CN101492239B - Height regulator for screen grid of fiberglass strengthened apparatus - Google Patents

Height regulator for screen grid of fiberglass strengthened apparatus Download PDF

Info

Publication number
CN101492239B
CN101492239B CN2008100260516A CN200810026051A CN101492239B CN 101492239 B CN101492239 B CN 101492239B CN 2008100260516 A CN2008100260516 A CN 2008100260516A CN 200810026051 A CN200810026051 A CN 200810026051A CN 101492239 B CN101492239 B CN 101492239B
Authority
CN
China
Prior art keywords
air grid
flat air
lifting support
transmission shaft
fuselage
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.)
Expired - Fee Related
Application number
CN2008100260516A
Other languages
Chinese (zh)
Other versions
CN101492239A (en
Inventor
周军山
周灿明
李伯申
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN2008100260516A priority Critical patent/CN101492239B/en
Publication of CN101492239A publication Critical patent/CN101492239A/en
Application granted granted Critical
Publication of CN101492239B publication Critical patent/CN101492239B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention discloses a device for adjusting the height of a flat air grid of a glass toughened device, which comprises a machine body, an upper flat air grid and a lower flat air grid which are arranged on the machine body, and a lifting rack arranged on the machine body, wherein the bottom of the lifting rack is connected with the upper flat air grid; the lifting rack is also fixed with a lifting worm; the machine body is also provided with a driving device which is matched with the lifting worm and drives the lifting rack to move upwards and downwards; the machine body and the lifting rack are provided with at least one pair of left and right chain wheels respectively; the lifting rack is also provided with a middle takeup wheel; the left and the right chain wheels on the machine body are positioned above the corresponding left and right chain wheels on the lifting rack respectively; and two ends of the lower flat air grid are connected with one end of the left and the right chain wheels respectively, and the other ends of the left and the right chain wheels are fixed on the takeup wheel again through the corresponding chain wheels on the machine body and the lifting rack sequentially. The height adjusting device has simple and easy operation, and the distance between the upper flat air grid and the lower flat air grid is controlled by the driving device, thus the adjustment rate is precise and the glass toughening effect is effectively improved.

Description

A kind of flat air grid arrangement for adjusting height of glass tempering equipment
Technical field
The present invention relates to the glass tempering apparatus technology, especially a kind of flat air grid arrangement for adjusting height of glass tempering equipment.
Background technology
At present, be used for the equipment of processing toughened glass, its structure mainly contains heating unit, glass conveyer device, upper and lower flat air grid and air supply device thereof; Wherein, described upper and lower flat air grid is fixed on the fuselage, and the air outlet of upper and lower flat air grid is with the relative direction setting.During work, send into by e Foerderanlage between the upper and lower flat air grid through heat treated glass, the flat up and down air grid air blast of air supply device, and from the air outlet of upper and lower flat air grid with the upper and lower surface of wind, to realize cooling tempering to glass at glass.The effect of glass cools tempering tends to be subjected to the distance affects between upper and lower flat air grid air outlet and the glass surface; Perhaps, the glass cools tempering of different thickness need be adjusted to some extent to the height between the upper and lower flat air grid; But, existing toughened glass equipment, because upper and lower flat air grid is fixed on the fuselage, during adjustment, need staff earlier upper and lower flat air grid to be pulled down, again it is installed in the height correct position and fixes, the entire operation trouble, and upper and lower flat air grid has certain weight, and therefore, it adjusts extremely inconvenient; Moreover staff is adjusted upper and lower flat air grid height, and its tolerance range is poor, influences the effect of glass cools tempering.
Summary of the invention
The objective of the invention is to overcome the deficiency that above-mentioned prior art exists, and provide a kind of height control simple, convenient, it is adjusted accurately, can improve the flat air grid arrangement for adjusting height of the glass tempering equipment of glass tempering effect.
The objective of the invention is to adopt following technical measures to solve:
A kind of flat air grid arrangement for adjusting height of glass tempering equipment, comprise fuselage and be installed in upper and lower flat air grid on the fuselage, also be provided with lifting support on the described fuselage, the lifting support bottom is connected with flat air grid, also be fixed with elevating endless screw on the lifting support, also be provided with on the fuselage to cooperate and make lifting support make upper and lower mobile drive unit with elevating endless screw; Be respectively arranged with at least one pair of left and right sprocket wheel on described fuselage and the lifting support, tighten up wheel in the middle of also being provided with on the lifting support, left and right sprocket wheel on the fuselage lays respectively at the top of left and right sprocket wheel corresponding on the lifting support, flat air grid two ends connect left and right chain one end respectively down, and the left and right chain the other end successively is fixed on by sprocket wheel corresponding on fuselage and the lifting support again and tightens up on the wheel.When need adjusting upper and lower flat air grid height, start drive unit earlier, make elevating endless screw make the upper and lower lifting support that moves and drive, go up flat air grid and be subjected to lifting support effect meeting to do upper and lower moving; Simultaneously, the left and right sprocket wheel of going up on the flat air grid can be along upper and lower the moving of left and right chain row culture, make left and right chain drive the middle wheel that tightens up and rotate and left and right chain is tightened up or decontrols, following flat air grid can be done reverse upper and lower moving relative to going up flat air grid under left and right chain effect.That is, adjust distance between the upper and lower flat air grid simultaneously.Entire operation is simple, easy, because the distance between the upper and lower flat air grid is by drive control, its regulation is accurate, effectively improves the glass tempering effect;
Described drive unit comprises drive-motor and worm type of reduction gearing, and the drive-motor output shaft drives the input terminus that connects worm type of reduction gearing, and the output terminal of worm type of reduction gearing is inserted in the elevating endless screw upper end.Drive-motor makes elevating endless screw do upper and lower moving along worm type of reduction gearing by driving worm type of reduction gearing;
Because lifting support and last flat air grid have certain weight and area, for making its lifting moving more steady, be fixed with a plurality of elevating endless screws on the described lifting support, the upper end of each elevating endless screw is provided with worm type of reduction gearing, drive unit also includes transmission shaft, and the transmission shaft divider that drives by drive-motor, have a plurality of transmission shaft interfaces on the transmission shaft divider, each transmission shaft interface connects transmission shaft one end, and the transmission shaft the other end links to each other with the input terminus of corresponding worm type of reduction gearing.By the transmission shaft divider is installed, make same drive-motor can pass through the transmission shaft divider on the fuselage, drive a plurality of elevating endless screws simultaneously;
The output shaft of described drive-motor inserts a worm type of reduction gearing input terminus that is adjacent, also has the transmission shaft interface on this worm type of reduction gearing, the transmission shaft interface also connects a transmission shaft, and this transmission shaft the other end links to each other with a transmission shaft interface of transmission shaft divider.The particular location setting of above-mentioned drive-motor can also otherwise replace.
Purpose of the present invention can also adopt following technical measures to solve:
At least one end of described lifting support is located on the lifting sliding rail of fuselage one side, during the lifting support lifting, can slide along the lifting sliding rail of fuselage one side, improves the stationarity of its lifting.
Flat air grid also has certain weight and area down, for it is steadily moved, be separately installed with many on described fuselage and the lifting support to left and right sprocket wheel, corresponding following flat air grid is provided with many to left and right chain, a plurality of centres also are installed on the lifting support tighten up wheel, many left and right chain one end is fixedlyed connected with following flat air grid, the other end tightens up wheel with corresponding centre respectively and connects; Therefore, following flat air grid can be done up-and-down movement under left and right chain is driven better many.
Can link up for making above-mentioned a plurality of centre tighten up wheel, reach synchronous rotary action, described a plurality of centres are tightened up wheel and all are arranged in the same rotating shaft, and the rotating shaft two ends are on the movable shaft seat that is installed in lifting support.
Described centre is tightened up left and right chain one end on the wheel and is the relative position direction respectively and fixes, and can tighten up or decontrol left and right chain so that wheel is tightened up in the centre simultaneously when rotating, to realize down being relative or the reverse direction lifting between flat air grid and the last flat wind canopy.
The beneficial effect of type of the present invention is: the flat air grid arrangement for adjusting height of (1) glass tempering equipment of the present invention, by being set, drive unit, elevating endless screw, sprocket wheel, chain and centre tighten up wheel on fuselage and lifting support, can realize that the height of upper and lower flat air grid adjusts relatively, it is simple to operate, easy, speed of cooling and temperature are even, and glass tempering is effective; Moreover because the distance between the upper and lower flat air grid is by drive control, it adjusts the accurate rate height, can further improve the glass tempering effect.
Description of drawings
Fig. 1 is the flat air grid arrangement for adjusting height synoptic diagram of glass tempering equipment of the present invention;
Fig. 2 is the side-looking enlarged view of Fig. 1;
Fig. 3 is the vertical view of Fig. 1;
Fig. 4 is the another embodiment of the present invention synoptic diagram.
Embodiment
Embodiment 1: as shown in Figure 1 to Figure 3, a kind of flat air grid arrangement for adjusting height of glass tempering equipment, comprise fuselage 1 and be installed in upper and lower flat air grid 2,3 on the fuselage 1, also be provided with lifting support 4 on the described fuselage 1, lifting support 4 at least one ends are located on the lifting sliding rail 5 of fuselage 1 one sides, lifting support 4 bottoms are connected with flat air grid 2, also are fixed with elevating endless screw 6 on the lifting support 4, also are provided with on the fuselage 1 to cooperate with elevating endless screw 6 to make lifting support 4 make upper and lower mobile drive unit 7; Be respectively arranged with at least one pair of left and right sprocket wheel 901,902,801,802 on described fuselage 1 and the lifting support 4, tighten up wheel 10 in the middle of also being provided with on the lifting support 4, left and right sprocket wheel 901,902 on the fuselage 1 lays respectively at the top of left and right sprocket wheel 801,802 corresponding on the lifting support 4, flat air grid 3 two ends connect left and right chain 11,12 1 ends respectively down, and left and right chain 11,12 the other ends are successively by sprocket wheel 901,801 corresponding on fuselage 1 and the lifting support 4; 902,802 be fixed on again and tighten up on the wheel 10, tighten up left and right chain 11,12 one ends of wheel on 10 and be the relative position direction respectively and fix.
Described drive unit 7 comprises drive-motor 701 and worm type of reduction gearing 702, and the drive-motor output shaft drives the input terminus that connects worm type of reduction gearing 702, and the output terminal of worm type of reduction gearing 702 is inserted in elevating endless screw 6 upper ends.
Be fixed with a plurality of elevating endless screws 6 on the described lifting support 4, the upper end of each elevating endless screw 6 is provided with worm type of reduction gearing 702, drive unit 7 also includes transmission shaft 703, and the transmission shaft divider 704 that drives by drive-motor 701, have a plurality of transmission shaft interfaces on the transmission shaft divider 704, each transmission shaft interface connects transmission shaft 703 1 ends, and transmission shaft 703 the other ends link to each other with the input terminus of corresponding worm type of reduction gearing 702.Wherein, the output shaft of drive-motor 701 inserts a worm type of reduction gearing 702 input terminuss that are adjacent, also has the transmission shaft interface on this worm type of reduction gearing 702, the transmission shaft interface also connects a transmission shaft 703, and these transmission shaft 703 the other ends link to each other with a transmission shaft interface of transmission shaft divider 704.
Be separately installed with many on described fuselage 1 and the lifting support 4 to left and right sprocket wheel 901,902,801,802, corresponding following flat air grid 3 is provided with many to left and right chain 11,12, a plurality of centres also are installed on the lifting support 4 tighten up wheel 10, many left and right chain 11,12 1 ends are fixedlyed connected with following flat air grid 3, the other end tightens up wheel 10 with corresponding centre respectively and connects.Described a plurality of centre is tightened up wheel and 10 all is arranged in the same rotating shaft 13, and rotating shaft 13 two ends are on the movable shaft seat 401 that is installed in lifting support 4.
Principle of work: when needing the upper and lower flat air grid 2,3 of adjustment highly, start drive unit 7 earlier, make elevating endless screw 6 do upper and lower moving and drive lifting support 4, upward flat air grid 2 is subjected to lifting support 4 effects can do upper and lower moving; Simultaneously, the left and right sprocket wheel of going up on the flat air grid 2 801,802 can be done upper and lower moving along left and right chain 11,12, making left and right chain 11,12 drive the middle wheel 10 that tightens up rotates and left and right chain 11,12 is tightened up or decontrols, flat air grid 3 can be done reverse upper and lower moving relative to going up flat air grid 2 under left and right chain 11,12 effects down.That is, adjust distance between the upper and lower flat air grid 2,3 simultaneously.Entire operation is simple, easy, because the distance between the upper and lower flat air grid 2,3 is that its regulation is accurate, effectively improves the glass tempering effect by drive unit 7 controls.
Embodiment 2: as shown in Figure 4, its structure is similar to embodiment 1, and difference is, lifting sliding rail is not set on the fuselage 1, and lifting support 4 does not need to slide along the lifting sliding rail 5 of fuselage 1 one sides, also can go up flat air grid 2 pullings and realizes lifting.

Claims (5)

1. the flat air grid arrangement for adjusting height of a glass tempering equipment, comprise fuselage (1) and be installed in upper and lower flat air grid (2,3) on the fuselage (1), it is characterized in that, also be provided with lifting support (4) on the described fuselage (1), lifting support (4) bottom is connected with flat air grid (2), also be fixed with elevating endless screw (6) on the lifting support (4), also be provided with on the fuselage (1) to cooperate and make lifting support (4) make upper and lower mobile drive unit (7) with elevating endless screw (6); Be respectively arranged with at least one pair of left and right sprocket wheel (901,902,801,802) on described fuselage (1) and the lifting support (4), tighten up wheel (10) in the middle of also being provided with on the lifting support (4), left and right sprocket wheel on the fuselage (1) (901,902) lays respectively at the top that lifting support (4) is gone up corresponding left and right sprocket wheel (801,802), flat air grid (3) two ends connect left and right chain (11, a 12) end respectively down, and left and right chain (11, the 12) the other end is successively gone up corresponding sprocket wheel (901,801 by fuselage (1) and lifting support (4); 902,802) be fixed on again and tighten up on the wheel (10); Described drive unit (7) comprises drive-motor (701) and worm type of reduction gearing (702), and the drive-motor output shaft drives the input terminus that connects worm type of reduction gearing (702), and the output terminal of worm type of reduction gearing (702) is inserted in elevating endless screw (6) upper end; Be fixed with a plurality of elevating endless screws (6) on the described lifting support (4), the upper end of each elevating endless screw (6) is provided with worm type of reduction gearing (702), drive unit (7) also includes transmission shaft (703), and the transmission shaft divider (704) that drives by drive-motor (701), have a plurality of transmission shaft interfaces on the transmission shaft divider (704), each transmission shaft interface connects transmission shaft (703) one ends, and transmission shaft (703) the other end is continuous with the input terminus of corresponding worm type of reduction gearing (702); The output shaft of described drive-motor (701) inserts a worm type of reduction gearing (702) input terminus that is adjacent, this worm type of reduction gearing also has the transmission shaft interface on (702), the transmission shaft interface also connects a transmission shaft (703), and this transmission shaft (703) the other end links to each other with a transmission shaft interface of transmission shaft divider (704).
2. according to the flat air grid arrangement for adjusting height of the described glass tempering equipment of claim 1, it is characterized in that at least one end of described lifting support (4) is located on the lifting sliding rail of fuselage (1) one side.
3. according to the flat air grid arrangement for adjusting height of claim 1 or 2 described glass tempering equipment, it is characterized in that, be separately installed with many on described fuselage (1) and the lifting support (4) to left and right sprocket wheel (901,902,801,802), corresponding following flat air grid (3) is provided with many to left and right chain (11,12), a plurality of centres also are installed on the lifting support (4) tighten up wheel (10), many left and right chain (11, a 12) end is fixedlyed connected with following flat air grid (3), the other end tightens up wheel (10) connection with corresponding centre respectively.
4. according to the flat air grid arrangement for adjusting height of the described glass tempering equipment of claim 3, it is characterized in that, described a plurality of centre is tightened up wheel (10) and all is arranged in the same rotating shaft (13), and rotating shaft (13) two ends are on the movable shaft seat (401) that is installed in lifting support (4).
5. according to the flat air grid arrangement for adjusting height of the described glass tempering equipment of claim 3, it is characterized in that described centre is tightened up left and right chain (11, a 12) end on the wheel (10) and is the relative position direction respectively and fixes.
CN2008100260516A 2008-01-25 2008-01-25 Height regulator for screen grid of fiberglass strengthened apparatus Expired - Fee Related CN101492239B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2008100260516A CN101492239B (en) 2008-01-25 2008-01-25 Height regulator for screen grid of fiberglass strengthened apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2008100260516A CN101492239B (en) 2008-01-25 2008-01-25 Height regulator for screen grid of fiberglass strengthened apparatus

Publications (2)

Publication Number Publication Date
CN101492239A CN101492239A (en) 2009-07-29
CN101492239B true CN101492239B (en) 2011-05-11

Family

ID=40923053

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2008100260516A Expired - Fee Related CN101492239B (en) 2008-01-25 2008-01-25 Height regulator for screen grid of fiberglass strengthened apparatus

Country Status (1)

Country Link
CN (1) CN101492239B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103538871B (en) * 2013-10-24 2017-07-28 镇江中化聚氨酯工业设备有限公司 Laminating conveyor elevating mechanism
CN110422996B (en) * 2019-09-11 2022-04-19 巢湖市伟业玻璃有限公司 Cooling device for toughened glass production

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1454790A1 (en) * 1987-06-05 1989-01-30 Специальное конструкторско-технологическое бюро по изоляторам и арматуре Всесоюзного производственного объединения "Союзэлектросетьизоляция" Apparatus for air-jet hardening of glass articles
SU1525121A1 (en) * 1987-07-16 1989-11-30 Львовский политехнический институт им.Ленинского комсомола Method of glass hardening
CN2607370Y (en) * 2003-03-20 2004-03-24 杭州大光明玻璃有限公司 Air grate lifting mechanism for annealing furnace
CN2853790Y (en) * 2005-08-10 2007-01-03 云南明泰玻璃股份有限公司 Air cooling equipment
CN201193216Y (en) * 2008-01-25 2009-02-11 周军山 Flat wind gating height adjuster of glass toughening equipment

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1454790A1 (en) * 1987-06-05 1989-01-30 Специальное конструкторско-технологическое бюро по изоляторам и арматуре Всесоюзного производственного объединения "Союзэлектросетьизоляция" Apparatus for air-jet hardening of glass articles
SU1525121A1 (en) * 1987-07-16 1989-11-30 Львовский политехнический институт им.Ленинского комсомола Method of glass hardening
CN2607370Y (en) * 2003-03-20 2004-03-24 杭州大光明玻璃有限公司 Air grate lifting mechanism for annealing furnace
CN2853790Y (en) * 2005-08-10 2007-01-03 云南明泰玻璃股份有限公司 Air cooling equipment
CN201193216Y (en) * 2008-01-25 2009-02-11 周军山 Flat wind gating height adjuster of glass toughening equipment

Also Published As

Publication number Publication date
CN101492239A (en) 2009-07-29

Similar Documents

Publication Publication Date Title
CN204171589U (en) Workpiece docking facilities and workpiece posture adjustment rack thereof
CN209721189U (en) A kind of cable conveying device
CN206156248U (en) Track conveyor that syllogic is adjustable
CN107352258A (en) A kind of forming machine feeding device
CN101492239B (en) Height regulator for screen grid of fiberglass strengthened apparatus
CN207310097U (en) Thermal insulation board cutting machine
CN109760899A (en) A kind of double column automatic hoisting mechanisms being oriented to using slide block guide rail
CN110423866A (en) The method that intelligence manufacture production line is quenched automatically with workpiece
CN206366898U (en) The pipe clamping device of full-automatic pipe cutting machine
CN208326653U (en) A kind of automatic loading/unloading flame processing machine
CN111974653A (en) Online oven
CN201193216Y (en) Flat wind gating height adjuster of glass toughening equipment
CN104780717B (en) A kind of structure improved double end chip mounter
CN212370526U (en) Online oven
CN215853522U (en) Move machine of carrying convenient to fine setting
CN212900595U (en) But device of shooing of automatically regulated interval
CN210790396U (en) Polishing wire drawing device
CN209720148U (en) A kind of double column automatic hoisting mechanisms being oriented to using slide block guide rail
CN219729406U (en) Synchronous vertical lifting conveying type curing oven
CN207029754U (en) A kind of conveying device for labeling for flat sheet
CN206408098U (en) A kind of double curved glass forming area roller-way is installed and adjustment structure
CN102320460A (en) Lift
CN105603481A (en) Continuous collecting system and continuous vertical electroplating production line
CN207434556U (en) A kind of Gui Zheng mechanisms
CN201058874Y (en) Distributing chute replacing apparatus

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20110511

Termination date: 20170125