CN105501661A - Surface protection device for transferring of rotors - Google Patents
Surface protection device for transferring of rotors Download PDFInfo
- Publication number
- CN105501661A CN105501661A CN201510953697.9A CN201510953697A CN105501661A CN 105501661 A CN105501661 A CN 105501661A CN 201510953697 A CN201510953697 A CN 201510953697A CN 105501661 A CN105501661 A CN 105501661A
- Authority
- CN
- China
- Prior art keywords
- rotor
- stay bearing
- arc
- plates
- plate
- 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.)
- Granted
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D61/00—External frames or supports adapted to be assembled around, or applied to, articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
- B65D85/00—Containers, packaging elements or packages, specially adapted for particular articles or materials
- B65D85/68—Containers, packaging elements or packages, specially adapted for particular articles or materials for machines, engines or vehicles in assembled or dismantled form
Abstract
The invention provides a surface protection device for transferring of rotors. The surface protection device comprises a plurality of arc-shaped plates, rubber plates are fixedly connected to the inner sides of the arc-shaped plates respectively, the outer sides of the arc-shaped plates are connected with supporting plates through elastic parts, the elastic parts are uniformly distributed between the supporting plates and the arc-shaped plates, supporting frames are arranged at the position adjacent to every two supporting plates and are provided with through holes, and the through holes in every two adjacent supporting frames are fixedly connected through bolts; vertex points of each arc-shaped plate are fixedly connected with sleeves, and each supporting plate is provided with threaded holes matched with the sleeves in position. The surface protection device further comprises a plurality of screw rods, and the screw rods are connected into the threaded holes in a threaded mode and are connected into the sleeves in a rotating mode. Compared with the prior art, the surface protection device has the advantages that the surfaces of the rotors are surrounded tightly, then foam is sprayed, and therefore the problem that existing wire winding grooves are damaged can be solved.
Description
Technical field
The present invention relates to a kind of compression tools, be specifically related to a kind of rotor transhipment surfacecti proteon device.
Background technology
Rotor is called by the swivel of bearings.Rotor mostly is the main rotation member in power machine and work mechanism; Typical rotor has Turbomachine Rotor, rotor, the rotor of various pump and the rotor etc. of turbocompressor, being there is very large distortion and cause resonance in rotor, causes rotating speed during resonance to be called the critical speed of rotor when rotating under some specific rotating speed; In engineering, working speed is called rigid rotor lower than the rotor of first critical speed, and the rotor being greater than first critical speed is called flex rotor; Because high speed rotary motion made by rotor, so need balance, static balance is mainly used in the force of inertia balancing discal rotor; The kinetic balance of rigid rotor can come balance inertial force and inertia couple by universal balancing machine, eliminates the vibration of rotor on elastic support.
Most of rotor directly builds out, has part rotor after building, and needs at rotor surface, uses cutting knife to process winding slot further, after cutting, needs to use sander machine, polish to winding slot surface, burring.
In the process of processing winding slot, cutting and sanding operation can produce a large amount of iron filings, and iron filings can enter in winding slot, if do not cleaned out by iron filings, in rotor transportation, between rotor and rotor, or between other objects of rotor, generation is collided, cause iron filings to be compacted on the coiling cell wall of rotor, coiling cell wall is caused to occur cut, or iron filings cannot be removed, cause, when use rotor, occurring the problem that rotor cutting magnetic induction line is uneven.
Summary of the invention
The invention is intended to provide a kind of rotor transhipment surfacecti proteon device protecting rotor winding rooved face.
Rotor transhipment surfacecti proteon device in this programme, comprise several arcs, several arcs can form a first circular cylinder, all rubber plate is fixedly connected with inside several arcs, several rubber plates also can form a second circular cylinder, all stay bearing plate is connected with by elastic component outside several arcs, elastic component is evenly distributed between stay bearing plate and arc, several stay bearing plates can form a 3rd circular cylinder, the position that every two stay bearing plates are adjacent is equipped with bracing frame, each bracing frame all offers through hole, through hole on adjacent supports frame is bolted to connection, the summit of each arc is all fixedly connected with sleeve, each stay bearing plate all offers the tapped bore coordinated with sleeve portion, also comprise several screw rods, screw rod is threaded in tapped bore respectively and is rotatably connected in sleeve.
The know-why of this programme and beneficial effect are: first fetch several rubber plate that can form a cylinder and arcs, rubber plate is fixedly connected on arc, upper bush is fixedly connected with at the summit place of arc, fetch the stay bearing plate that several can form a cylinder again, the position of stay bearing plate relevant sleeve is offered the tapped bore coordinated with sleeve, elastic component on the inner side of stay bearing plate connects equably again, the other end of elastic component is connected on arc, fetching screw rod is socketed in sleeve through tapped bore, make each stay bearing plate, arc and rubber plate form one and hold unit tightly, finally on the position that every two stay bearing plates are adjacent, all connect upper support frame.
After rotor completes, fetch several and hold unit tightly, rubber plate is all made to contact with rotor surface, screw and establish several screw rods on the supporting plate, stay bearing plate moves near the direction of arc, elastic component will be compressed, the end of all adjacent with it stay bearing plate in the end of each stay bearing plate is finally made to offset, same bolt is all inserted in the through hole of the bracing frame of two adjacent stay bearing plates, two nuts are screwed at the two ends of all bolts, all stay bearing plates are made to form an entirety, now continuing to screw screw rod, because stay bearing plate has been fixed as a whole, each stay bearing plate can not move mutually, move so screw rod promotes sleeve near the direction of rotor, spring will be stretched, promotion arc moves near the direction of rotor by sleeve, drive rubber plate is pressed on rotor by last arc.
Finally use foam gun, in the winding slot of rotor, spray into foam again, foam will be set between rubber plate and rotor winding groove bottom wall, then deliver on conveying arrangement by the rotor with this protective device, foam has the protection of protective device, can not depart from winding slot; When on the other hand coiling cell wall is stressed, only have the winding slot edge of apex rotor and bottom can be stressed, and the stressed also mutability of foam, can not compacting iron filings, more can not scratch cell wall.
Further, bracing frame welding on the supporting plate.Welding can make bracing frame more firmly connect on the supporting plate.
Further, bolt is thru-bolt.Thru-bolt facilitates locks mutually by adjacent stay bearing plate.
Further, elastic component is spring.Spring is a kind of mechanical component utilizing elasticity to carry out work, deformation is there is under external force with the part that elastomeric material is made, restore to the original state again after removing external force, be connected to the spring between stay bearing plate and arc, stay bearing plate and arc can be made always to there is the tensile force of spring, stay bearing plate is connected with arc more stable.
Further, rubber plate is soft rubber plate.Can when compressing rotor, soft rubber plate and rotor are fitted more.
Accompanying drawing explanation
Fig. 1 is the structural representation on embodiment of the present invention rotor transhipment surfacecti proteon device;
Fig. 2 is the partial left side view of Fig. 1.
Detailed description of the invention
Below by detailed description of the invention, the present invention is further detailed explanation:
Reference numeral in Figure of description comprises: stay bearing plate 1, arc 2, soft rubber plate 3, spring 4, screw rod 5, sleeve 6, thru-bolt 7, nut 8, bracing frame 9.
Shown in the basic reference diagram 1 of embodiment and Fig. 2: rotor transhipment surfacecti proteon device, comprise four stay bearing plates 1, four stay bearing plates 1 can form a cylinder, the two ends of the position that every two stay bearing plates 1 are adjacent are all welded with bracing frame 9, each bracing frame 9 all offers through hole, same thru-bolt 7 is inserted with in two adjacent through holes, also comprise 16 nuts 8, every two nuts 8 are screwed in the two ends of thru-bolt 7 respectively, all arc 2 is connected with by spring 4 inside four stay bearing plates 1, four arcs 2 also can form a cylinder, spring 4 is evenly distributed between stay bearing plate 1 and arc 2, four summits of each arc 2 are all fixedly connected with sleeve 6, each stay bearing plate 1 all offers four tapped bore coordinated with sleeve 6 position, also comprise several screw rods 5, screw rod 5 is threaded in respectively in tapped bore and is rotatably connected in sleeve 6, soft rubber plate 3 is all bonded with inside four arcs 2, four soft rubber plates 3 also can form a cylinder.
First fetch soft rubber plate 3 and arc 2 that four can form a cylinder, soft rubber plate 3 is bonded on arc 2, at four summits place of arc 2 welding upper bush 6, fetch the stay bearing plate 1 that four can form a cylinder again, the position of each stay bearing plate 1 relevant sleeve 6 uses tapping machine, offer the tapped bore coordinated with four sleeves 6, upper spring 4 is welded equably again in the inner side of a stay bearing plate 1 that goes out, the other end of spring 4 is welded on arc 2, fetching screw rod 5 is socketed in sleeve 6 through tapped bore, make each stay bearing plate 1, arc 2 and soft rubber plate 3 form one and hold unit tightly, finally on the position that every two stay bearing plates 1 are adjacent, all weld upper support frame 9, each support use tapping machine all to offer through hole.
After rotor completes, fetch four and hold unit tightly, soft rubber plate 3 is all made to contact with rotor surface, screw and be located at four screw rods 5 on stay bearing plate 1, stay bearing plate 1 moves near the direction of arc 2, spring 4 will be compressed, the end of all adjacent with it stay bearing plate 1 in the end of each stay bearing plate 1 is finally made to offset, same thru-bolt 7 is all inserted in the through hole of the bracing frame 9 of two adjacent stay bearing plates 1, two nuts 8 are screwed at the two ends of four thru-bolts 7, four stay bearing plates 1 are made to form an entirety, now continuing to screw screw rod 5, because stay bearing plate 1 has been fixed as a whole, each stay bearing plate 1 can not move mutually, move so screw rod 5 promotes sleeve 6 near the direction of rotor, spring 4 will be stretched, promotion arc 2 moves near the direction of rotor by sleeve 6, drive soft rubber plate 3 is pressed on rotor by last arc 2.
Finally use foam gun, then spray into foam in the winding slot of rotor, foam will be set between soft rubber plate 3 and rotor winding groove bottom wall, then be delivered on conveying arrangement by the rotor with this protective device.
Above-described is only embodiments of the invention, and in scheme, the general knowledge such as known concrete structure and characteristic does not do too much description at this.Should be understood that; for a person skilled in the art, under the prerequisite not departing from structure of the present invention, some distortion and improvement can also be made; these also should be considered as protection scope of the present invention, and these all can not affect effect of the invention process and practical applicability.The protection domain that this application claims should be as the criterion with the content of its claim, and the detailed description of the invention in specification sheets etc. record the content that may be used for explaining claim.
Claims (5)
1. rotor transhipment surfacecti proteon device, it is characterized in that, comprise several arcs, several arcs can form a first circular cylinder, all rubber plate is fixedly connected with inside several arcs, several rubber plates also can form a second circular cylinder, all stay bearing plate is connected with by elastic component outside several arcs, elastic component is evenly distributed between stay bearing plate and arc, several stay bearing plates can form a 3rd circular cylinder, the position that every two stay bearing plates are adjacent is equipped with bracing frame, each bracing frame all offers through hole, through hole on adjacent supports frame is bolted to connection, the summit of each arc is all fixedly connected with sleeve, each stay bearing plate all offers the tapped bore coordinated with sleeve portion, also comprise several screw rods, screw rod is threaded in tapped bore respectively and is rotatably connected in sleeve.
2. rotor transhipment surfacecti proteon device according to claim 1, is characterized in that: support frame as described above welding on the supporting plate.
3. rotor transhipment surfacecti proteon device according to claim 2, is characterized in that: described bolt is thru-bolt.
4. rotor transhipment surfacecti proteon device according to claim 3, is characterized in that: described elastic component is spring.
5. rotor transhipment surfacecti proteon device according to claim 4, is characterized in that: described rubber plate is soft rubber plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510953697.9A CN105501661B (en) | 2015-12-20 | 2015-12-20 | Rotor transports surfacecti proteon device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510953697.9A CN105501661B (en) | 2015-12-20 | 2015-12-20 | Rotor transports surfacecti proteon device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105501661A true CN105501661A (en) | 2016-04-20 |
| CN105501661B CN105501661B (en) | 2018-08-03 |
Family
ID=55710059
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510953697.9A Active CN105501661B (en) | 2015-12-20 | 2015-12-20 | Rotor transports surfacecti proteon device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105501661B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108674792A (en) * | 2018-05-23 | 2018-10-19 | 成都飞机工业（集团）有限责任公司 | A kind of V-type vice type airplane wheel hold-fast body |
| CN111734939A (en) * | 2020-06-28 | 2020-10-02 | 金陵科技学院 | Building stand vibrations detection instrument frame |
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| CN204304743U (en) * | 2014-12-18 | 2015-04-29 | 重庆赛力盟电机有限责任公司 | Big-and-middle-sized synchronous motor damping ring syndeton |
| CN104696600A (en) * | 2015-03-26 | 2015-06-10 | 上海外高桥造船有限公司 | Fixing support used for supporting ship pipeline |
| CN204512671U (en) * | 2015-03-25 | 2015-07-29 | 湘潭新奥燃气有限公司 | A kind of natural gas tube proof protecting device |
| CN204592563U (en) * | 2015-01-20 | 2015-08-26 | 莱芜钢铁集团有限公司 | Tube support arrangement |
| CN105422992A (en) * | 2015-12-16 | 2016-03-23 | 苏州市皓东金属压延五金厂 | Composite tube clamp |
| CN205366514U (en) * | 2015-12-20 | 2016-07-06 | 重庆赛力盟电机有限责任公司 | Surface protection device is transported to rotor |
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2015
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| CN201779102U (en) * | 2010-07-07 | 2011-03-30 | 李一品 | Diameter-variable anchor ear |
| CN102052518A (en) * | 2011-01-28 | 2011-05-11 | 浙江大学 | Tuned mass damper structure for reducing pipeline vibration |
| CN202244672U (en) * | 2011-10-27 | 2012-05-30 | 山东齐鲁电机制造有限公司 | Novel vacuum packaging structure for rotor of large-sized turbo generator |
| CN202594145U (en) * | 2012-03-29 | 2012-12-12 | 国电联合动力技术(宜兴)有限公司 | Radial shifting movement preventing transport protection device for motor |
| KR101296396B1 (en) * | 2012-05-04 | 2013-08-14 | 서울산업기술주식회사 | Jig for pipe support |
| CN103807511A (en) * | 2014-01-20 | 2014-05-21 | 江苏海事职业技术学院 | Adjustable lantern ring structure capable of restraining ship pipeline vibration noise |
| CN203857135U (en) * | 2014-05-28 | 2014-10-01 | 浙江华西科技有限公司 | Fixing clamp for high-voltage cable |
| CN203979038U (en) * | 2014-07-22 | 2014-12-03 | 乐清市东博机电有限公司 | A kind of clip |
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| CN204304659U (en) * | 2014-12-18 | 2015-04-29 | 重庆赛力盟电机有限责任公司 | Big-and-middle-sized synchronous electric motor rotor damping ring connecting structure |
| CN204304743U (en) * | 2014-12-18 | 2015-04-29 | 重庆赛力盟电机有限责任公司 | Big-and-middle-sized synchronous motor damping ring syndeton |
| CN204592563U (en) * | 2015-01-20 | 2015-08-26 | 莱芜钢铁集团有限公司 | Tube support arrangement |
| CN204512671U (en) * | 2015-03-25 | 2015-07-29 | 湘潭新奥燃气有限公司 | A kind of natural gas tube proof protecting device |
| CN104696600A (en) * | 2015-03-26 | 2015-06-10 | 上海外高桥造船有限公司 | Fixing support used for supporting ship pipeline |
| CN105422992A (en) * | 2015-12-16 | 2016-03-23 | 苏州市皓东金属压延五金厂 | Composite tube clamp |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108674792A (en) * | 2018-05-23 | 2018-10-19 | 成都飞机工业（集团）有限责任公司 | A kind of V-type vice type airplane wheel hold-fast body |
| CN111734939A (en) * | 2020-06-28 | 2020-10-02 | 金陵科技学院 | Building stand vibrations detection instrument frame |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105501661B (en) | 2018-08-03 |
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