CN207425141U - Two shaft staggered formula rotating mechanisms - Google Patents
Two shaft staggered formula rotating mechanisms Download PDFInfo
- Publication number
- CN207425141U CN207425141U CN201720013264.XU CN201720013264U CN207425141U CN 207425141 U CN207425141 U CN 207425141U CN 201720013264 U CN201720013264 U CN 201720013264U CN 207425141 U CN207425141 U CN 207425141U
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- China
- Prior art keywords
- ring
- rotation axis
- swing
- lower frame
- around trajectory
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- Expired - Fee Related
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Abstract
The utility model discloses a kind of two shaft staggered formula rotating mechanisms, include lower frame, swing-around trajectory and cockpit, the lower frame includes symmetrically arranged left lower frame and bottom right frame, and the top of the left lower frame and bottom right frame is equipped with movable span；The swing-around trajectory includes orthogonal two ring rings and two ring rings are fixedly connected；One of ring ring is arranged with a pair of the first rotation axis being adapted with the movable block, and a pair of second rotation axis is arranged on another ring ring；The cockpit is equipped with the turn hole being adapted with second rotation axis；The rotation of cockpit is realized by the first rotation axis on swing-around trajectory and the second rotation axis, achievees the purpose that reduce production cost, improve experience sense and convenient for control.
Description
Technical field
The utility model is related to skimulated motion mechanisms, and in particular to two shaft staggered formula rotating mechanisms.
Background technology
In existing skimulated motion mechanism, the Three Degree Of Freedom that generally uses, six degree of freedom or based on multi link parallel machine
The mode of structure carries out, and causes the increase of production cost in such cases, but also experience sense is poor, and multivariant control
It is more complicated.
Utility model content
In order to solve the above technical problems, the utility model proposes two shaft staggered formula rotating mechanisms, production is reduced to reach
Cost improves experience sense and the purpose convenient for control.
In order to achieve the above objectives, the technical solution of the utility model is as follows：
A kind of two shaft staggered formula rotating mechanisms, include lower frame, swing-around trajectory and cockpit, and the lower frame includes pair
The top of the left lower frame and bottom right frame that title is set, the left lower frame and bottom right frame is equipped with movable span；The rotation
Track includes orthogonal two ring rings and two ring rings are fixedly connected；One of ring ring is arranged with
A pair of the first rotation axis being adapted with the movable block is arranged with a pair of second rotation axis on another ring ring；Institute
It states cockpit and is equipped with the turn hole being adapted with second rotation axis.
The utility model realizes the rotation of cockpit by the first rotation axis on swing-around trajectory and the second rotation axis, reaches reduction
Production cost improves experience sense and the purpose convenient for control.
As preference, the cockpit, which can surround the second rotation axis, carries out 360 ° of rotations, the swing-around trajectory can surround institute
It states the first rotation axis and carries out 360 ° of rotations.
As preference, a pair of first rotation axis and the second rotation of a pair are in same plane.By the way that first is rotated
Axis and the second rotation axis are set in the same plane, be ensure that the quality of simulation, are also ensured the experience sense of user.
As preference, the swing-around trajectory includes horizontal ring ring and vertical ring ring, the horizontal ring ring and
Vertical ring ring is fixedly connected, and the horizontal ring ring is equipped with first rotation axis, and the vertical ring ring is equipped with institute
State the second rotation axis.
As preference, it is additionally provided with protection pedestal below swing-around trajectory.Using pedestal is protected to protect whole equipment,
It directly drops when avoiding the occurrence of accident, ensure that user security.
The utility model has the following advantages that：
1. the utility model realizes the rotation of cockpit by the first rotation axis on swing-around trajectory and the second rotation axis, reach drop
Low production cost improves experience sense and the purpose convenient for control.
2. the utility model ensure that simulation by the way that the first rotation axis and the second rotation axis are set in the same plane
Quality also ensures the experience sense of user.
3. the utility model is directly dropped using pedestal is protected to protect whole equipment when avoiding the occurrence of accident, protect
User security is demonstrate,proved.
Description of the drawings
It in order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described.
Fig. 1 is the expanded schematic diagram of two shaft staggered formula rotating mechanisms disclosed in the utility model embodiment；
Fig. 2 is the scheme of installation of two shaft staggered formula rotating mechanisms disclosed in the utility model embodiment.
Corresponding component title of the number represented by with letter in figure：
1. 13. movable span of lower frame 11. left lower frame, 12. bottom right frame, 2. swing-around trajectory
21. 22. second rotation axis of the first rotation axis, 23. horizontal ring ring 24. indulges ring ring
3. 31. turn hole 4. of cockpit protects pedestal.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe.
The utility model provides two shaft staggered formula rotating mechanisms, and operation principle is by the first rotation on swing-around trajectory
Axis and the second rotation axis realize the rotation of cockpit, achieve the purpose that reduce production cost, improve experience sense and convenient for control.
The utility model is described in further detail with reference to embodiment and specific embodiment.
As depicted in figs. 1 and 2, a kind of two shaft staggered formula rotating mechanisms, include lower frame 1, swing-around trajectory 2 and cockpit 3,
The lower frame includes the top of symmetrically arranged left lower frame 11 and bottom right frame 12, the left lower frame and bottom right frame
It is equipped with movable span 13；The swing-around trajectory includes orthogonal two ring rings and two ring rings are fixedly connected；
One of ring ring is arranged with a pair of the first rotation axis 21 being adapted with the movable block, on another ring ring
It is arranged with a pair of second rotation axis 22；The cockpit is equipped with the turn hole 31 being adapted with second rotation axis.
The utility model realizes the rotation of cockpit by the first rotation axis on swing-around trajectory and the second rotation axis, reaches reduction
Production cost improves experience sense and the purpose convenient for control.
As preference, the cockpit, which can surround the second rotation axis, carries out 360 ° of rotations, the swing-around trajectory can surround institute
It states the first rotation axis and carries out 360 ° of rotations.
As preference, a pair of first rotation axis and the second rotation of a pair are in same plane.By the way that first is rotated
Axis and the second rotation axis are set in the same plane, be ensure that the quality of simulation, are also ensured the experience sense of user.
As preference, the swing-around trajectory includes horizontal ring ring 23 and vertical ring ring 24, the horizontal annulus rail
Road is fixedly connected with vertical ring ring, and the horizontal ring ring is equipped with first rotation axis, is set on the vertical ring ring
There is second rotation axis.
As preference, protection pedestal 4 is additionally provided with below swing-around trajectory.Whole equipment is protected using pedestal is protected
Shield, directly drops when avoiding the occurrence of accident, ensure that user security.
The specifically used step of the utility model is as follows：Again as depicted in figs. 1 and 2, in the actual use process, utilize
First rotation axis 21 is that reference makes cockpit 3 do 360 degree of rotary motions with lower frame 1；Using the second rotation axis 22 with horizontal annulus rail
Road is that reference makes cockpit do 360 ° rotation movement, is rotated with reference to above two so that cockpit gathers around the rotating range there are one 720 °.
By above mode, two shaft staggered formula rotating mechanism provided by the utility model passes through on swing-around trajectory
One rotation axis and the second rotation axis realize the rotation of cockpit, and reaching reduces production cost, improves experience sense and the mesh convenient for control
's.
Above-described is only the preferred embodiment of disclosed in the utility model two shaft staggered formula rotating mechanisms, should
It points out, for those of ordinary skill in the art, on the premise of not departing from the utility model and creating design, can also do
Go out several modifications and improvements, these belong to the scope of protection of the utility model.
Claims (5)
1. a kind of two shaft staggered formula rotating mechanisms, which is characterized in that include lower frame, swing-around trajectory and cockpit, the lower frame
Frame includes symmetrically arranged left lower frame and bottom right frame, and the top of the left lower frame and bottom right frame is equipped with activity
Hole；The swing-around trajectory includes orthogonal two ring rings and two ring rings are fixedly connected；One of annulus
Orbital Symmetry is equipped with a pair of the first rotation axis being adapted with the movable block, and a pair the is arranged on another ring ring
Two rotation axis；The cockpit is equipped with the turn hole being adapted with second rotation axis.
2. two shaft staggered formula rotating mechanism according to claim 1, which is characterized in that the cockpit can surround the second rotation
Axis carries out 360 ° of rotations, and the swing-around trajectory can surround first rotation axis and carry out 360 ° of rotations.
3. two shaft staggered formula rotating mechanism according to claim 1, which is characterized in that a pair of first rotation axis and a pair of the
Two rotations are in same plane.
4. two shaft staggered formula rotating mechanism according to claim 1, which is characterized in that the swing-around trajectory includes horizontal circle
Loop orbit and vertical ring ring, the horizontal ring ring are fixedly connected with vertical ring ring, and the horizontal ring ring is equipped with institute
The first rotation axis is stated, the vertical ring ring is equipped with second rotation axis.
5. two shaft staggered formula rotating mechanism according to claim 1, which is characterized in that be additionally provided with protection below swing-around trajectory
Pedestal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720013264.XU CN207425141U (en) | 2017-01-06 | 2017-01-06 | Two shaft staggered formula rotating mechanisms |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720013264.XU CN207425141U (en) | 2017-01-06 | 2017-01-06 | Two shaft staggered formula rotating mechanisms |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207425141U true CN207425141U (en) | 2018-05-29 |
Family
ID=62397971
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720013264.XU Expired - Fee Related CN207425141U (en) | 2017-01-06 | 2017-01-06 | Two shaft staggered formula rotating mechanisms |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207425141U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112598960A (en) * | 2020-12-03 | 2021-04-02 | 南京全控航空科技有限公司 | Multi-degree-of-freedom motion platform for flight simulator and operation method |
| CN112792985A (en) * | 2020-12-17 | 2021-05-14 | 淮阴工学院 | Double-shaft rotary stirring machine |
-
2017
- 2017-01-06 CN CN201720013264.XU patent/CN207425141U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112598960A (en) * | 2020-12-03 | 2021-04-02 | 南京全控航空科技有限公司 | Multi-degree-of-freedom motion platform for flight simulator and operation method |
| CN112792985A (en) * | 2020-12-17 | 2021-05-14 | 淮阴工学院 | Double-shaft rotary stirring machine |
| CN112792985B (en) * | 2020-12-17 | 2022-05-17 | 淮阴工学院 | Double-shaft rotary stirring machine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20180529 Termination date: 20200106 |