CN202654722U - Dual-mode model airplane remote controller with simple structure - Google Patents
Dual-mode model airplane remote controller with simple structure Download PDFInfo
- Publication number
- CN202654722U CN202654722U CN 201220291046 CN201220291046U CN202654722U CN 202654722 U CN202654722 U CN 202654722U CN 201220291046 CN201220291046 CN 201220291046 CN 201220291046 U CN201220291046 U CN 201220291046U CN 202654722 U CN202654722 U CN 202654722U
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- gauge tap
- mentioned
- remote controller
- compressing tablet
- control crank
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Abstract
The utility model provides a dual-mode model airplane remote controller with a simple structure. The dual-mode model airplane remote controller comprises a shell, two control handle assemblies and a control switch, and the lower parts of the control handle assemblies are connected with damping structures. The dual-mode model airplane remote controller is characterized in that the control switch is arranged in the right center of the shell; the damping structures are respectively arranged on one sides, which are close to the control switch, of the two control handle assemblies; a contactable elastic piece is arranged between each damping structure and the control switch; the elastic pieces are popped up or pressed downwards by shifting the control switch so as to change the damping effect of the two control handle assemblies and change control signals of the two control handle assemblies; design requirements of the remote controller can be met regardless of a left-hand mode or a right-hand mode; and moreover, the shell is not required to be turned reversely when the modes of the remote controller are switched, the modes are switched conveniently and quickly, and the structural design is simple. The dual-mode model airplane remote controller can be produced integrally, is low in production cost, and can be well received by model airplane enthusiasts, dual-mode integration is realized, and the utility model can be widely applied to model airplane remote controllers or other model remote controllers.
Description
Technical field
The utility model relates to a kind of remote controller, specifically a kind of dual mode type aeromodelling remote controller simple in structure.
Background technology
It is similar mostly that the remote controller mechanical mechanism of at present popular model airplane is laid with control crank.All be to comprise a housing, described housing each side is provided with and is positioned at control crank, and two handles can be done the manipulation of front, rear, left and right four direction.But owing to left and right directions reason habitually, remote controller is divided into two kinds of left hand operating pattern and right hand operating patterns at operating pattern, thereby the airplane hobbyist who satisfies without operating habit uses, the manufacturer just needs to produce the remote controller of different mode like this, and this is disadvantageous for large-scale production and reduction cost.Therefore, a kind of remote controller that has two kinds of operating patterns concurrently is just given birth at once, as utilize a P cock to select the conversion of remote controller operating pattern, but this mode conversion function only is to exchange on the electric position, the frame for movement of control crank then can't change, therefore it is very difficult that manipulation is got up, and easily causes aircraft accident, its different design closes specification requirement; Be that the utility model patent file of ZL200820155365.1 discloses a kind of model aeroplane remote controller such as Patent Office of the People's Republic of China in the patent No. of on December 16th, 2009 bulletin, be characterized in when remote controller arranges the switch of a conversion operating pattern, add again a signal gathering unit, when the needs translative mode, the remote controller housing is rotated 180 °, and the conversion by mode selection switch and control signal, realize the exchange of left and right sides operating pattern, owing to being to rotate 180 °, forwarded the control crank of original on the left side to the right, so the frame for movement of control crank need not to change the specification requirement that also can meet remote controller.But this remote controller comparatively bothers when pattern is changed, housing need to be turned 180 °, and at design aspect also relative complex, need remote controller is designed to laterally zygomorphic shape, also need to arrange a signal gathering unit, complex structure has increased the manufacturing cost of this remote controller greatly, and guarantees that the sensation that hand-held hand is taken is not very comfortable relatively.
Summary of the invention
For the existing problem of above-mentioned prior art, the purpose of this utility model provides a kind of dual mode type aeromodelling remote controller simple in structure ingenious, that the pattern conversion is simple, easy to operate that designs.
For achieving the above object, the technical scheme that the utility model adopts is: a kind of dual mode type aeromodelling remote controller simple in structure, comprise a housing, be arranged on the housing about two control crank groups and gauge tap, the bottom of described control crank group is connected with damping structure, be characterized in that described gauge tap is arranged at the middle of housing, described damping structure is arranged at respectively two control crank groups near a side of gauge tap, be provided with the elastic component that can contact between described damping structure and the gauge tap, described elastic component cooperated and makes the control crank group at this damping structure place have damping with the damping structure of a side wherein when described gauge tap was allocated to arbitrary end, made elastic component upspring or press down to realize the control signal that changes the damping of two control crank groups and change two control crank groups by stirring gauge tap.
Wherein, above-mentioned gauge tap is switch of T-shape, the vertical portion of described gauge tap reaches on the above-mentioned housing and forms the clicking section, the transverse part two ends of described gauge tap are associated with above-mentioned elastic component respectively, elastic component on the left of its transverse part promoted when described gauge tap was stirred forward breaks away from the damping structure of Left-Hand Drive handle group bottom and cooperates, and the elastic component on its transverse part promotion right side cooperated with the damping structure disengaging of the control crank group bottom on right side when described gauge tap was stirred backward.
In order to realize that gauge tap can change the damping of two control crank groups, above-mentioned gauge tap is provided with push rod in the long end of above-mentioned compressing tablet and the junction of short end, the compressing tablet that push rod promotes the left side when described gauge tap is stirred forward is bent downwardly compressing tablet and realizes that the short end section of compressing tablet leaves damping structure, and the compressing tablet that push rod promotes the right side when described gauge tap is stirred backward is bent downwardly compressing tablet and realizes that the short end section of compressing tablet leaves damping structure.
In order to realize the damping action of two control crank groups, above-mentioned damping structure is the semicircle tabular body that an arcwall face is provided with the pointed tooth tooth, the one-body molded design in the side of described damping structure and above-mentioned startup seat and described pointed tooth tooth are down, and the short end of above-mentioned compressing tablet is provided with fin facing up, and described fin matches with the pointed tooth tooth of above-mentioned damping structure and has damping when realizing above-mentioned control crank swing.
In order to realize that gauge tap also changes the control signal of two control crank groups when changing the damping of two control crank groups, the bottom of above-mentioned gauge tap is provided with connected travel switch, the position of stirring of described travel switch is connected with the transverse part of gauge tap, the housing of described travel switch is fixed on the above-mentioned housing, makes travel switch change the control signal that signal realizes changing above-mentioned Left-Hand Drive handle group and control crank group by stirring gauge tap.
The utility model is owing to adopting a structure that can change control signal and realize the gauge tap that damping is switched, this gauge tap is arranged at the middle of housing, damping structure is arranged at respectively two control crank groups near a side of gauge tap, described elastic component cooperates and makes the control crank group at this damping structure place have damping with the damping structure of a side wherein when gauge tap is allocated to arbitrary end, make elastic component upspring or press down to realize the control signal that changes the damping of two control crank groups and change two control crank groups by stirring gauge tap, therefore no matter be the designing requirement that left-handed mode or right-handed mode can both meet remote controller, and this remote controller need not housing is turned 180 ° when pattern is changed, change convenient and swift, structural design is simple, utilize a gauge tap can realize the remote controller design of two kinds of patterns and the unification of producing, effectively reduce production cost, better met the requirement of using the model plane person of different mode remote controller; Again because the control crank group includes operating grip, half-cylindrical seat and the pedestal of starting, wherein starting seat can rotate with the control crank swing, and damping structure is arranged at a side lower end that starts seat, therefore can realize that a control crank makes up with damping structure and produce as a unit, can realize output, be installed on the housing by demand after producing and the setup control signal gets final product, not only being convenient to design produces, and can change separately, improved the service life of whole remote controller.In sum, dual mode type aeromodelling remote controller simple in structure of the present utility model, its design is ingenious, simple to operation, real realization is double mode integrated, can obtain liking of more model plane persons, also make things convenient for production and selling, can be widely used on model aeroplane remote controller or other model remote controllers.
The utility model is described in further detail below in conjunction with drawings and Examples.
Description of drawings
Fig. 1 is perspective view of the present utility model.
Fig. 2 is decomposition texture schematic diagram of the present utility model.
Fig. 3 is the decomposition texture schematic diagram between the utility model gauge tap and the control crank group.
The specific embodiment
As shown in Figure 1 to Figure 3, a kind of dual mode type aeromodelling remote controller simple in structure, comprise a housing 1, be arranged on the housing 1 about two control crank groups 2 and gauge tap 3, the bottom of this control crank group 2 is connected with damping structure 4, wherein this gauge tap 3 is arranged at the middle of housing 1, damping structure 4 is arranged at respectively two control crank groups 2 near a side of gauge tap 3, be provided with the elastic component that can contact between damping structure 4 and the gauge tap 3, elastic component cooperated and makes the control crank group 2 at these damping structure 4 places have damping with the damping structure 4 of a side wherein when gauge tap 3 was allocated to arbitrary end, make elastic component upspring or press down to realize the control signal that changes the damping of two control crank groups 2 and change two control crank groups 2 by stirring gauge tap 3, therefore no matter be the designing requirement that left-handed mode or right-handed mode can both meet remote controller, and this remote controller need not housing is turned 180 ° when pattern is changed, change convenient and swift, structural design is simple, utilize a gauge tap 3 can realize the remote controller design of two kinds of patterns and the unification of producing, effectively reduce production cost, better met the requirement of using the model plane person of different mode remote controller.
As shown in Figure 2, the gauge tap 3 of this embodiment is switch of T-shape, the vertical portion 31 of this gauge tap 3 reaches on the housing 1 and forms the clicking section, its transverse part 32 two ends are associated with elastic component respectively, the elastic component of this embodiment is a compressing tablet 5 that is " L " type, the long end end of this compressing tablet 5 is fixed on the bottom of control crank group 2 by screw 24, compressing tablet 5 presses in the below of damping structure 4 from the oblique downward-extension of stiff end and short end section, wherein the compressing tablet 5 in left side is that stiff end is front and backward downward-sloping, the compressing tablet 5 on right side is that stiff end is rear and downward-sloping forward, compressing tablet 5 on the left of its transverse part promotes when this gauge tap 3 is stirred forward breaks away from the damping structure of Left-Hand Drive handle group 2 bottoms 4 and cooperates, the compressing tablet 5 on its transverse part promotion right side cooperated with damping structure 4 disengagings of control crank group 2 bottoms on right side when described gauge tap 3 was stirred backward, its gauge tap 3 that is embodied as this embodiment is provided with push rod 61 in the long end of compressing tablet 5 and the junction of short end, the compressing tablet 5 that push rod 61 promotes the left side when gauge tap 3 is stirred forward is bent downwardly compressing tablet 5 and realizes that the short end section of compressing tablet 5 leaves damping structure 4, the compressing tablet 5 that push rod 61 promotes right sides when gauge tap 3 is stirred backward is bent downwardly compressing tablet 5 and realizes that the short end section of compressing tablet 5 leaves damping structure 4, the end of the transverse part 31 of the gauge tap 3 of this embodiment is connected with riser 6, and this riser 6 is arranged on the side of riser 6 lower sides to downward-extension and push rod 61.In addition, inboard and the below of the control crank group 2 of this embodiment are equipped with inching switch 8, this inching switch 8 is used for regulating the control signal of control crank group 2, the inching switch 8 that wherein is positioned at the below is used for regulating the control signal that control crank group 2 is laterally stirred, and is positioned at inboard inching switch 8 and is used for regulating the control signal that control crank group 2 is vertically stirred.Housing 1 upper end of this embodiment is provided with the convenient portable handle that carries, and also is provided with in addition mast 9 accessories such as grade.
As shown in Figure 3, the half round post that the control crank group 2 of this embodiment includes operating grip 21, be arranged at operating grip 21 bottoms starts seat 22 and is used for the fixing pedestal 23 that starts seat 22, this startup seat 22 can rotate with control crank 21 swings, and damping structure 4 is arranged at a side lower end that starts seat 22.The damping structure 4 of this embodiment is the semicircle tabular body that an arcwall face is provided with pointed tooth tooth 41, the one-body molded design in side of damping structure 4 and startup seat 22 and pointed tooth tooth 41 are down, and the short end of compressing tablet 5 is provided with fin 51 facing up, when fin 51 matched with the pointed tooth tooth 41 of damping structure 4, this control crank 21 had damping when swing.In addition, in order to realize that gauge tap 3 also changes the control signal of two control crank groups 2 when changing the damping of two control crank groups 2, the bottom of this gauge tap 3 is provided with connected travel switch 7, the position of stirring of the trip switch 7 is connected with the transverse part 31 of gauge tap 3, the shell block of travel switch 7 is fixed on the housing 1, make travel switch 7 change the control signal that signal realizes changing Left-Hand Drive handle group 2 and control crank group 2 by stirring gauge tap 3, the convex snapping plate 33 that is provided with in the centre position of the transverse part 31 of the gauge tap 3 of this embodiment, the stirring that the position is buckled on the snapping plate 33 of the trip switch 7 and when realizing that gauge tap 3 front and back are stirred travel switch 7 stir synchronously.
Although the utility model is to describe with reference to specific embodiment, this description and not meaning that is construed as limiting the utility model.With reference to description of the present utility model, other of the disclosed embodiments change, and all can expect for those skilled in the art, and this variation should belong in the affiliated claim limited range.
Claims (10)
1. dual mode type aeromodelling remote controller simple in structure, comprise a housing (1), be arranged on the housing (1) about two control crank groups (2) and gauge tap (3), the bottom of described control crank group (2) is connected with damping structure (4), it is characterized in that described gauge tap (3) is arranged at the middle of housing (1), described damping structure (4) is arranged at respectively two control crank groups (2) near a side of gauge tap (3), be provided with the elastic component that can contact between described damping structure (4) and the gauge tap (3), described gauge tap (3) when being allocated to arbitrary end described elastic component cooperate and make the control crank group (2) at this damping structure (4) place have damping with the damping structure of a side (4) wherein, make elastic component upspring or press down to realize the control signal that changes the damping of two control crank groups (2) and change two control crank groups (2) by stirring gauge tap (3).
2. dual mode type aeromodelling remote controller simple in structure according to claim 1, it is characterized in that above-mentioned gauge tap (3) is switch of T-shape, the vertical portion (31) of described gauge tap (3) reaches the upper clicking section that forms of above-mentioned housing (1), transverse part (32) two ends of described gauge tap (3) are associated with above-mentioned elastic component respectively, the elastic component in described gauge tap (3) its transverse part (32) promotion left side when stirring forward breaks away from the damping structure (4) of Left-Hand Drive handle group (2) bottom and cooperates, and the elastic component on described gauge tap (3) its transverse part (32) promotion right side when stirring backward breaks away from the damping structure (4) of control crank group (2) bottom on right side and cooperates.
3. dual mode type aeromodelling remote controller simple in structure according to claim 2, it is characterized in that above-mentioned elastic component is a compressing tablet (5) that is " L " type, the long end end of described compressing tablet (5) is fixed on the bottom of above-mentioned control crank group (2) by screw (24), described compressing tablet (5) presses in the below of above-mentioned damping structure (4) from the oblique downward-extension of stiff end and short end section, wherein the left side compressing tablet (5) be stiff end front and backward downward-sloping, the compressing tablet on right side (5) is that stiff end is rear and downward-sloping forward.
4. dual mode type aeromodelling remote controller simple in structure according to claim 3, it is characterized in that above-mentioned gauge tap (3) is provided with push rod (61) in the long end of above-mentioned compressing tablet (5) and the junction of short end, when described gauge tap (3) compressing tablet (5) that push rod (61) promotes the left side when stirring forward is bent downwardly compressing tablet (5) and realizes that the short end section of compressing tablet (5) leaves damping structure (4), when described gauge tap (3) compressing tablet (5) that push rod (61) promotes the right side when stirring backward is bent downwardly compressing tablet (5) and realizes that the short end section of compressing tablet (5) leaves damping structure (4).
5. dual mode type aeromodelling remote controller simple in structure according to claim 4, the end that it is characterized in that the transverse part of above-mentioned gauge tap (3) is connected with riser (6), and described riser (6) is arranged on the side of riser (6) lower side to downward-extension and above-mentioned push rod (61).
6. dual mode type aeromodelling remote controller simple in structure according to claim 3, it is characterized in that above-mentioned control crank group (2) includes operating grip (21), is arranged at the half round post startup seat (22) of operating grip (21) bottom and is used for a fixing pedestal (23) that starts (22), described startup seat (22) can rotate with control crank (21) swing, and above-mentioned damping structure (4) is arranged at a described side lower end that starts seat (22).
7. dual mode type aeromodelling remote controller simple in structure according to claim 6, it is characterized in that above-mentioned damping structure (4) is the semicircle tabular body that an arcwall face is provided with pointed tooth tooth (41), the one-body molded design in side of described damping structure (4) and above-mentioned startup seat (22) and described pointed tooth tooth (41) are down.
8. dual mode type aeromodelling remote controller simple in structure according to claim 7, the short end that it is characterized in that above-mentioned compressing tablet (5) is provided with fin (51) facing up, and described fin (51) matches with the pointed tooth tooth (41) of above-mentioned damping structure (4) and has damping when realizing above-mentioned control crank (21) swing.
9. dual mode type aeromodelling remote controller simple in structure according to claim 2, the bottom that it is characterized in that above-mentioned gauge tap (3) is provided with connected travel switch (7), the position of stirring of described travel switch (7) is connected with the transverse part of gauge tap (3), the shell block of described travel switch (7) is fixed on the above-mentioned housing (1), makes travel switch (7) change the control signal that signal realizes changing above-mentioned Left-Hand Drive handle group (2) and right side control crank group (2) by stirring gauge tap (3).
10. dual mode type aeromodelling remote controller simple in structure according to claim 9, the convex snapping plate (33) that is provided with in centre position that it is characterized in that the transverse part (31) of above-mentioned gauge tap (3), above-mentioned travel switch (8) stir the position be buckled on described snapping plate (33) upper and when realizing stirring before and after the gauge tap (3) described travel switch (7) stir synchronously.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220291046 CN202654722U (en) | 2012-06-20 | 2012-06-20 | Dual-mode model airplane remote controller with simple structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220291046 CN202654722U (en) | 2012-06-20 | 2012-06-20 | Dual-mode model airplane remote controller with simple structure |
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| Publication Number | Publication Date |
|---|---|
| CN202654722U true CN202654722U (en) | 2013-01-09 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220291046 Expired - Lifetime CN202654722U (en) | 2012-06-20 | 2012-06-20 | Dual-mode model airplane remote controller with simple structure |
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| CN (1) | CN202654722U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018107954A1 (en) * | 2016-12-16 | 2018-06-21 | 深圳市道通智能航空技术有限公司 | Rocker mechanism and remote controller |
| CN110097745A (en) * | 2018-01-31 | 2019-08-06 | 广东美嘉欣创新科技股份有限公司 | A kind of changeable gear remote controler |
| CN110989629A (en) * | 2019-12-28 | 2020-04-10 | 天津大学 | Special integrated controller for ship model |
| CN114815957A (en) * | 2022-03-23 | 2022-07-29 | 北京轩宇智能科技有限公司 | Remote control device for electromechanical apparatus |
-
2012
- 2012-06-20 CN CN 201220291046 patent/CN202654722U/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018107954A1 (en) * | 2016-12-16 | 2018-06-21 | 深圳市道通智能航空技术有限公司 | Rocker mechanism and remote controller |
| CN110097745A (en) * | 2018-01-31 | 2019-08-06 | 广东美嘉欣创新科技股份有限公司 | A kind of changeable gear remote controler |
| CN110097745B (en) * | 2018-01-31 | 2023-11-14 | 广东美嘉欣创新科技股份有限公司 | Gear-switchable remote controller |
| CN110989629A (en) * | 2019-12-28 | 2020-04-10 | 天津大学 | Special integrated controller for ship model |
| CN114815957A (en) * | 2022-03-23 | 2022-07-29 | 北京轩宇智能科技有限公司 | Remote control device for electromechanical apparatus |
| CN114815957B (en) * | 2022-03-23 | 2023-03-03 | 北京轩宇智能科技有限公司 | Remote control device for electromechanical apparatus |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: Chenghai District of Guangdong province 515800 Shantou Laimei industrial zone of Laiwu Economic Development Zone Industrial Road Patentee after: GUANGDONG MEIJIAXIN INNOVATIVE TECHNOLOGY CO.,LTD. Address before: Chenghai District of Guangdong province 515800 Shantou Laimei industrial zone of Laiwu Economic Development Zone Industrial Road Patentee before: MEIJIAXIN TOYS CO.,LTD. |
|
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130109 |