CN207372688U - Steel machine and its fuselage locking device - Google Patents
Steel machine and its fuselage locking device Download PDFInfo
- Publication number
- CN207372688U CN207372688U CN201721387126.4U CN201721387126U CN207372688U CN 207372688 U CN207372688 U CN 207372688U CN 201721387126 U CN201721387126 U CN 201721387126U CN 207372688 U CN207372688 U CN 207372688U
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- CN
- China
- Prior art keywords
- fuselage
- locating part
- postive stop
- stop baffle
- steel machine
- 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.)
- Withdrawn - After Issue
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 40
- 239000010959 steel Substances 0.000 title claims abstract description 40
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 32
- 238000009987 spinning Methods 0.000 claims abstract description 3
- 239000004744 fabric Substances 0.000 claims description 3
- 238000007514 turning Methods 0.000 claims description 3
- 238000003754 machining Methods 0.000 claims description 2
- 230000013011 mating Effects 0.000 claims description 2
- 238000009434 installation Methods 0.000 claims 1
- 239000007787 solid Substances 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 239000000463 material Substances 0.000 abstract description 3
- 230000009471 action Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
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- Conveying And Assembling Of Building Elements In Situ (AREA)
Abstract
This application discloses a kind of steel machine and its fuselage locking device, wherein steel machine includes：Pedestal；Fuselage can be connected on the pedestal with spinning upside down around horizontal axis；Elastic element is arranged between pedestal and fuselage and the elastic force that it is promoted to be flipped up around horizontal axis is applied with to fuselage；Postive stop baffle is fixed with the pedestal；First locating part is connected on the fuselage and is engaged with the postive stop baffle, the fuselage /V is turned over angle first；Second locating part is connected on the fuselage and is engaged with the postive stop baffle, the fuselage /V is turned over angle second；Described first turns over angle turns over angle more than described second.The simple material saving of the application structure, low manufacture cost, and also it is easy to use.
Description
Technical field
This application involves a kind of fuselage locking device of steel machine and the steel machines of this device of configuration.
Background technology
The fuselage locking device of steel machine is one of important feature of steel machine, is used to limit steel machine fuselage in steel
Flip angle on machine base, to improve security when it handles steel.
However existing steel machine fuselage locking mechanism is more there are parts, it is complicated, and make and assembly technology
It is very cumbersome in addition may be overturn in use because fuselage dynamics it is larger and the problem of /V is caused to be failed.
The content of the invention
The purpose of the application is：In view of the above-mentioned problems, the application proposes a kind of steel machine of new structure and its fuselage lock
Determine device, material saving simple in structure, low manufacture cost, and also it is easy to use.
The technical solution of the application is：
A kind of steel machine, including：
Pedestal,
Fuselage, can be connected to spinning upside down around horizontal axis on the pedestal and
Elastic element, be arranged between the pedestal and the fuselage and the fuselage is applied with promote its around
The elastic force that the horizontal axis is flipped up；
It further includes：
Postive stop baffle is fixed with the pedestal；
First locating part is connected on the fuselage and is engaged with the postive stop baffle, with by the fuselage /V
Angle is turned over first；And
Second locating part is connected on the fuselage and is engaged with the postive stop baffle, with by the fuselage /V
Angle is turned over second；
Described first turns over angle turns over angle more than described second.
This steel machine of the application based on the above technical solutions, further includes following preferred embodiment：
The first locating part mounting hole and the second locating part mounting hole, first locating part and institute are offered on the fuselage
It states the second locating part and is connected to the first locating part connecting hole and the second locating part connecting hole.
The first locating part connecting hole is threaded hole, and the second locating part connecting hole light wall pin hole, described first limits
Position part is tightened in the bolt in the first locating part connecting hole for screw thread, and second locating part limits to be plugged in described second
Position part connecting hole in axis pin, and axial position of second locating part in the second locating part connecting hole it is adjustable,
And the mating reaction of second locating part and postive stop baffle is caused to release/regain.
The postive stop baffle is integrally formed on the pedestal.
The postive stop baffle protrudes horizontally up portion including one, when the fuselage turns over angle position in described first, institute
It states the first locating part and is resisted against the bottom for protruding horizontally up portion, overturning is continued up so as to limit the fuselage；When the machine
It is in when described second turns over angle position, second locating part is resisted against the bottom for protruding horizontally up portion, so as to limit
It makes the fuselage and continues up overturning.
Second locating part is circular axis pin, and ring cloth is provided with the circular ring shape that a circle is recessed inwardly on its periphery
The limiting groove being adapted with the postive stop baffle.
The fuselage is to be connected by a horizontally disposed connecting shaft with the base turning, and the horizontal axis is institute
State the central axes of connecting shaft.
The elastic element is the torsion for being sheathed in the connecting shaft and being resisted against between the fuselage and the pedestal
Spring.
The connecting shaft is fixed with pedestal riveting, and the connecting shaft is rotated with the pin hole opened up on the fuselage to be connected
It connects.
A kind of fuselage locking device of steel machine, including：
With the fixed postive stop baffle of steel machining unit base；
The first locating part being connected on steel machine fuselage, first locating part is engaged with the postive stop baffle, with
The fuselage /V is turned over into angle first；And
The second locating part being connected on steel machine fuselage, second locating part is engaged with the postive stop baffle, with
The fuselage /V is turned over into angle second；
Described first turns over angle turns over angle more than described second.
The application has the advantages that：The simple material saving of fuselage locking device structure of the application, low manufacture cost, and
It is and easy to use.
Description of the drawings
The application is described further in the following with reference to the drawings and specific embodiments：
Fig. 1 is the exploded view of steel machine in the embodiment of the present application.
Wherein：
1- pedestals, 2- fuselages, 2a- the first locating part mounting holes, 2b- the second locating part mounting holes, 3- postive stop baffles, 3a-
Protrude horizontally up portion, the first locating parts of 4-, the second locating parts of 5-, 5a- limiting grooves, 6- connecting shafts, 7- torsional springs.
Specific embodiment
The application is described in further detail below by specific embodiment combination attached drawing.The application can be with a variety of
Different forms is realized, however it is not limited to the present embodiment described embodiment.The purpose of detailed description below is provided
It is easy for becoming apparent from present disclosure thorough explanation, the words of the wherein indicating positions such as upper and lower, left and right is only pin
To shown structure in respective figure for position.
Fig. 1 shows a preferred embodiment of this steel machine of the application, identical with traditional steel machine structure, should
Steel machine also includes：Pedestal 1 and fuselage 2, wherein, fuselage 2 is connected by a horizontally disposed connecting shaft 6 and the overturning of pedestal 1, even
The torsional spring 7 being resisted against between fuselage 2 and pedestal 1 is arranged in spindle 6, torsional spring 7, which is applied with fuselage 2, promotes fuselage 2 around foregoing
The elastic force that connecting shaft 6 is flipped up.
The key improvements of the present embodiment are that the steel machine employs the fuselage locking device of special construction, fuselage locking
Device is mainly made of postive stop baffle 3, the first locating part 4 and the second locating part 5.Wherein, postive stop baffle 3 is integrally formed at pedestal
1, the directly punch forming on pedestal 1, the two are structure as a whole (one is fixed).First locating part 4 is connected on fuselage 2,
And it is engaged with postive stop baffle 3, is flipped up with limiting fuselage 2.Second locating part 5 is connected on fuselage 2 and and postive stop baffle
It 3 is engaged, is also used for limitation fuselage 2 and is flipped up.Wherein, 2 /V of fuselage can be turned over angle by the first locating part 4 first,
2 /V of fuselage is turned over angle by the second locating part 5 second, and first turns over angle turns over angle more than second.Specifically, it is foregoing
First turns over angle turns over extreme angles for fuselage 2, and second turns over the extreme angles that angle is downwardly turned over close to fuselage 2.
In the present embodiment, the first locating part mounting hole 2a and the second locating part mounting hole 2b are offered on the fuselage 2,
In, the first locating part connecting hole 2a be threaded hole, the second locating part connecting hole 2b light wall pin holes.First locating part 4 revolves for screw thread
The tightly bolt in the first locating part connecting hole 2a, the second locating part 5 are to be plugged in the second locating part connecting hole 2b
Axis pin.And what axial position of second locating part 5 in the second locating part connecting hole 2b can be adjusted manually (is similar to bolt
Structure), when user presses second locating part 5 close to that one end of postive stop baffle 3, the second locating part 5 is away from limiting block
Plate 3 moves, and loses the position-limiting action to fuselage 2；When user presses that away from postive stop baffle 3 of second locating part 5
During end, the second locating part 5 is moved close to postive stop baffle 3, and recaptures the position-limiting action to fuselage 2.
Postive stop baffle 3 protrudes horizontally up portion 3a including one, and the first locating part 4 is always in the lower section for protruding horizontally up portion 3a.When
When the steel machine is in non-working condition (shutdown), operator presses the second locating part 5 close to that one end of postive stop baffle 3 in advance
(i.e. in Fig. 1 the right end of the second locating part 5 or directly by the second locating part remove), and cause the second locating part 5 lose to machine
The position-limiting action of body 2.Operator, which buttresses fuselage 2, makes it be downwardly turned over around connecting shaft 6, until turning to the limit under the first locating part 4
During position, that one end (i.e. the left end of the second locating part 5 in Fig. 1) of the second locating part 5 away from postive stop baffle 3 is pressed, makes second
Locating part 5 stretches into the lower position for protruding horizontally up portion 3a, unclamps fuselage 2, and under the elastic force effect of torsional spring 7, fuselage 2 is flipped up
After very little angle, the second locating part 5, which presses to be resisted against, protrudes horizontally up portion 3a bottoms, and so as to prevent to be lifted on fuselage 2, fuselage 2 is locked
Fixed, fuselage 2 and pedestal 1 close up, security of the collateral security steel machine under non-working condition (shutdown).When steel machine needs to start shooting
During normal use, then the second locating part 5 is pressed close to that one end of postive stop baffle 3, the second locating part 5 is made to lose to fuselage 2
Position-limiting action, fuselage 2 can freely be overturn.During use of starting shooting, if fuselage 2 is flipped up larger angle and cause the first limit
Position part 4 contradict to when protruding horizontally up portion 3a bottoms, fuselage 2 can not continue to turn over, can equally avoid 2 flip angle of fuselage excessive and
Bring danger.
Above-mentioned second locating part 5 is circular axis pin, and ring cloth is provided with the annulus that a circle is recessed inwardly on its periphery
The width that width and the postive stop baffle of the limiting groove 5a of shape, limiting groove 5a protrude horizontally up portion 3a is suitable, when the second locating part 5
When being abutted against each other together with postive stop baffle 3, the portion 3a of protruding horizontally up is embedded just below in limiting groove 5a, to prevent fuselage 2 or so
Offset.
In the present embodiment, above-mentioned connecting shaft 6 is fixed with the riveting of pedestal 1, and connecting shaft 6 is rotated with the pin hole opened up on fuselage 2
Connection.
Certainly, above-described embodiment is only the technical concepts and features for illustrating the application, and its object is to make people much of that
Solution present context is simultaneously implemented according to this, and the protection domain of the application can not be limited with this.It is all according to the application major technique
The equivalent transformation or modification that the Spirit Essence of scheme is done, should all cover within the protection domain of the application.
Claims (10)
1. a kind of steel machine, including：
Pedestal (1),
Fuselage (2), can be connected to spinning upside down around horizontal axis on the pedestal (1) and
Elastic element, is arranged between the pedestal (1) and the fuselage (2) and the fuselage (2) is applied with and promote
Its elastic force being flipped up around the horizontal axis；
It is characterized in that, it further includes：
Postive stop baffle (3), it is fixed with the pedestal (1)；
First locating part (4) is connected on the fuselage (2) and is engaged with the postive stop baffle (3), with by the machine
Body (2) /V turns over angle first；And
Second locating part (5) is connected on the fuselage (2) and is engaged with the postive stop baffle (3), with by the machine
Body (2) /V turns over angle second；
Described first turns over angle turns over angle more than described second.
2. steel machine according to claim 1, which is characterized in that the installation of the first locating part is offered on the fuselage (2)
Hole (2a) and the second locating part mounting hole (2b), first locating part (4) and second locating part (5) are connected to institute
It states in the first locating part mounting hole (2a) and the second locating part mounting hole (2b).
3. steel machine according to claim 2, which is characterized in that the first locating part mounting hole (2a) is threaded hole,
Second locating part mounting hole (2b) the light wall pin hole, first locating part (4) are tightened in first locating part for screw thread
Bolt in mounting hole (2a), second locating part (5) are the axis pin being plugged in the second locating part mounting hole (2b),
And axial position of second locating part (5) in the second locating part mounting hole (2b) is adjustable and causes described the
Two locating parts (5) and the mating reaction of postive stop baffle (3) are released/regained.
4. steel machine according to claim 1, which is characterized in that the postive stop baffle (3) is integrally formed at the pedestal
(1) on.
5. steel machine according to claim 1, which is characterized in that the postive stop baffle (3) protrudes horizontally up portion including one
(3a), when the fuselage (2) turns over angle position in described first, first locating part (4) is resisted against the level
The bottom of extension (3a) continues up overturning so as to limit the fuselage (2)；When the fuselage (2) is on described second
When turning over angle position, second locating part (5) is resisted against the bottom for protruding horizontally up portion (3a), so as to limit the fuselage
(2) overturning is continued up.
6. steel machine according to claim 5, which is characterized in that second locating part (5) is circular axis pin, and its
Ring cloth is provided with the limiting groove being adapted with the postive stop baffle (3) for the circular ring shape that a circle is recessed inwardly on periphery
(5a)。
7. steel machine according to claim 1, which is characterized in that the fuselage (2) is by a horizontally disposed connection
Axis (6) and the pedestal (1) overturning connection, the horizontal axis is the central axes of the connecting shaft (6).
8. steel machine according to claim 7, which is characterized in that the elastic element is to be sheathed on the connecting shaft (6)
Torsional spring (7) that is upper and being resisted against between the fuselage (2) and the pedestal (1).
9. steel machine according to claim 7, which is characterized in that the connecting shaft (6) and the pedestal (1) riveting are solid
Fixed, the connecting shaft (6) is rotatablely connected with the pin hole opened up on the fuselage (2).
10. the fuselage locking device of a kind of steel machine, it is characterised in that the device includes：
With steel machining unit base (1) fixed postive stop baffle (3)；
The first locating part (4) being connected on steel machine fuselage (2), first locating part (4) and the postive stop baffle (3) phase
Cooperation, the fuselage (2) /V is turned over angle first；And
The second locating part (5) being connected on steel machine fuselage (2), second locating part (5) and the postive stop baffle (3) phase
Cooperation, the fuselage (2) /V is turned over angle second；
Described first turns over angle turns over angle more than described second.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721387126.4U CN207372688U (en) | 2017-10-25 | 2017-10-25 | Steel machine and its fuselage locking device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721387126.4U CN207372688U (en) | 2017-10-25 | 2017-10-25 | Steel machine and its fuselage locking device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207372688U true CN207372688U (en) | 2018-05-18 |
Family
ID=62337238
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721387126.4U Withdrawn - After Issue CN207372688U (en) | 2017-10-25 | 2017-10-25 | Steel machine and its fuselage locking device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207372688U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107553151A (en) * | 2017-10-25 | 2018-01-09 | 锐奇控股股份有限公司 | Steel machine and its fuselage locking device |
| CN110962107A (en) * | 2018-09-28 | 2020-04-07 | 科沃斯商用机器人有限公司 | Robot and mounting method |
-
2017
- 2017-10-25 CN CN201721387126.4U patent/CN207372688U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107553151A (en) * | 2017-10-25 | 2018-01-09 | 锐奇控股股份有限公司 | Steel machine and its fuselage locking device |
| CN107553151B (en) * | 2017-10-25 | 2024-04-16 | 锐奇控股股份有限公司 | Steel machine and machine body locking device thereof |
| CN110962107A (en) * | 2018-09-28 | 2020-04-07 | 科沃斯商用机器人有限公司 | Robot and mounting method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20180518 Effective date of abandoning: 20240416 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20180518 Effective date of abandoning: 20240416 |
|
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |