CN104444774A - 40-ton cabin module lifting bracket - Google Patents
40-ton cabin module lifting bracket Download PDFInfo
- Publication number
- CN104444774A CN104444774A CN201410717547.3A CN201410717547A CN104444774A CN 104444774 A CN104444774 A CN 104444774A CN 201410717547 A CN201410717547 A CN 201410717547A CN 104444774 A CN104444774 A CN 104444774A
- Authority
- CN
- China
- Prior art keywords
- cross beam
- welded
- vertical beams
- cabin module
- lifting
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C1/00—Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles
- B66C1/10—Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means
- B66C1/22—Rigid members, e.g. L-shaped members, with parts engaging the under surface of the loads; Crane hooks
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Body Structure For Vehicles (AREA)
Abstract
The invention discloses a 40-ton cabin module lifting bracket, belonging to the technical field of machinery. The 40-ton cabin module lifting bracket comprises an upper cross beam, vertical beams, upper lifting lugs, lower lifting plugs, reinforcing plates, transverse lifting lugs and a lower cross beam, wherein a plurality of vertical beams are welded between the upper cross beam and the lower cross beam; the reinforcing plates are arranged on the welded parts of the upper cross beam, the lower cross beam and the vertical beams; the ten lower lifting lugs are welded on the lower part of the upper cross beam, and the four upper lifting lugs are welded on the upper part of the upper cross beam; the two transverse lifting lugs are welded on the vertical beams. The ten vertical beams are directly welded on the upper cross beam and the lower cross beam with a mutual spacing of 1000m. The outer surfaces of the vertical beams are sealed by thin plates, welding beams between the thin plates are double-sided angle welding seams, the thickness of welding legs is 0.7 time that of the thin plates, and the leg-binding welding thickness is 1.2 times the thickness of the thin plates. The 40-ton cabin module lifting bracket has the advantages that weight borne by sections of a cabin is effectively decomposed, the lifting is relatively stable and safe, and the market development space is wide.
Description
Technical field
The present invention relates to 40 tons of cabin module hoisting suspension brackets, belong to field of mechanical technique.
Background technology
Along with the development of modern science and technology, the shortage of land resources, the step of ocean exploitation is more and more faster, the demand of large ship is also increasing, be all that sectional type is built at present, a cabin segmentation just weighs 40 tons, directly falls very dangerous with hook, easy mis-use breakdown is a urgent problem.
Summary of the invention
The object of this invention is to provide 40 tons of cabin module hoisting suspension brackets.
The problem to be solved in the present invention is safety is directly fallen in the segmentation of existing cabin deficiency with hook.
For realizing object of the present invention, the technical solution used in the present invention is:
40 tons of cabin module hoisting suspension brackets, comprise entablatrance, vertical beam, upper hanger, lower hanger, brace panel, horizontal hanger and cross sill, many vertical beams are welded with in the middle of described entablatrance and cross sill, the weld of crossbeam, cross sill and vertical beam is provided with brace panel, entablatrance lower weld has ten lower hangers, upper weld has four upper hangers, vertical beam is welded with two horizontal hangers.
Described crossbeam and cross sill are directly welded with ten vertical beams, and mutual spacing is 1000 meters.
Described entablatrance and vertical beam outside face adopt thin plate front cover, and mutual weld seam is two-sided fillet welding, and leg gets 0.7 times of thin plate, and weldering of binding foot is 1.2 times.
Advantage of the present invention: the weight that cabin segmentation carries by this equipment, carries out actv. decomposition, lifts more steady safety, should have market development space widely.
Accompanying drawing explanation
Fig. 1 is the front view of the present invention's 40 tons of cabin module hoisting suspension brackets;
Fig. 2 is the birds-eye view of the present invention's 40 tons of cabin module hoisting suspension brackets;
Fig. 3 is the lateral plan of the present invention's 40 tons of cabin module hoisting suspension brackets;
In figure: 1, entablatrance 2, vertical beam 3, upper hanger 4, lower hanger 5, brace panel 6, horizontal hanger 7, cross sill.
Detailed description of the invention
Below in conjunction with drawings and Examples, the present invention is further illustrated.
40 tons of cabin module hoisting suspension brackets, comprise entablatrance 1, vertical beam 2, upper hanger 3, lower hanger 4, brace panel 5, horizontal hanger 6 and cross sill 7, many vertical beams 2 are welded with in the middle of described entablatrance 1 and cross sill 7, make it have good load-carrying capacity, the weld of crossbeam 1, cross sill 7 and vertical beam 2 is provided with brace panel 5, prevent structural distortion, entablatrance 1 lower weld has ten lower hangers 4, for being connected with cabin segmentation, upper weld has four upper hangers 3, vertical beam 2 is welded with two horizontal hangers 6, facilitates side direction tiltedly to hang.
Described crossbeam 1 and cross sill 7 are directly welded with ten vertical beams 2, and mutual spacing is 1000 meters, and the structural bearing point meeting cabin segmentation is arranged.
Described entablatrance 1 and vertical beam 2 outside face adopt thin plate front cover, and mutual weld seam is two-sided fillet welding, and leg gets 0.7 times of thin plate, and weldering of binding foot is 1.2 times, good looking appearance, uniform force.
Using method of the present invention: cabin segmentation is arranged according to inner stress point, be lifted on the upper hanger 3 of side and lower hanger 4 respectively, the upper hanger 3 of opposite side is connected with loop wheel machine with lower hanger 4, make stressed wire rope more, power dispersion is average, lifting is arranged long, just very steady during such loop wheel machine lifting, can not arbitrarily rock.
Claims (3)
1.40 tons of cabin module hoisting suspension brackets, comprise entablatrance (1), vertical beam (2), upper hanger (3), lower hanger (4), brace panel (5), horizontal hanger (6) and cross sill (7), it is characterized in that: in the middle of described entablatrance (1) and cross sill (7), be welded with many vertical beams (2), the weld of crossbeam (1), cross sill (7) and vertical beam (2) is provided with brace panel (5), entablatrance (1) lower weld has ten lower hangers (4), upper weld has four upper hangers (3), vertical beam (2) is welded with two horizontal hangers (6).
2. 40 tons of cabin module hoisting suspension brackets according to claim 1, is characterized in that: described crossbeam (1) and cross sill (7) are directly welded with ten vertical beams (2), and mutual spacing is 1000 meters.
3. 40 tons of cabin module hoisting suspension brackets according to claim 1, is characterized in that: described entablatrance (1) and vertical beam (2) outside face adopt thin plate front cover, and mutual weld seam is two-sided fillet welding, and leg gets 0.7 times of thin plate, and weldering of binding foot is 1.2 times.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410717547.3A CN104444774A (en) | 2014-12-03 | 2014-12-03 | 40-ton cabin module lifting bracket |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410717547.3A CN104444774A (en) | 2014-12-03 | 2014-12-03 | 40-ton cabin module lifting bracket |
Publications (1)
Publication Number | Publication Date |
---|---|
CN104444774A true CN104444774A (en) | 2015-03-25 |
Family
ID=52891649
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410717547.3A Pending CN104444774A (en) | 2014-12-03 | 2014-12-03 | 40-ton cabin module lifting bracket |
Country Status (1)
Country | Link |
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CN (1) | CN104444774A (en) |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH10157967A (en) * | 1996-12-02 | 1998-06-16 | Morimi Unyu Kk | Carrier basket |
JP2004250188A (en) * | 2003-02-20 | 2004-09-09 | Asahi Kasei Homes Kk | Hoisting fixture |
CN101224849A (en) * | 2007-12-12 | 2008-07-23 | 大连理工大学 | Hanging bracket for integral hoisting of ship superstructure and hoisting process |
CN201092510Y (en) * | 2007-05-23 | 2008-07-30 | 上海国际港务(集团)股份有限公司军工路分公司 | Articulated type vehicle handling sling |
CN201217608Y (en) * | 2008-04-23 | 2009-04-08 | 天津赛瑞机器设备有限公司 | Integral component suspending beam for hoisting |
CN202670988U (en) * | 2012-07-24 | 2013-01-16 | 中国化学工程第十六建设公司 | Multi-lifting-point self-forming equalizing beam |
CN202785266U (en) * | 2012-04-20 | 2013-03-13 | 天津港第一港埠有限公司 | Sling special for electrode loading and unloading operation |
CN202967862U (en) * | 2012-11-14 | 2013-06-05 | 中铁四局集团第五工程有限公司 | Lifting appliance for beam channel reinforcement cage |
-
2014
- 2014-12-03 CN CN201410717547.3A patent/CN104444774A/en active Pending
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH10157967A (en) * | 1996-12-02 | 1998-06-16 | Morimi Unyu Kk | Carrier basket |
JP2004250188A (en) * | 2003-02-20 | 2004-09-09 | Asahi Kasei Homes Kk | Hoisting fixture |
CN201092510Y (en) * | 2007-05-23 | 2008-07-30 | 上海国际港务(集团)股份有限公司军工路分公司 | Articulated type vehicle handling sling |
CN101224849A (en) * | 2007-12-12 | 2008-07-23 | 大连理工大学 | Hanging bracket for integral hoisting of ship superstructure and hoisting process |
CN201217608Y (en) * | 2008-04-23 | 2009-04-08 | 天津赛瑞机器设备有限公司 | Integral component suspending beam for hoisting |
CN202785266U (en) * | 2012-04-20 | 2013-03-13 | 天津港第一港埠有限公司 | Sling special for electrode loading and unloading operation |
CN202670988U (en) * | 2012-07-24 | 2013-01-16 | 中国化学工程第十六建设公司 | Multi-lifting-point self-forming equalizing beam |
CN202967862U (en) * | 2012-11-14 | 2013-06-05 | 中铁四局集团第五工程有限公司 | Lifting appliance for beam channel reinforcement cage |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150325 |
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RJ01 | Rejection of invention patent application after publication |