CN109578277A - Blade-tape compressor - Google Patents
Blade-tape compressor Download PDFInfo
- Publication number
- CN109578277A CN109578277A CN201811137169.6A CN201811137169A CN109578277A CN 109578277 A CN109578277 A CN 109578277A CN 201811137169 A CN201811137169 A CN 201811137169A CN 109578277 A CN109578277 A CN 109578277A
- Authority
- CN
- China
- Prior art keywords
- discharge
- blade
- valve
- room
- cylinder body
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/30—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
- F04C18/344—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 inner member
-
- 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
- F04C18/344—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 inner member
- F04C18/3446—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 inner member the inner and outer member being in contact along more than one line or surface
-
- 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
- F04C28/24—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids characterised by using valves controlling pressure or flow rate, e.g. discharge valves or unloading valves
-
- 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
- F04C29/12—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
- F04C29/124—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet with inlet and outlet valves specially adapted for rotary or oscillating piston pumps
- F04C29/126—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet with inlet and outlet valves specially adapted for rotary or oscillating piston pumps of the non-return type
- F04C29/128—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet with inlet and outlet valves specially adapted for rotary or oscillating piston pumps of the non-return type of the elastic type, e.g. reed valves
-
- 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
- F04C2230/00—Manufacture
- F04C2230/60—Assembly methods
-
- 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
- F04C2240/70—Use of multiplicity of similar components; Modular construction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Rotary Pumps (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
The present invention provides a kind of blade-tape compressor that can be cut down number of components, assembling can be made simplified.It is formed through to be formed in back side panel (50) and the pilot channel (53) of a part on the pilot road that room (35a) is connected to back pressure chamber (41) will be discharged.Sphere (64) forms the spool for the open and close valve (80) that pilot channel (53) are opened and closed.It is formed with discharge valve portion (62) in discharge valve plate (60), and is formed with the restriction plate portion (63) of the movement of limitation sphere (64).
Description
Technical field
The present invention relates to blade-tape compressors.
Background technique
About previous blade-tape compressor, disclosed in Japanese Unexamined Patent Publication 2004-44414 bulletin (patent document 1)
A kind of following composition: in order to which early stage at the start promptly imports to blade backpressure annular groove as blade backpressure, stream
The pressure of body, and the access for connecting blade backpressure annular groove with discharge room is provided with the anti-valve (Japanese: チ ャ タ リ Application グ that quivers
Prevent バ Le Block).
Existing technical literature
Patent document
Patent document 1: Japanese Unexamined Patent Publication 2004-44414 bulletin
Summary of the invention
Subject to be solved by the invention
The anti-valve that quivers disclosed in patent document 1 is following composition: by what is formed in the access of blade backpressure annular groove side
Valve seat is blocked up by spherical spool from discharge room side seal, and applies valve opening to spool from blade backpressure annular groove side by compressed spring
The power in direction.Because being that compressed spring and spool are put into the composition covered after access with cover member, number of components is more, group
Dress is complicated.
The blade-tape compressor that number of components can be cut down the object of the present invention is to provide one kind and assembling can be made simplified.
A technical solution to solve project
In order to achieve the above objectives, blade-tape compressor of the invention has: rotary shaft, which is arranged to revolve
Turn;Rotor, which is arranged to integrally rotate with rotary shaft, and is formed on the outer periphery multiple blade grooves;Blade, the leaf
Piece can stretch out each blade groove being installed on submerging in multiple blade grooves;And cylinder body (English: cylinder), which exists
Inside is formed with the cylinder body room of storage rotor and blade.In cylinder body room, discharge chambe is marked by cylinder body, rotor and vane region.
In rotor, zoning goes out to assign blade the back pressure chamber of back pressure between each blade groove and blade of multiple blade grooves.Blade type
Compressor is also equipped with discharge room forming portion and valve cell.Discharge room forming portion is formed in inside for being compressed by discharge chambe
Refrigerant discharge discharge room.Valve cell zoning goes out discharge chambe and discharge room.It is formed in valve cell by discharge chambe and discharge
The discharge path of room connection and the pilot road for being connected to discharge room with back pressure chamber.Valve cell is laminated with to have and open discharge path
The discharge valve plate for the discharge reed valve portion closed, limitation are discharged the holding plate of the aperture of reed valve portion and form discharge leaf valve
The seat board of the valve seat in portion, and the valve for having the open and close valve that pilot road is opened and closed between valve plate and seat board is being discharged
Core.The restriction plate portion and discharge reed valve portion for limiting the movement of spool are formed together in discharge valve plate.
According to this constitution, restriction plate portion is also integrated with having the discharge discharge valve plate of reed valve portion, therefore can cut down
The number of components of blade-tape compressor.The open and close valve that pilot road is opened and closed is configured to include spool and the shifting for limiting spool
Dynamic restriction plate portion can be such that the assembling of open and close valve simplifies because being the composition without compressed spring.
In above-mentioned blade-tape compressor, being also possible to spool is sphere.According to this constitution, can be easily split
Valve closing is opened and closed.
In above-mentioned blade-tape compressor, it is also possible to the U by being formed with perforation discharge valve plate in a thickness direction
Width of the width than restriction plate portion of reed valve portion is discharged so that discharge reed valve portion and restriction plate portion be arranged in the gap of shape
Greatly.According to this constitution, the rigidity needed for capable of being assigned to discharge reed valve portion.
In above-mentioned blade-tape compressor, it is also possible to pilot road and extends in the axial direction of the rotation shaft.According to the structure
At open and close valve is the composition without compressed spring, without configuring compressed spring in pilot road, therefore even if along rotary shaft
Axial setting pilot road there will not be the case where thickness of wall member becomes larger.Moreover, the pilot road axially extended can be easy
Ground is processed.
In above-mentioned blade-tape compressor, the length for being also possible to pilot road is smaller than the diameter of sphere.According to the structure
At without configuring compressed spring in pilot road, so the length axially extended on pilot road can be made than previous small and ratio
The diameter of sphere is small.
The effect of invention
Blade-tape compressor according to the present invention can cut down number of components, and assembling can be made to simplify.
Detailed description of the invention
Fig. 1 is the cross-sectional view for showing the composition of blade-tape compressor of embodiment.
Fig. 2 is the cross-sectional view of the cylinder body of storage rotor shown in FIG. 1.
Fig. 3 is the main view of cover portion.
Fig. 4 is the exploded perspective view that a part of the blade-tape compressor of embodiment is constituted.
Fig. 5 is the top view that valve plate is discharged.
Fig. 6 is the cross-sectional view for showing the composition for the open and close valve that pilot road is opened and closed.
Fig. 7 is the cross-sectional view for showing the pilot road closed by open and close valve.
Fig. 8 is the cross-sectional view for showing the composition of blade-tape compressor of variation.
Description of symbols
10 blade-tape compressors, 11 front side shells, 13 bottom wall parts, the end face 13s, 14 cylinder bodies, 14c inner peripheral surface, 14d cylinder body
Room, 16 rotary shafts, 18 rotors, 18a blade groove, 18c outer peripheral surface, 18f front end face, 18r rear end face, 19 blades, 20 suction chambers, 21
Room, the reservoir compartment 35b, 36 cover portions, 41 back pressure chambers, 42 valve cells, 50 back side panels, 52 rows are discharged in discharge chambe, 22 suction passages, 35a
Channel out, 53 pilot channels, 53a storage space, 53b plane, the 53c conical surface, 55 back pressure feed troughs, 58,68,78 pin holes, 60 rows
Valve plate out, 62 discharge valve portions, 63 restriction plate portions, 64 spheres, 65,75 oil-through-holes, 66,67 gaps, 70 holding plates, 72 maintaining parts,
73 pressure supply holes, the 1st rib of 76a, the 2nd rib of 76b, 77 openings, 80 open and close valves, D diameter, L length, the direction of rotation R, W1, W2 wide
Degree.
Specific embodiment
Hereinafter, the blade-tape compressor about embodiment, is described with reference to the accompanying drawings.To the same part and comparable
Component marks same appended drawing reference, and repeat description is not repeated sometimes.
[composition]
Fig. 1 is the cross-sectional view for showing the composition of blade-tape compressor of embodiment.Blade-tape compressor 10 shown in FIG. 1
It is for example, equipped on the compressor of vehicle, is used in the refrigerant compression of idle call in the car.Blade-tape compressor 10 is installed on
The indoor engine of the engine of vehicle.
As shown in Figure 1, blade-tape compressor 10 mainly have front side shell 11, rotary shaft 16, rotor 18, valve cell 42 with
And cover portion 36.It includes the back side panel 50 of stacking that valve cell 42, which is configured to, valve plate 60 and holding plate 70 is discharged.In the following description
So-called axial, radial direction and the circumferential rotary shaft 16 and the axial of rotor 18, radial direction and circumferential direction indicated as rotary body.It will
Left direction in axial direction, in Fig. 1 is known as front, and right direction in axial direction, in Fig. 1 is known as rear.
Front side shell 11 has cylinder body 14 and bottom wall part 13.The inner peripheral surface 14c of cylinder body 14 is formed as ellipticity.In cylinder
The inside in body portion 14 is formed with cylinder body room 14d.Bottom wall part 13 has the end face 13s of zoning cylinder body room 14d.By cylinder body 14, bottom
Wall portion 13 and 50 zoning of back side panel go out cylinder body room 14d.
In front side, the peripheral side of shell 11 is formed with middle casing 12.It is formed between front side shell 11 and middle casing 12
There is suction chamber 20.Suction inlet 23 is formed in middle casing 12.It is connected to connector (English: joint) portion 24 in suction inlet 23,
Connector portions 24 are connected to sucking piping 25.Middle casing 12 is fixed relative to front side shell 11 using bolt (not shown).
Rotary shaft 16 is by the bearing and back side panel 50 (not shown) bearing for being set to front side shell 11 can be around rotary shaft
Heart rotation.Rotary shaft 16 penetrates through bottom wall part 13, prominent into cylinder body room 14d from the end face 13s of bottom wall part 13, extends to front side shell
The outside of body 11.
Rotor 18 is arranged to integrally rotate with rotary shaft 16.Rotor 18 is incorporated in cylinder body room 14d.Rotor 18
Front end face 18f it is opposite with the end face 13s of bottom wall part 13.The rear end face 18r and back side panel 50 of rotor 18 are opposite.
Fig. 2 is the cross-sectional view of the cylinder body 14 of storage rotor 18 shown in FIG. 1.As shown in Fig. 2, in the outer peripheral surface of rotor 18
18c is formed with multiple blade groove 18a.Blade 19 is separately installed in multiple blade groove 18a.Blade 19 be arranged to relative to
Blade groove 18a stretching is submerged.Lubricating oil is supplied respectively to multiple blade groove 18a.
As shown in Fig. 2, in rotor 18, the bottom surface by blade groove 18a and the blade 19 that is incorporated in blade groove 18a
Bottom surface zoning goes out back pressure chamber 41.Back pressure chamber 41 by the bottom surface of the end face 13s of bottom wall part 13, the bottom surface of blade groove 18a, blade 19 with
And 50 zoning of back side panel goes out.Lubricating oil in back pressure chamber 41 assigns back pressure to blade 19.
By the outer peripheral surface 18c of rotor 18, the inner peripheral surface 14c of cylinder body 14, in the circumferential adjacent 2 blades 19, bottom walls
The end face 13s and 50 zoning of back side panel in portion 13 go out discharge chambe 21.As shown in Fig. 2, in the present embodiment, in cylinder body room 14d
Inside it is formed with multiple discharge chambes 21.
As shown in Figure 1, being formed with suction passage 22 in bottom wall part 13.Suction passage 22 is by the inside of cylinder body room 14d and suction
It enters the room 20 connections.
As shown in Figure 1, 2, a pair of of passing away 52 is formed in back side panel 50.A pair of of passing away 52 is formed in around formation
The axle center of the rotation center of rotary shaft 16 separates 180 ° of position.
Fig. 3 is the main view of cover portion 36.Cover portion 36 is with by back side panel 50 shown in FIG. 1, discharge valve plate 60 and holding plate
70 modes for being clipped between front side shell 11 are fixed on front side shell 11.It is formed in cover portion 36 for the quilt in discharge chambe 21
The discharge room 35a for the refrigerant discharge having compressed.Cover portion 36 has to be formed as the discharge room for being formed with discharge room 35a in inside
The function in portion.Cover portion 36 has the peripheral wall portion 36c for surrounding discharge room 35a and aftermentioned reservoir compartment 35b.
The oil separation chamber 36s for having oily cylinder 36w in inside is formed in cover portion 36.Room 35a and oil separation chamber is discharged
Gone out by wall portion 36j come zoning.It is formed with communication access 36k in wall portion 36j, room 35a and oil separation chamber will be discharged in communication access 36k
36s connection.
It is formed with the 1st protruding portion 36a configured in the position of the rear end of rotary shaft 16 in wall portion 36j and is connected to the 1st and dash forward
Portion 36a and the cricoid 2nd protruding portion 36b extended downward out.1st protruding portion 36a and the 2nd protruding portion 36b from wall portion 36j to
Front is prominent.
In cover portion 36, abutted by the 1st protruding portion 36a and the 2nd protruding portion 36b with holding plate 70, to provide out to store
Grease chamber 35b.The oil discharge outlet 36v (Fig. 1) for being connected to reservoir compartment 35b with oil separation chamber 36s is formed in cover portion 36.
The outlet 37 being communicated with the outside is formed in cover portion 36.Connector portions 38 are connected in outlet 37.It is connecing
Head 38 is connected to the external discharge piping 39 extended towards blade-tape compressor 10.
The refrigerant being compressed by the discharge chambe 21 (Fig. 2) passes sequentially through back side panel 50 shown in FIG. 1, discharge valve plate
60, holding plate 70 and to discharge room 35a discharge.Narration forms back side panel 50, the dump valve of the discharge path of refrigerant in detailed below
The construction of plate 60 and holding plate 70.Fig. 4 is the exploded perspective view that a part of the blade-tape compressor of embodiment is constituted.
As shown in figure 4, back side panel 50, discharge valve plate 60, holding plate 70 have substantially disk-shaped shape as a whole.It protects
Holding plate 70 is the gasket that the surface of metal plate is covered with rubber.Valve plate 60 and holding plate 70, which is discharged, to be had than back side panel 50
The small thickness of thickness.In the central portion radially of each plate 50,60,70, be formed with to perforation in a thickness direction axis hole 51,
61,71.Inserted with rotary shaft 16 in axis hole 51,61,71.
The pin hole 58,68,78 penetrated through in a thickness direction is formed in each plate 50,60,70.Pin hole 58,68,78 is formed in
Position corresponding with the pin hole (not shown) of front side shell 11, and insert and have the pin of positioning (not shown), complete plate 50,
60, the positioning in 70 circumferential direction relative to front side shell 11.
In back side panel 50, a pair of of passing away 52 is formed with to perforation on the thickness direction of back side panel 50 and pilot is logical
Road 53.
Each comfortable cylinder body 14 of a pair of of passing away 52 and the opening that lands opposite at 18 close position of rotor.Back side panel 50
It is clamped and fastened between shell 11,12 and cover portion 36 together with discharge valve plate 60 and holding plate 70.
Pilot channel 53 is formed in the circumferential from a pair of of passing away 52 and equally spaced positions away from.A pair of discharge is logical
Road 52 is formed in 180 ° of position separated from each other in the circumferential, and pilot channel 53 is formed in each discharge from passing away 52
90 ° of position is left in the circumferential in channel 52.Pilot channel 53 is formed in (ratio more against the top than the axis of rotation position of rotary shaft 16
Axis hole 51 is against the top) position.
In the front surface opposite with front side shell 11 of back side panel 50, it is formed with the connectivity slot that can be connected to back pressure chamber 41
54 (Fig. 1).Pilot channel 53 is connected to connectivity slot 54.
In the rear surface opposite with discharge valve plate 60 of back side panel 50, the back pressure for being formed with a part recess of rear surface is supplied
To slot 55.Back pressure feed trough 55 is formed as leaving from axis hole 51.Back pressure feed trough 55 includes in radially extending radial slot.Diameter
Extend in the up-down direction to slot in the position of the axis of rotation position than rotary shaft 16 on the lower (on the lower than axis hole 51).Back
Pressure feed trough 55 includes the circumferential slot for being connected to the upper end of radial slot and extending in the circumferential.Circumferential slot is connected to back side panel 50
The connectivity slot 54 of front surface.
Fig. 5 is the top view that valve plate 60 is discharged.
By forming the gap 66,67 of the U-shaped of perforation discharge valve plate 60 in a thickness direction, to valve plate 60 be discharged being in
Notch is cut out to ligule, discharge valve portion 62 and the restriction plate portion 63 of leaf valve shape are formd, in the dump valve of single plate
Plate 60 is provided with discharge valve portion 62 and restriction plate portion 63.Passing away 52 is opened and closed in discharge valve portion 62.Restriction plate portion 63 is
Limit the retainer of the movement of the spool (sphere 64) of aftermentioned open and close valve 80.
A pair of discharge valve portion 62 is respectively arranged at and a pair of of passing away 52 opposite position respectively.Discharge valve portion 62 passes through
It is abutted and is left to be valve seat around the passing away 52 in back side panel 50, to open passing away 52
It closes.In the state that valve cell 42 is held between shell 11,12 and cover portion 36,62 row of being overlapped in of valve portion is discharged in the axial direction
Channel 52 out, observe from the rear, passing away 52 are discharged valve portion 62 and are covered with.
Restriction plate portion 63 is set to the position opposite with pilot channel 53.Valve cell 42 be held in shell 11,12 with
In the state of between cover portion 36, restriction plate portion 63 is overlapped in pilot channel 53 in the axial direction, observe from the rear, 53 quilt of pilot channel
Restriction plate portion 63 is covered with.
Restriction plate portion 63 is formed in the circumferential in a manner of corresponding with pilot channel 53 from a pair of discharge valve portion 62 etc.
Compartment of terrain positions away from.A pair of discharge valve portion 62 is formed in 180 ° of position separated from each other, restriction plate portion 63 in the circumferential
It is formed in the position that each discharge valve portion 62 from discharge valve portion 62 leaves 90 ° in the circumferential.Restriction plate portion 63 is formed in than rotation
The position of the axis of rotation position of shaft 16 against the top (against the top than axis hole 61).
Discharge valve portion 62 linearly extends along the periphery of discharge valve plate 60.Restriction plate portion 63 is in a generally radial direction
Linearly extend.The top in restriction plate portion 63 is towards radially inner side.Valve portion 62, which is discharged, has width W1, and restriction plate portion 63 has
Width W2.The width W1 that valve portion 62 is discharged is bigger than the width W2 in restriction plate portion 63.
Holding plate 70 has a pair of of maintaining part 72.The aperture of the limitation discharge valve portion 62 of maintaining part 72.In the formation of holding plate 70
There is the opening 77 of outer rim corresponding, with U-shaped with the discharge gap 66 of valve plate 60.Make holding plate 70, by that will open
Mouthfuls 77 open and the ligule that provides out is partially toward rear bending deformation, thus form maintaining part 72.The formation of maintaining part 72
To be left with the top towards ligule from discharge valve plate 60.Passing away 52, gap 66 and opening 77 are formd and will be pressed
The discharge path that contracting room 21 is connected to discharge room 35a.
A pair of of maintaining part 72 is respectively arranged at and a pair of of discharge valve portion 62 opposite position respectively.It is clamped in valve cell 42
In the state of between shell 11,12 and cover portion 36, maintaining part 72 is overlapped in discharge valve portion 62 in the axial direction.
The pressure supply hole 73 for penetrating through holding plate 70 in a thickness direction is formed in holding plate 70.73 shape of pressure supply hole
The opposite position in Cheng Yuyu restriction plate portion 63.In the state that valve cell 42 is held between shell 11,12 and cover portion 36,
Restriction plate portion 63 is overlapped in pressure supply hole 73 in axial direction.Pilot channel 53, gap 67 and pressure supply hole 73 form by
The pilot road that back pressure chamber 41 is connected to discharge room 35a.
Pressure supply hole 73 is formed in the circumferential from a pair of of maintaining part 72 and equally spaced positions away from.A pair of of maintaining part
72 are formed in 180 ° of position separated from each other in the circumferential, and pressure supply hole 73 is formed in each maintaining part 72 from maintaining part 72
90 ° of position is left in the circumferential.Pressure supply hole 73 is formed in the axis of rotation position than rotary shaft 16 and (compares axis hole against the top
71 against the top) position.
In the rear surface opposite with cover portion 36 (Fig. 1,3) of holding plate 70, it is formed with a part of outstanding 1st of rear surface
Rib 76a and the 2nd rib 76b.
1st rib 76a is set to the position of the rear end of rotary shaft 16.1st rib 76a has the 1st protruding portion 36a with cover portion 36
Outer rim same shape.2nd rib 76b has the outer rim same shape with the 2nd protruding portion 36b of cover portion 36.
In the state that valve cell 42 is held between shell 11,12 and cover portion 36, it is prominent that the 1st rib 76a is connected to the 1st
The portion top 36a, the 2nd rib 76b are connected to the top of the 2nd protruding portion 36b.1st rib 76a and the 2nd rib 76b provide out reservoir compartment 35b
(Fig. 1,3).
In discharge valve plate 60 and holding plate 70 are respective, the oil-through-hole 65,75 penetrated through in a thickness direction is formed in each other
Opposite position.Oil-through-hole 65,75 is formed in the lower section (lower section of axis hole 61,71) of the axis of rotation position of rotary shaft 16.?
In the state that valve cell 42 is held between shell 11,12 and cover portion 36, oil-through-hole 65 and oil-through-hole 75 are interconnected.Logical oil
Hole 65 is opposite with the lower end of the radial slot of back pressure feed trough 55 and is connected to connectivity slot 54.Oil-through-hole 75 is formed in the 2nd rib 76b
Inside, and be connected to reservoir compartment 35b (Fig. 1,3).
In the state that valve cell 42 is held between shell 11,12 and cover portion 36, discharge valve plate 60 is connected to rear side
Plate 50, the back pressure feed trough 55 being consequently formed in back side panel 50 are covered by discharge valve plate 60, and back pressure feed trough 55 is by discharge valve plate
60 cover.Form as a result, it is via oil-through-hole 75, oil-through-hole 65 and back pressure feed trough 55, from reservoir compartment 35b to back pressure chamber
The access of lubricating oil until 41.
Fig. 6 is the cross-sectional view for showing the composition for the open and close valve 80 that pilot channel 53 is opened and closed.In Fig. 6, enlargedly
It illustrates back side panel 50, in the construction that valve plate 60 and holding plate 70 are successively overlappingly kept in the order, formation is discharged
Near the pilot channel 53 of back side panel 50.Up and down direction in Fig. 6 is above-mentioned axial direction, lower direction, upper direction in Fig. 6
Respectively above-mentioned front, rear.
Between back side panel 50 and restriction plate portion 63, as the open and close valve 80 that pilot channel 53 is opened and closed spool and
Configured with sphere 64.Pilot channel 53 is in the front surface opening of back side panel 50.The rear surface of back side panel 50 is in pilot channel 53
Surrounding, a part are recessed and form the storage space 53a of storage sphere 64.The bottom surface of storage space 53a is as open and close valve 80
The valve seat of (sphere 64) functions.The bottom surface of storage space 53a has the plane parallel with the rear surface of back side panel 50
53b and relative to the inclined conical surface 53c of plane 53b.
It is connected to the conical surface 53c of back side panel 50 by sphere 64, is closed so that open and close valve 80 becomes.By sphere 64 from rear
Side plate 50 leaves, and opens so that open and close valve 80 becomes.Open and close valve 80 shown in fig. 6 is in an open state.
As shown in fig. 6, pilot channel 53 is upwardly extended in the axis of rotary shaft 16.Sphere 64 has diameter D.Pilot channel 53
It is designed smaller than the diameter D of sphere 64 in the length L that the axis of rotary shaft 16 upwardly extends.The length L in pilot channel 53 is designed
Thickness than back side panel 50 is small.
[work of blade-tape compressor 10]
Then, the work of the blade-tape compressor of embodiment 10 is illustrated.
In the blade-tape compressor 10 of embodiment, rotary shaft 16 receives the rotation from the driving sources such as motor or engine
Turn driving force and rotates.With the rotation of rotary shaft 16, rotor 18 is shown with arrows into Fig. 2 in cylinder body room 14d
Direction of rotation R rotation.With the rotation of rotor 18, the volume in discharge chambe 21 (Fig. 2) expands and reduces repeatedly.About rotor
18 direction of rotation R, the stroke that discharge chambe 21 expands volume become suction stroke, and the stroke that discharge chambe 21 reduces volume becomes pressure
Indention journey.
In suction stroke, the refrigerant that suction chamber 20 is directed to via suction inlet 23 utilizes the (figure of suction passage 22
1) with the connection of discharge chambe 21 out of suction passage 22 inflow discharge chambe 21.Volume in compression travel, in discharge chambe 21
It reduces, refrigerant is compressed.The refrigerant for the high pressure being compressed by discharge stroke in from discharge chambe 21 flow into passing away 52,
Pressing is discharged valve portion 62 and makes that the rearward bending deformation of valve portion 62 is discharged.Refrigerant is arranged by opening 77 to discharge room 35a
Out.Passing away 52 is formd a part of discharge chambe 21 and the discharge room 35a discharge path being connected to.
In such a series of stroke, it is subject to because of the centrifugal force being subject to when rotor 18 rotates and from back pressure chamber 41
Back pressure, blade 19 is from stress on the direction outstanding blade groove 18a, and the top of blade 19 is on one side and the inner peripheral surface of cylinder body room 14d
14c contacts one side moving in rotation.Have the top end face effect of blade 19 by blade from the elliptoid inner peripheral surface 14c of cylinder body 14
19 power pressed to the direction for submerging blade groove 18a.Because by the power acted on above-mentioned opposite direction, blade 19 with
The rotation of rotor 18 and stretch out and submerge repeatedly from blade groove 18a.It is contacted by blade 19 with the inner peripheral surface 14c of cylinder body room 14d, from
And zoning goes out discharge chambe 21 between adjacent blade 19 (referring to Fig. 2).
The refrigerant for being discharged to discharge room 35a flows to oil separation chamber 36s by the access 36k that communicates from discharge room 35a.System
Lubricating oil contained by cryogen is separated from refrigerant in oil separation chamber 36s.Refrigerant after isolating lubricating oil is via row
Outlet 37 is discharged to the external of blade-tape compressor 10.
The lubricating oil come is separated from refrigerant in oil separation chamber 36s, flows into reservoir compartment 35b from oil separation chamber 36s and is store
It is stored in the bottom of reservoir compartment 35b.Lubricating oil is due to the pressure of the refrigerant in reservoir compartment 35b successively via oil-through-hole 75, logical oil
Hole 65, back pressure feed trough 55 and connectivity slot 54 are supplied to back pressure chamber 41, act on back pressure to blade 19.
[effect and effect]
Then, the effect and effect of the blade-tape compressor 10 of above-mentioned embodiment are illustrated.
Under the steady running state of blade-tape compressor 10, the pressure for the lubricating oil stored in reservoir compartment 35b is enough
Height, therefore it is able to carry out the supply of stable back pressure.On the other hand, sometimes in the starting of blade-tape compressor 10, to store oil
The pressure that lubricating oil in the 35b of room applies does not rise sufficiently, and keeps blade 19 insufficient from blade groove 18a back pressure outstanding.?
In this case, it is unable to maintain that the state that the top of blade 19 is contacted with the inner peripheral surface 14c of cylinder body room 14d, blade 19 and cylinder body room
The inner peripheral surface 14c of 14d is intermittently collided, and it is therefore possible to generate noise (chattering, flutter).
For the phenomenon, in the blade-tape compressor 10 of embodiment, pilot channel 53 is opened and closed when stopping
Open and close valve 80 become opening state, in the starting of blade-tape compressor 10, discharge room 35a it is low with the pressure difference of back pressure chamber 41
In threshold value, open and close valve 80 is in an open state.Specifically, during the pressure difference of discharge room 35a and back pressure chamber 41 is small, such as Fig. 6
Shown, restriction plate portion 63 is indeformable, and sphere 64 is located at from the position that the conical surface 53 has left because of self weight.After sphere 64 is not connected to
Side plate 50 is formed with gap between sphere 64 and back side panel 50.It is compressed in discharge chambe 21 and is discharged to discharge room 35a's
The refrigerant gas of high pressure is flowed by the gap guide pressure passageway 53, and is supplied to back pressure chamber 41.53 shape of pilot channel
At a part on the pilot road for being connected to discharge room 35a with back pressure chamber 41.Pressure in back pressure chamber 41 promptly rises, to leaf
Piece 19 supplies enough back pressures, thus prevents the generation of flutter.
Pilot channel 53 is formed in the position of (more against the top than axis hole 51) against the top than the axis of rotation position of rotary shaft 16,
Pilot channel 53 is connected to the gas phase portion in discharge room 35a, and thus, it is possible to reliably supply to back pressure chamber 41 via pilot channel 53
To refrigerant gas, can promptly increase back pressure.
Pressure in discharge room 35a acts on restriction plate portion 63 via pressure supply hole 73.If the system in the 35a of room is discharged
The pressure of refrigerant gas rises, discharge room 35a and the pressure difference of back pressure chamber 41 become threshold value or more, then receives discharge room 35a
The restriction plate portion 63 of the pressure of interior refrigerant gas is bent, the bending deformation forwards of restriction plate portion 63.The restriction plate deformed
Portion 63 moves sphere 64 to close to the direction of back side panel 50.Sphere 64 is pressed to back side panel 50 by restriction plate portion 63, from
And as shown in fig. 7, sphere 64 is connected to back side panel 50, open and close valve 80 becomes closed state.In addition, Fig. 7 is to show by open and close valve
The cross-sectional view in the 80 pilot channels 53 closed.
If open and close valve 80 is closed, room 35a is discharged and pilot channel 53 becomes non-interconnected, become difficult to from discharge room
35a supplies refrigerant gas to back pressure chamber 41, and the back pressure supplied to back pressure chamber 41 becomes the lubricating oil supplied from reservoir compartment 35b.
In the blade-tape compressor of embodiment, as shown in figure 4, being formed through multiple passing aways in back side panel 50
52 and pilot channel 53.Back side panel 50 has the function of the seat board as discharge valve portion 62 and open and close valve 80.As shown in figure 5,
Discharge valve plate 60 is with as the discharge valve plate with multiple discharge valve portions 62 and restriction plate portion 63.As shown in Figure 6,7,
It is configured to include forming spool to the open and close valve 80 that the pilot channel 53 that room 35a is connected to back pressure chamber 41 is opened and closed will be discharged
Sphere 64 and the restriction plate portion 63 for pressing sphere 64 to back side panel 50.Restriction plate portion 63 and multiple discharge valve portions 62 are integrally
It constitutes.That is, restriction plate portion 63 is also integrated with by the integrated discharge valve plate 60 of multiple discharge valve portions 62.Restriction plate portion 63 has
For as the function of being kept and limited mobile restriction plate in such a way that sphere 64 is not fallen off.
As a result, compared with the anti-valve that quivers disclosed in patent document 1, number of components can be cut down, therefore blade can be lowered
The manufacturing cost of type compressor 10.Different from the anti-valve that quivers disclosed in patent document 1, open and close valve 80 is without compressed spring
It constitutes, therefore the assembling of open and close valve 80 can be made to simplify.Moreover, following situation reliably can be avoided: due to small pressure
Contracting spring is mistakenly with multiple state assemblings wound mutually, and thus the spring constant of compressed spring deviates significantly from design value and leads
The anti-valve that quivers is caused to become normally to be opened and closed.
In addition, restriction plate portion 63 makes open and close valve 80 close and deform from reaching in the starting of blade-tape compressor 10,
The deformed shape is maintained during the usual operating of blade-tape compressor 10.On the other hand, discharge valve portion 62 is in blade type
Become repeatedly during the usual operating of compressor 10, every time when the refrigerant that discharge chambe 21 is compressed by is discharged to discharge room 35a
Shape.Therefore, discharge valve portion 62 needs to have the rigidity bigger than restriction plate portion 63.As shown in figure 5, can be by being set as making dump valve
The composition width W1 in portion 62 bigger than the width W2 in restriction plate portion 63, to assign required rigidity to discharge valve portion 62.
In addition, in the case where configuring the previous composition of the compressed spring of the anti-valve that quivers in the access for being formed in back side panel,
In order to avoid the thickness of back side panel becomes larger, need to be formed as access relative to axially inclined.In the blade type pressure of embodiment
In contracting machine 10, as shown in Figure 6,7, pilot channel 53 is upwardly extended in the axis of rotary shaft 16.Open and close valve 80 is without compression bullet
The composition of spring, without configuring compressed spring in pilot channel 53, therefore even if along the axial setting pilot channel of rotary shaft 16
53, it there will not be the case where thickness of back side panel 50 becomes larger.Moreover, the pilot channel 53 extended in the axial direction can easily into
Row processing.
In addition, as shown in fig. 6, the length L that extends in the axial direction of pilot channel 53 is smaller than the diameter D of sphere 64.Open and close valve
80 be the composition without compressed spring, without configuring compressed spring in pilot channel 53, therefore can make pilot channel 53
The length L extended in the axial direction is smaller and smaller than the diameter D of sphere 64 than previous.Therefore, even if the axial direction along rotary shaft 16 is arranged
Pilot channel 53 there will not be the case where thickness of back side panel 50 becomes larger.
In addition, as shown in figure 5, restriction plate portion 63, which is formed in the circumferential from a pair of, is discharged what valve portion 62 was equally spaced left
Position, restriction plate portion 63 are big at a distance from discharge valve portion 62.Thereby, it is possible to reduce the vibration pair of the discharge valve portion 62 moved repeatedly
The influence that restriction plate portion 63 generates.In addition, can reduce discharge valve portion 62 is pushed open from passing away 52 and the system of the high pressure of flowing
The influence that refrigerant gas generates restriction plate portion 63.
In addition, the base end part in the restriction plate portion 63 of ligule is set to as shown in figure 5, restriction plate portion 63 extends radially
The top end part of radial outside, the restriction plate portion 63 of ligule is set to radially inner side.Therefore, can make to be opened and closed by open and close valve 80
Pilot channel 53 be formed in radial inside, therefore pilot channel 53 can be made more easily to be connected to back pressure chamber with short distance
41。
In addition, being formed with back pressure feed trough 55 in the rear surface of back side panel 50 as shown in Fig. 1,4.As shown in Figure 6,7, it arranges
Valve plate 60 is connected to the rear surface of back side panel 50 out.Back pressure feed trough 55 is covered by the way that valve plate 60 is discharged, so as to form from storage
Lubricating oil from grease chamber 35b to back pressure chamber 41 access.Therefore, the access of lubricating oil is formed with through hole is formed in back side panel 50
Previous composition compare, processing becomes easy.
The discharge valve plate 60 of embodiment is but also to can have 2 integrated compositions of discharge valve portion 62 more
Valve portion 62 is discharged.For example, it can be formed with the passing away of 2 or more (4 or more total) in 50 unilateral side of back side panel
52, discharge valve plate 60 is the composition of the discharge valve portion 62 with quantity identical as passing away 52.
The plate 50,60,70 of embodiment is to extend to the composition of the gabarit of compressor, but as shown in figure 8, be also possible to
It is fastenedly connected the packet of plate 50,60,70 in cylinder body in shell, and through bolt.Fig. 8 is the blade type compression for showing variation
The cross-sectional view of the composition of machine 10.In fig. 8, middle casing 12 is integrally formed with cover portion 36, and the periphery of cover portion 36 is more than rear side
Extend to the periphery of plate 50.Plate 50,60,70 wraps in cover portion 36.
Restriction plate portion 63 is the composition that sphere 64 is pressed by flexure, bending deformation, but not limited to this.Restriction plate portion 63
As long as being able to maintain sphere 64, even if can also be with without pressing.Alternatively, it is also possible to be set as following composition: limiting
Through hole is arranged in plate portion 63, and the refrigerant gas of discharge room 35a presses sphere 64 from through hole.
In embodiments, sphere 64 forms the spool of open and close valve 80, but the spool of open and close valve 80 is not limited to spherical, example
Such as, or the combined shaped of cone shape or circular cone and cylinder.But, if it is application sphere 64 as open and close valve
The composition of the embodiment of 80 spool, even if then sphere 64 rotates, the shape opposite with back side panel 50 be also spherical surface without
Variation, therefore the posture regardless of sphere 64, can be by whether sphere 64 be connected to the conical surface 53c of back side panel 50 and blocks
Pilot channel 53 switches the opening and closing of open and close valve 80.Therefore, easily open and close valve 80 can be opened and closed.
It is believed that presently disclosed embodiment is the content illustrated and not restrictive in all respects.The present invention
Range be not by above-mentioned explanation but indicated by claims, it is intended that including claims and and claims
Being had altered in impartial meaning and range.
Claims (5)
1. a kind of blade-tape compressor, has:
Rotary shaft, the rotary shaft are arranged to rotate;
Rotor, which is arranged to integrally rotate with the rotary shaft, and is formed on the outer periphery multiple blade grooves;
Blade, the blade can stretch out be installed on the multiple blade groove each blade groove with submerging;And
Cylinder body, the cylinder body are formed with the cylinder body room for storing the rotor and the blade in inside,
In the cylinder body room, discharge chambe is marked by the cylinder body, the rotor and the vane region,
In the rotor, zoning, which goes out, between each blade groove and the blade of the multiple blade groove assigns the blade
The back pressure chamber of back pressure,
The blade-tape compressor is also equipped with:
Room forming portion is discharged, which is formed with the refrigerant row for being compressed by the discharge chambe in inside
Discharge room out;With
Valve cell, the valve cell zoning go out the discharge chambe and the discharge room, and be formed with by the discharge chambe with it is described
The discharge path of discharge room connection and the pilot road for being connected to the discharge room with the back pressure chamber,
The valve cell is laminated with described in the discharge valve plate for having the discharge reed valve portion that the discharge path is opened and closed, limitation
The holding plate of the aperture of reed valve portion is discharged and forms the seat board of the valve seat of the discharge reed valve portion, and described
Have the spool that the pilot road is opened and closed between discharge valve plate and the seat board,
The restriction plate portion and the discharge reed valve portion for limiting the movement of the spool are formed together in the discharge valve plate.
2. blade-tape compressor according to claim 1,
The spool is sphere.
3. blade-tape compressor according to claim 1 or 2,
The gap for penetrating through the U-shaped of the discharge valve plate in a thickness direction by being formed with, so that the discharge reed be arranged
Valve portion and the restriction plate portion,
The width of the discharge reed valve portion is bigger than the width in the restriction plate portion.
4. blade-tape compressor described in any one of claim 1 to 3,
The pilot road extends in the axial direction of the rotation axis.
5. blade-tape compressor according to claim 2,
The length on the pilot road is smaller than the diameter of the sphere.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2017192146A JP2019065771A (en) | 2017-09-29 | 2017-09-29 | Vane compressor |
JP2017-192146 | 2017-09-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN109578277A true CN109578277A (en) | 2019-04-05 |
Family
ID=65919878
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201811137169.6A Withdrawn CN109578277A (en) | 2017-09-29 | 2018-09-28 | Blade-tape compressor |
Country Status (3)
Country | Link |
---|---|
JP (1) | JP2019065771A (en) |
KR (1) | KR20190038337A (en) |
CN (1) | CN109578277A (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2020203414A1 (en) | 2019-03-29 | 2020-10-08 | 京セラ株式会社 | Cutting insert, turning tool, and method for producing cut workpiece |
IT201900009213A1 (en) * | 2019-06-17 | 2020-12-17 | Vhit Spa | VOLUMETRIC MACHINE |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004044414A (en) * | 2002-07-09 | 2004-02-12 | Nippon Soken Inc | Variable displacement fluid machine |
US20050031465A1 (en) * | 2003-08-07 | 2005-02-10 | Dreiman Nelik I. | Compact rotary compressor |
CN103511268A (en) * | 2012-06-20 | 2014-01-15 | 株式会社丰田自动织机 | Tandem blade compressor |
JP2015140705A (en) * | 2014-01-28 | 2015-08-03 | カルソニックカンセイ株式会社 | compressor |
CN205047434U (en) * | 2015-09-10 | 2016-02-24 | 常州康普瑞汽车空调有限公司 | Vane formula compressor steady voltage ball spring valve |
-
2017
- 2017-09-29 JP JP2017192146A patent/JP2019065771A/en active Pending
-
2018
- 2018-09-17 KR KR1020180110800A patent/KR20190038337A/en not_active Application Discontinuation
- 2018-09-28 CN CN201811137169.6A patent/CN109578277A/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004044414A (en) * | 2002-07-09 | 2004-02-12 | Nippon Soken Inc | Variable displacement fluid machine |
US20050031465A1 (en) * | 2003-08-07 | 2005-02-10 | Dreiman Nelik I. | Compact rotary compressor |
CN103511268A (en) * | 2012-06-20 | 2014-01-15 | 株式会社丰田自动织机 | Tandem blade compressor |
JP2015140705A (en) * | 2014-01-28 | 2015-08-03 | カルソニックカンセイ株式会社 | compressor |
CN205047434U (en) * | 2015-09-10 | 2016-02-24 | 常州康普瑞汽车空调有限公司 | Vane formula compressor steady voltage ball spring valve |
Also Published As
Publication number | Publication date |
---|---|
JP2019065771A (en) | 2019-04-25 |
KR20190038337A (en) | 2019-04-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP3874300B2 (en) | Vane pump | |
JP2009275640A (en) | Scroll compressor | |
CN109578277A (en) | Blade-tape compressor | |
KR20090105964A (en) | Motor rotor and compressor with the same | |
CN103362806A (en) | Rotary vane compressor | |
CN102374156A (en) | Compressor | |
US4468180A (en) | Vane compressor having intermittent oil pressure to the vane back pressure chamber | |
US20190101119A1 (en) | Compressor | |
KR20110140120A (en) | Vane pump | |
US9169835B2 (en) | Piston-type compressor | |
CN109578278A (en) | Blade-tape compressor | |
JP5708570B2 (en) | Vane type compressor | |
EP1300593A2 (en) | Vane compressor | |
CN108779775A (en) | Scrawl compressor | |
CN102575672A (en) | Scroll fluidic device | |
JPH0968161A (en) | Compressor | |
JP2015175280A (en) | compressor | |
JP4970902B2 (en) | Scroll compressor | |
JP2014001697A (en) | Tandem type vane compressor | |
CN108506210A (en) | Blade-tape compressor | |
CN103511268A (en) | Tandem blade compressor | |
JP2990877B2 (en) | Swash plate compressor | |
CN108691766A (en) | Blade-tape compressor | |
JP2019056314A (en) | Vane-type compressor | |
JPS5817356B2 (en) | vane compressor |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WW01 | Invention patent application withdrawn after publication | ||
WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190405 |