WO2019186695A1 - ロータリコンプレッサおよび冷凍サイクル装置 - Google Patents
ロータリコンプレッサおよび冷凍サイクル装置 Download PDFInfo
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- WO2019186695A1 WO2019186695A1 PCT/JP2018/012424 JP2018012424W WO2019186695A1 WO 2019186695 A1 WO2019186695 A1 WO 2019186695A1 JP 2018012424 W JP2018012424 W JP 2018012424W WO 2019186695 A1 WO2019186695 A1 WO 2019186695A1
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- crank
- connecting shaft
- crank portion
- axial direction
- cylinder body
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/30—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F04C18/34—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members
- F04C18/356—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member
- F04C18/3562—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member the inner and outer member being in contact along one line or continuous surfaces substantially parallel to the axis of rotation
- F04C18/3564—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member the inner and outer member being in contact along one line or continuous surfaces substantially parallel to the axis of rotation the surfaces of the inner and outer member, forming the working space, being surfaces of revolution
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C23/00—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
- F04C23/001—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids of similar working principle
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C23/00—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
- F04C23/008—Hermetic pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C28/00—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
- F04C28/02—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids specially adapted for several pumps connected in series or in parallel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0021—Systems for the equilibration of forces acting on the pump
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0042—Driving elements, brakes, couplings, transmissions specially adapted for pumps
- F04C29/005—Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions
- F04C29/0057—Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions for eccentric movement
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2210/00—Fluid
- F04C2210/24—Fluid mixed, e.g. two-phase fluid
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/20—Rotors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/60—Shafts
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/60—Shafts
- F04C2240/601—Shaft flexion
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/80—Other components
- F04C2240/804—Accumulators for refrigerant circuits
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/80—Other components
- F04C2240/807—Balance weight, counterweight
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/06—Silencing
Definitions
- Embodiments of the present invention relate to a multi-cylinder rotary compressor and a refrigeration cycle apparatus including the rotary compressor.
- a three-cylinder rotary compressor in which three sets of refrigerant compression portions are arranged in the axial direction of a rotating shaft has been developed in order to increase the refrigerant compression capability.
- the rotary shaft used in this type of rotary compressor has first to third crank portions that rotate eccentrically in the cylinder chamber of the refrigerant compression portion, between the first crank portion and the second crank portion, and second A pair of connecting shaft portions straddling between the crank portion and the third crank portion.
- the three-cylinder rotary compressor has a total length of the rotating shaft and a pair of supporting the rotating shaft in comparison with the two-cylinder rotary compressor in which two sets of refrigerant compression portions are arranged in the axial direction of the rotating shaft.
- the distance between the bearings becomes longer. For this reason, in order to suppress shaft runout of the rotating shaft during high-speed rotation, it is necessary to increase the rigidity of the connecting shaft portion located between the first to third crank portions.
- Japanese Patent No. 4594302 Japanese Patent No. 5441982 Japanese Patent No. 5117503
- the eccentric direction of adjacent crank portions is set to be shifted by 120 ° in the circumferential direction of the rotating shaft in order to suppress the torque fluctuation when the three refrigerant compression portions compress the refrigerant. Is desirable.
- the unbalanced rotating shaft is one factor that promotes the vibration of the three-cylinder rotary compressor.
- An object of the present invention is to obtain a rotary compressor that can maintain a good balance of the rotating shaft while ensuring the rigidity of the connecting shaft portion of the rotating shaft, and can reduce vibration and noise.
- the rotary compressor includes a first journal part supported by a first bearing, and a second journal provided coaxially with the first journal part and supported by a second bearing. Provided between the first journal portion and the second journal portion, and arranged in the axial direction of the journal portion with an interval therebetween, and the eccentric direction in the circumferential direction of the journal portion.
- First to third crank portions having a circular cross-sectional shape arranged in a shifted manner, a first connecting shaft portion straddling between the first crank portion and the second crank portion, and the second And a second connecting shaft portion straddling between the crank portion and the third crank portion, and the eccentric direction of the adjacent crank portions is circumferential with respect to the rotation center of the journal portion.
- a ring-shaped roller fitted to the outer peripheral surface of the first to third crank portions of the rotating shaft A first cylinder body that accommodates the roller fitted to the first crank portion and defines a first cylinder chamber in which the roller rotates eccentrically with the first crank portion; A second cylinder body that accommodates the roller fitted in the second crank portion and defines a second cylinder chamber in which the roller rotates eccentrically with the second crank portion; A third cylinder body that accommodates the roller fitted to the third crank portion and defines a third cylinder chamber in which the roller rotates eccentrically with the third crank portion; A first intermediate partition plate interposed between the first cylinder body and the second cylinder body and through which the first connecting shaft portion of the rotating shaft passes; A second intermediate partition plate interposed between the second cylinder body and the third cylinder body and through which the second connecting shaft portion of the rotating shaft passes.
- the first connecting shaft portion of the rotating shaft is located at the same position as the outer peripheral surface of the first crank portion located on the opposite side of the eccentric direction of the first crank portion, or the rotation from the outer peripheral surface.
- a first outer surface formed at a position offset toward the rotation center side of the shaft and having at least an intermediate portion curved in an arc shape, and the second crank located on the opposite side of the eccentric direction of the second crank portion A second outer surface that is formed at the same position as the outer peripheral surface of the portion, or a position that is offset from the outer peripheral surface toward the rotation center of the rotary shaft, and at least a middle portion is curved in an arc shape, and the rotary shaft And a third outer surface straddling between the first outer surface and the second outer surface at a position deviating from the rotation center.
- L1 is the distance from the side intersection to the rotation center of the rotation shaft
- L2 is the distance from the intersection on the other end where the first outer surface and the second outer surface intersect to the rotation center of the rotation shaft
- FIG. 1 is a circuit diagram schematically showing the configuration of the refrigeration cycle apparatus according to the embodiment.
- FIG. 2 is a cross-sectional view of the three-cylinder rotary compressor according to the embodiment.
- FIG. 3 is an enlarged cross-sectional view showing a compression mechanism portion of a three-cylinder rotary compressor in the embodiment.
- FIG. 4 is a diagram illustrating a relative positional relationship between the first crank portion, the second crank portion, the third crank portion, and the first connecting shaft portion when the rotation shaft is viewed from the axial direction.
- FIG. 5A is a diagram showing the maximum thickness Tmax of the first connecting shaft portion when the angle difference ⁇ in the eccentric direction between the first crank portion and the second crank portion is 120 °.
- FIG. 1 is a circuit diagram schematically showing the configuration of the refrigeration cycle apparatus according to the embodiment.
- FIG. 2 is a cross-sectional view of the three-cylinder rotary compressor according to the embodiment.
- FIG. 3 is an enlarged cross-sectional view showing a compression mechanism portion of
- FIG. 5B is a diagram showing the maximum thickness Tmax of the first connecting shaft portion when the angular difference ⁇ in the eccentric direction between the first crank portion and the second crank portion is 180 °.
- FIG. 4 is a cross-sectional view showing the positional relationship between the vane and the roller in the embodiment.
- FIG. 7 is a characteristic diagram showing the torque fluctuation rate of the three-cylinder rotary compressor when the phase angle ⁇ in the eccentric direction of adjacent crank portions is changed.
- FIG. 8A is a cross-sectional view showing a state where a roller corresponding to the second crank portion is guided from the first journal portion to the outer peripheral surface of the first crank portion.
- FIG. 8B is a cross-sectional view showing a state in which the roller corresponding to the second crank portion is tilted outside the first connecting shaft portion.
- FIG. 8C is a cross-sectional view showing a state in which the roller corresponding to the second crank portion is moved in the radial direction of the rotating shaft at the position of the first connecting shaft portion.
- FIG. 8D is a cross-sectional view illustrating a state in which a roller is fitted to the outer peripheral surface of the second crank portion.
- FIG. 1 is a refrigeration cycle circuit diagram of an air conditioner 1 which is an example of a refrigeration cycle apparatus, for example.
- the air conditioner 1 includes a rotary compressor 2, a four-way valve 3, an outdoor heat exchanger 4, an expansion device 5, and an indoor heat exchanger 6 as main elements.
- the plurality of elements constituting the air conditioner 1 are connected via a circulation circuit 7 in which the refrigerant circulates.
- the discharge side of the rotary compressor 2 is connected to the first port 3 a of the four-way valve 3.
- the second port 3 b of the four-way valve 3 is connected to the outdoor heat exchanger 4.
- the outdoor heat exchanger 4 is connected to the indoor heat exchanger 6 via an expansion device 5.
- the indoor heat exchanger 6 is connected to the third port 3 c of the four-way valve 3.
- the fourth port 3 d of the four-way valve 3 is connected to the suction side of the rotary compressor 2 via the accumulator 8.
- the four-way valve 3 is switched so that the first port 3a communicates with the second port 3b and the third port 3c communicates with the fourth port 3d.
- the outdoor heat exchanger in which the high-temperature and high-pressure gas-phase refrigerant compressed by the rotary compressor 2 functions as a radiator (condenser) via the four-way valve 3 Led to 4.
- the gas-phase refrigerant led to the outdoor heat exchanger 4 is condensed by heat exchange with the air and changed into a high-pressure liquid-phase refrigerant.
- the high-pressure liquid-phase refrigerant is reduced in pressure in the process of passing through the expansion device 5 and is changed to a low-pressure gas-liquid two-phase refrigerant.
- the gas-liquid two-phase refrigerant is guided to the indoor heat exchanger 6 that functions as a heat absorber (evaporator) and exchanges heat with air in the process of passing through the indoor heat exchanger 6.
- the gas-liquid two-phase refrigerant takes heat from the air, evaporates, and changes to a low-temperature / low-pressure gas-phase refrigerant.
- the air passing through the indoor heat exchanger 6 is cooled by the latent heat of vaporization of the liquid phase refrigerant, and is sent to a place to be air-conditioned (cooled) as cold air.
- the low-temperature and low-pressure gas-phase refrigerant that has passed through the indoor heat exchanger 6 is guided to the accumulator 8 via the four-way valve 3. If liquid refrigerant that could not evaporate is mixed in the refrigerant, the accumulator 8 separates it into liquid phase refrigerant and gas phase refrigerant.
- the low-temperature and low-pressure gas-phase refrigerant from which the liquid-phase refrigerant has been separated is sucked into the rotary compressor 2 and is compressed again into a high-temperature and high-pressure gas-phase refrigerant by the rotary compressor 2 and discharged to the circulation circuit 7.
- the four-way valve 3 switches so that the first port 3a communicates with the third port 3c and the second port 3b communicates with the fourth port 3d. Therefore, the high-temperature and high-pressure gas-phase refrigerant discharged from the rotary compressor 2 is guided to the indoor heat exchanger 6 through the four-way valve 3 and exchanges heat with air passing through the indoor heat exchanger 6. That is, the indoor heat exchanger 6 functions as a condenser.
- the gas-phase refrigerant passing through the indoor heat exchanger 6 is condensed by heat exchange with the air and changed into a high-pressure liquid-phase refrigerant.
- the air passing through the indoor heat exchanger 6 is heated by heat exchange with the gas-phase refrigerant, and is sent to a place to be air-conditioned (heated) as warm air.
- the high-temperature liquid-phase refrigerant that has passed through the indoor heat exchanger 6 is guided to the expansion device 5 and is reduced in pressure in the process of passing through the expansion device 5 to be changed into a low-pressure gas-liquid two-phase refrigerant.
- the gas-liquid two-phase refrigerant is led to the outdoor heat exchanger 4 functioning as an evaporator, and evaporates by exchanging heat with air here, and changes to a low-temperature / low-pressure gas-phase refrigerant.
- the low-temperature and low-pressure gas-phase refrigerant that has passed through the outdoor heat exchanger 4 is sucked into the rotary compressor 2 via the four-way valve 3 and the accumulator 8.
- FIG. 2 is a sectional view showing a vertical three-cylinder rotary compressor 2.
- the three-cylinder rotary compressor 2 includes a sealed container 10, an electric motor 11, and a compression mechanism unit 12 as main elements.
- the sealed container 10 has a cylindrical peripheral wall 10a and is erected along the vertical direction.
- a discharge pipe 10 b is provided at the upper end of the sealed container 10.
- the discharge pipe 10 b is connected to the first port 3 a of the four-way valve 3 through the circulation circuit 7. Furthermore, a lubricating oil that lubricates the compression mechanism 12 is stored in the lower part of the sealed container 10.
- the electric motor 11 is accommodated in an intermediate portion along the axial direction of the sealed container 10 so as to be positioned above the oil level A of the lubricating oil.
- the electric motor 11 is a so-called inner rotor type motor, and includes a stator 13 and a rotor 14.
- the stator 13 is fixed to the inner surface of the peripheral wall 10 a of the sealed container 10.
- the rotor 14 is coaxially positioned on the central axis O ⁇ b> 1 of the sealed container 10 and is surrounded by the stator 13.
- the compression mechanism part 12 is accommodated in the lower part of the airtight container 10 so that it may be immersed in lubricating oil.
- the compression mechanism unit 12 includes a first refrigerant compression unit 15A, a second refrigerant compression unit 15B, a third refrigerant compression unit 15C, a first intermediate partition plate 16, and a second The intermediate partition plate 17, the first bearing 18, the second bearing 19, and the rotating shaft 20 are provided as main elements.
- coolant compression part 15A, 15B, 15c is located in a line in the axial direction of the airtight container 10 at intervals.
- the first to third refrigerant compressors 15A, 15B, and 15c have a first cylinder body 21a, a second cylinder body 21b, and a third cylinder body 21c, respectively.
- the first to third cylinder bodies 21a, 21b, and 21c are set to have the same thickness along the axial direction of the sealed container 10, for example.
- the first intermediate partition plate 16 is interposed between the first cylinder body 21a and the second cylinder body 21b.
- the upper surface of the first intermediate partition plate 16 is overlaid on the lower surface of the first cylinder body 21a so as to cover the inner diameter portion of the first cylinder body 21a from below.
- the lower surface of the first intermediate partition plate 16 is overlaid on the upper surface of the second cylinder body 21b so as to cover the inner diameter portion of the second cylinder body 21b from above.
- a circular through hole 16 a is formed at the center of the first intermediate partition plate 16.
- the through hole 16a is located between the inner diameter part of the first cylinder body 21a and the inner diameter part of the second cylinder body 21b.
- the second intermediate partition plate 17 is interposed between the second cylinder body 21b and the third cylinder body 21c.
- the upper surface of the second intermediate partition plate 17 is overlaid on the lower surface of the second cylinder body 21b so as to cover the inner diameter portion of the second cylinder body 21b from below.
- the lower surface of the second intermediate partition plate 17 is overlaid on the upper surface of the third cylinder body 21c so as to cover the inner diameter portion of the third cylinder body 21c from above.
- a circular through hole 17 a is formed at the center of the second intermediate partition plate 17.
- the through hole 17a is located between the inner diameter part of the second cylinder body 21b and the inner diameter part of the third cylinder body 21c.
- the first intermediate partition plate 16 and the second intermediate partition plate 17 have thicknesses T1 and T2 along the axial direction of the sealed container 10, respectively. According to this embodiment, the thickness T1 of the first intermediate partition plate 16 is thicker than the thickness T2 of the second intermediate partition plate 17.
- the first bearing 18 is positioned on the first cylinder body 21a.
- the first bearing 18 has a flange portion 23 that projects toward the inner surface of the peripheral wall 10 a of the sealed container 10.
- the flange portion 23 is overlaid on the upper surface of the first cylinder body 21a so as to cover the inner diameter portion of the first cylinder body 21a from above.
- the flange portion 23 of the first bearing 18 is surrounded by the ring-shaped support frame 24.
- the support frame 24 is fixed to a predetermined position on the inner surface of the peripheral wall 10a of the sealed container 10 by means such as welding.
- the lower surface of the support frame 24 is overlaid on the upper surface of the outer peripheral portion of the first cylinder body 21a.
- the outer peripheral portion of the first cylinder body 21a is coupled to the support frame 24 via a plurality of first fastening bolts 25 (only one is shown).
- the flange portion 23 of the first bearing 18, the first cylinder body 21 a, the first intermediate partition plate 16, and the second cylinder body 21 b are stacked in the axial direction of the sealed container 10, and a plurality of They are integrally connected via a second fastening bolt 26 (only one is shown).
- the second bearing 19 is positioned below the third cylinder body 21c.
- the second bearing 19 has a flange portion 27 that protrudes toward the inner surface of the peripheral wall 10 a of the sealed container 10.
- the flange portion 27 is superimposed on the lower surface of the third cylinder body 21c so as to cover the inner diameter portion of the third cylinder body 21c from below.
- the flange portion 27 of the second bearing 19, the third cylinder body 21 c, the second intermediate partition plate 17, and the second cylinder body 21 b are stacked in the axial direction of the sealed container 10, and a plurality of third Are connected together via a fastening bolt 28 (only one is shown).
- first bearing 18 and the second bearing 19 are separated from each other in the axial direction of the sealed container 10, and the first to third cylinder bodies are provided between the first bearing 18 and the second bearing 19.
- 21a, 21b, 21c, the first intermediate partition plate 16 and the second intermediate partition plate 17 are alternately positioned.
- the area surrounded by the inner diameter portion of the first cylinder body 21 a, the first intermediate partition plate 16, and the flange portion 23 of the first bearing 18 defines the first cylinder chamber 30. Yes.
- the area surrounded by the inner diameter portion of the second cylinder body 21 b, the first intermediate partition plate 16 and the second intermediate partition plate 17 defines the second cylinder chamber 31.
- a region surrounded by the inner diameter portion of the third cylinder body 21 c, the second intermediate partition plate 17 and the flange portion 27 of the second bearing 19 defines a third cylinder chamber 32.
- the first intermediate partition plate 16 is made thicker than the second intermediate partition plate 17, so that the axis of the second cylinder chamber 31 is extended from an intermediate point along the axial direction of the first cylinder chamber 30.
- the distance D1 to the intermediate point along the direction is larger than the distance D2 from the intermediate point along the axial direction of the second cylinder chamber 31 to the intermediate point along the axial direction of the third cylinder chamber 32.
- the second intermediate partition plate 17 is thinner than the first intermediate partition plate 16, the second cylinder chamber 31 and the third cylinder chamber 32 are brought close to each other in the axial direction of the sealed container 10. It is kept.
- the first discharge muffler 33 is attached to the first bearing 18.
- a first silencing chamber 34 is formed between the first discharge muffler 33 and the first bearing 18.
- the first silencing chamber 34 is opened inside the hermetic container 10 through a plurality of exhaust holes (not shown) of the first discharge muffler 33.
- a second discharge muffler 35 is attached to the second bearing 19.
- a second silencing chamber 36 is formed between the second discharge muffler 35 and the second bearing 19.
- the second silencing chamber 36 communicates with the first silencing chamber 34 via a discharge passage (not shown) extending in the axial direction of the sealed container 10.
- the rotating shaft 20 is coaxially positioned on the central axis O1 of the hermetic container 10.
- the rotary shaft 20 includes a first journal portion 38, a second journal portion 39, first to third crank portions 40a, 40b, 40c, a first connecting shaft portion 41, and a second connecting shaft portion 42. It is a monolithic structure.
- the first journal portion 38 is positioned at an intermediate portion along the axial direction of the rotary shaft 20 and is rotatably supported by the first bearing 18.
- the rotor 14 of the electric motor 11 is connected to the upper end portion of the rotating shaft 20 protruding from the first bearing 18.
- the second journal portion 39 is provided coaxially with the first journal portion 38 so as to be positioned at the lower end portion of the rotating shaft 20.
- the second journal portion 39 is rotatably supported by the second bearing 19.
- the first to third crank portions 40 a, 40 b, and 40 c are located between the first journal portion 38 and the second journal portion 39, and are arranged at intervals in the axial direction of the rotary shaft 20. Yes. As shown in FIG. 4, the first to third crank portions 40 a, 40 b, and 40 c are disk-shaped elements each having a circular cross-sectional shape, and in the present embodiment, are along the axial direction of the rotary shaft 20. The thickness dimension and diameter are set to be the same.
- the first to third crank portions 40a, 40b, 40c are eccentric with respect to the rotation center line O2 of the rotating shaft 20 passing through the rotation centers of the first journal portion 38 and the second journal portion 39. That is, as shown in FIG. 4, the eccentric directions of the first to third crank portions 40 a, 40 b, 40 c with respect to the rotation center line O ⁇ b> 2 of the rotation shaft 20 are equally shifted in the circumferential direction of the rotation shaft 20.
- eccentric amounts e of the first to third crank portions 40a, 40b, 40c with respect to the rotation center line O2 of the rotating shaft 20 are equal to each other.
- the first crank portion 40 a is positioned in the first cylinder chamber 30.
- the second crank portion 40 b is located in the second cylinder chamber 31.
- the third crank portion 40 c is located in the third crank chamber 32.
- the first connecting shaft portion 41 is positioned between the first crank portion 40a and the second crank portion 40b on the rotation center line O2 of the rotating shaft 20 and penetrates the first intermediate partition plate 16. It penetrates the hole 16a.
- the second connecting shaft portion 42 is located between the second crank portion 40b and the third crank portion 40c on the rotation center line O2 of the rotating shaft 20, and penetrates the second intermediate partition plate 17. It penetrates the hole 17a.
- a ring-shaped roller 45 is fitted to the outer peripheral surface of the first crank portion 40a.
- the roller 45 rotates eccentrically in the first cylinder chamber 30 following the rotary shaft 20, and a part of the outer peripheral surface of the roller 45 can slide on the inner peripheral surface of the inner diameter portion of the first cylinder body 21a. Line contact is made.
- the upper end surface of the roller 45 is slidably in contact with the lower surface of the flange portion 23 of the first bearing 18.
- the lower end surface of the roller 45 is slidably in contact with the upper surface of the first intermediate partition plate 16. Thereby, the airtightness of the first cylinder chamber 30 is ensured.
- a ring-shaped roller 46 is fitted to the outer peripheral surface of the second crank portion 40b.
- the roller 46 follows the rotation shaft 20 and rotates eccentrically in the second cylinder chamber 31, and a part of the outer peripheral surface of the roller 46 can slide on the inner peripheral surface of the inner diameter portion of the second cylinder body 21b. Line contact is made.
- the upper end surface of the roller 46 is slidably in contact with the lower surface of the first intermediate partition plate 16.
- the lower end surface of the roller 46 is slidably in contact with the upper surface of the second intermediate partition plate 17. Thereby, the airtightness of the second cylinder chamber 31 is ensured.
- a ring-shaped roller 47 is fitted to the outer peripheral surface of the third crank portion 40c.
- the roller 47 eccentrically rotates in the third cylinder chamber 32 following the rotation shaft 20, and a part of the outer peripheral surface of the roller 47 can slide on the inner peripheral surface of the inner diameter portion of the third cylinder body 21c. Line contact is made.
- the upper end surface of the roller 47 is slidably in contact with the lower surface of the second intermediate partition plate 17.
- the lower end surface of the roller 47 is slidably in contact with the upper surface of the flange portion 27 of the second bearing 19. Thereby, the airtightness of the third cylinder chamber 32 is ensured.
- the rollers 45, 46, 47 have a larger inner diameter than the first connecting shaft portion 41 and the second connecting shaft portion 42 of the rotating shaft 20.
- the first to third cylinder chambers 30, 31, and 32 are partitioned into a suction region R1 and a compression region R2 by vanes 50, respectively. Therefore, when the rollers 45, 46, 47 are eccentrically rotated in the first to third cylinder chambers 30, 31, 32, the volumes of the suction region R1 and the compression region R2 of the cylinder chambers 30, 31, 32 change. It has become.
- a first connection port 51a connected to the suction region R1 of the first cylinder chamber 30 is formed inside the first cylinder body 21a.
- the first connection port 51a is opened on the side surface of the first cylinder body 21a.
- a second connection port 51b is formed in the second cylinder body 21b so as to communicate with the suction region R1 of the second cylinder chamber 31.
- the second connection port 51b is opened on the side surface of the second cylinder body 21b.
- the open ends of the first and second connection ports 51a and 51b are arranged at intervals in the axial direction of the sealed container 10.
- the cylindrical accumulator 8 is attached to the side of the hermetic container 10 in a vertically upright posture.
- the bottom of the accumulator 8 is positioned near the upper end of the compression mechanism unit 12.
- the accumulator 8 includes a first suction pipe 52a and a second suction pipe 52b that distribute the gas-phase refrigerant from which the liquid-phase refrigerant has been separated to the first to third cylinder chambers 30, 31, and 32 of the compression mechanism section 12. Have.
- the first and second suction pipes 52 a and 52 b penetrate the bottom of the accumulator 8 and are guided out of the accumulator 8.
- the first suction pipe 52a is curved in an elbow shape toward the peripheral wall 10a of the sealed container 10 under the accumulator 8.
- the distal end portion of the first suction pipe 52a passes through the peripheral wall 10a of the sealed container 10 and is connected to the first connection port 51a of the first cylinder body 21a.
- the second suction pipe 52b is larger in diameter than the first suction pipe 52a, and is bent in an elbow shape toward the peripheral wall 10a of the sealed container 10 under the first suction pipe 52a.
- the distal end of the second suction pipe 52b penetrates the peripheral wall 10a of the sealed container 10 and is connected to the second connection port 51b of the second cylinder body 21b.
- the second intermediate partition plate 17 that partitions between the second cylinder chamber 31 and the third cylinder chamber 32 has a refrigerant distribution port 53 that communicates with the second connection port 51b of the second cylinder body 21b. ing.
- the refrigerant distribution port 53 communicates with the third cylinder chamber 32 via an introduction passage 54 formed in the third cylinder body 21c.
- a first discharge valve 56 that opens when the pressure in the compression region R ⁇ b> 2 of the first cylinder chamber 30 reaches a predetermined value is provided in the flange portion 23 of the first bearing 18. Yes.
- the discharge side of the first discharge valve 56 communicates with the first silencing chamber 34.
- a second discharge valve 57 that opens when the pressure in the compression region R2 of the second cylinder chamber 31 reaches a predetermined value is provided on the first intermediate partition plate 16.
- the discharge side of the second discharge valve 57 communicates with the first muffler chamber 34 via a discharge passage (not shown) provided in the first intermediate partition plate 16 and in the first cylinder body 21a.
- a third discharge valve 58 that opens when the pressure in the compression region R2 of the third cylinder chamber 32 reaches a predetermined value is provided in the flange portion 27 of the second bearing 19. The discharge side of the third discharge valve 58 communicates with the second silencer chamber 36.
- the gas-phase refrigerant sucked into the suction region R1 of the first cylinder chamber 30 from the first suction pipe 52a is gradually compressed in the process of moving the suction region R1 to the compression region R2.
- the first discharge valve 56 is opened, and the gas-phase refrigerant compressed in the first cylinder chamber 30 is discharged into the first silencing chamber 34.
- a part of the gas-phase refrigerant guided from the second suction pipe 52b to the second connection port 51b of the second cylinder body 21b is sucked into the suction region R1 of the second cylinder chamber 30.
- the remaining gas-phase refrigerant guided to the second connection port 51b is sucked into the third cylinder chamber 31 through the refrigerant distribution port 53 of the second intermediate partition plate 17 and the introduction passage 54 of the third cylinder body 21c. Sucked into region R1.
- the gas-phase refrigerant sucked into the suction region R1 of the second cylinder chamber 31 is gradually compressed in the process of moving the suction region R1 to the compression region R2.
- the second discharge valve 57 is opened, and the gas-phase refrigerant compressed in the second cylinder chamber 31 passes through the discharge passage and enters the first silencing chamber 34. Led.
- the gas-phase refrigerant sucked into the suction region R1 of the third cylinder chamber 32 is gradually compressed in the process in which the suction region R1 moves to the compression region R2.
- the third discharge valve 58 is opened, and the gas-phase refrigerant compressed in the third cylinder chamber 32 is discharged into the second silencing chamber 36.
- the gas-phase refrigerant discharged to the second silencing chamber 36 is guided to the first silencing chamber 34 through the discharge passage.
- the first to third crank portions 40a, 40b, and 40c are formed so that the eccentric direction is evenly shifted in the circumferential direction of the rotary shaft 20. Therefore, there is a phase difference equivalent to the timing at which the gas-phase refrigerant compressed in the first to third cylinder chambers 30, 31, 32 is discharged.
- the gas-phase refrigerant compressed in the first to third cylinder chambers 30, 31, 32 merges in the first silencing chamber 34 and continues from the exhaust hole of the first discharge muffler 33 into the sealed container 10. Is discharged.
- the gas-phase refrigerant discharged into the sealed container 10 passes through the electric motor 11 and then is guided to the four-way valve 3 from the discharge pipe 10b.
- the rollers 45, 46, 47 rotate eccentrically in the first to third cylinder chambers 30, 31, 32, so that the suction region R ⁇ b> 1 of each cylinder chamber 30, 31, 32. And the gas-phase refrigerant
- coolant is compressed by changing the volume of compression area
- FIG. 7 shows the torque with respect to the rotation angle of the rotating shaft 20 when the angle difference ⁇ in the eccentric direction of the first to third crank portions 40a, 40b, and 40c of the rotating shaft 20 is 110 °, 120 °, and 130 °. It is a characteristic view which shows a fluctuation rate.
- the torque fluctuation rate when the angle difference ⁇ is 110 ° is 38.8%
- the torque fluctuation rate when the angle difference ⁇ is 120 ° is 27.1%
- the angle difference ⁇ The torque fluctuation rate when the angle is 130 ° is 40.4%.
- the torque fluctuation rate when the angle difference ⁇ is 140 ° is 54.2%.
- the torque fluctuation rate of a rotary compressor is generally desired to be 50% or less. Therefore, in the present embodiment, the eccentric directions of the first to third crank portions 40a, 40b, and 40c are 110 ° to 130 ° (120 ° in the circumferential direction of the rotation shaft 20 with respect to the rotation center line O2 of the rotation shaft 20. In particular, the angle difference ⁇ is preferably 120 ° with the smallest torque fluctuation rate.
- the second suction pipe 52b connected to the accumulator 8 is connected to the second cylinder body 21b, and the gas-phase refrigerant compressed in the second cylinder chamber 31 of the second cylinder body 21b is the first. Is discharged into a discharge passage inside the intermediate partition plate 16.
- the first intermediate partition plate 16 that partitions between the first cylinder chamber 30 and the second cylinder chamber 31 is a second partition that partitions between the second cylinder chamber 31 and the third cylinder chamber 32. Therefore, the volume of the discharge passage inside the first intermediate partition plate 16 can be sufficiently secured.
- the second discharge valve 57 is provided in the first intermediate partition plate 16 located above the second cylinder chamber 31, the second discharge valve 57 is placed from the second cylinder chamber 31 to the top of the compression mechanism portion 12.
- the path length to the exhaust hole of the located first silencing chamber 34 is shortened. For this reason, coupled with the large volume of the discharge passage inside the first intermediate partition plate 16, it occurs until the gas-phase refrigerant compressed in the second cylinder chamber 31 reaches the first silencing chamber 34.
- the discharge loss of the gas phase refrigerant can be suppressed as much as possible.
- the second suction pipe 52b is provided.
- the distance from the connected second cylinder body 21b to the third cylinder chamber 32 can be shortened.
- the gas-phase refrigerant led from the second suction pipe 52b to the second connection port 51b of the second cylinder body 21b becomes the refrigerant distribution port 53 of the second intermediate partition plate 17 and the third cylinder body. It is possible to suppress the suction loss of the gas-phase refrigerant generated between the passage 21c and the third cylinder chamber 32 as much as possible.
- the second suction pipe 52b By connecting the second suction pipe 52b to the second cylinder body 21b located above the third cylinder body 21c, the second suction pipe connecting the accumulator 8 and the compression mechanism portion 12 is obtained.
- the overall length of 52b can be shortened. As a result, the suction loss that occurs when the gas-phase refrigerant passes through the second suction pipe 32b can be minimized.
- the second cylinder chamber 31 and the third cylinder chamber 32 share one second suction pipe 52b, the gas-phase refrigerant returned from the accumulator 8 is transferred to the second cylinder chamber 31 and the second cylinder chamber 31. 3 cylinder chambers 32 can be efficiently compressed and discharged into the sealed container 10.
- FIG. 4 shows the relative positional relationship between the first crank portion 40a, the second crank portion 40b, and the third crank portion 40c when the rotary shaft 20 is viewed from the axial direction, and the rotation center line of the rotary shaft 20.
- the cross-sectional shape of the 1st connection shaft part 41 of the direction orthogonal to O2 is shown.
- the center C1 of the first crank portion 40a is deviated from the rotation center line O2 of the rotary shaft 20 by an eccentric amount e.
- the center C2 of the second crank portion 40b is shifted by an eccentric amount e on the side opposite to the eccentric direction of the first crank portion 40a with respect to the rotation center line O2 of the rotating shaft 20.
- the first connecting shaft portion 41 straddling between the first crank portion 40 a and the second crank portion 40 b is provided with the first intermediate partition plate 16 that is thicker than the second intermediate partition plate 17. Since it penetrates, the axial length is longer than that of the second connecting shaft portion 42.
- the first connecting shaft portion 41 ensures sufficient rigidity by making the cross-sectional shape in the direction orthogonal to the rotation center line O2 of the rotating shaft 20 into a substantially leaf shape as shown in FIG. More specifically, the first connecting shaft portion 41 has a first outer surface S1, a second outer surface S2, and a third outer surface S3.
- the first outer surface S1 is located on the opposite side of the eccentric direction of the first crank portion 40a with respect to the rotation center line O2 of the rotary shaft 20, and the rotation of the rotary shaft 20 is greater than the outer peripheral surface of the first crank portion 40a. It is slightly offset toward the center line O2. Further, the first outer surface S1 is formed of a cylindrical surface coaxial with the center C1 of the first crank portion 40a, and the radius of the first outer surface S1 is the first journal portion 38 and the second journal portion. It is larger than the radius of 39.
- the second outer surface S2 is located on the side opposite to the eccentric direction of the second crank portion 40b with respect to the rotation center line O2 of the rotation shaft 20, and the rotation of the rotation shaft 20 is greater than the outer peripheral surface of the second crank portion 40b. It is slightly offset toward the center line O2. Further, the second outer surface S2 is formed of a cylindrical surface coaxial with the center C2 of the second crank portion 40b, and the radius of the second outer surface S2 is the first journal portion 38 and the second journal portion. It is larger than the radius of 39.
- one end of the first outer surface S1 along the circumferential direction and one end of the second outer surface S2 along the circumferential direction abut each other, and the edge portion 60 extends in the axial direction of the first connecting shaft portion 41.
- the edge part 60 can be rephrased as an intersection where one end of the first outer surface S1 and one end of the second outer surface S2 intersect.
- the third outer surface S3 straddles between the first outer surface S1 and the second outer surface S2 on the opposite side of the edge portion 60 with the rotation center line O2 of the rotating shaft 20 interposed therebetween. That is, as shown in FIG. 4, when the intersection point where the virtual extension line S1a when the first outer surface S1 is extended and the virtual extension line S2a when the second outer surface S2 is extended is defined as P, The outer surface S ⁇ b> 3 of 3 is located between the intersection P and the rotation center line O ⁇ b> 2 of the rotation shaft 20, and is configured by a cylindrical surface coaxial with the rotation center line O ⁇ b> 2 of the rotation shaft 20.
- intersection point P is located at one end along the direction of the long axis Z of a substantially tree-like shape that defines the cross-sectional shape of the first connecting shaft portion 41. Furthermore, the edge part 60 as an intersection is located at the other end along the direction of the long axis Z of the substantially leaf shape that defines the cross-sectional shape of the first connecting shaft part 41.
- the distance from the intersection P located at one end along the direction of the major axis Z of the substantially tree-like shape to the rotation center line O2 of the rotary shaft 20 is L1, and the edge portion located at the other end of the long axis Z (Intersection) If the distance from 60 to the rotation center line O2 of the rotation shaft 20 is L2, and the distance from the third outer surface S3 to the rotation center line O2 of the rotation shaft 20 is L3, then L1, L2, and L3 are L1> L3 ⁇ L2 Meet the relationship.
- the angle difference ⁇ in the eccentric direction between the first crank portion 40a and the second crank portion 40b is set to 120 °, a difference occurs between the L1 and L2, for example, the first When one connecting shaft portion 41 is formed by only the first outer surface S1 and the second outer surface S2, the center of the first connecting shaft portion 41 is the rotation center line O2 of the rotating shaft 20 by the difference. Eccentric from. If the center of the first connecting shaft portion 41 is decentered, the position of the center of gravity of the connecting shaft portion 41 deviates from the rotation center line O2 of the rotating shaft 20, and the balance of the rotating shaft 20 becomes worse.
- the first connecting shaft portion 41 of the present embodiment has a third outer surface S3 straddling between the first outer surface S1 and the second outer surface S2, and the third outer surface S3 is at the intersection P. It is located between the rotation center line O2. For this reason, the position of the center of gravity of the first connecting shaft portion 41 can be brought closer to the rotation center line O2 side of the rotation shaft 20.
- the rigidity of the first connecting shaft portion 41 can be increased by making L3 slightly larger than L2.
- the first connecting shaft portion 41 perpendicular to the direction of the major axis Z of the first connecting shaft portion 41 is compared with the case where the angle difference ⁇ is 180 °.
- the width dimension Tmax can be increased.
- FIG. 5A shows the width dimension Tmax of the first connecting shaft portion 41 when the angle difference ⁇ is 120 °
- FIG. 5B shows the first dimension when the angle difference ⁇ is 180 °.
- the width dimension Tmax of the connecting shaft part 41 is shown.
- the distance D3 from the intermediate point along the axial direction of the second crank portion 40b of the rotary shaft 20 to the intermediate point along the axial direction of the third crank portion 40c is: It is shorter than the distance D2 from the intermediate point along the axial direction of the second cylinder chamber 31 to the intermediate point along the axial direction of the third cylinder chamber 32.
- a distance D4 from an intermediate point along the axial direction of the first crank portion 40a of the rotating shaft 20 to an intermediate point along the axial direction of the second crank portion 40b is an intermediate point along the axial direction of the first cylinder chamber 30. To a middle point along the axial direction of the second cylinder chamber 31 is longer than the distance D1.
- the length H1 along the axial direction of the rollers 45, 46, and 47 fitted to the first to third crank portions 40a, 40b, and 40c is set to the first to the third. 3 is longer than the length H2 along the axial direction of the crank portions 40a, 40b, 40c.
- the length H1 along the axial direction of the rollers 45, 46, 47 is longer than the length H3 of the first connecting shaft portion 41 of the rotating shaft 20.
- the first outer surface S1 of the first connecting shaft portion 41 is slightly offset from the outer peripheral surface of the first crank portion 40a toward the rotation center line O2 of the rotating shaft 20.
- the second outer surface S2 of the first connecting shaft portion 41 is slightly offset toward the rotation center line O2 of the rotating shaft 20 with respect to the outer peripheral surface of the second crank portion 40b. Therefore, it is possible to guide the roller 46 fitted to the outer peripheral surface of the second crank portion 40b from the first crank portion 40a side to the second crank portion 40b through the outside of the first connecting shaft portion 41. It becomes.
- chamfered portions 61a and 61b are provided at the opening edges at both ends along the axial direction of the inner diameter portion of the roller 46, respectively. Due to the presence of the chamfered portions 61a and 61b, the opening edge of the roller 46 is cut obliquely in the direction of increasing the inner diameter over the entire circumference.
- rollers 45, 46 and 47 are common parts, similar chamfered portions 61a and 61b are also provided at the opening edges of the inner diameter portions of the other rollers 45 and 47.
- FIG. 8 (A) to 8 (D) sequentially show the work steps from attaching the roller 46 to the outer peripheral surface of the second crank portion 40b through the outside of the first connecting shaft portion 41 from the first crank portion 40a. It shows.
- FIG. 8A shows a state in which the roller 46 inserted from the first journal portion 38 side of the rotating shaft 20 is moved to the outside of the first crank portion 40a. Since the roller 46 includes chamfered portions 61a and 61b at the opening edge of the inner diameter portion, the inner diameter portion of the roller 46 is moved when the roller 46 is moved from the first journal portion 38 toward the first crank portion 40a. It can be avoided that the opening edge of the first and second opening portions interferes with the outer peripheral surface of the first crank portion 40a. Therefore, the roller 46 can be easily moved from the first journal portion 38 toward the first crank portion 40a.
- FIG. 8B shows a state in which the roller 46 is moved from the first crank portion 40a to the outside of the first connecting shaft portion 41.
- the first outer surface S1 of the first connecting shaft portion 41 is slightly offset toward the rotation center line O2 side of the rotating shaft 20 from the outer peripheral surface of the first crank portion 40a. Therefore, when the roller 46 is moved from the first crank portion 40a to the outside of the first connecting shaft portion 41, it is possible to avoid the inner diameter portion of the roller 46 from interfering with the first outer surface S1.
- the chamfered portions 61a and 61b are formed at the opening edge of the inner diameter portion of the roller 46. Therefore, when the roller 46 reaches the outside of the first connecting shaft portion 41, FIG. As shown, the roller 46 is tilted with respect to the rotating shaft 20.
- the portion of the inner diameter portion of the roller 46 that faces the second outer surface S2 of the first connecting shaft portion 41 is positioned below the first crank portion 40a, and the inner peripheral surface of the inner diameter portion of the roller 46 And the second outer surface S2 of the first connecting shaft portion 41 is formed with a gap g. Further, the outer peripheral edge of the first crank portion 40 a located on the first connecting shaft portion 41 side enters the chamfered portion 61 a of the roller 46.
- FIG. 8C shows a state in which the roller 46 tilted outside the first connecting shaft portion 41 is moved in the radial direction of the rotary shaft 20.
- the roller 46 moves in a direction in which the inner peripheral surface of the inner diameter portion approaches the second outer surface S2 of the first connecting shaft portion 41, and a part of the upper end surface of the roller 46 enters below the first crank portion 40a.
- the outer peripheral edge of the second crank portion 40 b located on the first connecting shaft portion 41 side enters the chamfered portion 61 b of the roller 46.
- the roller 46 is positioned on the outside of the first connecting shaft portion 41 and directly above the second crank portion 40b.
- FIG. 8D shows a state where the roller 46 is moved from the first connecting shaft portion 41 to the second crank portion 40b. In a state where a part of the upper end surface of the roller 46 enters below the first crank portion 40a, the roller 46 and the second crank portion 40b are coaxially aligned with each other if the inclination of the roller 46 is eliminated. .
- roller 46 if the roller 46 is moved from the first connecting shaft portion 41 side to the second crank portion 40b, the roller 46 shifts to a state where it is fitted to the outer peripheral surface of the second crank portion 40b.
- the angle difference ⁇ in the eccentric direction between the first crank portion 40a and the second crank portion 40b is set within a range of 110 ° to 130 ° (120 ° ⁇ 10 °). Accordingly, the width dimension Tmax of the first connecting shaft portion 41 can be sufficiently secured while suppressing the torque fluctuation of the rotating shaft 20. Thereby, the cross-sectional area of the 1st connection shaft part 41 along the direction orthogonal to the axial direction of the rotating shaft 20 increases.
- the first connecting shaft portion 41 is coupled with an increase in the cross-sectional area.
- the rigidity of the 1st connecting shaft part 41 straddling between the crank part 40a and the 2nd crank part 40b can be hardened.
- first connecting shaft portion 41 has a cross-sectional shape defined by the first outer surface S1, the second outer surface S2, and the third outer surface S3, the center of gravity of the first connecting shaft portion 41 is rotated. It can be as close as possible to the rotation center line O2 side of the shaft 20.
- the balance of the rotary shaft 20 becomes good, and also in this respect, the shaft runout of the rotary shaft 20 is suppressed and the vibration of the three-cylinder rotary compressor 2 is reduced.
- the first outer surface S1 of the first connecting shaft portion 41 is configured by a cylindrical surface coaxial with the center C1 of the first crank portion 40a, and the second outer surface S2 is the second crank. It is comprised by the cylindrical surface coaxial with the center C2 of the part 40b. For this reason, the roller 46 fitted to the outer peripheral surface of the second crank portion 40b is guided from the direction of the first crank portion 40a to the second crank portion 40b through the outside of the first connecting shaft portion 41.
- the rigidity of the first connecting shaft portion 41 can be increased while making it possible.
- the third outer surface S3 of the first connecting shaft portion 41 is configured by a cylindrical surface coaxial with the first journal portion 38 of the rotating shaft 20. For this reason, for example, when the first crank portion 40a, the second crank portion 40b, and the first journal portion 38 are cut using a lathe, the first outer surface S1, the first outer surface S2, and the third The outer surface S3 can also be cut by the same process.
- the first outer surface S1 is offset toward the rotation center line O2 side of the rotary shaft 20 from the outer peripheral surface of the first crank portion 40a.
- the second outer surface S2 is formed at a position offset from the outer peripheral surface of the second crank portion 40b toward the rotation center line O2 of the rotary shaft 20, the present invention is not limited to this.
- first outer surface S1 is formed on the same surface as the outer peripheral surface of the first crank portion 40a
- second outer surface S2 is formed on the same surface as the outer peripheral surface of the second crank portion 40b. You may do it.
- the distance D4 from the intermediate point along the axial direction of the first crank portion 40a of the rotary shaft 20 to the intermediate point along the axial direction of the second crank portion 40b is the distance of the first cylinder chamber 30. It is longer than the distance D1 from the intermediate point along the axial direction to the intermediate point along the axial direction of the second cylinder chamber 31.
- the roller 46 when the roller 46 is moved from the direction of the first crank portion 40a toward the second crank portion 40b through the outside of the first connecting shaft portion 41, the roller 46 is moved to the first connecting shaft portion 41. It becomes difficult to get caught. Therefore, the roller 46 can be easily moved, and workability when the roller 46 is assembled to the rotary shaft 20 is improved.
- the distance D3 from the intermediate point along the axial direction of the second crank portion 40b of the rotating shaft 20 to the intermediate point along the axial direction of the third crank portion 40c is the second cylinder chamber 31.
- the distance D2 from the intermediate point along the axial direction of the third cylinder chamber 32 to the intermediate point along the axial direction of the third cylinder chamber 32 is shorter. For this reason, when compressing the vapor phase refrigerant, even if the rotary shaft 20 tries to bend from the first bearing 18 and the second bearing 19, the bending stress acting on the rotary shaft 20 can be reduced.
- the third outer surface S3 of the first connecting shaft portion 41 is provided on one side along the long axis direction of the substantially leaf shape with respect to the rotation center line O2 of the rotation shaft 20.
- the present invention is not limited to this.
- a pair of third third shafts configured by a cylindrical surface coaxial with the first journal portion 38 at both ends along the major axis direction of the first connecting shaft portion 41.
- the outer surface S3 may be provided and the edge portion 60 may be omitted.
- first outer surface S1 and the second outer surface S2 of the first connecting shaft portion 41 do not need to be curved in an arc shape over the entire length along the circumferential direction. It suffices that at least the intermediate portion of the first outer surface S1 and the intermediate portion of the second outer surface S2 that define Tmax are curved in an arc shape.
- a general rotary compressor has been described as an example in which the vane advances into the cylinder chamber following the eccentric rotation of the roller or reciprocates in the direction away from the cylinder chamber.
- the present invention can be similarly applied to a so-called swing type rotary compressor in which vanes are integrally protruded radially outward from the outer peripheral surface.
- 2nd crank part 40c ... 3rd , 41... First connecting shaft portion, 42... Second connecting shaft portion, 45, 46, 47... Roller, 60... Edge portion (intersection point), P. ... second outer surface, S3 ... third outer surface, O2 ... rotation center line.
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Abstract
Description
前記回転軸の前記第1ないし第3のクランク部の外周面に嵌合されたリング状のローラと、
前記第1のクランク部に嵌合された前記ローラが収容され、前記ローラが前記第1のクランク部と共に偏心回転する第1のシリンダ室を規定する第1のシリンダボディと、
前記第2のクランク部に嵌合された前記ローラが収容され、前記ローラが前記第2のクランク部と共に偏心回転する第2のシリンダ室を規定する第2のシリンダボディと、
前記第3のクランク部に嵌合された前記ローラが収容され、前記ローラが前記第3のクランク部と共に偏心回転する第3のシリンダ室を規定する第3のシリンダボディと、
前記第1のシリンダボディと前記第2のシリンダボディとの間に介在され、前記回転軸の前記第1の連結軸部が貫通する第1の中間仕切り板と、
前記第2のシリンダボディと前記第3のシリンダボディとの間に介在され、前記回転軸の前記第2の連結軸部が貫通する第2の中間仕切り板と、を備えている。
L1>L3≧L2
の関係を満たす。
L1>L3≧L2
の関係を満たしている。
Claims (8)
- 第1の軸受で支持される第1のジャーナル部と、前記第1のジャーナル部と同軸状に設けられ、第2の軸受で支持される第2のジャーナル部と、前記第1のジャーナル部と前記第2のジャーナル部との間に設けられ、前記ジャーナル部の軸方向に間隔を存して配列されるとともに、前記ジャーナル部の周方向に偏心方向をずらして配置された円形の断面形状を有する第1ないし第3のクランク部と、前記第1のクランク部と前記第2のクランク部との間に跨る第1の連結軸部と、前記第2のクランク部と前記第3のクランク部との間に跨る第2の連結軸部と、を一体に有し、隣り合う前記クランク部の偏心方向が前記ジャーナルの回転中心に対して周方向に120°±10°の範囲内でずらして設けられた回転軸と、
前記回転軸の前記第1ないし第3のクランク部の外周面に嵌合されたリング状のローラと、
前記第1のクランク部に嵌合された前記ローラが収容され、前記ローラが前記第1のクランク部と共に偏心回転する第1のシリンダ室を規定する第1のシリンダボディと、
前記第2のクランク部に嵌合された前記ローラが収容され、前記ローラが前記第2のクランク部と共に偏心回転する第2のシリンダ室を規定する第2のシリンダボディと、
前記第3のクランク部に嵌合された前記ローラが収容され、前記ローラが前記第3のクランク部と共に偏心回転する第3のシリンダ室を規定する第3のシリンダボディと、
前記第1のシリンダボディと前記第2のシリンダボディとの間に介在され、前記回転軸の前記第1の連結軸部が貫通する第1の中間仕切り板と、
前記第2のシリンダボディと前記第3のシリンダボディとの間に介在され、前記回転軸の前記第2の連結軸部が貫通する第2の中間仕切り板と、を具備し、
前記回転軸の前記第1の連結軸部は、
前記第1のクランク部の偏心方向の反対側に位置する前記第1のクランク部の外周面と同一の位置、あるいは当該外周面よりも前記回転軸の回転中心の側に片寄った位置に形成され、少なくとも中間部が円弧状に湾曲された第1の外面と、
前記第2のクランク部の偏心方向とは反対側に位置する前記第2のクランク部の外周面と同一の位置、あるいは当該外周面よりも前記回転軸の回転中心の側に片寄った位置に形成され、少なくとも中間部が円弧状に湾曲された第2の外面と、
前記回転軸の回転中心を外れた位置で前記第1の外面と前記第2の外面との間に跨る第3の外面と、を含む断面形状を有し、
前記第1の連結軸部の前記回転軸の軸方向と直交する断面において、前記第1の外面と前記第2の外面を延長した時に前記第1の外面と前記第2の外面とが交わる一端側の交点から前記回転軸の回転中心までの距離をL1、前記第1の外面と前記第2の外面とが交わる他端側の交点から前記回転軸の回転中心までの距離をL2、前記第3の外面から前記回転軸の回転中心までの距離をL3とすれば、
L1>L3≧L2
の関係を満たすロータリコンプレッサ。 - 前記第1の連結軸部の前記第1の外面は、前記第1のクランク部の同軸の円弧面で構成され、前記第1の連結軸部の前記第2の外面は、前記第2のクランク部と同軸の円弧面で構成され、前記第1の連結軸部の前記第3の外面は、前記回転軸の回転中心と同軸の円弧面で構成された請求項1に記載のロータリコンプレッサ。
- 前記第1のクランク部の軸方向に沿う中間点から前記第2のクランク部の軸方向に沿う中間点までの距離が、前記第1のシリンダ室の軸方向に沿う中間点から前記第2のシリンダ室の軸方向に沿う中間点までの距離よりも大きい請求項1又は請求項2に記載のロータリコンプレッサ。
- 前記第1の連結軸部の軸方向に沿う長さが前記第2のクランク部の外周面に嵌合される前記ローラの軸方向に沿う長さよりも短く形成され、
前記第2のクランク部に対応する前記ローラは、前記第1の連結軸部よりも大きな内径を有するとともに、前記ローラの内径部の軸方向の両端に位置する開口縁に夫々前記第1のクランク部の外周縁および前記第2のクランク部の外周縁を避けるようにカットされた面取り部が形成され、
前記第2のクランク部に対応する前記ローラを前記第1のクランク部の外側を通して前記第1の連結軸部の外側に導いた状態で傾けた時に、前記第1のクランク部の外周縁および前記第2のクランク部の外周縁が前記面取り部に入り込む請求項1に記載のロータリコンプレッサ。 - 前記第1の中間仕切り板が前記第2の中間仕切り板よりも厚く形成された請求項1に記載のロータリコンプレッサ。
- 前記第1のシリンダ室に連通するように前記第1のシリンダボディの周面に開口され、アキュームレータに連なる第1の吸入管が接続される第1の接続口と、
前記第2のシリンダ室に連通するように前記第2のシリンダボディの周面に開口され、前記アキュームレータに連なる第2の吸入管が接続される第2の接続口と、をさらに備え、
前記第2の接続口は、前記第2の中間仕切り板に設けた冷媒分配口を通じて前記第3のシリンダ室に連通された請求項5に記載のロータリコンプレッサ。 - 前記第2のクランク部の軸方向に沿う中間点から前記第3のクランク部の軸方向に沿う中間点までの距離が、前記第2のシリンダ室の軸方向に沿う中間点から前記第3のシリンダ室の軸方向に沿う中間点までの距離よりも短い請求項5又は請求項6に記載のロータリコンプレッサ。
- 冷媒が循環するとともに、放熱器、膨張装置および吸熱器が接続された循環回路と、
前記放熱器と前記吸熱器との間で前記循環回路に接続された請求項1に記載のロータリコンプレッサと、
を備えた冷凍サイクル装置。
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| PCT/JP2018/012424 WO2019186695A1 (ja) | 2018-03-27 | 2018-03-27 | ロータリコンプレッサおよび冷凍サイクル装置 |
| KR1020207029354A KR102340873B1 (ko) | 2018-03-27 | 2018-03-27 | 로터리 컴프레서 및 냉동 사이클 장치 (rotary compressor and refrigeration cycle device) |
| JP2020510238A JP6922077B2 (ja) | 2018-03-27 | 2018-03-27 | ロータリコンプレッサおよび冷凍サイクル装置 |
| CN201880091666.9A CN111954761B (zh) | 2018-03-27 | 2018-03-27 | 旋转式压缩机以及冷冻循环装置 |
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| JP2010071265A (ja) * | 2008-09-22 | 2010-04-02 | Toshiba Carrier Corp | 回転式圧縮機と冷凍サイクル装置 |
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| US12140347B2 (en) | 2020-02-25 | 2024-11-12 | Carrier Japan Corporation | Rotary compressor and refrigeration cycle device |
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| CN111954761A (zh) | 2020-11-17 |
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