mm,从而确保该部分具有所需的强度。As shown in Figures 2c and 2d, in this embodiment the guide groove 2460 is preferably provided to extend to the top surface 247 of the orbiting scroll head section 246, and is preferably provided in two sections, That is, the guide groove 2460 includes a first groove section 2461 and a second groove section 2462 that are spaced apart from each other. That is, there is unremoved material included between the first groove section 2461 and the second groove section 2462. spacer section 2463. As mentioned before, the guide groove 2460 still preferably extends from the above-mentioned starting point A, that is, the first groove section 2461 starts from the starting point A, so as to better accelerate the exhaust, and more preferably, the first groove section 2461 extends from the starting point A. A groove section 2461 has a relatively larger recessed depth at the starting point A - that is, a depth recessed into the orbiting scroll head section 246 along the normal direction of the tangent plane of the inner wall 2466, so that it can be formed at the starting point A. Starting point A, that is, when exhaust is just beginning, the fluid is accelerated into the exhaust chamber E more quickly. In general, the guide groove 2460 is preferably configured to have different recessed depths at different locations, preferably with a maximum recessed depth near the starting point A. More preferably, the recessed depth of the guide groove 2460 is less than or equal to 7/8 of the thickness of the orbiting scroll head section 246, that is, the portion of the orbiting scroll head section 246 including the guide groove 2460 - That is, the thickness of the remaining portion after the material is removed should be no less than 1/8 of its original thickness, and more preferably, the portion of the orbiting scroll head section 246 including the guide groove 2460 - that is, The thickness of the remaining part after the material is removed is greater than or equal to 0.5mm, thereby ensuring that the part has the required strength.
并且,优选地,导流槽2460在涡旋压缩机构CM的轴向方向上的延伸高度小于等于动涡旋涡卷246的轴向总高度的2/3,以确保具有所需的强度。并且优选地,导流槽2460设置为整体上更靠近动涡卷头部部段246的顶表面247、 而远离动涡卷头部部段246的连接至动涡旋端板241的根部,以保证动涡卷头部部段246的强度。Furthermore, preferably, the extension height of the guide groove 2460 in the axial direction of the scroll compression mechanism CM is less than or equal to 2/3 of the total axial height of the orbiting scroll wrap 246 to ensure required strength. And preferably, the guide groove 2460 is disposed closer to the top surface 247 of the orbiting scroll head section 246 as a whole. The root of the orbiting scroll end plate 241 is connected to the root of the orbiting scroll head section 246 away from the orbiting scroll head section 246 to ensure the strength of the orbiting scroll head section 246 .
关于第二槽部段2462,如图2c和图2c所示,第二槽部段2462优选地延伸至动涡卷头部部段246的终端,以便在整个排气过程中更好地加速流体流入排气腔E中。但本公开不限于此,也就是说,可以根据实际需求来设置导流槽2460的沿着动涡卷头部部段246的型线方向延伸的长度(弧度),以便在实现优化的排气效果的同时确保良好地覆盖排气阀口P、同时确保涡卷的强度。Regarding the second groove section 2462, as shown in Figures 2c and 2c, the second groove section 2462 preferably extends to the terminal end of the orbiting scroll head section 246 to better accelerate the fluid throughout the exhaust process. flows into the exhaust chamber E. However, the present disclosure is not limited thereto. That is to say, the length (radius) of the guide groove 2460 extending along the profile direction of the orbiting scroll head section 246 can be set according to actual needs in order to achieve optimized exhaust gas. This effect ensures good coverage of the exhaust valve port P and ensures the strength of the scroll.
至于间隔部段2463,可以依据实际情况——例如,排气阀口P的位置和尺寸、包括有导流槽2460的涡卷部分的强度要求等,来设置其位置和尺寸,其目的在于:首先,通过设置间隔部段2463,可以更好地覆盖排气阀口P,以提高压缩效率;同时,间隔部段2463有利于进一步提高包括有导流槽2460的涡卷部分的强度,特别是有利于减小导流槽2460与其余的涡卷部分的连接根部处的应力集中以及动涡卷头部部段246与动涡旋端板241之间的连接根部处的应力集中。As for the spacing section 2463, its position and size can be set according to the actual situation - for example, the position and size of the exhaust valve port P, the strength requirements of the scroll part including the guide groove 2460, etc. The purpose is to: First, by providing the spacer section 2463, the exhaust valve port P can be better covered to improve compression efficiency; at the same time, the spacer section 2463 is conducive to further improving the strength of the scroll part including the guide groove 2460, especially It is beneficial to reduce the stress concentration at the connection root between the guide groove 2460 and the remaining scroll parts and the stress concentration at the connection root between the orbiting scroll head section 246 and the orbiting scroll end plate 241 .
并且,基于本公开的目的——确保良好地覆盖排气阀口P,可以依据排气阀口P的位置和尺寸来灵活地设置导流槽2460各个不同位置处的凹入深度,例如图2d中示出的,第一槽部段2461和第二槽部段2462各自在不同位置处具有不同的凹入深度;同样地,尽管在本实施例中导流槽2460具有一致的轴向高度,但是,本公开不限于此,根据例如上述强度要求等,导流槽2460可以灵活地设置成在不同位置处具有不同的轴向高度,并且,可以理解的是,导流槽2460也可以在轴向上是多段式的,即包括在轴向上间隔开的多个槽部段。Moreover, based on the purpose of this disclosure - to ensure good coverage of the exhaust valve port P, the recessed depth at various positions of the guide groove 2460 can be flexibly set according to the position and size of the exhaust valve port P, for example, Figure 2d As shown in , the first groove section 2461 and the second groove section 2462 each have different recessed depths at different locations; similarly, although the guide groove 2460 has a consistent axial height in this embodiment, However, the present disclosure is not limited thereto. According to, for example, the above-mentioned strength requirements, etc., the guide groove 2460 can be flexibly arranged to have different axial heights at different positions, and it is understood that the guide groove 2460 can also be arranged on the axis. It is upwardly multi-segmented, ie it includes a plurality of groove sections spaced apart in the axial direction.
此外,尽管上述实施例中将导流槽2460设置成两段式的,即,包括彼此间隔开的第一槽部段2461和第二槽部段2462,但是本公开不限于此,应当理解的是,在一些情况下,导流槽2460也可以设置成包括更多个部段——例如三个部段、四个部段等等,或者设置成连续的单一部段、而在不同位置处具有不同的凹入深度,只要能够确保良好地覆盖排气阀口P即可。并且,根据实际情况,导流槽2460可以具有任何合适的形状,对此没有特别限制。In addition, although the guide groove 2460 is provided in two sections in the above embodiment, that is, including a first groove section 2461 and a second groove section 2462 spaced apart from each other, the present disclosure is not limited thereto, and it should be understood that Yes, in some cases, the guide groove 2460 can also be configured to include more sections—for example, three sections, four sections, etc., or it can be configured as a continuous single section at different locations. It has different recessed depths, as long as it can ensure good coverage of the exhaust valve port P. Moreover, according to actual conditions, the guide groove 2460 may have any suitable shape, and there is no particular limitation on this.
尽管上述实施例中的导流槽2460设置成延伸至动涡卷头部部段246的顶表面247,但是也可以将其设置成未延伸至动涡卷头部部段246的顶表面247。下面参照图3a至图3c来描述根据本公开的涡旋压缩机构CM的第二实施例, 其中,图3a示出根据本公开的第二实施例的涡旋压缩机构CM中的动涡旋24的立体图;图3b示出根据本公开的第二实施例的涡旋压缩机构CM的组装状态的侧视图及其相应的M-M截面图;以及图3c示出根据本公开的第二实施例的涡旋压缩机构CM的组装状态的侧视图及其相应的L-L截面图。如图3a和图3b所示,导流槽2460设置成连续的单一槽部段的形式,并且如前所述地,导流槽2460在此实施例中也优选地从起始点A处开始延伸,不同之处在于,导流槽2460设置成未延伸至动涡卷头部部段246的顶表面247,从而不占用顶表面247的面积。具体地,如图3b示出了在更靠近动涡旋端板241的M-M截面处截取的截面图,其示出了导流槽2460;如图3c示出了在更靠近动涡旋涡卷242的顶表面247的L-L截面处截取的截面图,从图3c中可见,导流槽2460在L-L截面处不可见,顶表面247为完整的而没有被导流槽2460占用。由此可以在确保良好地覆盖排气阀口P的同时,确保有效地改善排气效率。Although the guide groove 2460 in the above embodiment is configured to extend to the top surface 247 of the orbiting scroll head section 246 , it may also be configured not to extend to the top surface 247 of the orbiting scroll head section 246 . A second embodiment of the scroll compression mechanism CM according to the present disclosure will be described below with reference to Figures 3a to 3c, 3a shows a perspective view of the orbiting scroll 24 in the scroll compression mechanism CM according to the second embodiment of the present disclosure; FIG. 3b shows the assembled state of the scroll compression mechanism CM according to the second embodiment of the present disclosure. 3c shows a side view of the scroll compression mechanism CM and its corresponding LL cross-sectional view in an assembled state according to the second embodiment of the present disclosure. As shown in Figures 3a and 3b, the guide groove 2460 is provided in the form of a continuous single groove section, and as previously mentioned, the guide groove 2460 also preferably extends from the starting point A in this embodiment. , the difference is that the guide groove 2460 is configured not to extend to the top surface 247 of the orbiting scroll head section 246, so as not to occupy the area of the top surface 247. Specifically, FIG. 3b shows a cross-sectional view taken at the MM section closer to the orbiting scroll end plate 241, which shows the guide groove 2460; FIG. 3c shows a cross-section closer to the orbiting scroll wrap 242. The cross-sectional view taken at the LL section of the top surface 247, as can be seen from Figure 3c, the guide groove 2460 is not visible at the LL section, and the top surface 247 is complete and is not occupied by the guide groove 2460. This ensures that the exhaust valve port P is well covered and the exhaust efficiency is effectively improved.
当然,可以想到的是,本实施例中的导流槽2460也可以设置成类似于第一实施例中的两段式或更多部段式的构型,区别仅在于本实施例中的导流槽2460未延伸至动涡卷头部部段246的顶表面247。Of course, it is conceivable that the guide groove 2460 in this embodiment can also be configured in a two-section or more-section configuration similar to that in the first embodiment. The only difference lies in the guide groove 2460 in this embodiment. The flow channels 2460 do not extend to the top surface 247 of the orbiting scroll head section 246 .
此外,本公开还提供一种涡旋压缩机100,涡旋压缩机100包括根据本公开的涡旋压缩机构CM,该涡旋压缩机构CM例如可以是上述实施例中的涡旋压缩机构CM、或者可以具有其他可能的变型。In addition, the present disclosure also provides a scroll compressor 100. The scroll compressor 100 includes a scroll compression mechanism CM according to the present disclosure. The scroll compression mechanism CM may be, for example, the scroll compression mechanism CM in the above embodiment. Or there could be other possible variations.
实验结果表明,通过如上所述地对导流槽进行改进,能够有效提升涡旋压缩机的工作效率达0.95%左右,同时减少动力损耗约0.85%左右,并且能够略微增大涡旋压缩机构CM的容量达0.16%左右。Experimental results show that by improving the guide groove as mentioned above, the working efficiency of the scroll compressor can be effectively improved by about 0.95%, while the power loss can be reduced by about 0.85%, and the CM of the scroll compression mechanism can be slightly increased. The capacity reaches about 0.16%.
尽管在前述实施方式中描述了根据本公开的涡旋压缩机构和涡旋压缩机的示例性实施方式,但是,本公开并不局限于此,而是在不背离本公开的保护范围的情况下,可以进行各种改型、替换和组合。Although exemplary embodiments of the scroll compression mechanism and the scroll compressor according to the present disclosure are described in the foregoing embodiments, the present disclosure is not limited thereto without departing from the scope of the present disclosure. , various modifications, replacements and combinations can be made.
显而易见的是,通过将不同的实施方式、各个技术特征以不同的方式进行组合或者对其进行改型,可以进一步设计得出各种不同的实施方式。It is obvious that various different implementations can be further designed by combining or modifying different implementations and technical features in different ways.
上文结合具体实施方式描述了根据本公开的优选实施方式的涡旋压缩机构和涡旋压缩机。可以理解,以上描述仅为示例性的而非限制性的,在不背离本公开的范围的情况下,本领域技术人员参照上述描述可以想到多种变型和修改。这些变型和修改同样包含在本公开的保护范围内。 The scroll compression mechanism and the scroll compressor according to the preferred embodiments of the present disclosure are described above in conjunction with specific embodiments. It is to be understood that the above description is only illustrative and not restrictive, and those skilled in the art can think of various variations and modifications with reference to the above description without departing from the scope of the present disclosure. These variations and modifications are also included in the protection scope of the present disclosure.

Claims (11)

  1. 一种涡旋压缩机构,包括:A scroll compression mechanism, including:
    定涡旋,所述定涡旋包括定涡旋端板和从所述定涡旋端板的一侧延伸的定涡旋涡卷;以及a fixed scroll, the fixed scroll including a fixed scroll end plate and a fixed scroll wrap extending from one side of the fixed scroll end plate; and
    动涡旋,所述动涡旋包括动涡旋端板和从所述动涡旋端板的一侧延伸的动涡旋涡卷,An orbiting scroll, the orbiting scroll includes an orbiting scroll end plate and an orbiting scroll wrap extending from one side of the orbiting scroll end plate,
    所述定涡旋与所述动涡旋接合以在其之间限定从径向外侧至径向内侧依次排列的开放的吸气腔、至少一个封闭的压缩腔以及中心处的排气腔,the fixed scroll is engaged with the orbiting scroll to define therebetween an open suction chamber, at least one closed compression chamber, and a discharge chamber at the center, arranged in sequence from radially outward to radially inward,
    所述定涡旋端板包括与所述排气腔流体联通的排气口以及与所述压缩腔流体联通以提前排气的至少一个排气阀口,The fixed scroll end plate includes an exhaust port in fluid communication with the exhaust chamber and at least one exhaust valve port in fluid communication with the compression chamber for early exhaust,
    所述动涡旋涡卷包括动涡卷头部部段,所述定涡旋涡卷包括定涡卷头部部段,所述动涡卷头部部段和所述定涡卷头部部段限定如下状态的所述排气腔:所述排气腔处于即将与所述压缩腔流体连通但仍未与所述压缩腔流体连通的状态,在所述动涡卷头部部段的内壁上设置有内凹的导流槽以在所述动涡卷头部部段和所述定涡卷头部部段分离时增加流体从所述压缩腔流入所述排气腔内的流量,The orbiting scroll wrap includes an orbiting scroll head section, the fixed scroll wrap includes a fixed scroll head section, and the orbiting scroll head section and the fixed scroll head section define The exhaust chamber in the following state: the exhaust chamber is about to be in fluid communication with the compression chamber but is not yet in fluid communication with the compression chamber, and is provided on the inner wall of the orbiting scroll head section There is a concave guide groove to increase the flow of fluid from the compression chamber into the exhaust chamber when the movable scroll head section and the fixed scroll head section are separated,
    所述动涡卷头部部段构造成在操作期间通过所述动涡卷头部部段的顶表面覆盖所述至少一个排气阀口的至少一部分而防止经由所述至少一个排气阀口将所述压缩腔与所述排气腔流体连通。The orbiting scroll head section is configured to prevent passage through the at least one exhaust valve port by covering at least a portion of the at least one exhaust valve port with a top surface of the orbiting scroll head section during operation. The compression chamber is in fluid communication with the exhaust chamber.
  2. 根据权利要求1所述的涡旋压缩机构,其特征在于,所述导流槽的至少一部分延伸至所述动涡卷头部部段的顶表面。The scroll compression mechanism according to claim 1, wherein at least a portion of the guide groove extends to a top surface of the orbiting scroll head section.
  3. 根据权利要求1所述的涡旋压缩机构,其特征在于,所述导流槽定位成与所述动涡卷头部部段的顶表面相距预定距离处。The scroll compression mechanism according to claim 1, wherein the guide groove is positioned at a predetermined distance from the top surface of the orbiting scroll head section.
  4. 根据权利要求3所述的涡旋压缩机构,其特征在于,所述导流槽设置为相比于距离所述动涡旋涡卷的连接至所述动涡旋端板的根部的距离而更靠 近所述动涡卷头部部段的顶表面。The scroll compression mechanism according to claim 3, wherein the guide groove is disposed closer than a distance from a root of the orbiting scroll wrap connected to the orbiting scroll end plate. Near the top surface of the orbiting scroll head section.
  5. 根据权利要求1所述的涡旋压缩机构,其特征在于,所述导流槽设置成从如下起始点开始朝向所述动涡卷头部部段的内端延伸预定距离:所述起始点是所述动涡卷头部部段的与所述定涡卷头部部段接合并且即将与所述定涡卷头部部段开始脱离接合的位置。The scroll compression mechanism according to claim 1, wherein the guide groove is arranged to extend a predetermined distance toward the inner end of the orbiting scroll head section from the following starting point: the starting point is The position where the orbiting scroll head section is engaged with the fixed scroll head section and is about to begin to disengage from the fixed scroll head section.
  6. 根据权利要求5所述的涡旋压缩机构,其特征在于,所述导流槽构造成在不同位置处具有不同的凹入深度,并且在所述起始点处具有最大凹入深度。The scroll compression mechanism according to claim 5, wherein the guide groove is configured to have different concave depths at different positions and has a maximum concave depth at the starting point.
  7. 根据权利要求1所述的涡旋压缩机构,其特征在于,所述导流槽在所述涡旋压缩机构的轴向方向上的延伸高度小于等于所述动涡旋涡卷的轴向高度的2/3。The scroll compression mechanism according to claim 1, wherein the extension height of the guide groove in the axial direction of the scroll compression mechanism is less than or equal to 2 times the axial height of the orbiting scroll wrap. /3.
  8. 根据权利要求1所述的涡旋压缩机构,其特征在于,所述导流槽的凹入深度小于等于所述动涡卷头部部段的相应部段的厚度的7/8。The scroll compression mechanism according to claim 1, wherein the recessed depth of the guide groove is less than or equal to 7/8 of the thickness of the corresponding section of the orbiting scroll head section.
  9. 根据权利要求1所述的涡旋压缩机构,其特征在于,所述动涡卷头部部段的设置有所述导流槽的部分的厚度大于等于0.5mm。The scroll compression mechanism according to claim 1, wherein the thickness of the portion of the orbiting scroll head section where the guide groove is provided is greater than or equal to 0.5 mm.
  10. 根据权利要求2或3所述的涡旋压缩机构,其特征在于,所述导流槽构造为包括至少一个部段。The scroll compression mechanism according to claim 2 or 3, characterized in that the guide groove is configured to include at least one section.
  11. 一种涡旋压缩机,所述涡旋压缩机包括根据权利要求1-10中任一项所述的涡旋压缩机构。 A scroll compressor comprising the scroll compression mechanism according to any one of claims 1-10.
PCT/CN2023/090467 2022-04-25 2023-04-25 Vortex compression mechanism, and vortex compressor comprising same WO2023207934A1 (en)

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CN202220969524.1 2022-04-25
CN202220969524.1U CN217152298U (en) 2022-04-25 2022-04-25 Scroll compression mechanism and scroll compressor comprising same
CN202210439484.4 2022-04-25
CN202210439484.4A CN116988971A (en) 2022-04-25 2022-04-25 Scroll compression mechanism and scroll compressor comprising same

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5249943A (en) * 1991-06-27 1993-10-05 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Scroll type compressor having recessed buffer means in a spiral wrap flat face
JPH11303775A (en) * 1998-04-23 1999-11-02 Denso Corp Scroll compressor
CN101806302A (en) * 2003-09-25 2010-08-18 艾默生环境优化技术有限公司 Scroll machine
CN104235016A (en) * 2013-06-14 2014-12-24 艾默生环境优化技术(苏州)有限公司 Scroll compressor, and fixed scroll member and orbiting scroll member
CN217152298U (en) * 2022-04-25 2022-08-09 艾默生环境优化技术(苏州)有限公司 Scroll compression mechanism and scroll compressor comprising same

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5249943A (en) * 1991-06-27 1993-10-05 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Scroll type compressor having recessed buffer means in a spiral wrap flat face
JPH11303775A (en) * 1998-04-23 1999-11-02 Denso Corp Scroll compressor
CN101806302A (en) * 2003-09-25 2010-08-18 艾默生环境优化技术有限公司 Scroll machine
CN104235016A (en) * 2013-06-14 2014-12-24 艾默生环境优化技术(苏州)有限公司 Scroll compressor, and fixed scroll member and orbiting scroll member
CN217152298U (en) * 2022-04-25 2022-08-09 艾默生环境优化技术(苏州)有限公司 Scroll compression mechanism and scroll compressor comprising same

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