CN103896013A - Automatic hoister - Google Patents
Automatic hoister Download PDFInfo
- Publication number
- CN103896013A CN103896013A CN201210597937.2A CN201210597937A CN103896013A CN 103896013 A CN103896013 A CN 103896013A CN 201210597937 A CN201210597937 A CN 201210597937A CN 103896013 A CN103896013 A CN 103896013A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- bar
- support
- cross
- cross rod
- 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.)
- Pending
Links
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 16
- 239000010959 steel Substances 0.000 claims abstract description 16
- 239000000463 material Substances 0.000 claims description 6
- 230000001174 ascending effect Effects 0.000 abstract 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
Images
Landscapes
- Lift-Guide Devices, And Elevator Ropes And Cables (AREA)
Abstract
The invention discloses an automatic hoister which comprises a body, a belt and a support. An automatic hoisting mechanism used for hoisting the support is arranged on the support and arranged at the lower end of the body, and comprises a motor, a body cross rod and a support cross rod. The body cross rod is located at the rear end of the support cross rod, the body cross rod and the support cross rod are respectively provided with at least one pulley, a steel wire rope is arranged between the support cross rod and the motor, one end of the steel wire rope is fixedly connected with the body cross rod, the other end of the steel wire rope penetrates through the pulleys to be fixedly connected with a main shaft of the motor, the motor drives the main shaft to rotate and pulls the steel wire rope, and the support cross rod slides along the bottom of the body and hoists the body. By the adoption of the technical scheme, the motor is adopted to pull the steel wire rope, the steel wire rope drives the support to ascend and hoist the body, the automatic hoister is simple in structure and convenient to operate, the body cross rod is connected with the support cross rod through the pulleys, and ascending and descending operations of the body are more reliable.
Description
Technical field
The present invention relates to material lift equipment, be specifically related to a kind of self-lift.
Background technology
At present, existing material elevator generally comprises fuselage, be arranged on fuselage belt in order to transmit material and fuselage below for supporting the support of fuselage, in the time of the lifting of needs gig, generally draw support to make fuselage lifting to same direction together by multiple workmans, the mode of this artificial lifting fuselage, troublesome poeration, needs workman many, and has the potential safety hazard to workman in the time of lifting.
Summary of the invention
The deficiency existing for prior art, the object of the present invention is to provide one rational in infrastructure, and hoist casing lifting is convenient, lifting safety of operation failure-free self-lift.
For achieving the above object, the invention provides following technical scheme: a kind of self-lift, comprise fuselage, be arranged on fuselage upper end for transmitting the belt of material and for supporting the support of fuselage, described support and fuselage lower end are provided with the automatic lifting mechanism for support lifting, described automatic lifting mechanism comprises the motor being fixedly mounted on fuselage, fixedly be located at the fuselage cross bar of fuselage bottom and the rack cross-bar of support upper end, described fuselage cross bar is positioned at rack cross-bar rear end, and on fuselage cross bar and rack cross-bar, be at least provided with respectively a pulley, between rack cross-bar and motor, be provided with steel rope, described steel rope one end is fixedly connected with fuselage cross bar, the other end is fixedly connected with the main shaft of motor through each pulley, rotate and tense wire rope by motor drive shaft, rack cross-bar is slided and lifting fuselage along fuselage bottom.
By adopting technique scheme, adopt motor to pull steel rope, steel rope drives support to rise and lifting fuselage, simple in structure, easy to operate, and adopts pulley to be connected between fuselage cross bar and rack cross-bar, makes fuselage descending operation more reliable.
The present invention is further set to: the corresponding fuselage bottom in described rack cross-bar two ends is provided with friction wheel, and when described fuselage lifting, friction wheel compresses fuselage and along sliding machine body.By this setting, set up friction wheel, service life that can extending bracket.
The present invention is also further set to: described fuselage cross bar and rack cross-bar be arranged in parallel.By this setting, make work of the present invention more reliable.
The present invention is also further set to: rack cross-bar one end is provided with the safety rope for preventing that fuselage from declining, and described safety rope one end is fixedly connected with rack cross-bar.By this setting, the present invention's operation is safer.
Advantage of the present invention is: the present invention adopts motor to pull steel rope, and steel rope drives support to rise and lifting fuselage, simple in structure, easy to operate, and adopts pulley to be connected between fuselage cross bar and rack cross-bar, makes fuselage descending operation more reliable.
Below in conjunction with specification drawings and specific embodiments, the invention will be further described.
Accompanying drawing explanation
Fig. 1 is the structural representation of the embodiment of the present invention;
Fig. 2 is the structural representation of automatic lifting mechanism in Fig. 1.
The specific embodiment
Referring to Fig. 1 and Fig. 2, a kind of self-lift disclosed by the invention, comprise fuselage 1, be arranged on fuselage 1 upper end for transmitting the belt 2 of material and for supporting the support 3 of fuselage 1, described support 3 is provided with the automatic lifting mechanism 4 for support 1 lifting with fuselage 1 lower end, described automatic lifting mechanism 4 comprises the motor 41 being fixedly mounted on fuselage 1, fixedly be located at the fuselage cross bar 42 of fuselage 1 bottom and the rack cross-bar 43 of support 3 upper ends, described fuselage cross bar 42 is positioned at rack cross-bar, 43 rear ends, described fuselage cross bar 42 and rack cross-bar 43 be arranged in parallel, and on fuselage cross bar 42 and rack cross-bar 43, be at least provided with respectively a pulley 44, between rack cross-bar 43 and motor 41, be provided with steel rope 45, described steel rope 45 one end are fixedly connected with fuselage cross bar 42, the other end is fixedly connected with the main shaft of motor 41 through each pulley 44, rotate and tense wire rope 45 by motor 41 drive shaft, make rack cross-bar 43 along fuselage 1 basal sliding lifting fuselage 1.
Corresponding fuselage 1 bottom, described rack cross-bar 43 two ends is provided with friction wheel 5, and when described fuselage 1 lifting, friction wheel 5 compresses fuselage 1 and slides along fuselage 1.
For making the present invention more safe and reliable, as preferably, described in the present embodiment, rack cross-bar 43 one end are provided with the safety rope 6 for preventing that fuselage 1 from declining, described safety rope 6 one end are fixedly connected with rack cross-bar 43, after fuselage 1 liftings such as safety rope 6 other ends, be fixedly connected with fuselage 1 or with fuselage 1 easily fixture be connected.
When practical application, fuselage cross bar 42 is fixedly connected with fuselage 1 bottom, support 3 has with fuselage cross bar 42 hinged, rack cross-bar 43 is arranged on fuselage cross bar 42 fronts, rack cross-bar 43 is fixedly installed on support 3 upper ends, in the time of needs lifting fuselage, starter motor 41, the main shaft of motor 41 rotates tense wire rope 45, make on rack cross-bar 43 friction wheel 5 along fuselage 1 edge down sliding, now friction wheel 5 compresses fuselage 1 and to one, fuselage thrust upwards, when fuselage 1 is lifted to appropriate location, disable motor 41, and the safety rope on rack cross-bar 43 6 is locked, prevent fuselage 1 landing.Simple in structure, easy to operate, and machine adopts pulley 44 to be connected between cross bar 42 and rack cross-bar 43, makes fuselage 1 descending operation more reliable.
Above-described embodiment is to specific descriptions of the present invention; only be used to further illustrate the present invention; can not be interpreted as limiting the scope of the present invention, the technician of this area according to the content of foregoing invention to the present invention make some nonessential improvement and adjust all fall into protection scope of the present invention within.
Claims (4)
1. a self-lift, comprise fuselage (1), be arranged on fuselage (1) upper end for transmitting the belt (2) of material and for supporting the support (3) of fuselage (1), it is characterized in that: described support (3) is provided with the automatic lifting mechanism (4) for support (3) lifting with fuselage (1) lower end, described automatic lifting mechanism (4) comprises the motor (41) being fixedly mounted on fuselage (1), fixedly be located at the fuselage cross bar (42) of fuselage (1) bottom and the rack cross-bar (43) of support (3) upper end, described fuselage cross bar (42) is positioned at rack cross-bar (43) rear end, and be at least provided with respectively a pulley (44) on fuselage cross bar (42) and rack cross-bar (43), between rack cross-bar (43) and motor (41), be provided with steel rope (45), described steel rope (45) one end is fixedly connected with fuselage cross bar (42), the other end is fixedly connected with the main shaft of motor (41) through each pulley (44), rotate and tense wire rope (45) by motor (41) drive shaft, make rack cross-bar (43) along fuselage (1) basal sliding lifting fuselage (1).
2. a kind of self-lift according to claim 1, it is characterized in that: the corresponding fuselages in described rack cross-bar (43) two ends (1) bottom is provided with friction wheel (5), and when described fuselage (1) lifting, friction wheel (5) compresses fuselage (1) and slides along fuselage (1).
3. a kind of self-lift according to claim 1 and 2, is characterized in that: described fuselage cross bar (42) and rack cross-bar (43) be arranged in parallel.
4. a kind of self-lift according to claim 3, it is characterized in that: rack cross-bar (43) one end is provided with the safety rope (6) for preventing that fuselage (1) from declining, and described safety rope (6) one end is fixedly connected with rack cross-bar (43).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210597937.2A CN103896013A (en) | 2012-12-27 | 2012-12-27 | Automatic hoister |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210597937.2A CN103896013A (en) | 2012-12-27 | 2012-12-27 | Automatic hoister |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103896013A true CN103896013A (en) | 2014-07-02 |
Family
ID=50987655
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210597937.2A Pending CN103896013A (en) | 2012-12-27 | 2012-12-27 | Automatic hoister |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103896013A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201062160Y (en) * | 2007-08-01 | 2008-05-21 | 曹全礼 | Mobile bales-off dual-purpose rubber belt conveyor |
| CN201626689U (en) * | 2010-04-10 | 2010-11-10 | 张应兴 | Steel wire rope traction lifting device of conveyor |
| CN202449547U (en) * | 2011-12-21 | 2012-09-26 | 贵阳铝镁设计研究院有限公司 | Conveyer plugging device |
| CN102745465A (en) * | 2012-06-29 | 2012-10-24 | 北方重工集团有限公司 | Caisson device of movably-arranged rubber belt conveyor |
| JP2013023376A (en) * | 2011-07-25 | 2013-02-04 | Hi-Lex Corporation | Lifting mechanism |
| CN202864281U (en) * | 2012-10-18 | 2013-04-10 | 金仙惠 | Movable belt conveyor with adjustable dip angle |
-
2012
- 2012-12-27 CN CN201210597937.2A patent/CN103896013A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201062160Y (en) * | 2007-08-01 | 2008-05-21 | 曹全礼 | Mobile bales-off dual-purpose rubber belt conveyor |
| CN201626689U (en) * | 2010-04-10 | 2010-11-10 | 张应兴 | Steel wire rope traction lifting device of conveyor |
| JP2013023376A (en) * | 2011-07-25 | 2013-02-04 | Hi-Lex Corporation | Lifting mechanism |
| CN202449547U (en) * | 2011-12-21 | 2012-09-26 | 贵阳铝镁设计研究院有限公司 | Conveyer plugging device |
| CN102745465A (en) * | 2012-06-29 | 2012-10-24 | 北方重工集团有限公司 | Caisson device of movably-arranged rubber belt conveyor |
| CN202864281U (en) * | 2012-10-18 | 2013-04-10 | 金仙惠 | Movable belt conveyor with adjustable dip angle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106081904B (en) | Jib-type crane container spreader stabilizer | |
| CN203699606U (en) | Lifter and iron tower | |
| CN105217416A (en) | The engagement type cage lifter of screw mandrel | |
| CN103742720A (en) | Cable moving device | |
| CN105016165A (en) | Overspeed anti-falling protection device of elevator | |
| CN203699595U (en) | Double-rope material hoister | |
| CN204530513U (en) | The manned maintenance Hanging Basket of suspension cable | |
| CN101428732A (en) | Ultra-long electric block | |
| CN201125127Y (en) | Ultralong electric gourd | |
| CN203111983U (en) | Automatic lifting machine | |
| CN204173715U (en) | Iron tower of power transmission line jacking system | |
| CN103896013A (en) | Automatic hoister | |
| CN103738809B (en) | Do not meet the method for being detained lift car buffer-braking under operating mode and device thereof | |
| CN102874709B (en) | A kind of transversely movable double pulleies unit vertical lifting equipment | |
| CN102455254A (en) | Safety lock test stand | |
| CN202016810U (en) | Electric hoist crane | |
| CN204847997U (en) | Manual winch of adjustable height | |
| CN204474228U (en) | Hoist ceiling crane inhibiting device | |
| CN211813104U (en) | Mine material is with equipment of lifting by crane | |
| CN205045656U (en) | Engagement type elevator of lead screw | |
| CN203159000U (en) | Elevator with weight-compensating device | |
| CN203372943U (en) | Machine-roomless elevator rescue device | |
| CN212151364U (en) | Crane lifting device | |
| CN203794485U (en) | Single-main-beam hook gantry crane | |
| CN204057551U (en) | A kind of emergency rescue device for elevator |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140702 |