CN103891445B - Machine of working soil locks wing mechanism automatically - Google Patents
Machine of working soil locks wing mechanism automatically Download PDFInfo
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- CN103891445B CN103891445B CN201310052942.XA CN201310052942A CN103891445B CN 103891445 B CN103891445 B CN 103891445B CN 201310052942 A CN201310052942 A CN 201310052942A CN 103891445 B CN103891445 B CN 103891445B
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Abstract
The invention belongs to talents for agri-mechanization, be that a kind of machine of working soil locks wing mechanism automatically.It includes girder combination, spar combination, flap oil cylinder, little frame and connecting plate；Girder combination is hinged with spar combination, and pin joint is positioned at above end of main beam；Two connecting plates lay respectively at lock wing mechanism both sides automatically, the lower left quarter of connecting plate is hinged with girder combination, pin joint is positioned at below end of main beam, bearing pin by the long slot bore on the hole F of connecting plate upper right quarter and little frame by hinged to connecting plate, little frame and flap oil cylinder piston rod end；The round-meshed one end of little frame is hinged with spar combination by the hole E on spar side plate, and pin joint is positioned at above spar end；Bolt is arranged on square steel, the U-lag contacts side surfaces on its end and connecting plate.Use the invention has the beneficial effects as follows: after spar generated duty, can automatically spar and girder be locked together, and makes whole machine provide steady, a balanced downward pressure, it is prevented that machine of working soil both wings are upper shifting because of insufficient pressure.
Description
Technical field
The invention belongs to a kind of farm working machinery, what particularly relate to a kind of wide level soil preparation machine locks wing mechanism automatically.
Background technology
Currently known wide level soil preparation machine tool is made up of host machine part and two shoulder portion, and host machine part for being flexibly connected, is handled the lifting of flank with shoulder portion by flap oil cylinder, is travel position when being duty, rise when flank falls, it does not have lock wing mechanism.Said structure there is the problem that when flank expansion becomes duty, flank is with main frame for being flexibly connected, and flank is due to lightweight, it is easy to floats, and causes tilling depth unstable and site preparation quality declines, and directly influences the growth with crop of emerging of seed.
Summary of the invention
It is an object of the invention to the deficiency overcoming prior art to exist, it is provided that a kind of relatively simple for structure, use reliable, easy to operate wide level soil preparation machine automatically to lock wing mechanism.
In order to realize foregoing invention purpose, the technical scheme is that and realized by following measures: a kind of machine of working soil locks wing mechanism automatically, including girder combination, spar combination, flap oil cylinder, little frame and connecting plate；Girder combination is hinged with spar combination, and pin joint is positioned at above end of main beam；Two connecting plates lay respectively at lock wing mechanism both sides automatically, the lower left quarter of connecting plate is hinged with girder combination, pin joint is positioned at below end of main beam, bearing pin by the long slot bore on the hole F of connecting plate upper right quarter and little frame by hinged to connecting plate, little frame and flap oil cylinder piston rod end；The round-meshed one end of little frame is hinged with spar combination by the hole E on spar side plate, and pin joint is positioned at above spar end；Bolt is arranged on the U-lag contacts side surfaces on the square steel of spar combination, on bolt end and connecting plate；The oil cylinder seat of flap oil cylinder one end and girder combination is hinged, the other end and hinge.
Above-mentioned machine of working soil locks wing mechanism automatically, it is characterised in that: the combination of described girder is made up of oil cylinder seat, girder, girder side plate；There is a hole A girder side plate lower end, there is a hole B upper end, hole A and hole B is positioned on the longitudinally asymmetric line of girder side plate, two girder side plates are respectively welded at end of main beam both sides, hole B is positioned at above girder, hole A is positioned at below girder adjacent with girder lower plane, and oil cylinder seat is positioned on the left of girder side plate, is welded on above girder.
Above-mentioned machine of working soil locks wing mechanism automatically, it is characterised in that: the combination of described spar is made up of spar side plate, square steel and spar；On spar side plate, porose C and hole D, hole D are positioned at the spar side plate upper left corner, and hole C is positioned at the lower right of hole D；Two spar side plates lay respectively at spar both sides, are welded on square steel, and square steel two ends have screw, square steel to be welded on below spar end, and hole C and hole D is positioned at above spar, and hole D is in left side, and hole C is on right side.
Above-mentioned machine of working soil locks wing mechanism automatically, it is characterised in that: described little frame is made up of pipe between little frame side plate and little frame, and between little frame, pipe and two little frame side plates are solidly installed, and there is circular hole E little frame side plate one end, and the other end has a long slot bore.
Above-mentioned machine of working soil locks wing mechanism automatically, it is characterised in that: having two holes on described connecting plate, hole F is positioned at the connecting plate upper right corner, and hole G is positioned at the lower left corner；A U-lag is had on the right side of the bottom of connecting plate, hole G.
Use the invention has the beneficial effects as follows: after spar generated duty, can automatically spar and girder be locked together, and makes whole machine provide steady, a balanced downward pressure, it is prevented that machine of working soil both wings are upper shifting because of insufficient pressure.Adopt the present invention that machine of working soil tilling depth on whole working width can be made consistent, wholely more smooth.
Accompanying drawing explanation
Accompanying drawing 1 is the front view of the present invention.
Accompanying drawing 2 is the top view of the present invention.
Accompanying drawing 3 is the front view of middle girder of the present invention combination.
Accompanying drawing 4 is the top view of middle girder of the present invention combination.
Accompanying drawing 5 is the front view of central spar of the present invention combination.
Accompanying drawing 6 is the top view of central spar of the present invention combination.
Accompanying drawing 7 is the front view of the medium and small frame of the present invention.
Accompanying drawing 8 is the left view of the medium and small frame of the present invention.
Accompanying drawing 9 is the front view of connecting plate in the present invention.
Coding in accompanying drawing is respectively as follows: 1 for flap oil cylinder, and 2 combine for girder, and 3 is bolt, and 4 is connecting plate, and 5 combine for spar, and 6 is little frame, and 7 is bearing pin, and 8 is cylinder support, and 9 is girder, and 10 is girder side plate.11 is hole A, and 12 is hole B, and 13 is spar side plate, and 14 is square steel, and 15 is spar, and 16 is hole E, and 17 is hole D, and 18 is little frame side plate, and 19 is manage between little frame, and 20 is circular hole E, and 21 is long slot bore, and 22 is circular hole F, and 23 is U-lag, and 24 is circular hole G.
Detailed description of the invention
Below in conjunction with embodiment and accompanying drawing, the invention will be further described.
In fig. 1 and 2, this machine of working soil is automatically locked wing mechanism and is included flap oil cylinder 1, girder combination 2, bolt 3, connecting plate 4, spar combination 5, little frame 6 and bearing pin 7.Girder combination 2 is combined 5 hinged with spar, and pin joint is positioned at above girder 9 end；Two connecting plates 4 lay respectively at machine of working soil and automatically lock wing mechanism both sides, it is hinged that the lower left quarter of connecting plate 4 and girder combine 2, pin joint is positioned at below girder 9 end, bearing pin 7 by the long slot bore on the hole F of connecting plate 4 upper right quarter and little frame by hinged to connecting plate 4, little frame 6 and flap oil cylinder 1 tailpiece of the piston rod；Little round-meshed one end of frame 6 is combined 5 hinged by the hole E on spar side plate and spar, and pin joint is positioned at above spar end；Bolt 3 is arranged on the U-lag contacts side surfaces on the square steel of spar combination, on bolt end and connecting plate 4；Flap oil cylinder 1 one end is hinged with the oil cylinder seat 8 of girder combination, and the other end is hinged with bearing pin 7.
As shown in Figure 3 and Figure 4: girder combination 2 is made up of oil cylinder seat 8, girder 9, girder side plate 10.There is a hole A11 girder side plate 10 lower end, there is a hole B12 upper end, hole A and hole B is positioned on the longitudinally asymmetric line of girder side plate 10, two girder side plates 10 are respectively welded at both sides, girder 9 end, hole B12 is positioned at above girder 9, hole A11 is positioned at below girder 9 adjacent with girder 9 lower plane, and oil cylinder seat 8 is positioned on the left of girder side plate 10, is welded on above girder 9.
As shown in Figure 5 and Figure 6: spar combination 5 is made up of spar side plate 13, square steel 14 and spar 15；On spar side plate, porose C16 and hole D17, hole D17 are positioned at spar side plate 13 upper left corner, and hole C16 is positioned at the lower right of hole D17；Two spar side plates 13 lay respectively at spar 15 both sides, are welded on square steel (14), and square steel 14 two ends have screw, square steel 14 to be welded on below spar 15 end, and hole C16 and hole D17 is positioned at above spar, and hole D17 is in left side, and hole C16 is on right side.
As shown in Figure 7 and Figure 8: little frame 6 is made up of pipe 19 between little frame side plate 18 and little frame, between little frame, pipe 19 and two little frame side plates 18 are solidly installed, and there is circular hole E20 little frame side plate 18 one end, and the other end has a long slot bore 21.
As shown in Figure 9: have two holes on connecting plate 4, hole F22 is positioned at connecting plate 4 upper right corner, and hole G24 is positioned at connecting plate 4 lower left corner；A U-lag 23 is had on the right side of the bottom of connecting plate 4, hole G24.
The work process of the present invention is: when spar is launched into duty (as shown in Figure 1), bolt head end face contacts with the grooved surface of connecting plate 4, spar and girder are locked into one, make whole machine provide steady, a balanced downward pressure, effectively stop both wings upper shifting because of insufficient pressure.Adopt the present invention that machine of working soil tilling depth on whole working width can be made consistent, wholely more smooth.When machine of working soil is converted to travel position by duty by needs, flap oil cylinder is retracted backward, first pulls side plate 4 to rotate so that it is go out of lock position, then drives little frame to rotate, and then drives spar to rotate, until it reaches travel position.
Claims (5)
1. a machine of working soil locks wing mechanism automatically, it is characterised in that include girder combination (2), spar combination (5), flap oil cylinder (1), little frame (6) and connecting plate (4)；Girder combination (2) is hinged with spar combination (5), and pin joint is positioned at above girder (9) end；Two connecting plates (4) lay respectively at machine of working soil and automatically lock wing mechanism both sides, the lower left quarter of connecting plate (4) is hinged with girder combination (2), pin joint is positioned at below girder (9) end, and bearing pin (7) is by the hole F(22 of connecting plate (4) upper right quarter) and little frame on long slot bore (21) by hinged to connecting plate (4), little frame (6) and flap oil cylinder (1) tailpiece of the piston rod；Little frame (6) round-meshed one end is by the hole E(16 on spar side plate (13)) hinged with spar combination (5), pin joint is positioned at above spar (15) end；Bolt (3) is arranged on U-lag (23) contacts side surfaces on the square steel (14) of spar combination, on bolt end and connecting plate (4)；Flap oil cylinder (1) one end is hinged with the oil cylinder seat (8) of girder combination, and the other end is hinged with bearing pin (7).
2. automatically lock wing mechanism by the machine of working soil described in claim 1, it is characterized in that: described girder combination (2) is by oil cylinder seat (8), girder (9), girder side plate (10) forms, there is a hole A(11 girder side plate (10) lower end), there is a hole B(12 upper end), hole A(11) and hole B(12) be positioned on the longitudinally asymmetric line of girder side plate (10), two girder side plates (10) are respectively welded at girder (9) both sides, end, hole B(12) it is positioned at girder (9) top, hole A(11) it is positioned at girder (9) lower section, adjacent with girder (9) lower plane, oil cylinder seat (8) is positioned at girder side plate (10) left side, it is welded on girder (9) above.
3. automatically lock wing mechanism by the machine of working soil described in claim 1, it is characterised in that: described spar combination (5) is made up of spar side plate (13), square steel (14) and spar (15)；The upper porose C(16 of spar side plate (13)) and hole D(17), hole D(17) be positioned at spar side plate (13) upper left corner, hole C(16) be positioned at hole D(17) and lower right；Two spar side plates (13) lay respectively at spar (15) both sides, are welded on square steel (14), there is screw at square steel (14) two ends, square steel (14) is welded on below spar (15) end, hole C(16) and hole D(17) be positioned at above spar, hole D(17) in left side, hole C(16) on right side.
4. automatically lock wing mechanism by the machine of working soil described in claim 1, it is characterized in that: described little frame (6) is made up of pipe (19) between little frame side plate (18) and little frame, manage (19) between little frame to be solidly installed with two little frame side plates (18), there is circular hole E(20 little frame side plate (18) one end), the other end has a long slot bore (21).
5. automatically lock wing mechanism by the machine of working soil described in claim 1, it is characterised in that: described connecting plate (4) has two holes, hole F(22) it is positioned at connecting plate (4) upper right corner, hole G(24) it is positioned at the lower left corner；In the bottom of connecting plate (4), hole G(24) right side have a U-lag (23).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310052942.XA CN103891445B (en) | 2013-02-19 | 2013-02-19 | Machine of working soil locks wing mechanism automatically |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310052942.XA CN103891445B (en) | 2013-02-19 | 2013-02-19 | Machine of working soil locks wing mechanism automatically |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103891445A CN103891445A (en) | 2014-07-02 |
| CN103891445B true CN103891445B (en) | 2016-07-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310052942.XA Active CN103891445B (en) | 2013-02-19 | 2013-02-19 | Machine of working soil locks wing mechanism automatically |
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| CN (1) | CN103891445B (en) |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3814191A (en) * | 1972-12-26 | 1974-06-04 | Case Co J I | Powered lift and lock for a foldable implement frame |
| US4030551A (en) * | 1976-04-12 | 1977-06-21 | International Harvester Company | Folding flex toolbar |
| JP3426466B2 (en) * | 1997-05-01 | 2003-07-14 | 小橋工業株式会社 | How to lock a folding farm work machine |
| CN2741333Y (en) * | 2004-10-14 | 2005-11-23 | 黑山县机械制造有限公司 | High speed amplitude modulation hydraulic turning plow |
| CN2912219Y (en) * | 2006-07-07 | 2007-06-20 | 新疆科神农业装备科技开发有限公司 | Foldable beam frame for seed planter |
| CN201430753Y (en) * | 2009-03-11 | 2010-03-31 | 常用旺 | Foldable paddy field tillage machine |
| CN202565672U (en) * | 2011-11-09 | 2012-12-05 | 王新平 | Hydraulic reversible plow adjustable in plow width |
| CN203057812U (en) * | 2013-02-19 | 2013-07-17 | 新疆农垦科学院 | Automatic wing locking mechanism of soil preparation machine |
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2013
- 2013-02-19 CN CN201310052942.XA patent/CN103891445B/en active Active
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| CN103891445A (en) | 2014-07-02 |
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