CN205243956U - Rotatory circle micromatic setting of high speed centrifugation fan import stator - Google Patents

Rotatory circle micromatic setting of high speed centrifugation fan import stator Download PDF

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Publication number
CN205243956U
CN205243956U CN201520944488.3U CN201520944488U CN205243956U CN 205243956 U CN205243956 U CN 205243956U CN 201520944488 U CN201520944488 U CN 201520944488U CN 205243956 U CN205243956 U CN 205243956U
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CN
China
Prior art keywords
circle
guide bearing
micromatic setting
plain washer
centre
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Withdrawn - After Issue
Application number
CN201520944488.3U
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Chinese (zh)
Inventor
马永新
熊翠雯
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.)
Jiangsu Gl-Turbo Corp
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Jiangsu Gl-Turbo Corp
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 Jiangsu Gl-Turbo Corp filed Critical Jiangsu Gl-Turbo Corp
Priority to CN201520944488.3U priority Critical patent/CN205243956U/en
Application granted granted Critical
Publication of CN205243956U publication Critical patent/CN205243956U/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model relates to a rotatory circle micromatic setting of high speed centrifugation fan import stator, including the rotatory circle of import, hexagon socket head cap screw, eccentric cover, guide bearing, plain washer and centre circle, rotatory circle sets up in the centre circle inboardly, installs eccentric cover in the guide bearing, and guide bearing and inner circle are provided with the plain washer within a definite time, and eccentric cover, guide bearing and plain washer are installed through hexagon socket head cap screw and is circled in. The utility model discloses simple structure, the design compactness, convenient to use uses on the high speed centrifugation fan of suitable all specifications, is interference fit between eccentric cover and bearing, and the zero clearance is just imported and is formed rolling friction between rotatory circle and the guide bearing, reduces the resistance, can guarantee the rotation and enclose steady rotation, is favorable to ensureing the concentricity.

Description

A kind of rotation circle micromatic setting of high-speed centrifugal fan entry guide vane
Technical field
The utility model relates to a kind of rotation circle micromatic setting of high-speed centrifugal fan entry guide vane, belongs to frame for movement technical field.
Background technology
In the prior art, the rotation circle of high-speed centrifugal fan entry guide vane and centre circle are matched in clearance, spacing by spacing pressing plate. When rotation, rotation circle is plane contact with centre circle, and frictional force is large, and both radial fit gaps are larger, can produce rotation circle and centre circle decentraction, causes rotation to iris out existing bite phenomenon, causes the entry guide vane blade cannot normal rotation; Secondly the wall thickness of rotation circle is thinner, processing difficulties, and after processing, form error is larger, and concentricity is difficult to ensure.
Summary of the invention
The purpose of this utility model is to overcome deficiency of the prior art, and a kind of rotation circle micromatic setting of high-speed centrifugal fan entry guide vane simple in structure, compact to design is provided.
The utility model adopts following technical scheme: a kind of rotation circle micromatic setting of high-speed centrifugal fan entry guide vane, comprise import rotation circle, hexagon socket head cap screw, eccentric bushing, guide bearing, plain washer and centre circle, described import rotation circle is arranged at centre circle inner side, in described guide bearing, eccentric bushing is installed, between described guide bearing and centre circle, be provided with plain washer, described eccentric bushing, guide bearing and plain washer are arranged on centre circle by hexagon socket head cap screw.
Further, between described eccentric bushing and guide bearing, be interference fit.
Further, the external diameter center of described eccentric bushing and guide bearing endoporus centre deviation are a, and the span of a is 0.5~1.5mm.
Further, the surface of described guide bearing is W type and can forms rolling friction with import rotation circle.
The utility model is simple in structure, compact to design, easy to use, on the high-speed centrifugal fan of applicable all specifications, using, is interference fit between eccentric bushing and bearing, gapless, and form rolling friction between import rotation circle and guide bearing, reduce resistance, can ensure the uniform rotation of rotation circle, be conducive to guarantee concentricity.
Brief description of the drawings
Fig. 1 is the utility model structural principle schematic diagram.
Fig. 2 is local structure for amplifying schematic diagram of the present utility model.
Reference numeral: import rotation circle 1, hexagon socket head cap screw 2, eccentric bushing 3, guide bearing 4, plain washer 5, centre circle 6.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model will be further described.
As Figure 1-Figure 2, a kind of rotation circle micromatic setting of high-speed centrifugal fan entry guide vane, comprise import rotation circle 1, hexagon socket head cap screw 2, eccentric bushing 3, guide bearing 4, plain washer 5 and centre circle 6, import rotation circle 1 is arranged at centre circle 6 inner sides, eccentric bushing 3 is installed in guide bearing 4, between eccentric bushing 3 and guide bearing 4, it is interference fit, the external diameter center of eccentric bushing 3 and guide bearing 4 endoporus centre deviations are a, the span of a is 0.5~1.5mm, between guide bearing 4 and centre circle 6, be provided with plain washer 5, eccentric bushing 3, guide bearing 4 and plain washer 5 are arranged on centre circle 6 by hexagon socket head cap screw 2, the surface of guide bearing 4 is W type can form rolling friction with import rotation circle 1.
Operation principle: centered by guide bearing 4 endoporus, fine setting eccentric bushing 3, make pivot and centre circle 6 centres of import rotation circle 1, guide bearing 4 and import rotation circle 1 close contact, gapless, when operation, the 1 energy uniform rotation of import rotation circle, thus drive entry guide vane blade normal rotation.

Claims (4)

1. the rotation circle micromatic setting of a high-speed centrifugal fan entry guide vane, it is characterized in that: comprise import rotation circle (1), hexagon socket head cap screw (2), eccentric bushing (3), guide bearing (4), plain washer (5) and centre circle (6), described import rotation circle (1) is arranged at centre circle (6) inner side, eccentric bushing (3) is installed in described guide bearing (4), between described guide bearing (4) and centre circle (6), be provided with plain washer (5), described eccentric bushing (3), guide bearing (4) and plain washer (5) are arranged on centre circle (6) by hexagon socket head cap screw (2).
2. the rotation circle micromatic setting of high-speed centrifugal fan entry guide vane as claimed in claim 1, is characterized in that: between described eccentric bushing (3) and guide bearing (4), be interference fit.
3. the rotation circle micromatic setting of high-speed centrifugal fan entry guide vane as claimed in claim 1, is characterized in that: the external diameter center of described eccentric bushing (3) and guide bearing (4) endoporus centre deviation are a, and the span of a is 0.5~1.5mm.
4. the rotation circle micromatic setting of high-speed centrifugal fan entry guide vane as claimed in claim 1, is characterized in that: the surface of described guide bearing (4) is W type can form rolling friction with import rotation circle (1).
CN201520944488.3U 2015-11-24 2015-11-24 Rotatory circle micromatic setting of high speed centrifugation fan import stator Withdrawn - After Issue CN205243956U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520944488.3U CN205243956U (en) 2015-11-24 2015-11-24 Rotatory circle micromatic setting of high speed centrifugation fan import stator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520944488.3U CN205243956U (en) 2015-11-24 2015-11-24 Rotatory circle micromatic setting of high speed centrifugation fan import stator

Publications (1)

Publication Number Publication Date
CN205243956U true CN205243956U (en) 2016-05-18

Family

ID=55943041

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520944488.3U Withdrawn - After Issue CN205243956U (en) 2015-11-24 2015-11-24 Rotatory circle micromatic setting of high speed centrifugation fan import stator

Country Status (1)

Country Link
CN (1) CN205243956U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105298922A (en) * 2015-11-24 2016-02-03 江苏杰尔科技股份有限公司 Slewing ring fine-adjustment device for inlet guide vane of high-speed centrifugal fan
CN111664110A (en) * 2020-05-25 2020-09-15 中科澳能(北京)节能技术有限公司 Compressor inlet guide vane adjusting mechanism and control method thereof

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105298922A (en) * 2015-11-24 2016-02-03 江苏杰尔科技股份有限公司 Slewing ring fine-adjustment device for inlet guide vane of high-speed centrifugal fan
CN111664110A (en) * 2020-05-25 2020-09-15 中科澳能(北京)节能技术有限公司 Compressor inlet guide vane adjusting mechanism and control method thereof
CN111664110B (en) * 2020-05-25 2021-09-07 中国科学院工程热物理研究所 Compressor inlet guide vane adjusting mechanism and control method thereof

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
AV01 Patent right actively abandoned

Granted publication date: 20160518

Effective date of abandoning: 20171020

AV01 Patent right actively abandoned