CN204017385U - A kind of remote controller - Google Patents
A kind of remote controller Download PDFInfo
- Publication number
- CN204017385U CN204017385U CN201420389642.0U CN201420389642U CN204017385U CN 204017385 U CN204017385 U CN 204017385U CN 201420389642 U CN201420389642 U CN 201420389642U CN 204017385 U CN204017385 U CN 204017385U
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- CN
- China
- Prior art keywords
- remote controller
- circuit board
- battery
- cell piece
- rifle body
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- 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 discloses a kind of remote controller, comprise the housing that is small of the stock shape, described housing comprises the shank part that holds battery, the rifle body of containment circuit board, and as the trigger portion of throttle lever, described circuit board is connected by described powered battery and with described battery circuit, described trigger portion is arranged on described circuit board and under its action and controls the flying speed of described circuit board with remotely-piloted vehicle, here pass through shank part, the housing that is small of the stock shape that rifle body and trigger portion form makes remote controller have the shape of the profiling pistol small of the stock, in the time of remote control induction type aircraft, interest is stronger.
Description
Technical field
The utility model relates to a kind of field of remote control, particularly a kind of remote controller.
Background technology
Common induction type aircraft (for example infrared-sensing type aircraft), generally comprise the remote controller of aircraft and remotely-piloted vehicle thereof, the remote controller shape of the shape of common remote controller and remote control conventional toy (for example toy car) is similar, and the single shortage of shape is interesting.
Utility model content
Main purpose of the present utility model (technical problem of solution) is to provide a kind of stronger remote controller of interest with profiling shape.For example remote-controlled induction type aircraft of this remote controller (for example infrared-sensing type aircraft).
In order to achieve the above object, the utility model proposes a kind of remote controller, it is characterized in that, comprise the housing that is small of the stock shape, described housing comprises the rifle body of the shank part, the containment circuit board that hold battery and the trigger portion as throttle lever, described circuit board is connected by described powered battery and with described battery circuit, and described trigger portion is arranged on described circuit board and under its action and controls the flying speed of described circuit board with remotely-piloted vehicle.
Described shank part comprises the battery case that holds battery and the battery cover that seals described battery case, and described battery is for comprising dry cell or rechargeable battery.
Described battery case is located at the back side of described shank part, and after described battery packs described battery case into, its both positive and negative polarity is in contact with one another with the cell piece of being located on described battery case and/or circuit board respectively.
Described battery comprises three batteries, described battery case is provided with the first cell piece and the second cell piece in its one end, described circuit board is provided with three cell piece corresponding with the other end position of described battery case and the 4th cell piece, described the first cell piece and the 3rd cell piece contact with positive pole and the negative pole of two batteries after series connection respectively, and described the second cell piece and the 4th cell piece contact with positive pole and the negative pole of residue one batteries respectively.
Described circuit board is provided with the rotary knob of the flying speed gear that switches aircraft, and described trigger portion is arranged on described rotary knob.
Described rifle body is provided with in the time of the action of described rotary knob the first infrarede emitting diode of the flying speed control signal for launching described circuit board output in its side.
Between described trigger portion and described rifle body, be provided with spring, one end of described spring is fixed on described trigger portion, and the other end is fixed on described rifle body, after the action of described trigger portion under the pulling force of described spring return.
Described circuit board is provided with for connecting/cut off the remote controller switch being connected with the circuit of described battery and being used to indicate the switch indication light of the connection/cut-out of described remote controller switch, and described rifle body is provided with corresponding with described remote controller switch and switch indication light position and makes it expose the perforate of described rifle body at its end face.
Described rifle body is provided with the start button of controlling aircraft startup flare maneuver in its front, described start button is connected with described board circuit.
Described rifle body is provided with the second infrarede emitting diode that starts control signal in the time of described start button action for launching the flight of described circuit board output in its side.
Compared with prior art, the utlity model has following advantage: the housing that is small of the stock shape consisting of shank part, rifle body and trigger portion makes remote controller of the present utility model roughly be small of the stock shape (also having the shape of the profiling pistol small of the stock), for example, when for example induction type aircraft of remote control (infrared-sensing type aircraft), interest is stronger.
Brief description of the drawings
For clearer explanation the technical solution of the utility model, below the accompanying drawing of required use during embodiment is described is briefly described, apparent, accompanying drawing in the following describes is only embodiment more of the present utility model, for those of ordinary skill in the art, do not paying under the prerequisite of creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Fig. 1 is the decomposition texture schematic diagram of the remote controller of the utility model embodiment;
Fig. 2 is the front view after the remote controller of the utility model embodiment is assembled.
Fig. 3 is the rearview after the remote controller of the utility model embodiment is assembled.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment; technical scheme in the utility model embodiment is carried out to clear, complete description; obvious described embodiment is only a part of embodiment of the present utility model; not whole embodiment; based on the embodiment in the utility model; those of ordinary skill in the art are not paying the every other embodiment obtaining under creative work prerequisite, all belong to the scope of the utility model protection.
As Figure 1-3, the utility model embodiment provides a kind of remote controller, comprise the housing 1 that is small of the stock shape, described housing comprises the rifle body 5 of the shank part 3, the containment circuit board 4 that hold battery 2 and the trigger portion 6 as throttle lever, described circuit board is connected by described powered battery and with described battery circuit, and described trigger portion is arranged on described circuit board and under its action and controls the flying speed of described circuit board with remotely-piloted vehicle.
Here, the housing that is small of the stock shape consisting of shank part, rifle body and trigger portion makes remote controller of the present utility model roughly be small of the stock shape (also having the shape of the profiling pistol small of the stock), for example, when for example induction type aircraft of remote control (infrared-sensing type aircraft), interest is stronger.In addition, shank part is received battery (for circuit board power supply), rifle body containment circuit board is (by for example single-chip microcomputer and peripheral circuit thereof, send remote signal, the flying speed of for example remotely-piloted vehicle), trigger portion is used as throttle lever (by the action of trigger portion, control described circuit board so that circuit board sends corresponding control signal, with the flying speed of remote control change of flight device, for example, when there is skew in or heading too low in aircraft altitude, control its flying speed, provide larger lift to make aircraft increase, under normal circumstances in inapplicable remote controller remotely-piloted vehicle, aircraft relies on its induction flight performance, for example infrared induction flying height is controlled its rise/fall automatically, be stabilized in a certain flying height to maintain it, realize general induction type flight function).
Described shank part 3 comprises the battery case 30 that holds battery and the battery cover 31 that seals described battery case, and described battery is for comprising dry cell or rechargeable battery.
Here, user's grasped of the available remote controller of shank part, be difficult for slippage, very easy to use, in shank part, be closed with battery by battery case and battery cover, outward appearance is more attractive in appearance, if adopt rechargeable battery, can take off battery charging or corresponding charging inlet (corresponding charging circuit is set on circuit board) is directly set on shank part and realize charge function.
Described battery case is located at the back side A of described shank part, and after described battery packs described battery case into, its both positive and negative polarity is in contact with one another with the cell piece of being located on described battery case and/or circuit board respectively.
Here, battery case can adopt a groove or multiple groove, if adopt a groove, can will after a batteries or multiple batteries series connection, pack into wherein, now both positive and negative polarity can be in contact with one another with the cell piece of being located on described battery case and/or circuit board respectively, as long as the power supply of battery can be introduced to circuit board, the position of cell piece can arrange flexibly, for example can be arranged on the two ends (being connected with circuit board by wire again) of battery case, or can be arranged on the two ends (now cell piece contacts with the battery in battery case by the perforate on battery case) of circuit board, or can be arranged on respectively battery case and (now the cell piece on circuit board can directly can be connected with other circuit on circuit board) on circuit board.If adopt multiple grooves, for example two grooves, can for example will after a batteries or multiple batteries series connection, be respectively charged in two grooves respectively, then the both positive and negative polarity in each groove can for example be in contact with one another with the cell piece of being located on described battery case and/or circuit board respectively.
Described battery comprises three batteries, described battery case 30 is provided with the first cell piece 32 and the second cell piece 33 in its one end, described circuit board is provided with three cell piece 34 corresponding with the other end position of described battery case and the 4th cell piece 35, described the first cell piece and the 3rd cell piece contact with positive pole and the negative pole of two batteries after series connection respectively, and described the second cell piece and the 4th cell piece contact with positive pole and the negative pole of residue one batteries respectively.
Here, in battery case, pack in two separate ranks three batteries into, wherein two batteries after series connection pack in the row of one in battery case, both positive and negative polarity contacts with the 3rd cell piece on the first cell piece and the circuit board of battery case respectively, remain a batteries and pack in another row in battery case, both positive and negative polarity contacts with the 4th cell piece on the second cell piece and the circuit board of battery case respectively.
Described circuit board 4 is provided with the rotary knob 40 of the flying speed gear that switches aircraft, and described trigger portion is arranged on described rotary knob.
Here, the flying speed of remotely-piloted vehicle can be switched the flying speed gear of aircraft by the rotary knob on circuit board, and (there is corresponding flying speed gear in corresponding each flying speed for example, and the different gear remote signal that flying speed gear sends from circuit board is corresponding, convert and send different gear remote signals by switching push button), on switching push button, trigger portion can be installed, for example roughly semicircular in shape of switching push button, trigger portion is fastened on switching push button by its semicircular hole portion, thereby realize rotation and adjust the object to switch gear.
As shown in Figure 2, described rifle body 5 in the time that its side B is provided with in the action of described rotary knob for launching first infrarede emitting diode 50 of flying speed control signal of described circuit board output.
Here, the gear remote signal of corresponding different flying speed gears when the first infrarede emitting diode in rifle sides of body for example can be launched described rotary knob action, to realize the object of Remote flying speed.
Between described trigger portion 6 and described rifle body, be provided with spring 60, one end of described spring is fixed on described trigger portion, and the other end is fixed on described rifle body, after the action of described trigger portion under the pulling force of described spring return.
Here, described trigger portion is by spring return (homing) under the pulling force at spring fast after it is to the flying speed control of aircraft, thereby conveniently again flying speed regulated.
As shown in Figure 2, described circuit board 4 is provided with for connecting/cut off the remote controller switch 41 being connected with the circuit of described battery and being used to indicate the switch indication light 42 of the connection/cut-out of described remote controller switch, and described rifle body is provided with corresponding with described remote controller switch and switch indication light position and makes it expose the perforate of described rifle body at its end face C.
Here, remote controller switch is for remote controller is carried out to power switch control, thereby in the time not using a teleswitch, cut-out circuit board is connected with the circuit of battery, in the time using a teleswitch, connects and connects.Remote controller switch and switch indication light are exposed in perforate on the end face of described rifle body, with handled easily and observation.
As shown in Figure 2, described rifle body 5 is provided with the start button 51 of controlling aircraft startup flare maneuver at its positive D, and described start button is connected with described board circuit.
Here, aircraft for example infrared-sensing type aircraft after the power switch of opening on it, can for example, make aircraft start flare maneuver by the start button on remote controller (rifle body), thereby realize the distant control function of remote controller to aircraft startup flare maneuver.
As shown in Figure 2, described rifle body starts the second infrarede emitting diode 52 of control signal in the time that its side B is provided with in described start button action for launching the flight of described circuit board output.
Here, the remote signal of the startup flare maneuver that the second infrarede emitting diode in rifle sides of body is sent to aircraft by circuit board for example can launch described start button action time, to realize the object of Remote aircraft startup flare maneuver.s
Through the above description of the embodiments, those skilled in the art can be well understood to the utility model and can also realize by other structures, and feature of the present utility model is not limited to above-mentioned preferred embodiment.Any personnel that are familiar with this technology are in technical field of the present utility model, and the variation that can expect easily or modification, within all should being encompassed in scope of patent protection of the present utility model.
Claims (10)
1. a remote controller, it is characterized in that, comprise the housing that is small of the stock shape, described housing comprises the rifle body of the shank part, the containment circuit board that hold battery and the trigger portion as throttle lever, described circuit board is connected by described powered battery and with described battery circuit, and described trigger portion is arranged on described circuit board and under its action and controls the flying speed of described circuit board with remotely-piloted vehicle.
2. remote controller as claimed in claim 1, is characterized in that, described shank part comprises the battery case that holds battery and the battery cover that seals described battery case, and described battery is for comprising dry cell or rechargeable battery.
3. remote controller as claimed in claim 2, is characterized in that, described battery case is located at the back side of described shank part, and after described battery packs described battery case into, its both positive and negative polarity is in contact with one another with the cell piece of being located on described battery case and/or circuit board respectively.
4. remote controller as claimed in claim 3, it is characterized in that, described battery comprises three batteries, described battery case is provided with the first cell piece and the second cell piece in its one end, described circuit board is provided with three cell piece corresponding with the other end position of described battery case and the 4th cell piece, described the first cell piece and the 3rd cell piece contact with positive pole and the negative pole of two batteries after series connection respectively, and described the second cell piece and the 4th cell piece contact with positive pole and the negative pole of residue one batteries respectively.
5. the remote controller as described in claim 1-4 any one, is characterized in that, described circuit board is provided with the rotary knob of the flying speed gear that switches aircraft, and described trigger portion is arranged on described rotary knob.
6. remote controller as claimed in claim 5, is characterized in that, described rifle body is provided with in the time of the action of described rotary knob the first infrarede emitting diode of the flying speed control signal for launching described circuit board output in its side.
7. as claim 1-4, remote controller described in 6 any one, it is characterized in that, between described trigger portion and described rifle body, be provided with spring, one end of described spring is fixed on described trigger portion, the other end is fixed on described rifle body, after the action of described trigger portion under the pulling force of described spring return.
8. as claim 1-4, remote controller described in 6 any one, it is characterized in that, described circuit board is provided with for connecting/cut off the remote controller switch being connected with the circuit of described battery and being used to indicate the switch indication light of the connection/cut-out of described remote controller switch, and described rifle body is provided with corresponding with described remote controller switch and switch indication light position and makes it expose the perforate of described rifle body at its end face.
9. as claim 1-4, the remote controller described in 6 any one, is characterized in that, described rifle body is provided with the start button of controlling aircraft and start flare maneuver in its front, and described start button is connected with described board circuit.
10. remote controller as claimed in claim 9, is characterized in that, described rifle body is provided with the second infrarede emitting diode that starts control signal in the time of described start button action for launching the flight of described circuit board output in its side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420389642.0U CN204017385U (en) | 2014-07-15 | 2014-07-15 | A kind of remote controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420389642.0U CN204017385U (en) | 2014-07-15 | 2014-07-15 | A kind of remote controller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204017385U true CN204017385U (en) | 2014-12-17 |
Family
ID=52057300
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420389642.0U Expired - Fee Related CN204017385U (en) | 2014-07-15 | 2014-07-15 | A kind of remote controller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204017385U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109987239A (en) * | 2019-05-08 | 2019-07-09 | 成都航空职业技术学院 | A kind of multi-functional unmanned plane throttle lever |
| CN110362114A (en) * | 2019-07-26 | 2019-10-22 | 深圳市道通智能航空技术有限公司 | Starting method, unmanned vehicle and the remote control device of unmanned vehicle |
| WO2022134298A1 (en) * | 2020-12-24 | 2022-06-30 | SZ DJI Technology Co., Ltd. | Remote controllers and structures and systems thereof |
-
2014
- 2014-07-15 CN CN201420389642.0U patent/CN204017385U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109987239A (en) * | 2019-05-08 | 2019-07-09 | 成都航空职业技术学院 | A kind of multi-functional unmanned plane throttle lever |
| CN109987239B (en) * | 2019-05-08 | 2024-05-14 | 成都航空职业技术学院 | Multifunctional unmanned aerial vehicle throttle lever |
| CN110362114A (en) * | 2019-07-26 | 2019-10-22 | 深圳市道通智能航空技术有限公司 | Starting method, unmanned vehicle and the remote control device of unmanned vehicle |
| WO2022134298A1 (en) * | 2020-12-24 | 2022-06-30 | SZ DJI Technology Co., Ltd. | Remote controllers and structures and systems thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141217 Termination date: 20200715 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |