CN205047431U - Oil blanket structure of helical -lobe compressor projecting shaft - Google Patents

Oil blanket structure of helical -lobe compressor projecting shaft Download PDF

Info

Publication number
CN205047431U
CN205047431U CN201520689397.XU CN201520689397U CN205047431U CN 205047431 U CN205047431 U CN 205047431U CN 201520689397 U CN201520689397 U CN 201520689397U CN 205047431 U CN205047431 U CN 205047431U
Authority
CN
China
Prior art keywords
helical
axle sleeve
projecting shaft
lobe compressor
labyrinth seal
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.)
Active
Application number
CN201520689397.XU
Other languages
Chinese (zh)
Inventor
张开闯
吴霞俊
朱振中
陈锐
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shengang Wuxi Compressor Co.,Ltd.
Original Assignee
Wuxi Compressor Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wuxi Compressor Co Ltd filed Critical Wuxi Compressor Co Ltd
Priority to CN201520689397.XU priority Critical patent/CN205047431U/en
Application granted granted Critical
Publication of CN205047431U publication Critical patent/CN205047431U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model provides an oil blanket structure of helical -lobe compressor projecting shaft, it can solve the sealed problem that requires of current skeleton oil blanket incompatibility helical -lobe compressor. It includes projecting shaft, axle sleeve and end cover, and the axle sleeve suit is in the projecting shaft periphery and seal its characterized in that through O shape sealing washer between projecting shaft and the axle sleeve: it still includes the labyrinth seals seat, and the labyrinth seals seat is adorned admittedly on the end cover and to pass through O shape sealing washer sealed with the end cover, and the labyrinth seals seat is the labyrinth seals seat of contrahelical, the labyrinth seals seat cover adorn in the axle sleeve periphery and between axle sleeve clearance fit, axle sleeve and labyrinth seals seat are provided with in helical -lobe compressor inner chamber one side and keep off oily structure.

Description

A kind of oil seal structure of helical-lobe compressor projecting shaft
Technical field
The utility model relates to the field of sealing technology of helical-lobe compressor, is specially a kind of oil seal structure of helical-lobe compressor projecting shaft.
Background technique
In small-sized screw compressor, general projecting shaft many employings outside framework oil seal seals the leakage of main frame interior oil.Usual outside framework oil seal has certain requirement to PV value, and it requires that PV value is unsuitable too high, and outside framework oil seal installs the special frock of needs, and it installs complexity; In addition, requiring after outside framework oil seal installation can not be excessive with the degree of eccentricity of axle, and bias is excessive easily to be caused balladeur train oil seal lip and be coupling tactile uneven, thus easily produces leakage; And outside framework oil seal also belongs to easily damaged parts, often need change, thus can affect the continuous operating time of helical-lobe compressor and operating cost is high.Therefore, the helical-lobe compressor higher for PV value, operating mode is comparatively severe, existing outside framework oil seal is difficult to meet seal request.
Summary of the invention
For the problems referred to above, the utility model provides a kind of oil seal structure of helical-lobe compressor projecting shaft, and it can solve the problem that existing outside framework oil seal is not suitable with helical-lobe compressor seal request.
Its technological scheme is, a kind of oil seal structure of helical-lobe compressor projecting shaft, it comprises projecting shaft, axle sleeve and end cap, described axle sleeve is set in described projecting shaft periphery and is sealed by O-ring seals between described projecting shaft and axle sleeve, it is characterized in that: it also comprises labyrinth seal seat, described labyrinth seal seat to be installed on described end cap and to be sealed by O-ring seals with described end cap, described labyrinth seal seat is the labyrinth seal seat of reverse acting spiral, described labyrinth seal cover for seat be loaded on described axle sleeve periphery and and Spielpassung between described axle sleeve, described axle sleeve and labyrinth seal seat are positioned at described helical-lobe compressor inner chamber side and are provided with oil baffle structure.
Further, described oil baffle structure comprises flinger ring and gear oil groove, the outer circumferential face that described axle sleeve is positioned at described helical-lobe compressor inner chamber side is provided with described flinger ring, described labyrinth seal seat is positioned on described helical-lobe compressor inner chamber one side end face and is provided with gear oil groove, leaves clearance D between the bottom surface of described gear oil groove and the end face of described flinger ring.
Further, described clearance D is 1mm-2mm.
Further, the inner peripheral surface of described labyrinth seal seat has annular drain pan, has spill port in described labyrinth seal seat, and described spill port is communicated with described annular drain pan.
The beneficial effect of oil seal structure of the present utility model is: it is not by the restriction of PV value, and structure is simple, mounting or dismounting are convenient, good sealing effect, long service life, can be formed between the labyrinth seal seat of helical-lobe compressor reverse acting spiral in operation process and axle sleeve by the spiral air flow of atmospheric side to the inner pumping of helical-lobe compressor, thus effectively stop the oil of compressor inside to outward leakage; And oil baffle structure effectively can reduce the oil mass that helical-lobe compressor flows to labyrinth seal in running, thus further ensure sealing effect.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of the oil seal structure of a kind of helical-lobe compressor projecting shaft of the utility model;
Fig. 2 is I place close-up schematic view in Fig. 1;
Fig. 3 is II place's close-up schematic view in Fig. 1.
Embodiment
See Fig. 1, the oil seal structure of a kind of helical-lobe compressor projecting shaft of the utility model, it comprises projecting shaft 1, axle sleeve 2, end cap 3 and labyrinth seal seat 4, axle sleeve 2 is set in projecting shaft 1 periphery and is sealed by O-ring seals 9 between projecting shaft 1 and axle sleeve 2, labyrinth seal seat 4 to be installed on end cap 3 and and sealed by O-ring seals 10 between end cap 3, labyrinth seal seat 4 is the labyrinth seal seat of reverse acting spiral, reverse acting spiral wherein refers to that the spiral fluted Hand of spiral of labyrinth seal seat inner ring is contrary with the sense of rotation (observing from main frame private side) of compressor main shaft, Hand of spiral labyrinth seal seat 4 be set in axle sleeve 2 periphery and and Spielpassung between axle sleeve, axle sleeve 2 and labyrinth seal seat 4 are positioned at helical-lobe compressor inner chamber A side and are provided with oil baffle structure.In Fig. 1, B is atmospheric side.
See Fig. 2, oil baffle structure comprises flinger ring 5 and gear oil groove 6, the outer circumferential face that axle sleeve 2 is positioned at helical-lobe compressor inner chamber A side is provided with flinger ring 5, labyrinth seal seat 4 is positioned on helical-lobe compressor inner chamber A mono-side end face and is provided with gear oil groove 6, leave clearance D between the bottom surface of gear oil groove 6 and the end face of flinger ring 5, clearance D is 1mm-2mm; Wherein keeping off oil groove 6 can make oil droplet that end cap drips flow to bottom compressor box along gear oil groove 6, and the oil droplet that the axle sleeve 2 effectively preventing the oil droplet of helical-lobe compressor in running on end cap 3 to be directly dropped in rotation causes splashes; And flinger ring 5 is arranged on axle sleeve 2, at helical-lobe compressor in running, axle sleeve 2 rotates together along with projecting shaft 1, and flinger ring 5 effectively can stop the axial flow of the oil droplet of compressor inside, avoids the oil droplet of compressor inside to flow in labyrinth seal seat; Flinger ring 5 is with gear oil groove 6 mating reaction and the end face of flinger ring 5 retains the clearance D of 1mm-2mm with the bottom surface of gear oil groove 6, can reduce the oil mass flowing into labyrinth seal to a great extent, guarantee the reliable sealing performance of labyrinth seal.
See Fig. 3, the inner peripheral surface of labyrinth seal seat 4 has annular drain pan 7, has spill port 8 in labyrinth seal seat, and spill port 8 is communicated with annular drain pan 7.When helical-lobe compressor is in start or stopping process; the lower air-flow pumping DeGrain causing labyrinth seal seat of compressor rotary speed; now flowing into a small amount of oil droplet in labyrinth seal seat can flow into bottom compressor box by annular drain pan 7, spill port 8 under gravity, avoids oil leak.

Claims (4)

1. the oil seal structure of a helical-lobe compressor projecting shaft, it comprises projecting shaft (1), axle sleeve (2) and end cap (3), described axle sleeve (2) is set in described projecting shaft (1) periphery and is sealed by O-ring seals (9) between described projecting shaft (1) and axle sleeve (2), it is characterized in that: it also comprises labyrinth seal seat (4), described labyrinth seal seat (4) is installed in described end cap (3) and goes up and sealed by O-ring seals (10) with described end cap (3), the labyrinth seal seat that described labyrinth seal seat (4) is reverse acting spiral, described labyrinth seal seat (4) be set in described axle sleeve (2) periphery and and Spielpassung between described axle sleeve (2), described axle sleeve (2) and labyrinth seal seat (4) are positioned at described helical-lobe compressor inner chamber side and are provided with oil baffle structure.
2. the oil seal structure of a kind of helical-lobe compressor projecting shaft according to claim 1, it is characterized in that: described oil baffle structure comprises flinger ring (5) and gear oil groove (6), the outer circumferential face that described axle sleeve (2) is positioned at described helical-lobe compressor inner chamber side is provided with described flinger ring (5), described labyrinth seal seat (4) is positioned on described helical-lobe compressor inner chamber one side end face and is provided with gear oil groove (6), leaves clearance D between the bottom surface of described gear oil groove (6) and the end face of described flinger ring (5).
3. the oil seal structure of a kind of helical-lobe compressor projecting shaft according to claim 2, is characterized in that: described clearance D is 1mm-2mm.
4. according to the oil seal structure of described a kind of helical-lobe compressor projecting shaft arbitrary in claims 1 to 3, it is characterized in that: the inner peripheral surface of described labyrinth seal seat (4) has annular drain pan (7), have spill port (8) in described labyrinth seal seat (4), described spill port (8) is communicated with described annular drain pan (7).
CN201520689397.XU 2015-09-08 2015-09-08 Oil blanket structure of helical -lobe compressor projecting shaft Active CN205047431U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520689397.XU CN205047431U (en) 2015-09-08 2015-09-08 Oil blanket structure of helical -lobe compressor projecting shaft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520689397.XU CN205047431U (en) 2015-09-08 2015-09-08 Oil blanket structure of helical -lobe compressor projecting shaft

Publications (1)

Publication Number Publication Date
CN205047431U true CN205047431U (en) 2016-02-24

Family

ID=55341015

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520689397.XU Active CN205047431U (en) 2015-09-08 2015-09-08 Oil blanket structure of helical -lobe compressor projecting shaft

Country Status (1)

Country Link
CN (1) CN205047431U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105134601A (en) * 2015-09-08 2015-12-09 无锡压缩机股份有限公司 Oil seal structure for extension shaft of screw compressor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105134601A (en) * 2015-09-08 2015-12-09 无锡压缩机股份有限公司 Oil seal structure for extension shaft of screw compressor

Similar Documents

Publication Publication Date Title
CN201173293Y (en) Shell cover type slide bearing sealing structure
CN102954194B (en) Railway vehicle traveling gearbox sealing structure
WO2019184357A1 (en) Sealing structure of motor shaft extension end
CN202371169U (en) Sealing device for transmission shaft of speed reducer
CN201627928U (en) Combined sealing device of input shaft of gear box
CN202215736U (en) Sealing structure for traveling gearbox of railway vehicle
CN106286609A (en) A kind of punch press transmission shafts socket end seals structure
CN205047431U (en) Oil blanket structure of helical -lobe compressor projecting shaft
CN203476780U (en) Novel water cooling bearing pedestal for centrifugal fan
CN208078786U (en) The sealing structure at motor-shaft extending end
CN202327036U (en) Labyrinth type air exhaust system
CN204025371U (en) Combined bearing seal ring
CN105134601A (en) Oil seal structure for extension shaft of screw compressor
CN204827917U (en) Be suitable for roots blower who carries steam medium
CN204961224U (en) Oil gas seals seal structure of combination
CN211398303U (en) Bearing lubricating structure
CN104033576A (en) Vertical reducer seal structure and vertical reducer
CN203331726U (en) Oil storage car axle structure
CN206436734U (en) A kind of hub assembly sealing
CN202646398U (en) End cover type sliding bearing negative pressure resistance oil gas sealing device
CN104976116A (en) Roots blower for conveying steam medium
CN106838324B (en) Hybrid float-ring sealing device
CN206600269U (en) A kind of vacuum pump shaft seal structure
CN204573043U (en) A kind of combined type ring gear seal arrangement
CN205152702U (en) A sealing device for pressurized screen

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CP03 Change of name, title or address

Address after: 214145 No. 199, xixie Road, Hongshan street, Xinwu District, Wuxi City, Jiangsu Province

Patentee after: Shengang Wuxi Compressor Co.,Ltd.

Address before: 214145 Hongshan Photoelectric Industrial Park, Wuxi, Jiangsu (No. 199, tin Xie Road)

Patentee before: WUXI COMPRESSOR Co.,Ltd.

CP03 Change of name, title or address