CN207676474U - A kind of aircraft remote controler - Google Patents
A kind of aircraft remote controler Download PDFInfo
- Publication number
- CN207676474U CN207676474U CN201721807618.4U CN201721807618U CN207676474U CN 207676474 U CN207676474 U CN 207676474U CN 201721807618 U CN201721807618 U CN 201721807618U CN 207676474 U CN207676474 U CN 207676474U
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- China
- Prior art keywords
- main body
- armlet
- slot
- open slot
- remote controler
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Abstract
The utility model discloses a kind of aircraft remote controlers, including main body and two armlets being oppositely arranged on main body bottom plate, one armlet is arranged close to the left plate of main body, another armlet is arranged close to the right plate of main body, armlet is the shell of the hollow structure of a side opening, one end of shell is rotatably connected with main body, and the other end of shell has the open slot being arranged along its length；Bottom plate is equipped with limiting slot, and limiting slot is collinearly arranged with open slot and limiting slot is connected with open slot；Further include two limit assemblies, two limit assemblies are arranged in a one-to-one correspondence with two armlets, and limit assembly includes limited block, elastic component and fixed block；Fixed block is set to side of the bottom plate far from armlet, and limited block includes connected sliding part and limiting section, and in main body, limiting section is matched through limiting slot with open slot sliding position；One end of elastic component connects sliding part, the other end connection fixing block of elastic component.Aircraft remote controler, which is provided with, receives the function of object.
Description
Technical field
The utility model is related to unmanned vehicle technical field more particularly to a kind of aircraft remote controlers.
Background technology
As civilian unmanned vehicle industry technology develops, more and more people's purchase uses unmanned vehicle.Application number
A kind of remote controler is disclosed for 201630013411.2 Chinese appearance patent, as shown in Figure 1, examining for usage comfort
It measures, there are two the lug bosses of arc for the bottom case tool in the shell of the remote controler, and user is when using aircraft remote controler, both hands palm
The heart is close to two lug bosses respectively.
Although the comfort level that can improve user's operation of lug boss and user can be allowed preferably to control remote controler,
The effect of lug boss still seems insufficient, and lug boss also has other values that can excavate.
User's operation aircraft is certain to select outdoor environment, and user will certainly want carrying keys, money to being gone to open air
Coin etc., key, coin etc. often bring inconvenience and easy to be lost during user is run, if can be by key, coin etc.
It is put into aircraft remote controler, user will not have the risk that key, coin are lost again.
Utility model content
Technical problem to be solved in the utility model is：A kind of multifunction aircraft remote controler is provided.
In order to solve the above-mentioned technical problem, the technical solution adopted in the utility model is：A kind of aircraft remote controler, including
Main body and two armlets being oppositely arranged on main body bottom plate, an armlet are arranged close to the left plate of main body, another armlet
Right plate close to main body is arranged, and the armlet is the shell of the hollow structure of a side opening, one end of the shell and main body
It is rotatably connected, the other end of shell has the open slot being arranged along its length；The bottom plate is equipped with limiting slot, limit
Slot is collinearly arranged with open slot and limiting slot is connected with open slot；Further include two limit assemblies, two limit assemblies and two
A armlet is arranged in a one-to-one correspondence, and limit assembly includes limited block, elastic component and fixed block；Fixed block is set to the bottom plate far from shield
The side of arm, limited block include connected sliding part and limiting section, and for sliding position in the main body, limiting section runs through the limit
Position slot is matched with the open slot；One end of the elastic component connects the sliding part, described in the other end connection of elastic component
Fixed block.
Further, the width of the sliding part is more than the width of the limiting slot.
Further, the equivalent width of the width of the limiting slot and the open slot.
Further, the width of the limiting section is smaller 0-0.5mm than the width of the open slot.
Further, the one end of the limiting section far from sliding part has towards the extension extended away from armlet direction.
Further, side of the extension far from main body is equipped with several protrusions.
Further, opposite on the limiting section to set there are two fixture block, the fixture block is located at the bottom plate close to the shield
The side of arm, and the side of the fixture block supports the bottom plate.
The beneficial effects of the utility model are：Armlet is the shell of side open hollow structure, can be incited somebody to action when user gos out
The object that key, coin etc. are easily lost is put into the hollow structure of shell, and then rotating armlet makes open slot be aligned with limiting slot,
Limiting section is discharged again, and limiting section is made to be inserted into the open slot of shell, the object easily lost at this time is limited in an enclosure space, to
It allows aircraft remote controler to be provided with and receives the function of object, the confined space of aircraft remote controler is adequately utilized, eliminates user
The risk for losing fine pieces is conducive to enhance user experience.
Description of the drawings
Fig. 1 is the aircraft remote controler of the prior art；
Fig. 2 is the rearview of the aircraft remote controler of the utility model embodiment one；
Fig. 3 is the partial sectional view in the aircraft remote controler limit assembly region of the utility model embodiment one；
Fig. 4 is the structural schematic diagram of the limited block in the aircraft remote controler of the utility model embodiment one；
Fig. 5 is the vertical view of the armlet in the aircraft remote controler of the utility model embodiment one.
Label declaration：
1, main body；11, bottom plate；12, left plate；13, right plate；2, armlet；3, open slot；
4, limiting slot；5, limited block；51, sliding part；52, limiting section；53, extension；
54, fixture block；6, elastic component；7, fixed block.
Specific implementation mode
For technology contents, the objects and the effects of the utility model are described in detail, below in conjunction with embodiment and match
Attached drawing is closed to be explained.
The design of the utility model most critical is：Armlet is the shell of the hollow structure of a side opening, armlet and main body
It is rotatably connected；Setting limit assembly compatible with armlet upper open slot, passes through cooperation locking/solution of limiting section and open slot
Lock armlet.
It please refers to Fig. 2 to Fig. 5, a kind of aircraft remote controler, including main body 1 and two is oppositely arranged on 1 bottom plate 11 of main body
On armlet 2, an armlet 2 is arranged close to the left plate 12 of main body 1, another armlet 2 sets close to the right plate 13 of main body 1
It sets, the armlet 2 is the shell of the hollow structure of a side opening, and one end and the main body 1 of the shell are rotatably connected, shell
The other end has the open slot 3 being arranged along its length；The bottom plate 11 is equipped with limiting slot 4, limiting slot 4 and open slot 3
Collinearly it is arranged and limiting slot 4 is connected with open slot 3；Further include two limit assemblies, two limit assemblies and two armlets 2 one
One is correspondingly arranged, and limit assembly includes limited block 5, elastic component 6 and fixed block 7；Fixed block 7 is set to the bottom plate 11 far from armlet
2 side, limited block 5 include that connected sliding part 51 and limiting section 52, sliding part 51 are located in the main body 1, limiting section 52
It is matched with the open slot 3 through the limiting slot 4；One end of the elastic component 6 connects the sliding part 51, elastic component 6
The other end connect the fixed block 7.
The operation principle of the utility model is summarized as follows：User screws out armlet 2, and fine pieces are put into the hollow of armlet 2
After in structure, one hand of user moves the limiting section 52 of limited block 5, and another hand cycle armlet 2 makes the open slot 3 on armlet 2
It is aligned with the limiting slot 4 on bottom plate 11, then unclamps limited block 5, limited block 5 enters open slot 3 under the action of elastic component 6
In, to lock armlet 2.
As can be seen from the above description, the beneficial effects of the utility model are：Armlet is the shell of side open hollow structure,
The object that key, coin etc. are easily lost can be put into the hollow structure of shell by user when going out, and then rotating armlet makes opening
Slot is aligned with limiting slot, then discharges limiting section, so that limiting section is inserted into the open slot of shell, the object easily lost at this time is limited in
One enclosure space receives the function of object to allow aircraft remote controler to be provided with, the limited of aircraft remote controler is adequately utilized
Space eliminates the risk that user loses fine pieces, is conducive to enhance user experience.
Further, the width of the sliding part 51 is more than the width of the limiting slot 4.
Further, the equivalent width of the width of the limiting slot 4 and the open slot 3.
Further, the width of the limiting section 52 is smaller 0-0.5mm than the width of the open slot 3.
Further, the one end of the limiting section 52 far from sliding part 51 has towards the extension extended away from 2 direction of armlet
Portion 53.
Seen from the above description, extension is set, facilitates user to stir limited block, is conducive to further enhance user's body
It tests.
Further, side of the extension 53 far from main body 1 is equipped with several protrusions.
Seen from the above description, protrusion primarily serves anti-skidding effect, and the protrusion can be that raised line may be salient point.
Further, opposite on the limiting section 52 to set there are two fixture block 54, the fixture block 54 is located at the bottom plate 11 and leans on
The side of the nearly armlet 2, and the side of the fixture block 54 supports the bottom plate 11.
Seen from the above description, fixture block is set on limiting section, and the cooperation of fixture block and sliding part makes limited block that can only limit
It is slided in the slot of position, limited block cannot be detached with the bottom plate of main body, be conducive to the stability for improving aircraft remote controller structure.
Embodiment one
Fig. 2 to Fig. 5 is please referred to, the embodiments of the present invention one are：A kind of aircraft remote controler, including main body 1 and two
A armlet 2 being oppositely arranged on 1 bottom plate 11 of main body, an armlet 2 are arranged close to the left plate 12 of main body 1, another armlet 2
Right plate 13 close to main body 1 is arranged, and the armlet 2 is the shell of the hollow structure of a side opening, one end of the shell with
Main body 1 is rotatably connected, and the other end of shell has the open slot 3 being arranged along its length；The bottom plate 11 is equipped with limit
Position slot 4, limiting slot 4 is collinearly arranged with open slot 3 and limiting slot 4 is connected with open slot 3；Further include two limit assemblies, two
A limit assembly is arranged in a one-to-one correspondence with two armlets 2, and limit assembly includes limited block 5, elastic component 6 and fixed block 7；Fixed block
7 are set to side of the bottom plate 11 far from armlet 2, and limited block 5 includes the sliding part 51 being connected and limiting section 52, sliding part 51
In in the main body 1, limiting section 52 is matched through the limiting slot 4 with the open slot 3；One end of the elastic component 6 connects
The sliding part 51 is connect, the other end of elastic component 6 connects the fixed block 7.
Specifically, one end of armlet 2 is rotatably connected by shaft and the realization of main body 1.
The width of the sliding part 51 is more than the width of the limiting slot 4, the width of the limiting slot 4 and the open slot
3 equivalent width.
The width of the limiting section 52 is smaller 0-0.5mm than the width of the open slot 3.Preferably, the limiting section 52
Width is smaller 0.4mm than the width of the open slot 3.
Limited block 5 for user's convenience, the one end of the limiting section 52 far from sliding part 51 have towards away from 2 side of armlet
To the extension 53 of extension.
Preferably, side of the extension 53 far from main body 1 is equipped with several raised (not shown).
It is opposite on the limiting section 52 to set that there are two fixture blocks 54 to improve the stability of aircraft remote controller structure, it is described
Fixture block 54 is located at the bottom plate 11 close to the side of the armlet 2, and the side of the fixture block 54 supports the bottom plate 11.It is described
Fixture block 54 is detachably connected with the limited block 5, such as screw is connected, is threadedly coupled, is glued or is snapped connection.
In conclusion aircraft remote controler provided by the utility model, can easily lose key, coin etc. when user gos out
Object be put into the hollow structure of armlet, then rotating armlet makes open slot be aligned with limiting slot, then discharges limiting section, makes limit
Position portion is inserted into the open slot of shell, and the object easily lost at this time is limited in an enclosure space, to allow aircraft remote control appliance
Have and receive the function of object, the confined space of aircraft remote controler is adequately utilized, eliminates the wind that user loses fine pieces
Danger is conducive to enhance user experience；Extension is set, facilitates user to stir limited block, is conducive to further enhance user experience；
Fixture block is set on limiting section, and the cooperation of fixture block and sliding part makes limited block that can only be slided in limiting slot, and limited block cannot be with
The bottom plate of main body detaches, and is conducive to the stability for improving aircraft remote controller structure.
The above description is only the embodiments of the present invention, and it does not limit the scope of the patent of the present invention, every
Equivalents made based on the specification and figures of the utility model are applied directly or indirectly in relevant technology neck
Domain is equally included in the patent within the scope of the utility model.
Claims (7)
1. a kind of aircraft remote controler, including main body and two armlets being oppositely arranged on main body bottom plate, an armlet are close
The left plate of main body is arranged, another armlet is arranged close to the right plate of main body, it is characterised in that：The armlet is a side opening
Hollow structure shell, one end and the main body of the shell be rotatably connected, and the other end of shell has along its length
The open slot of setting；The bottom plate is equipped with limiting slot, and limiting slot is collinearly arranged with open slot and limiting slot is connected with open slot
It is logical；Further include two limit assemblies, two limit assemblies are arranged in a one-to-one correspondence with two armlets, limit assembly include limited block,
Elastic component and fixed block；Fixed block is set to side of the bottom plate far from armlet, and limited block includes connected sliding part and limit
Portion, in the main body, limiting section is matched through the limiting slot with the open slot sliding position；The one of the elastic component
End connects the sliding part, and the other end of elastic component connects the fixed block.
2. aircraft remote controler according to claim 1, it is characterised in that：The width of the sliding part is more than the limit
The width of slot.
3. aircraft remote controler according to claim 1, it is characterised in that：The width of the limiting slot and the open slot
Equivalent width.
4. aircraft remote controler according to claim 1, it is characterised in that：The width of the limiting section is than the open slot
The small 0-0.5mm of width.
5. aircraft remote controler according to claim 1, it is characterised in that：One end tool of the limiting section far from sliding part
Have towards the extension extended away from armlet direction.
6. aircraft remote controler according to claim 5, it is characterised in that：Side of the extension far from main body is equipped with
Several protrusions.
7. aircraft remote controler according to claim 1, it is characterised in that：Card there are two being set relatively on the limiting section
Block, the fixture block is located at the bottom plate close to the side of the armlet, and the side of the fixture block supports the bottom plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721807618.4U CN207676474U (en) | 2017-12-21 | 2017-12-21 | A kind of aircraft remote controler |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721807618.4U CN207676474U (en) | 2017-12-21 | 2017-12-21 | A kind of aircraft remote controler |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207676474U true CN207676474U (en) | 2018-07-31 |
Family
ID=62969795
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721807618.4U Active CN207676474U (en) | 2017-12-21 | 2017-12-21 | A kind of aircraft remote controler |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207676474U (en) |
-
2017
- 2017-12-21 CN CN201721807618.4U patent/CN207676474U/en active Active
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