CN102734216A - High-speed rotor structure of centrifugal blower - Google Patents
High-speed rotor structure of centrifugal blower Download PDFInfo
- Publication number
- CN102734216A CN102734216A CN201210250335XA CN201210250335A CN102734216A CN 102734216 A CN102734216 A CN 102734216A CN 201210250335X A CN201210250335X A CN 201210250335XA CN 201210250335 A CN201210250335 A CN 201210250335A CN 102734216 A CN102734216 A CN 102734216A
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- CN
- China
- Prior art keywords
- impeller
- gear shaft
- speed gear
- speed
- balancing disk
- Prior art date
Links
- 230000005484 gravity Effects 0.000 abstract description 7
- 238000005516 engineering processes Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 230000037250 Clearance Effects 0.000 description 1
- 210000003027 Ear, Inner Anatomy 0.000 description 1
- 210000003128 Head Anatomy 0.000 description 1
- 208000008425 Protein Deficiency Diseases 0.000 description 1
- 238000005273 aeration Methods 0.000 description 1
- 239000003570 air Substances 0.000 description 1
- 230000035512 clearance Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000000034 methods Methods 0.000 description 1
- 238000007790 scraping Methods 0.000 description 1
- 239000010865 sewage Substances 0.000 description 1
Abstract
Description
Technical field
The present invention relates to a kind of high speed rotor structure of centrifugal blower, specifically a kind of modified model high gear axle construction of single-stage high-speed centrifugal blower belongs to the mechanical structure technical field.
Background technique
At present, at the single-stage high-speed centrifugal blower that is used in the aeration in sewage treatment system, impeller obtains high rotational speed through gear speed increaser.Motor connects with lower velocity shaft, and impeller connects with high speed shaft.In existing technology, high speed gear shaft one end connects impeller, behind the maze type sealing configuration, is supported by radial bearing.The other end is also supported by radial bearing, and holds the end to contact with thrust bearing, and two bearings are adjacent.When impeller was big, an end quality was bigger than normal, can make outside deviation of gravity center to two radial bearing of rotor-support-foundation system; Form a kind of cantilever structure, thereby make impeller when high-speed rotation, produce bigger vibrations; Reduced the stability of system; Need enlarge the gap between impeller and the spiral case simultaneously, to prevent scraping, and the enlarged meeting in gap causes the reduction of blower efficiency.
Summary of the invention
The objective of the invention is to overcome above-mentioned deficiency, thereby a kind of high speed rotor structure of centrifugal blower is provided, the center of gravity of its efficient balance rotor-support-foundation system, the vibration amplitude of reduction impeller, the stability of raising system makes blower have higher efficient simultaneously.
According to technological scheme provided by the invention, a kind of high speed rotor structure of centrifugal blower comprises high speed gear shaft, impeller, stay-bolt, C shape ring, nut, safety cover and screw; Said stay-bolt one end connects high speed gear shaft, passes impeller and C shape ring then successively, and nut is fastened on impeller on the high speed gear shaft through screwing; Said screw screws in the tapped hole of stay-bolt one end, and safety cover and C shape ring connect.Said high speed gear shaft adopts the balancing disk structure between radial bearing supporting place and thrust bearing supporting place.
As further improvement of the present invention, said balancing disk is cylinder type and has the location shaft shoulder, and balancing disk is concentric with high speed gear shaft.
Compared with present technology the present invention has the following advantages:
The present invention is simple in structure, and the balancing disk structure of axle head helps balanced center of gravity, reduces the impeller vibration amplitude, improves the stability of system, and the load of efficient balance two radial bearings reduces the gap between impeller and the spiral case, thereby improves the efficient of blower.
Description of drawings
Fig. 1 is a structural representation of the present invention.
Embodiment
Following the present invention will combine the embodiment in the accompanying drawing to further describe:
As shown in Figure 1, comprise high speed gear shaft 1, impeller 2, stay-bolt 3, C shape ring 4, nut 5, safety cover 6 and screw 7.
Said stay-bolt 3 one ends connect high speed gear shaft 1, pass impeller 2 and C shape ring 4 then successively, thereby through the nut 5 of screwing impeller 2 are fastened on the high speed gear shaft 1 then.Said screw 7 screws in the tapped hole of stay-bolt 3 one ends, thereby safety cover 6 and C shape ring 4 are connected.The A of said high speed gear shaft 1, B two places contact with radial bearing respectively, and the C place contacts with thrust bearing.Said high speed gear shaft 1 is that balancing disk 1-1 structure is (on high speed gear shaft between radial bearing supporting place A and thrust bearing supporting place C; And between radial bearing supporting place and thrust bearing supporting place, being cylindrical section, this cylindrical section has the location shaft shoulder; Balancing disk structure for gear shaft; Be a part that belongs to gear shaft), balancing disk 1-1 is cylinder type and has the location shaft shoulder, and balancing disk 1-1 is concentric with high speed gear shaft.
Whole rotor-support-foundation system is supported by two radial bearings and a thrust bearing, and intercepts gear-box and spiral case by the labyrinth sealing system.Motor drives high speed gear shaft through low speed gear, so that impeller obtains higher rotation speed.When impeller quality bigger than normal lays particular stress on, the balancing disk of the other end of high speed gear shaft can balanced whole rotor-support-foundation system center of gravity, center of gravity is remained in the middle of A and the B.Like this with regard to balance the load of two radial bearings; Avoided the vibrations that produce because of outside deviation of gravity center to the two bearings, improved the stability of system, also less clearance can be set between spiral case and the impeller simultaneously; Make the blower air loss reduce, further improve the efficient of blower.
Claims (2)
Priority Applications (1)
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CN201210250335XA CN102734216A (en) | 2012-07-18 | 2012-07-18 | High-speed rotor structure of centrifugal blower |
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CN201210250335XA CN102734216A (en) | 2012-07-18 | 2012-07-18 | High-speed rotor structure of centrifugal blower |
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CN102734216A true CN102734216A (en) | 2012-10-17 |
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CN201210250335XA CN102734216A (en) | 2012-07-18 | 2012-07-18 | High-speed rotor structure of centrifugal blower |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103062095A (en) * | 2013-01-22 | 2013-04-24 | 安徽安风风机有限公司 | Wear-resistant fan |
CN105257591A (en) * | 2015-11-09 | 2016-01-20 | 江苏杰尔科技股份有限公司 | Impeller mounting structure of single-stage high-speed centrifugal fan |
CN106837849A (en) * | 2017-01-16 | 2017-06-13 | 湖南航翔燃气轮机有限公司 | Centrifugal blower high speed rotor structure |
CN107178521A (en) * | 2017-07-05 | 2017-09-19 | 沈阳透平机械股份有限公司 | A kind of single shaft centrifugal compressed machine rotor and its assembly method |
CN107289902A (en) * | 2017-06-20 | 2017-10-24 | 中国科学技术大学 | Binocular high-speed, high precision theodolite based on image recognition with tracking |
CN110701101A (en) * | 2019-10-14 | 2020-01-17 | 中国北方发动机研究所(天津) | Compressor impeller with elastic table |
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CN101975168A (en) * | 2010-11-05 | 2011-02-16 | 浙江科尔泵业股份有限公司 | Horizontal axial-suction sectional multistage high-pressure centrifugal pump |
CN201908874U (en) * | 2010-11-24 | 2011-07-27 | 无锡杰尔压缩机有限公司 | Clamping structure of single-stage high speed centrifugal fan impeller |
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CN102562641A (en) * | 2010-12-21 | 2012-07-11 | 哈米尔顿森德斯特兰德公司 | Fan rotor ring for an air cycle machine |
CN202746281U (en) * | 2012-07-18 | 2013-02-20 | 无锡杰尔压缩机有限公司 | High-speed rotor structure of centrifugal blower |
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2012
- 2012-07-18 CN CN201210250335XA patent/CN102734216A/en not_active Application Discontinuation
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US3601501A (en) * | 1970-02-26 | 1971-08-24 | John G Johnson | Gas compressor impeller and shaft assembly |
US4586872A (en) * | 1982-12-24 | 1986-05-06 | Klockner-Humboldt-Deutz Ag | Centrifugal pump |
CN2339794Y (en) * | 1998-05-12 | 1999-09-22 | 兰州三维科技应用研究院 | High-power magnetic drive pump |
JP2003139089A (en) * | 2001-10-31 | 2003-05-14 | Mitsubishi Heavy Ind Ltd | Single stage overhang type compressor |
US20060013693A1 (en) * | 2004-07-13 | 2006-01-19 | Honeywell International, Inc. | Outer diameter nut piloting for improved rotor balance |
CN2806843Y (en) * | 2005-07-22 | 2006-08-16 | 江津增压器厂 | Air compressor for turbocharger |
JP4876867B2 (en) * | 2006-11-27 | 2012-02-15 | 株式会社Ihi | Turbo compressor rotor |
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CN102562641A (en) * | 2010-12-21 | 2012-07-11 | 哈米尔顿森德斯特兰德公司 | Fan rotor ring for an air cycle machine |
CN202746281U (en) * | 2012-07-18 | 2013-02-20 | 无锡杰尔压缩机有限公司 | High-speed rotor structure of centrifugal blower |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103062095A (en) * | 2013-01-22 | 2013-04-24 | 安徽安风风机有限公司 | Wear-resistant fan |
CN103062095B (en) * | 2013-01-22 | 2016-05-04 | 安徽安风风机有限公司 | A kind of wearable fan |
CN105257591A (en) * | 2015-11-09 | 2016-01-20 | 江苏杰尔科技股份有限公司 | Impeller mounting structure of single-stage high-speed centrifugal fan |
CN106837849A (en) * | 2017-01-16 | 2017-06-13 | 湖南航翔燃气轮机有限公司 | Centrifugal blower high speed rotor structure |
CN106837849B (en) * | 2017-01-16 | 2018-01-30 | 湖南航翔燃气轮机有限公司 | Centrifugal blower high speed rotor structure |
CN107289902A (en) * | 2017-06-20 | 2017-10-24 | 中国科学技术大学 | Binocular high-speed, high precision theodolite based on image recognition with tracking |
CN107178521A (en) * | 2017-07-05 | 2017-09-19 | 沈阳透平机械股份有限公司 | A kind of single shaft centrifugal compressed machine rotor and its assembly method |
CN110701101A (en) * | 2019-10-14 | 2020-01-17 | 中国北方发动机研究所(天津) | Compressor impeller with elastic table |
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