CN209523920U - Vertical centrifugal compressor axial balancing device - Google Patents

Vertical centrifugal compressor axial balancing device Download PDF

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Publication number
CN209523920U
CN209523920U CN201822135660.7U CN201822135660U CN209523920U CN 209523920 U CN209523920 U CN 209523920U CN 201822135660 U CN201822135660 U CN 201822135660U CN 209523920 U CN209523920 U CN 209523920U
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CN
China
Prior art keywords
impeller
hub disk
radial seal
chamber
shroud
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Active
Application number
CN201822135660.7U
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Chinese (zh)
Inventor
冉素娟
孙鑫鑫
李志强
钱敏龙
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Shanghai Electric Blower Factory Co Ltd
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Shanghai Electric Blower Factory Co Ltd
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Priority to CN201822135660.7U priority Critical patent/CN209523920U/en
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Abstract

The utility model discloses a kind of vertical centrifugal compressor axial balancing devices, including impeller (1) and the impeller inlet axial seal (4) being arranged at impeller (1) shroud input end;It further include impeller hub disk radial seal (2) and impeller front disc radial seal (3);Impeller hub disk radial seal is fixed at the hub disk outlet end of impeller, forms hub disk chamber (P1) between the radial seal of impeller hub disk, impeller hub disk and the upper parts of impeller;The hub disk of impeller is equipped with several through holes (11), several through holes and hub disk chamber;Impeller front disc radial seal is fixed at the shroud outlet end of impeller, forms shroud chamber (P2) between impeller front disc radial seal, impeller front disc and the lower part of impeller, and shroud chamber is connected to by through-hole with shroud outlet end.The utility model effectively solves the problems, such as that vertical centrifugal compressor axial force is excessive by impeller hub disk chamber and impeller front disc chamber, simple to operation, guarantees the operating of unit normal reliable.

Description

Vertical centrifugal compressor axial balancing device
Technical field
The utility model relates to a kind of centrifugal compressor more particularly to a kind of vertical centrifugal compressor axial balancing devices.
Background technique
Centrofugal compressor structure is complicated, common horizontal arrangement.For certain particular applications, special construction requirement Vertical centrifugal compressor, can axial force size relation to unit normally, reliably operate.
Attached drawing 1 is referred to, the centrifugal compressor unit of the prior art is single-stage cantilever arrangement, and impeller 1 is relatively large in diameter, rotor Revolving speed is 4000rpm, and the shroud entrance of impeller 1 is disposed with impeller inlet axial seal 4, prevents the leakage current of gas.Work as unit When running at high speed, unit generates downward axial force, if cannot balance well, will cause unit that can not operate.
Summary of the invention
The purpose of this utility model is to provide a kind of vertical centrifugal compressor axial balancing devices, can effectively solve vertical The excessive problem of centrifugal compressor axial force guarantees that unit is normal, reliably operates.
The utility model is realized in this way:
A kind of vertical centrifugal compressor axial balancing device, the impeller including impeller and setting Pan Jinkouduanchu before the impeller Import axial seal;The vertical centrifugal compressor axial balancing device further includes the radial seal of impeller hub disk and impeller front disc Radial seal;Impeller hub disk radial seal is fixed at the hub disk outlet end of impeller, on the part of upper impeller, after impeller Hub disk chamber is formed between disk radial seal, impeller hub disk and the upper parts of impeller;Impeller hub disk runs through equipped with several Hole, several through holes and hub disk chamber;Impeller front disc radial seal is fixed at the shroud outlet end of impeller, is located at leaf On the part for taking turns lower part, shroud chamber, shroud are formed between impeller front disc radial seal, impeller front disc and the lower part of impeller Chamber is connected to by through-hole with impeller front disc outlet end.
The axial direction of several through holes is axial parallel with impeller.
Several described through holes are uniformly distributed along the circumferential direction of impeller.
The utility model compared with prior art, has the following beneficial effects:
1, the utility model hub disk chamber can obviously reduce axial force, while shroud chamber pressure is significantly greater than hub disk chamber Room, by the combination of hub disk chamber and shroud chamber, introduces impeller outlet gas to further decrease unit axial force To shroud chamber, meet limitation requirement of the vertical compressor unit to axial force.
2, the utility model increases radial seal structure, and radial seal structure belongs to static element, is easy to install and remove.
The utility model can effectively solve vertical centrifugal compressor by forming impeller hub disk chamber and impeller front disc chamber The excessive problem of axial force provides method simple to operation for Practical Project, guarantees that unit is normal, reliably operates.
Detailed description of the invention
Fig. 1 is the partial sectional view of prior art centrifugal compressor unit;
Fig. 2 is the partial sectional view of the utility model vertical centrifugal compressor axial balancing device.
In figure, 1 impeller, 11 through holes, 101 impeller hub disks, 102 impeller front discs, 2 impeller hub disk radial seals, before 3 impellers Disk radial seal, 4 impeller inlet axial seals, 5 through-holes, P1 hub disk chamber, P2 shroud chamber.
Specific embodiment
The utility model is described in further detail in the following with reference to the drawings and specific embodiments.
It refers to attached drawing 2, a kind of vertical centrifugal compressor axial balancing device, including impeller 1 and is arranged in 1 shroud of impeller Impeller inlet axial seal 4 at input end;Vertical centrifugal compressor axial balancing device further includes impeller hub disk radial seal 2 With impeller front disc radial seal 3;Impeller hub disk radial seal 2 is fixed at the hub disk outlet end of impeller 1, is located at 1 top of impeller Part on, between impeller hub disk radial seal 2, impeller hub disk 101 and the upper parts of impeller 1 formed hub disk chamber P1;Leaf It takes turns hub disk 101 and is equipped with several through holes 11, several through holes 11 are connected to hub disk chamber P1;Impeller front disc radial seal 3 are fixed at the shroud outlet end of impeller 1, on the part of 1 lower part of impeller, impeller front disc radial seal 3, impeller front disc Shroud chamber P2 is constituted between 102 and the lower part of impeller 1, shroud chamber P2 is connected by through-hole 5 and 1 shroud outlet end of impeller It is logical.
The axial direction of several through holes 11 is axial parallel with impeller 1, can reduce axial force.Described several Through hole 11 is uniformly distributed along the circumferential direction of impeller 1, is conducive to dynamic balance of impeller.
In circumferentially through hole 11 of impeller 1, and impeller hub disk radial seal 2 is arranged on disk 101 after the impeller, is formed Hub disk chamber P1 reduces axial force;In the shroud exit of impeller 1, arrangement impeller front disc radial seal 3, entrance arrange impeller Import axial seal 4, the shroud chamber constituted between impeller front disc radial seal 3, impeller front disc 102 and the lower part of impeller 1 Room P2 is sealing structure, and 1 exit gas of impeller is introduced shroud chamber P2 by the through-hole 5 on 1 lower part of impeller, thus into One step reduces axial force, meets limitation requirement of the vertical compressor unit to axial force.
The above is only the preferred embodiments of the present utility model only, is not intended to limit the protection scope of the utility model, Therefore, any modification, equivalent substitution, improvement and etc. made within the spirit and principle of the present invention, should be included in Within the protection scope of the utility model.

Claims (3)

1. a kind of vertical centrifugal compressor axial balancing device including impeller (1) and is arranged at impeller (1) shroud input end Impeller inlet axial seal (4);It is characterized in that: the vertical centrifugal compressor axial balancing device further includes impeller hub disk diameter To sealing (2) and impeller front disc radial seal (3);Impeller hub disk radial seal (2) is fixed on the hub disk outlet end of impeller (1) Place, be located at impeller (1) top part on, impeller hub disk radial seal (2), impeller hub disk (101) and impeller (1) top zero Hub disk chamber (P1) is formed between part;Impeller hub disk (101) be equipped with several through holes (11), several through holes (11) with Hub disk chamber (P1) connection;Impeller front disc radial seal (3) is fixed at the shroud outlet end of impeller (1), is located under impeller (1) On the part in portion, shroud chamber is formed between impeller front disc radial seal (3), impeller front disc (102) and the lower part of impeller (1) Room (P2), shroud chamber (P2) are connected to by through-hole (5) with impeller (1) shroud outlet end.
2. vertical centrifugal compressor axial balancing device according to claim 1, it is characterized in that: several described run through The axial direction in hole (11) is axial parallel with impeller (1).
3. vertical centrifugal compressor axial balancing device according to claim 1 or 2, it is characterized in that: several described Through hole (11) is uniformly distributed along the circumferential direction of impeller (1).
CN201822135660.7U 2018-12-19 2018-12-19 Vertical centrifugal compressor axial balancing device Active CN209523920U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201822135660.7U CN209523920U (en) 2018-12-19 2018-12-19 Vertical centrifugal compressor axial balancing device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201822135660.7U CN209523920U (en) 2018-12-19 2018-12-19 Vertical centrifugal compressor axial balancing device

Publications (1)

Publication Number Publication Date
CN209523920U true CN209523920U (en) 2019-10-22

Family

ID=68226764

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201822135660.7U Active CN209523920U (en) 2018-12-19 2018-12-19 Vertical centrifugal compressor axial balancing device

Country Status (1)

Country Link
CN (1) CN209523920U (en)

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