EP3557063B1 - Screw compressor - Google Patents
Screw compressor Download PDFInfo
- Publication number
- EP3557063B1 EP3557063B1 EP16923645.2A EP16923645A EP3557063B1 EP 3557063 B1 EP3557063 B1 EP 3557063B1 EP 16923645 A EP16923645 A EP 16923645A EP 3557063 B1 EP3557063 B1 EP 3557063B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- screw
- discharge
- rotor
- distal end
- tooth
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Links
- 230000002093 peripheral effect Effects 0.000 claims description 3
- 239000012530 fluid Substances 0.000 claims 3
- 230000006835 compression Effects 0.000 description 29
- 238000007906 compression Methods 0.000 description 29
- 239000003507 refrigerant Substances 0.000 description 19
- 230000000694 effects Effects 0.000 description 8
- 238000005299 abrasion Methods 0.000 description 6
- 230000001154 acute effect Effects 0.000 description 4
- 238000005057 refrigeration Methods 0.000 description 3
- 239000007787 solid Substances 0.000 description 2
- 230000032683 aging Effects 0.000 description 1
- 238000004378 air conditioning Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
Images
Classifications
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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
- F04C18/48—Rotary-piston pumps with non-parallel axes of movement of co-operating members
- F04C18/50—Rotary-piston pumps with non-parallel axes of movement of co-operating members the axes being arranged at an angle of 90 degrees
- F04C18/52—Rotary-piston pumps with non-parallel axes of movement of co-operating members the axes being arranged at an angle of 90 degrees of intermeshing engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
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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
- F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C18/082—Details specially related to intermeshing engagement type pumps
- F04C18/084—Toothed wheels
Definitions
- the present invention relates to a screw compressor and, more particularly, to measures to prevent damage to a gate rotor.
- a single screw compressor of Patent Literature 1 includes a screw rotor and disc-shaped two gate rotors.
- the screw rotor has a plurality of screw grooves at its outer peripheral portion.
- a plurality of tooth portions is disposed radially in each of the gate rotors.
- the screw rotor is rotatably located inside a cylindrical wall.
- the cylindrical wall is provided inside a casing of the compressor.
- each of the gate rotors is formed such that the tooth portions extend through the cylindrical wall and mesh with the screw grooves.
- the two gate rotors have axes perpendicular to an axis of the screw rotor, and are symmetrically arranged across the screw rotor.
- Two compression chambers are defined inside the cylindrical wall by an inner periphery of the cylindrical wall, the screw grooves, and the tooth portions of the gate rotors.
- the screw rotor rotates while, of a pair of circumferentially opposing lateral faces of any one of the tooth portions of each gate rotor, the suction-side lateral face located on a suction side in a state where the tooth portion is in mesh with the screw groove and a wall portion that defines the screw groove are in contact with each other.
- the screw rotor rotates in the reverse direction because of a difference in pressure, i.e., high and low, of refrigerant.
- the screw rotor rotates in the reverse direction, the screw rotor rotates while the discharge-side lateral face of the pair of lateral faces of any one of the tooth portions and the wall portion that defines the screw groove are in contact with each other. Damage or abrasion may occur in the gate rotors because of this reverse rotation.
- US5129800A discloses a single screw positive displacement compressor mechanism employing shallow gate rotor tooth penetration of the main rotor for purposes of reducing internal leakage and consequent compressor inefficiencies, wherein an interrupted main rotor thread for purposes of insuring multiple gate rotor teeth meshing with the drive portion of the main rotor thread, thereby reducing gate rotor tooth flank loads in the compressor section of the device. Provision is also made for main rotor thread baffling between the main rotor chamber section and the mechanism inlet.
- Patent Literature 1 Japanese Unexamined Patent Application Publication No. 2013-136957
- Patent Literature 1 is based on the fact that economizer ports for introducing refrigerant gas into compression chambers are provided, so the structure of Patent Literature 1 cannot be applied to a compressor with no economizer port.
- the present invention has been attained taking the problem mentioned above into consideration, and an object thereof is to suppress damage on or abrasion of a gate rotor during reverse rotation of a screw rotor.
- Embodiment 1 A screw compressor according to an embodiment of the present invention, hereinafter Embodiment 1, is defined in appended claim 1.
- At least part of the region in which the distal end portion of each of the tooth portions of the gate rotor and the discharge-side wall portion forming the screw groove, with which the distal end portion of the tooth portion meshes, face each other during reverse rotation has a non-contact structure, so damage on or abrasion of the gate rotor can be suppressed.
- a screw compressor according to Embodiment 1 will be described with reference to Fig. 1 to Fig. 6 .
- the screw compressor is connected to a refrigeration circuit that operates a vapor compression refrigeration cycle by circulating refrigerant.
- Fig. 1 is a schematic sectional view of the screw compressor according to Embodiment 1 of the present invention.
- the right side is a suction side
- the left side is a discharge side.
- Fig. 2 is a perspective view showing a portion at which screw grooves of a screw rotor and tooth portions of gate rotors mesh with each other in the screw compressor according to Embodiment 1 of the present invention.
- the upper right side indicates the suction side
- the lower left side indicates the discharge side.
- the solid arrow represents a rotation direction of a screw shaft, and the outline arrows represent how suction gas is sucked.
- the screw compressor 1 according to Embodiment 1 is a single screw compressor.
- Embodiment 1 will be described by way of an example of a single screw compressor of a type in which two gate rotors 7 are meshed with one screw rotor 5.
- the screw compressor 1 includes a cylindrical casing 2, a motor 3, a screw shaft 4, the screw rotor 5, and other components.
- the motor 3 is accommodated in the casing 2.
- the screw shaft 4 is fixed to the motor 3, and is driven to rotate by the motor 3.
- the screw rotor 5 is fixed to the screw shaft 4.
- An end portion of the screw shaft 4, not fixed to the motor 3, is rotatably supported via a bearing 6.
- the motor 3 is formed of a stator 3a and a motor rotor 3b.
- the stator 3a is fixed in the casing 2 so as to be internally in contact the casing 2.
- the motor rotor 3b is disposed radially inside the stator 3a.
- the motor rotor 3b, as well as the screw rotor 5, is fixed to the screw shaft 4, and is disposed along the same axis as the screw rotor 5.
- the screw rotor 5 has a cylindrical shape.
- a plurality of screw grooves 5a is formed at an outer peripheral portion of the screw rotor 5.
- the screw grooves 5a run spirally from one end of the screw rotor 5 toward the other end thereof.
- One end side (right side in Fig. 1 ) of the screw rotor 5 is the suction side from which refrigerant gas is sucked, and the other end side (left side in Fig. 1 ) is the discharge side from which refrigerant gas is discharged.
- the inside of the casing 2 is separated by a separation wall (not shown) into a suction pressure space and a discharge pressure space.
- the suction pressure space is filled with low-pressure refrigerant gas.
- the discharge pressure space is filled with high-pressure refrigerant gas.
- One end side of the screw rotor 5 communicates with the suction pressure space, and the other end side communicates with the discharge pressure space.
- the two gate rotors 7 are disposed on the sides of the screw rotor 5 so as to be symmetric across the screw shaft 4.
- Each of the gate rotors 7 has a disc shape.
- a plurality of tooth portions 7a is provided radially at an outer periphery of each gate rotor 7 along a circumferential direction.
- Each gate rotor 7 is supported by a gate rotor support 8.
- Each gate rotor 7 is disposed such that the tooth portions 7a are in mesh with the screw grooves 5a of the screw rotor 5.
- Compression chambers 10 are spaces each surrounded by the screw groove 5a, the tooth portions 7a of the gate rotor 7, an inner periphery of the casing 2, and a slide valve 9.
- the compression chambers 10 are filled with refrigerant gas sucked from the suction pressure space. Oil for lubricating the bearing 6 and sealing the compression chambers 10 is also introduced into the compression chambers 10.
- slide valves 9 are disposed between the inner periphery of the casing 2 and the screw rotor 5.
- Each of the slide valves 9 is provided so as to be slidable in the direction of the screw shaft 4 of the screw rotor 5 along the outer periphery of the screw rotor 5.
- Each slide valve 9 has an opening port 9a.
- Discharge ports 2a (see Fig. 3 , given later) are formed in the casing 2.
- the discharge ports 2a communicate with a discharge chamber 11 formed inside the casing 2.
- High-pressure refrigerant gas and oil filled in the compression chambers 10 pass through the opening ports 9a of the slide valves 9 and then discharged to the discharge chamber 11 via the discharge ports 2a.
- Fig. 3 illustrates the operation of the screw compressor according to Embodiment 1 of the present invention.
- the screw rotor 5 rotates with the rotation of the screw shaft 4.
- the screw rotates in the forward direction.
- the gate rotors 7 also rotate with the rotation of the screw rotor 5, and a suction stroke, a compression stroke, and a discharge stroke are repeated in each compression chamber 10.
- a compression operation will be described focusing on the compression chamber 10 dotted in Fig. 3 .
- Fig. 3(a) shows a state of the compression chamber 10 in the suction stroke.
- the screw groove 5a in which the compression chamber 10 is formed is meshed with the tooth portion 7a of the gate rotor 7.
- this tooth portion 7a relatively moves toward the terminal end of the screw groove 5a.
- the gate rotor 7 rotates in the narrow outline arrow direction.
- the compression chamber 10 in the suction stroke is expanded to have the largest volume, communicates with a suction-side space of the casing 2, and is filled with low-pressure refrigerant gas.
- the compression chamber 10 communicates with the discharge port 2a, as shown in Fig. 3(c) .
- high-pressure refrigerant gas compressed in the compression chamber is discharged via the opening port 9a of the slide valve 9 (not shown in Fig. 3 ) to the discharge chamber 11 through the discharge port 2a.
- Refrigerant discharged to the discharge chamber 11 is discharged to the outside of the screw compressor 1.
- the pressure in the compression chamber 10 gradually increases in order of (a), (b), and (c), and is high in (c).
- the screw rotor 5 rotates in the reverse direction as described above because of a pressure difference between the low-pressure side and high-pressure side of the screw rotor 5.
- the pressure in the compression chamber 10 is reduced to be lower than the suction-side pressure, and, when the gate rotor 7 has the existing configuration to which no improvement of the present invention is applied, the gate rotor 7 is damaged. This phenomenon will be described later with reference to Fig. 4 and Fig. 5 .
- Fig. 4 illustrates a location of the tooth portion of the gate rotor relative to the screw groove during forward rotation of the screw rotor.
- Fig. 5 illustrates a location of the tooth portion of the gate rotor relative to the screw groove during reverse rotation of the screw rotor.
- Fig. 4 and Fig. 5 both show an expansion plan of one screw groove together with the tooth portion of the gate rotor, meshed with the screw groove.
- the arrow in Fig. 4 indicates a moving direction during forward rotation of the screw rotor 5.
- the arrow in Fig. 5 indicates a moving direction of the screw rotor 5 during reverse rotation.
- the right side is the suction side
- the left side is the discharge side.
- the tooth portion 7a of the gate rotor 7 contacts a suction-side wall portion 5bb that is a wall portion on the suction side, of two wall portions 5b forming the screw groove 5a with which the tooth portion 7a meshes as shown in Fig. 2 and Fig. 4 . More specifically, a suction-side lateral face 7c of the tooth portion 7a contacts the suction-side wall portion 5bb.
- the suction-side lateral face 7c is, of a pair of circumferentially opposing lateral faces of the tooth portion 7a, the lateral face on the suction side in a state where the tooth portion 7a is in mesh with the screw groove 5a.
- the lateral face on the discharge side is referred to as the discharge-side lateral face 7b.
- the discharge-side wall portion 5ba is referred to as discharge-side wall portion 5ba.
- a pressing force acts on the gate rotor 7 in a direction opposing to that during operation, and the discharge-side lateral face 7b of the tooth portion 7a contacts the discharge-side wall portion 5ba as shown in Fig. 5 .
- the portion represented by dotted line in Fig. 5 shows the shape of the tooth portion of existing technologies in which the width of the tooth portion 7a is set to the same width from the proximal portion to the distal end portion.
- the solid line represents the tooth portion 7a of Embodiment 1.
- the distal end portion 70 of the discharge-side lateral face 7b of the tooth portion 7a contacts the discharge-side wall portion 5ba for a longer period of time during reverse rotation than the center portion and proximal portion of the discharge-side lateral face 7b, so damage or abrasion easily occurs at the distal end portion 70.
- the angle formed by the surface 7d of the tooth portion 7a and the suction-side lateral face 7c is an obtuse angle; whereas the angle formed by the surface 7d and the discharge-side lateral face 7b is an acute angle, that is, the discharge-side thickness of the tooth portion 7a is smaller.
- the angle formed by the surface 7d and the discharge-side side-surface 7b is an acute angle only at the discharge-side distal end portion, not entire portion of the discharge side of the tooth portion 7a.
- the angle formed by the surface 7d and the discharge-side lateral face 7b is an obtuse angle.
- the fact that the thickness of the discharge-side distal end portion of the tooth portion 7a is smaller also causes the tooth portion 7a to be easily damaged.
- the reason why the tooth portion 7a is formed such that the above-described angle is changed to an acute angle or an obtuse angle depending on a location is that the angle of tangent relative to the discharge-side wall portion 5b of the screw groove 5a approaches a right angle toward the discharge side.
- Embodiment 1 to avoid damage on the gate rotor 7 before it happens, the following structure is employed.
- Fig. 6 is a schematic enlarged view showing part of the screw compressor according to Embodiment 1 of the present invention.
- each tooth portion 7a has a shape in which a corner portion formed by the discharge-side lateral face 7b and distal end face 7e of the existing tooth portion 7a as represented by dashed line in Fig. 5 is cut out.
- the space 12 is uniform, and a space dimension is preferably set to, for example, 20 ⁇ m to 70 ⁇ m. This space 12 is constantly formed while the tooth portion 7a is in mesh with the screw groove 5a.
- the tooth portion 7a moves toward the discharge-side wall portion 5ba of the screw rotor 5 and contacts the discharge-side wall portion 5ba as shown in Fig. 5 ; however, a portion that contacts the discharge-side wall portion 5ba is the center to proximal portion of the tooth portion 7a, and the distal end portion does not contact the discharge-side wall portion 5ba. Thus, damage on the distal end portion of each tooth portion 7a is suppressed.
- the space 12 is provided between the discharge-side wall portion 5ba and the distal end portion of each of the tooth portions 7a of each gate rotor 7, so damage on and abrasion of the distal end portion of each tooth portion 7a of each gate rotor 7 during reverse rotation are suppressed.
- a portion that contacts the discharge-side wall portion 5ba in the tooth portion 7a is the center portion to proximal portion of each tooth portion 7a.
- each tooth portion 7a In the center to proximal portion of each tooth portion 7a, the angle formed by the suction-side lateral face 7c of the tooth portion 7a and the surface 7d is not an acute angle unlike the distal end portion but an obtuse angle, so the center to proximal portion has high strength.
- damage on the gate rotors 7 is reduced, and deterioration of performance by aging is reduced.
- each tooth portion 7a is obtained by just changing the distal end shape of each tooth portion of the existing configuration in which the facewidth is the same from the proximal portion to the distal end portion, so the space 12 is easily applicable to the existing products as well.
- Embodiment 1 as a configuration to form a space between the distal end portion of each tooth portion 7a and the discharge-side wall portion 5ba, the distal end-side facewidth of each tooth portion 7a is smaller than the proximal end-side facewidth of the tooth portion 7a because the position of the distal end portion 7ba of the discharge-side lateral face 7b of each tooth portion 7a shifts toward the suction side.
- Example 1 another mode different from that of Embodiment 1 will be described as a configuration to form a space between the distal end portion of each tooth portion 7a and the discharge-side wall portion 5ba.
- differences from Embodiment 1 will be mainly described, and components not described in Example 1 are similar to those of Embodiment 1.
- Fig. 7 is a schematic sectional view of an essential portion of a screw compressor according to Embodiment 2
- Fig. 8 is an expansion plan of a groove bottom of each screw groove of the screw compressor according to Example 1.
- Example 1 during reverse rotation, a region 5c facing the distal end portion of each tooth portion 7a in the discharge-side wall portion 5ba is located on the discharge side as compared to the other region, and a space 13 is formed between the distal end portion of each tooth portion 7a and the discharge-side wall portion 5ba.
- the alternate long and two short dashed line represents the location of the discharge-side wall portion 5ba in the other region that does not form the space 13 in the discharge-side wall portion 5ba.
- the region 5c is a region that lies in the groove direction (arrow direction in Fig. 8 ) of the screw groove 5a with a depth comparable to the thickness of the tooth portion 7a from the groove bottom within the discharge-side wall portion 5ba.
- the length of the space 13 in the groove direction is at least a length by which the tooth portion 7a moves along the screw groove 5a by the time the tooth portion 7a separates from the screw groove 5a from a state where the tooth portion 7a meshes with the screw groove 5a during reverse rotation. This space 13 is always formed while the tooth portion 7a is in mesh with the screw groove 5a.
- each space 13 is formed so as to extend in the groove direction of the screw groove 5a.
- the length of each space 13 in the groove direction is made smaller than that of Example 1, and the location of the space 13 is restricted.
- differences from Example 1 will be mainly described, and components not described in Example 2 are similar to those of Example 1.
- Fig. 9 is a schematic sectional view of an essential portion of a screw compressor according to Example 2.
- Fig. 10 is an expansion plan of a groove bottom of each screw groove of the screw compressor according to Example 2.
- Example 2 part of a region facing the distal end portion of the tooth portion 7a in the discharge-side wall portion 5ba during reverse rotation, that is, part of a region that extends in the groove direction (arrow direction in Fig. 10 ), is located on the discharge side as compared to the other region and, as a result, the groove width widens toward the discharge side and increases.
- the part is specifically an end region that is a distal end side in the rotation direction of the screw rotor 5 during reverse rotation within a region that extends in the groove direction (arrow direction in Fig. 10 ), that is, a region that communicates with the discharge port 2a (see Fig. 2 ).
- Example 2 improves performance during normal operation as compared to Embodiment 1 and Example 1.
- Example 2 advantageous effects similar to those of Example 1 are obtained, and additionally, since the location of the space 13 is restricted to the portion where damage on the tooth portion 7a can be suppressed more effectively than that of Example 1, that is, the region that communicates with the discharge port 2a, the following advantageous effect is obtained. That is, leakage of refrigerant through the space 13 during normal operation is suppressed as compared to those of Embodiment 1 and Example 1. Therefore, Example 2 improves performance during normal operation as compared to Embodiment 1 and Example 1.
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Description
- The present invention relates to a screw compressor and, more particularly, to measures to prevent damage to a gate rotor.
- Hitherto, there is known a single screw compressor that is used as a compressor for refrigeration and air-conditioning or other purposes. For example, a single screw compressor of
Patent Literature 1 includes a screw rotor and disc-shaped two gate rotors. The screw rotor has a plurality of screw grooves at its outer peripheral portion. A plurality of tooth portions is disposed radially in each of the gate rotors. The screw rotor is rotatably located inside a cylindrical wall. The cylindrical wall is provided inside a casing of the compressor. In addition, each of the gate rotors is formed such that the tooth portions extend through the cylindrical wall and mesh with the screw grooves. The two gate rotors have axes perpendicular to an axis of the screw rotor, and are symmetrically arranged across the screw rotor. Two compression chambers are defined inside the cylindrical wall by an inner periphery of the cylindrical wall, the screw grooves, and the tooth portions of the gate rotors. - In this single screw compressor, as the screw rotor rotates, the tooth portions of the gate rotors slide along the screw grooves, and the volumes of the compression chambers increase and then reduce. This operation is repeated. While the volumes of the compression chambers are increasing, refrigerant is sucked into the compression chambers. As the volumes of the compression chambers start reducing, the sucked refrigerant is compressed. As the screw grooves that define the compression chambers communicate with discharge ports, compressed high-pressure refrigerant is discharged from the compression chambers via the discharge ports.
- In the single screw compressor in operation, the screw rotor rotates while, of a pair of circumferentially opposing lateral faces of any one of the tooth portions of each gate rotor, the suction-side lateral face located on a suction side in a state where the tooth portion is in mesh with the screw groove and a wall portion that defines the screw groove are in contact with each other. On the other hand, while the single screw compressor is at rest, the screw rotor rotates in the reverse direction because of a difference in pressure, i.e., high and low, of refrigerant. As the screw rotor rotates in the reverse direction, the screw rotor rotates while the discharge-side lateral face of the pair of lateral faces of any one of the tooth portions and the wall portion that defines the screw groove are in contact with each other. Damage or abrasion may occur in the gate rotors because of this reverse rotation.
- In the single screw compressor of
Patent Literature 1, a difference in pressure, i.e., high and low, is reduced by refrigerant gas introduced into the screw grooves via economizer ports while the single screw compressor is at rest. Thus, duration of reverse rotation can be reduced. As a result, damage on or abrasion of each gate rotor can be suppressed. -
US5129800A discloses a single screw positive displacement compressor mechanism employing shallow gate rotor tooth penetration of the main rotor for purposes of reducing internal leakage and consequent compressor inefficiencies, wherein an interrupted main rotor thread for purposes of insuring multiple gate rotor teeth meshing with the drive portion of the main rotor thread, thereby reducing gate rotor tooth flank loads in the compressor section of the device. Provision is also made for main rotor thread baffling between the main rotor chamber section and the mechanism inlet. - Patent Literature 1:
Japanese Unexamined Patent Application Publication No. 2013-136957 - However, the structure of
Patent Literature 1 is based on the fact that economizer ports for introducing refrigerant gas into compression chambers are provided, so the structure ofPatent Literature 1 cannot be applied to a compressor with no economizer port. - The present invention has been attained taking the problem mentioned above into consideration, and an object thereof is to suppress damage on or abrasion of a gate rotor during reverse rotation of a screw rotor.
- A screw compressor according to an embodiment of the present invention, hereinafter
Embodiment 1, is defined in appendedclaim 1. - With the screw compressor according to the embodiment of the present invention, at least part of the region in which the distal end portion of each of the tooth portions of the gate rotor and the discharge-side wall portion forming the screw groove, with which the distal end portion of the tooth portion meshes, face each other during reverse rotation has a non-contact structure, so damage on or abrasion of the gate rotor can be suppressed.
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- [
Fig. 1] Fig. 1 is a schematic sectional view of a screw compressor according toEmbodiment 1 of the present invention. - [
Fig. 2] Fig. 2 is a perspective view showing a portion at which screw grooves of a screw rotor and tooth portions of gate rotors mesh with each other in the screw compressor according toEmbodiment 1 of the present invention. - [
Fig. 3] Fig. 3 illustrates an operation of the screw compressor according toEmbodiment 1 of the present invention. - [
Fig. 4] Fig. 4 illustrates a location of the tooth portion of the gate rotor relative to the screw groove during forward rotation of the screw rotor. - [
Fig. 5] Fig. 5 illustrates a location of the tooth portion of the gate rotor relative to the screw groove during reverse rotation of the screw rotor. - [
Fig. 6] Fig. 6 is a schematic enlarged view showing part of the screw compressor according toEmbodiment 1 of the present invention. - [
Fig. 7] Fig. 7 is a schematic sectional view of an essential portion of a screw compressor according to Example 1. - [
Fig. 8] Fig. 8 is an expansion plan of a groove bottom of each of screw grooves of the screw compressor according to Example 1. - [
Fig. 9] Fig. 9 is a schematic sectional view of an essential portion of a screw compressor according to Example 2. - [
Fig. 10] Fig. 10 is an expansion plan of a groove bottom of each of screw grooves of the screw compressor according to Example 2. - Hereinafter, embodiments of the present invention will be described with reference to the drawings. Examples 1 and 2 do not form part of the invention, but may be used for a better understanding of other aspects of the current invention.
- In the drawings, like reference signs denote the same or corresponding components, and this applies to the entire text of the specification. Furthermore, modes of elements described in the entire text of the specification are only illustrative, and the elements are not limited to these modes.
- A screw compressor according to
Embodiment 1 will be described with reference toFig. 1 to Fig. 6 . The screw compressor is connected to a refrigeration circuit that operates a vapor compression refrigeration cycle by circulating refrigerant. -
Fig. 1 is a schematic sectional view of the screw compressor according toEmbodiment 1 of the present invention. InFig. 1 , the right side is a suction side, and the left side is a discharge side.Fig. 2 is a perspective view showing a portion at which screw grooves of a screw rotor and tooth portions of gate rotors mesh with each other in the screw compressor according toEmbodiment 1 of the present invention. InFig. 2 , the upper right side indicates the suction side, and the lower left side indicates the discharge side. In addition, inFig. 2 , the solid arrow represents a rotation direction of a screw shaft, and the outline arrows represent how suction gas is sucked. - The
screw compressor 1 according to Embodiment 1 is a single screw compressor.Embodiment 1 will be described by way of an example of a single screw compressor of a type in which twogate rotors 7 are meshed with onescrew rotor 5. - As shown in
Fig. 1 , thescrew compressor 1 includes acylindrical casing 2, amotor 3, ascrew shaft 4, thescrew rotor 5, and other components. Themotor 3 is accommodated in thecasing 2. Thescrew shaft 4 is fixed to themotor 3, and is driven to rotate by themotor 3. Thescrew rotor 5 is fixed to thescrew shaft 4. An end portion of thescrew shaft 4, not fixed to themotor 3, is rotatably supported via abearing 6. - The
motor 3 is formed of astator 3a and amotor rotor 3b. Thestator 3a is fixed in thecasing 2 so as to be internally in contact thecasing 2. Themotor rotor 3b is disposed radially inside thestator 3a. Themotor rotor 3b, as well as thescrew rotor 5, is fixed to thescrew shaft 4, and is disposed along the same axis as thescrew rotor 5. - The
screw rotor 5 has a cylindrical shape. A plurality ofscrew grooves 5a is formed at an outer peripheral portion of thescrew rotor 5. Thescrew grooves 5a run spirally from one end of thescrew rotor 5 toward the other end thereof. One end side (right side inFig. 1 ) of thescrew rotor 5 is the suction side from which refrigerant gas is sucked, and the other end side (left side inFig. 1 ) is the discharge side from which refrigerant gas is discharged. The inside of thecasing 2 is separated by a separation wall (not shown) into a suction pressure space and a discharge pressure space. The suction pressure space is filled with low-pressure refrigerant gas. The discharge pressure space is filled with high-pressure refrigerant gas. One end side of thescrew rotor 5 communicates with the suction pressure space, and the other end side communicates with the discharge pressure space. - In addition, the two
gate rotors 7 are disposed on the sides of thescrew rotor 5 so as to be symmetric across thescrew shaft 4. - Each of the
gate rotors 7 has a disc shape. A plurality oftooth portions 7a is provided radially at an outer periphery of eachgate rotor 7 along a circumferential direction. Eachgate rotor 7 is supported by agate rotor support 8. Eachgate rotor 7 is disposed such that thetooth portions 7a are in mesh with thescrew grooves 5a of thescrew rotor 5.Compression chambers 10 are spaces each surrounded by thescrew groove 5a, thetooth portions 7a of thegate rotor 7, an inner periphery of thecasing 2, and aslide valve 9. Thecompression chambers 10 are filled with refrigerant gas sucked from the suction pressure space. Oil for lubricating thebearing 6 and sealing thecompression chambers 10 is also introduced into thecompression chambers 10. - In addition, the
slide valves 9 are disposed between the inner periphery of thecasing 2 and thescrew rotor 5. Each of theslide valves 9 is provided so as to be slidable in the direction of thescrew shaft 4 of thescrew rotor 5 along the outer periphery of thescrew rotor 5. Eachslide valve 9 has anopening port 9a. -
Discharge ports 2a (seeFig. 3 , given later) are formed in thecasing 2. Thedischarge ports 2a communicate with adischarge chamber 11 formed inside thecasing 2. High-pressure refrigerant gas and oil filled in thecompression chambers 10 pass through the openingports 9a of theslide valves 9 and then discharged to thedischarge chamber 11 via thedischarge ports 2a. - Next, the operation of the
screw compressor 1 according toEmbodiment 1 will be described. -
Fig. 3 illustrates the operation of the screw compressor according toEmbodiment 1 of the present invention. - As the
motor 3 is started in thescrew compressor 1, thescrew rotor 5 rotates with the rotation of thescrew shaft 4. Here, the screw rotates in the forward direction. Thegate rotors 7 also rotate with the rotation of thescrew rotor 5, and a suction stroke, a compression stroke, and a discharge stroke are repeated in eachcompression chamber 10. A compression operation will be described focusing on thecompression chamber 10 dotted inFig. 3 . -
Fig. 3(a) shows a state of thecompression chamber 10 in the suction stroke. Thescrew groove 5a in which thecompression chamber 10 is formed is meshed with thetooth portion 7a of thegate rotor 7. As thescrew rotor 5 is driven by themotor 3 to rotate in the direction indicated by the solid arrow, thistooth portion 7a relatively moves toward the terminal end of thescrew groove 5a. As a result, thegate rotor 7 rotates in the narrow outline arrow direction. Thecompression chamber 10 in the suction stroke is expanded to have the largest volume, communicates with a suction-side space of thecasing 2, and is filled with low-pressure refrigerant gas. - As the
screw rotor 5 further rotates, simultaneously with this rotation, thetooth portion 7a of thegate rotor 7 sequentially moves rotationally toward thedischarge port 2a. Thus, as shown inFig. 3(b) , the volume of thecompression chamber 10 reduces, and refrigerant gas in thecompression chamber 10 is compressed. - As the
screw rotor 5 continuously rotates, thecompression chamber 10 communicates with thedischarge port 2a, as shown inFig. 3(c) . Thus, high-pressure refrigerant gas compressed in the compression chamber is discharged via theopening port 9a of the slide valve 9 (not shown inFig. 3 ) to thedischarge chamber 11 through thedischarge port 2a. Refrigerant discharged to thedischarge chamber 11 is discharged to the outside of thescrew compressor 1. - During such operation of the
screw compressor 1, the pressure in thecompression chamber 10 gradually increases in order of (a), (b), and (c), and is high in (c). As the operation of thescrew compressor 1 is stopped, thescrew rotor 5 rotates in the reverse direction as described above because of a pressure difference between the low-pressure side and high-pressure side of thescrew rotor 5. As thescrew rotor 5 rotates in the reverse direction, the pressure in thecompression chamber 10 is reduced to be lower than the suction-side pressure, and, when thegate rotor 7 has the existing configuration to which no improvement of the present invention is applied, thegate rotor 7 is damaged. This phenomenon will be described later with reference toFig. 4 andFig. 5 . -
Fig. 4 illustrates a location of the tooth portion of the gate rotor relative to the screw groove during forward rotation of the screw rotor.Fig. 5 illustrates a location of the tooth portion of the gate rotor relative to the screw groove during reverse rotation of the screw rotor.Fig. 4 andFig. 5 both show an expansion plan of one screw groove together with the tooth portion of the gate rotor, meshed with the screw groove. The arrow inFig. 4 indicates a moving direction during forward rotation of thescrew rotor 5. The arrow inFig. 5 indicates a moving direction of thescrew rotor 5 during reverse rotation. In addition, inFig. 4 andFig. 5 , the right side is the suction side, and the left side is the discharge side. - During operation of the
screw compressor 1, that is, while thescrew rotor 5 is rotating in the forward direction, thetooth portion 7a of thegate rotor 7 contacts a suction-side wall portion 5bb that is a wall portion on the suction side, of twowall portions 5b forming thescrew groove 5a with which thetooth portion 7a meshes as shown inFig. 2 andFig. 4 . More specifically, a suction-side lateral face 7c of thetooth portion 7a contacts the suction-side wall portion 5bb. The suction-side lateral face 7c is, of a pair of circumferentially opposing lateral faces of thetooth portion 7a, the lateral face on the suction side in a state where thetooth portion 7a is in mesh with thescrew groove 5a. Hereinafter, of the pair of circumferentially opposing lateral faces of thetooth portion 7a, the lateral face on the discharge side is referred to as the discharge-sidelateral face 7b. In addition, of the twowall portions 5b, the discharge-side wall portion is referred to as discharge-side wall portion 5ba. - On the other hand, as the
screw rotor 5 rotates in the reverse direction and, as a result, the pressure in thecompression chamber 10 is reduced to be lower than the pressure in a suction chamber, a pressing force acts on thegate rotor 7 in a direction opposing to that during operation, and the discharge-sidelateral face 7b of thetooth portion 7a contacts the discharge-side wall portion 5ba as shown inFig. 5 . The portion represented by dotted line inFig. 5 shows the shape of the tooth portion of existing technologies in which the width of thetooth portion 7a is set to the same width from the proximal portion to the distal end portion. The solid line represents thetooth portion 7a ofEmbodiment 1. - When the
tooth portion 7a of thegate rotor 7 is in mesh with thescrew rotor 5 during reverse rotation, the discharge-sidelateral face 7b of thetooth portion 7a contacts the discharge-side wall portion 5ba. Adistal end portion 70 of the discharge-sidelateral face 7b of thetooth portion 7a constantly contacts the discharge-side wall portion 5ba during reverse rotation. - A discussion will be made focusing on the
tooth portion 7a that is in mesh with thescrew groove 5a communicating with thedischarge port 2a at the time of switching from forward rotation to reverse rotation. In the state shown inFig. 2 , thetooth portion 7a communicating with thedischarge port 2a is not in contact with the discharge-side wall portion 5ba from the center portion to the proximal portion within the discharge-sidelateral face 7b of thetooth portion 7a, and only thedistal end portion 70 contacts the discharge-side wall portion 5ba. Until thetooth portion 7a separates from thescrew groove 5a as a result of reverse rotation in this state, thedistal end portion 70 of the discharge-sidelateral face 7b of thetooth portion 7a constantly contacts the discharge-side wall portion 5ba. - In this way, the
distal end portion 70 of the discharge-sidelateral face 7b of thetooth portion 7a contacts the discharge-side wall portion 5ba for a longer period of time during reverse rotation than the center portion and proximal portion of the discharge-sidelateral face 7b, so damage or abrasion easily occurs at thedistal end portion 70. - In addition, as shown in
Fig. 4 andFig. 5 , in thetooth portion 7a of thegate rotor 7, the angle formed by thesurface 7d of thetooth portion 7a and the suction-side lateral face 7c is an obtuse angle; whereas the angle formed by thesurface 7d and the discharge-sidelateral face 7b is an acute angle, that is, the discharge-side thickness of thetooth portion 7a is smaller. In thetooth portion 7a of thegate rotor 7, the angle formed by thesurface 7d and the discharge-side side-surface 7b is an acute angle only at the discharge-side distal end portion, not entire portion of the discharge side of thetooth portion 7a. In the remaining portion, the angle formed by thesurface 7d and the discharge-sidelateral face 7b is an obtuse angle. The fact that the thickness of the discharge-side distal end portion of thetooth portion 7a is smaller also causes thetooth portion 7a to be easily damaged. The reason why thetooth portion 7a is formed such that the above-described angle is changed to an acute angle or an obtuse angle depending on a location is that the angle of tangent relative to the discharge-side wall portion 5b of thescrew groove 5a approaches a right angle toward the discharge side. - In
Embodiment 1, to avoid damage on thegate rotor 7 before it happens, the following structure is employed. -
Fig. 6 is a schematic enlarged view showing part of the screw compressor according toEmbodiment 1 of the present invention. - In
Embodiment 1, as shown inFig. 6 , aspace 12 is provided between the distal end portion of eachtooth portion 7a and the discharge-side wall portion 5ba. That is, the position of the distal end portion 7ba of the discharge-sidelateral face 7b of thetooth portion 7a is located on the suction side as compared with the other portion of thetooth portion 7a, and the facewidth of the distal end portion of eachtooth portion 7a is smaller than the facewidth of the other portion of thetooth portion 7a. More specifically, eachtooth portion 7a has a shape in which a corner portion formed by the discharge-sidelateral face 7b anddistal end face 7e of the existingtooth portion 7a as represented by dashed line inFig. 5 is cut out. In this way, in a state where thetooth portion 7a is in mesh with thescrew groove 5a, the distal end portion 7ba of the discharge-sidelateral face 7b of thetooth portion 7a does not contact the discharge-side wall portion 5ba, that is, a non-contact structure is provided. - In each of the
tooth portions 7a of eachgate rotor 7, thespace 12 is uniform, and a space dimension is preferably set to, for example, 20 µm to 70 µm. Thisspace 12 is constantly formed while thetooth portion 7a is in mesh with thescrew groove 5a. - Due to the above configuration, during reverse rotation, the
tooth portion 7a moves toward the discharge-side wall portion 5ba of thescrew rotor 5 and contacts the discharge-side wall portion 5ba as shown inFig. 5 ; however, a portion that contacts the discharge-side wall portion 5ba is the center to proximal portion of thetooth portion 7a, and the distal end portion does not contact the discharge-side wall portion 5ba. Thus, damage on the distal end portion of eachtooth portion 7a is suppressed. - According to
Embodiment 1, thespace 12 is provided between the discharge-side wall portion 5ba and the distal end portion of each of thetooth portions 7a of eachgate rotor 7, so damage on and abrasion of the distal end portion of eachtooth portion 7a of eachgate rotor 7 during reverse rotation are suppressed. With thespace 12 provided in this way, during reverse rotation, a portion that contacts the discharge-side wall portion 5ba in thetooth portion 7a is the center portion to proximal portion of eachtooth portion 7a. In the center to proximal portion of eachtooth portion 7a, the angle formed by the suction-side lateral face 7c of thetooth portion 7a and thesurface 7d is not an acute angle unlike the distal end portion but an obtuse angle, so the center to proximal portion has high strength. Thus, also in this regard, damage on thegate rotors 7 is reduced, and deterioration of performance by aging is reduced. - In addition, to suppress damage on the
gate rotors 7 in this way, no complicated control mechanism or component needs to be provided, and merely thespace 12 just needs to be provided, so suppression of damage on thegate rotors 7 is easily achieved without increasing the number of components. In addition, in providing thespace 12, the shape of the distal end portion of eachtooth portion 7a is obtained by just changing the distal end shape of each tooth portion of the existing configuration in which the facewidth is the same from the proximal portion to the distal end portion, so thespace 12 is easily applicable to the existing products as well. - In
Embodiment 1, as a configuration to form a space between the distal end portion of eachtooth portion 7a and the discharge-side wall portion 5ba, the distal end-side facewidth of eachtooth portion 7a is smaller than the proximal end-side facewidth of thetooth portion 7a because the position of the distal end portion 7ba of the discharge-sidelateral face 7b of eachtooth portion 7a shifts toward the suction side. In contrast, in Example 1, another mode different from that ofEmbodiment 1 will be described as a configuration to form a space between the distal end portion of eachtooth portion 7a and the discharge-side wall portion 5ba. Hereinafter, differences fromEmbodiment 1 will be mainly described, and components not described in Example 1 are similar to those ofEmbodiment 1. -
Fig. 7 is a schematic sectional view of an essential portion of a screw compressor according toEmbodiment 2Fig. 8 is an expansion plan of a groove bottom of each screw groove of the screw compressor according to Example 1. - In Example 1, during reverse rotation, a
region 5c facing the distal end portion of eachtooth portion 7a in the discharge-side wall portion 5ba is located on the discharge side as compared to the other region, and aspace 13 is formed between the distal end portion of eachtooth portion 7a and the discharge-side wall portion 5ba. InFig. 8 , the alternate long and two short dashed line represents the location of the discharge-side wall portion 5ba in the other region that does not form thespace 13 in the discharge-side wall portion 5ba. - The
region 5c is a region that lies in the groove direction (arrow direction inFig. 8 ) of thescrew groove 5a with a depth comparable to the thickness of thetooth portion 7a from the groove bottom within the discharge-side wall portion 5ba. The length of thespace 13 in the groove direction is at least a length by which thetooth portion 7a moves along thescrew groove 5a by the time thetooth portion 7a separates from thescrew groove 5a from a state where thetooth portion 7a meshes with thescrew groove 5a during reverse rotation. Thisspace 13 is always formed while thetooth portion 7a is in mesh with thescrew groove 5a. - According to Example 1, advantageous effects similar to those of
Embodiment 1 are obtained. - In Example 1, each
space 13 is formed so as to extend in the groove direction of thescrew groove 5a. In Example 2, the length of eachspace 13 in the groove direction is made smaller than that of Example 1, and the location of thespace 13 is restricted. Hereinafter, differences from Example 1 will be mainly described, and components not described in Example 2 are similar to those of Example 1. -
Fig. 9 is a schematic sectional view of an essential portion of a screw compressor according to Example 2.Fig. 10 is an expansion plan of a groove bottom of each screw groove of the screw compressor according to Example 2. - In Example 2, part of a region facing the distal end portion of the
tooth portion 7a in the discharge-side wall portion 5ba during reverse rotation, that is, part of a region that extends in the groove direction (arrow direction inFig. 10 ), is located on the discharge side as compared to the other region and, as a result, the groove width widens toward the discharge side and increases. The part is specifically an end region that is a distal end side in the rotation direction of thescrew rotor 5 during reverse rotation within a region that extends in the groove direction (arrow direction inFig. 10 ), that is, a region that communicates with thedischarge port 2a (seeFig. 2 ). - With the
space 13 provided in this region, no contact occurs between thescrew rotor 5 and eachgate rotor 7 in the region that communicates with thedischarge port 2a during reverse rotation, that is, no contact occurs between the discharge-side wall portion 5ba of thescrew rotor 5 and the discharge-sidelateral face 7b of thegate rotor 7. Thus, a duration during which the distal end portion of eachgate rotor 7 contacts the discharge-side wall portion 5ba of thescrew rotor 5 shortens, so the effect of reducing damage to eachgate rotor 7 is sufficiently obtained. - In addition, by restricting the region in which the
space 13 is provided to the region that communicates with thedischarge port 2a within thescrew groove 5a, the length of thespace 13 in the groove direction is reduced to be shorter than that ofEmbodiment 2. In this way, when the length of thespace 13 in the groove direction reduces, leakage of refrigerant through thespace 13 during forward rotation, that is, during normal operation, is reduced. Therefore, Example 2 improves performance during normal operation as compared toEmbodiment 1 and Example 1. - According to Example 2, advantageous effects similar to those of Example 1 are obtained, and additionally, since the location of the
space 13 is restricted to the portion where damage on thetooth portion 7a can be suppressed more effectively than that of Example 1, that is, the region that communicates with thedischarge port 2a, the following advantageous effect is obtained. That is, leakage of refrigerant through thespace 13 during normal operation is suppressed as compared to those ofEmbodiment 1 and Example 1. Therefore, Example 2 improves performance during normal operation as compared toEmbodiment 1 and Example 1. - 1
screw compressor 2casing 2a discharge port 3motor 3a stator3b motor rotor 4screw shaft 5screw rotor 5a screw groove 5b wall portion 5ba discharge-side wall portion 5bb suction-side wall portion 5cregion 6bearing 7gate rotor 7a tooth portion 7b discharge-side lateral face 7badistal end portion 7c suction-side lateral 7eface 7d surfacedistal end face 8gate rotor support 9slide valve 9a opening port 10compression chamber 11discharge chamber 12space 13space 70 distal end portion
Claims (3)
- A screw compressor (1) comprising: a screw rotor (5) including a plurality of screw grooves (5a) on an outer periphery, one end of the screw rotor being a suction side of a fluid, an other end of the screw rotor being a discharge side of the fluid; and two gate rotors (7) each including a plurality of tooth portions (7a) to be meshed with the screw groove (5a) at an outer peripheral portion, each of the gate rotors (7) rotating with rotation of the screw rotor (5) to compress the fluid, wherein
during reverse rotation of the screw rotor (5), at least part of a region (5c) in which a distal end portion of each of the tooth portions (7a) and a discharge-side wall portion (5b) as a discharge-side wall forming the screw groove (5a), with which the distal end portion of the tooth portion (7a) meshes, face each other has a non-contact structure, wherein the non-contact structure is formed as a space (12) provided between the distal end portion of each of the tooth portions (7a) and the discharge-side wall portion (5b),
the screw compressor (1) being characterized in that: a facewidth of the distal end portion of each of the tooth portions (7a) is smaller than that of an other portion of the tooth portion (7a). - The screw compressor (1) of claim 1, wherein each of the tooth portions (7a) has a shape in which a corner portion of the distal end portion on the discharge side is cut out.
- The screw compressor (1) of claim 2, wherein the space (12) is uniform and has a dimension of 20 µm to 70 µm.
Applications Claiming Priority (1)
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PCT/JP2016/087623 WO2018109939A1 (en) | 2016-12-16 | 2016-12-16 | Screw compressor |
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EP3557063A1 EP3557063A1 (en) | 2019-10-23 |
EP3557063A4 EP3557063A4 (en) | 2019-11-27 |
EP3557063B1 true EP3557063B1 (en) | 2021-07-07 |
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EP16923645.2A Active EP3557063B1 (en) | 2016-12-16 | 2016-12-16 | Screw compressor |
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JP (1) | JPWO2018109939A1 (en) |
CN (1) | CN210127943U9 (en) |
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WO2024134863A1 (en) * | 2022-12-23 | 2024-06-27 | 三菱電機株式会社 | Screw compressor and refrigeration cycle device |
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US5129800A (en) * | 1991-07-17 | 1992-07-14 | The United States Of America As Represented By The Secretary Of The Navy | Single screw interrupted thread positive displacement mechanism |
JP3840899B2 (en) * | 2001-01-05 | 2006-11-01 | ダイキン工業株式会社 | Single screw compressor |
EP2228537A4 (en) * | 2007-12-07 | 2015-08-19 | Daikin Ind Ltd | Single screw compressor |
JP2013136957A (en) | 2011-12-28 | 2013-07-11 | Daikin Industries Ltd | Screw compressor |
JP2014126028A (en) * | 2012-12-27 | 2014-07-07 | Daikin Ind Ltd | Screw compressor |
JP6221777B2 (en) * | 2014-01-28 | 2017-11-01 | オムロン株式会社 | Cylinder lock |
JP6301735B2 (en) * | 2014-05-26 | 2018-03-28 | 大豊工業株式会社 | Thrust bearing |
JP2016017438A (en) * | 2014-07-07 | 2016-02-01 | ダイキン工業株式会社 | Single screw compressor |
JP2016020644A (en) * | 2014-07-14 | 2016-02-04 | ダイキン工業株式会社 | Single screw compressor |
JP2016037150A (en) * | 2014-08-07 | 2016-03-22 | 株式会社Fts | Attachment structure of sub tank of fuel tank |
-
2016
- 2016-12-16 JP JP2018556155A patent/JPWO2018109939A1/en active Pending
- 2016-12-16 WO PCT/JP2016/087623 patent/WO2018109939A1/en unknown
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EP3557063A1 (en) | 2019-10-23 |
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CN210127943U9 (en) | 2020-04-17 |
CN210127943U (en) | 2020-03-06 |
JPWO2018109939A1 (en) | 2019-07-04 |
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