CN208176436U - A kind of model aircraft bracket - Google Patents
A kind of model aircraft bracket Download PDFInfo
- Publication number
- CN208176436U CN208176436U CN201820209545.7U CN201820209545U CN208176436U CN 208176436 U CN208176436 U CN 208176436U CN 201820209545 U CN201820209545 U CN 201820209545U CN 208176436 U CN208176436 U CN 208176436U
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- CN
- China
- Prior art keywords
- strut
- mandril
- fixing seat
- pedestal
- model aircraft
- 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.)
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Abstract
The utility model relates to a kind of bracket, in particular to a kind of model aircraft bracket.It include pedestal and the strut on pedestal, the strut is set to pedestal one end and rotates with pedestal and connects, strut is equipped with the regulating mechanism of adjustable support rod height, the other end of pedestal is equipped with the support rod that can be supported to strut, the support rod one end and pedestal rotation connect, the connection of the rotating middle part of the other end and strut, the support rod is equipped with the adjusting component of adjustable support pole length, model aircraft fixing seat is equipped at the top of the strut, the model aircraft fixing seat can be rotated along strut, the utility model provides the model aircraft bracket of a kind of adjustable height and angle.
Description
Technical field
The utility model relates to a kind of bracket, in particular to a kind of model aircraft bracket.
Background technique
Aircraft is one of most important invention of the mankind.Nowadays with the improvement of living condition, there is a large amount of model plane love
Good person.It is therefore desirable to design various model aircrafts for different demands.
Model aircraft generally all carries out display by bracket, and general model aircraft bracket includes pedestal and vertical
The strut being set on pedestal, model aircraft is fixed on strut, for the displaying of model aircraft, but this support angle is high
Degree is not adjustable, and model aircraft cannot be shown to best angle and watched for people.
Summary of the invention
In order to overcome the shortcomings of background technique, the utility model provides the model aircraft of a kind of adjustable height and angle
Bracket.
The technical scheme adopted by the utility model is a kind of model aircraft bracket, includes pedestal and be set on pedestal
Strut, the strut be set to pedestal one end and with pedestal rotate connect, strut be equipped with adjustable support rod height adjusting
Mechanism, the other end of pedestal are equipped with the support rod that can be supported to strut, and the support rod one end and pedestal rotation connect, the other end with
The rotating middle part of strut connects, and the support rod is equipped with the adjusting component of adjustable support pole length, the strut top
Portion is equipped with model aircraft fixing seat, which can rotate along strut.
Preferably, the regulating mechanism includes the mandril connecting with model aircraft fixing seat and the company that connect with pedestal
Extension bar, the connecting rod are equipped with the grafting chamber with opening towards one end of mandril, and the mandril is placed in by opening
It can reciprocatingly slide in grafting chamber and in grafting chamber, being equipped between the mandril and the cavity wall of grafting chamber can be to mandril fixation
Fixation kit.
Preferably, the fixation kit includes short slot, spring and steel ball, and the short slot is set to mandril and is placed in grafting
The cavity wall of the side wall of chamber one end, the grafting chamber is equipped at least two locating slots, and described steel ball one end is placed in short slot,
The other end can be placed in locating slot, and the spring is set to one end in short slot and connect with short slot bottom, and the other end is connect with steel ball.
Preferably, the adjusting component includes that the second mandril connecting with strut and second connect with pedestal connect
Bar, second connecting rod are equipped with the second grafting chamber with the second opening, second top towards one end of strut
Bar is placed in the second grafting chamber and can be reciprocatingly slided in the second grafting chamber by the second opening, second mandril and second
The second fixation kit that can be fixed to the second mandril is equipped between the cavity wall of grafting chamber.
Preferably, second fixation kit includes the second short slot, second spring and the second steel ball, and described second
Short slot is set to the side wall that the second mandril is placed in second grafting chamber one end, and the cavity wall of second grafting chamber is equipped at least two
Second locating slot, the second described steel ball one end are placed in the second short slot, and the other end can be placed in the second locating slot, and described
Two springs are set to one end in the second short slot and connect with the second short slot bottom, and the other end is connect with the second steel ball.
Preferably, the connecting rod bottom is equipped with connecting rod mounting base, and the pedestal is equipped with fixing seat, described
Connecting rod mounting base is bolted with fixing seat and is fixed by locking nut.
Preferably, mandril fixing seat is equipped at the top of the mandril, the model aircraft fixing seat bottom is equipped with arc
Fixing seat, the mandril fixing seat are bolted by second with arc fixing seat and are fixed by the second locking nut.
Preferably, the both ends of the support rod are respectively equipped with support rod fixing seat, the pedestal and strut and support rod
Junction be respectively equipped with the second fixing seat, the support rod fixing seat is bolted and is led to by third with the second fixing seat
Third locking nut is crossed to fix.
The beneficial effects of the utility model are: model aircraft is fixed in the model aircraft fixing seat at the top of connecting rod, by
It can be rotated relative to pedestal in strut, therefore, the angle of strut is adjustable, and model aircraft fixing seat can be revolved with respect to strut
Turn, therefore, the angle of model aircraft fixing seat is again adjustable, the adjusting of model aircraft multi-angle thus may be implemented, and
After regulating mechanism setting, mandril can extend or shorten in grafting chamber, for adjusting the whole height of strut, it can be achieved that bracket angle
The adjusting of degree and height, enables model aircraft to be shown when being fixed on bracket with best angle.
The utility model embodiment is described further with reference to the accompanying drawing.
Detailed description of the invention
Fig. 1 is the entirety sectional view of the utility model embodiment；
Fig. 2 is the B of Fig. 1 in the utility model embodiment to cross-sectional view；
Fig. 3 is the A of Fig. 1 in the utility model embodiment to cross-sectional view；
Fig. 4 is the C of Fig. 1 in the utility model embodiment to cross-sectional view.
Specific embodiment
As Figure 1-Figure 4, the utility model provides a kind of model aircraft bracket, includes that pedestal 1 and bottom are set to pedestal 1
On strut 2, the strut 2 be set to 1 one end of pedestal and with pedestal 1 rotate connect, strut 2 be equipped with adjustable support rod 2 it is high
The regulating mechanism 3 of degree, the other end of pedestal 1 are equipped with the support rod 4 that can be supported to strut 2, and 4 one end of support rod and pedestal 1 revolve
Turn connection, the other end is connect with the rotating middle part of strut 2, and the support rod 4 is equipped with the adjusting of 4 length of adjustable support bar
Component 5 is equipped with model aircraft fixing seat 6 at the top of the strut 2, which can rotate along strut 2, upper
It states in scheme, model aircraft is fixed in the model aircraft fixing seat 6 at 2 top of strut, and strut 2 and the rotation of pedestal 1 connect, therefore
Strut 2 can be rotated along pedestal 1, and for adjusting the angle of strut 2, support rod 4 is the fixation to strut 2, when strut 2 is the bottom of along
When seat 1 rotates, then also and then rotation is simultaneously rotated relative to strut 2 support rod 4 on pedestal 1, regulating mechanism is provided on strut 2
3, extended length or the shortening of strut 2 can be made, for adjusting the height of strut 2, and be provided on support rod 4 and adjust component 5, it can
So that extended length or the shortening of support rod 4, the adjusting of 4 length of support rod is comprehensive also for the angle for adjusting strut 2
Altogether, after model aircraft is fixed in the model aircraft fixing seat 6 on strut 2, the adjusting of Multi-orientation multi-angle may be implemented,
So that model aircraft can arbitrarily be adjusted on bracket according to the position needed self.
The regulating mechanism 3 includes the mandril 31 connecting with model aircraft fixing seat 6 and the connection connecting with pedestal 1
Bar 32, the connecting rod 32 are equipped with the grafting chamber 34 with opening 33 towards one end of mandril 31, and the mandril 31 is logical
Opening 33 is crossed to be placed in grafting chamber 34 and can reciprocatingly slide in grafting chamber 34, the cavity wall of the mandril 31 and grafting chamber 34 it
Between be equipped with can be fixed to mandril 31 fixation kit 7, in the above scheme, when strut 2 needs to extend, mandril 31 is from grafting chamber 34
Extend outwardly, then fixed by fixation kit 7, the whole height of such strut 2 increases, conversely, mandril 31 is retracted to slotting
It connects in chamber 34, the whole height of strut 2 reduces, and adjusts very convenient.
The fixation kit 7 includes short slot 71, spring 72 and steel ball 73, and the short slot 71 is set to mandril 31 and is placed in
The cavity wall of the side wall of 34 one end of grafting chamber, the grafting chamber 34 is equipped at least two locating slots 74, the steel ball 73 1
End is placed in short slot 71, and the other end can be placed in locating slot 74, and the spring 72 is set to one end and 71 bottom of short slot in short slot 71
Portion's connection, the other end are connect with steel ball 73, and in the above scheme, when mandril 31 slides in grafting chamber 34, steel ball 73 is retracted to
In short slot 71, when mandril 31 stops, spring 72 promotes steel ball 73 to be placed in locating slot 74, and at this moment mandril 31 is pushed not outer
Dynamic or in the case where pulling, mandril 31 is fixed, and will not be slided, multiple locating slots 74 in uniformly at intervals in connecting rod 32, this
Sample can be adjusted according to the needs the whole height of strut 2, and after being arranged in this way, the height of strut 2 can be adjusted quickly, only need to pull
Mandril can be pushed.
The adjusting component 5 includes the second mandril 51 connecting with strut 2 and the second connecting rod connecting with pedestal 1
52, second connecting rod 52 is equipped with the second grafting chamber 54 with the second opening 53 towards one end of strut 2, described
Second mandril 51 is placed in the second grafting chamber 54 and can be reciprocatingly slided in the second grafting chamber 54 by the second opening 53, described
It is equipped with the second fixation kit 8 that can be fixed to the second mandril 51 between second mandril 51 and the cavity wall of the second grafting chamber 54, adjusts
The principle of component 5 is the same with the principle of regulating mechanism 3, and the length of support rod 4 is adjusted by the extension and contraction of the second mandril 51
Degree.
Second fixation kit 8 includes the second short slot 81, second spring 82 and the second steel ball 83, and described second
Short slot 81 is set to the side wall that the second mandril 51 is placed in 54 one end of the second grafting chamber, and the cavity wall of second grafting chamber 54 is equipped with
At least two second locating slots 84, described 83 one end of the second steel ball are placed in the second short slot 81, and it is fixed that the other end can be placed in second
In the slot 84 of position, the second spring 82 is set to one end in the second short slot 81 and connect with 81 bottom of the second short slot, the other end and the
Two steel balls 83 connection, the second fixation kit 8 is the same with the principle of fixation kit 7, can quickly to the second mandril 51 after adjusting into
Row is fixed, and making the second mandril 51, fixation will not be slided automatically in the absence of external forces.
32 bottom of connecting rod is equipped with connecting rod mounting base 9, and the pedestal 1 is equipped with fixing seat 91, described
Connecting rod mounting base 9 is connect by bolt 92 with fixing seat 91 and is fixed by locking nut, and in the above scheme, connecting rod is solid
It is designed with the hole being sheathed on bolt 92 in reservation 9 and fixing seat 91, facilitates the rotation of connecting rod mounting base 9 and fixing seat 91,
And locking nut is sheathed on bolt 92, and when rotation, locking nut is unscrewed, connecting rod mounting base 9 is rotated along fixing seat 91,
It adjusts after needing position, locking nut is locked, at this moment connecting rod mounting base 9 and fixing seat 91 are fixed, cannot rotate.
Mandril fixing seat 93 is equipped at the top of the mandril 31,6 bottom of model aircraft fixing seat is solid equipped with arc
Reservation 94, the mandril fixing seat 93 are connect by the second bolt 95 with arc fixing seat 94 and by the second locking nuts 96
Fixed, in the above scheme, the coupling part that mandril fixing seat 93 connects arc fixing seat 94 connect solid with connecting rod mounting base 9
The coupling part of reservation 91 is identical.
The both ends of the support rod 4 are respectively equipped with support rod fixing seat 97, the pedestal 1 and strut 2 and support rod 4
Junction is respectively equipped with the second fixing seat 98, the support rod fixing seat 97 and the second fixing seat 98 and is connected by third bolt 99
It connects and passes through third locking nut and fix, support rod fixing seat 97 connects the coupling part of the second fixing seat 98 and connecting rod is installed
The coupling part structure that seat 9 is connected and fixed seat 91 is identical.
Every technical staff's notice: although the utility model is described according to above-mentioned specific embodiment, this
The invention thought of utility model is not limited to that the utility model, and any repacking with the utility model thought will all be received
Enter in this patent scope of patent protection.
Claims (8)
1. a kind of model aircraft bracket includes pedestal and the strut on pedestal, it is characterised in that: the strut is set to
Pedestal one end simultaneously rotates connection with pedestal, and strut is equipped with the regulating mechanism of adjustable support rod height, and the other end of pedestal is equipped with
The support rod that can be supported to strut, the support rod one end and pedestal rotation connect, and the rotating middle part of the other end and strut connects, institute
The support rod stated is equipped with the adjusting component of adjustable support pole length, is equipped with model aircraft fixing seat at the top of the strut,
The model aircraft fixing seat can be rotated along strut.
2. a kind of model aircraft bracket according to claim 1, it is characterised in that: the regulating mechanism includes and flies
The mandril of machine model fixing base connection and the connecting rod connecting with pedestal, the connecting rod are equipped with tool towards one end of mandril
There is the grafting chamber of opening, the mandril is placed in grafting chamber and can be reciprocatingly slided in grafting chamber by opening, the top
Fixation kit that can be fixed to mandril is equipped between bar and the cavity wall of grafting chamber.
3. a kind of model aircraft bracket according to claim 2, it is characterised in that: the fixation kit includes scarce
Slot, spring and steel ball, the short slot are set to the side wall that mandril is placed in grafting chamber one end, and the cavity wall of the grafting chamber is equipped with
At least two locating slots, described steel ball one end are placed in short slot, and the other end can be placed in locating slot, and the spring, which is set to, to be lacked
One end is connect with short slot bottom in slot, and the other end is connect with steel ball.
4. a kind of model aircraft bracket according to claim 1 or 2 or 3, it is characterised in that: the adjusting component includes
There are the second mandril connecting with strut and the second connecting rod connecting with pedestal, second connecting rod is towards one end of strut
It is equipped with the second grafting chamber with the second opening, second mandril is placed in the second grafting chamber by the second opening and can
It reciprocatingly slides in the second grafting chamber, being equipped between second mandril and the cavity wall of the second grafting chamber can be solid to the second mandril
The second fixed fixation kit.
5. a kind of model aircraft bracket according to claim 4, it is characterised in that: second fixation kit includes
Second short slot, second spring and the second steel ball, second short slot are set to the side that the second mandril is placed in second grafting chamber one end
The cavity wall of wall, second grafting chamber is equipped at least two second locating slots, and the second described steel ball one end is placed in second
In short slot, the other end can be placed in the second locating slot, and the second spring is set to one end and the second short slot bottom in the second short slot
Portion's connection, the other end are connect with the second steel ball.
6. a kind of model aircraft bracket according to claim 2, it is characterised in that: the connecting rod bottom is equipped with connection
Bar mounting base, the pedestal are equipped with fixing seat, and the connecting rod mounting base is bolted and passes through with fixing seat
Locking nut is fixed.
7. a kind of model aircraft bracket according to claim 6, it is characterised in that: solid equipped with mandril at the top of the mandril
Reservation, the model aircraft fixing seat bottom are equipped with arc fixing seat, and the mandril fixing seat passes through with arc fixing seat
Second is bolted and is fixed by the second locking nut.
8. a kind of model aircraft bracket according to claim 1, it is characterised in that: the both ends of the support rod are respectively equipped with
The junction of support rod fixing seat, the pedestal and strut and support rod is respectively equipped with the second fixing seat, the support rod
Fixing seat is bolted by third with the second fixing seat and passes through third locking nut and fixed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820209545.7U CN208176436U (en) | 2018-02-06 | 2018-02-06 | A kind of model aircraft bracket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820209545.7U CN208176436U (en) | 2018-02-06 | 2018-02-06 | A kind of model aircraft bracket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208176436U true CN208176436U (en) | 2018-12-04 |
Family
ID=64439742
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820209545.7U Expired - Fee Related CN208176436U (en) | 2018-02-06 | 2018-02-06 | A kind of model aircraft bracket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208176436U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109363444A (en) * | 2018-12-06 | 2019-02-22 | 徐州创航科技有限公司 | A kind of model display device with multi-angle regulation function |
| CN109887381A (en) * | 2019-03-22 | 2019-06-14 | 四川长江职业学院 | A kind of craftwork teaching demonstration device |
| CN110313763A (en) * | 2019-06-27 | 2019-10-11 | 恒昌工業有限公司 | The model aircraft bracket and model aircraft of multi-angle rotary fight maneuver device |
| CN112061418A (en) * | 2020-05-19 | 2020-12-11 | 中国飞机强度研究所 | Curved plate impact supporting device |
-
2018
- 2018-02-06 CN CN201820209545.7U patent/CN208176436U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109363444A (en) * | 2018-12-06 | 2019-02-22 | 徐州创航科技有限公司 | A kind of model display device with multi-angle regulation function |
| CN109887381A (en) * | 2019-03-22 | 2019-06-14 | 四川长江职业学院 | A kind of craftwork teaching demonstration device |
| CN110313763A (en) * | 2019-06-27 | 2019-10-11 | 恒昌工業有限公司 | The model aircraft bracket and model aircraft of multi-angle rotary fight maneuver device |
| CN110313763B (en) * | 2019-06-27 | 2020-11-13 | 恒昌工業有限公司 | Multi-angle rotating's aircraft model support and aircraft model fight exercise device |
| CN112061418A (en) * | 2020-05-19 | 2020-12-11 | 中国飞机强度研究所 | Curved plate impact supporting device |
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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 |
Granted publication date: 20181204 Termination date: 20220206 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |