CN202620714U - Dual-purpose handle mechanism for throttle control and attitude control in model plane remote controller - Google Patents
Dual-purpose handle mechanism for throttle control and attitude control in model plane remote controller Download PDFInfo
- Publication number
- CN202620714U CN202620714U CN 201120523211 CN201120523211U CN202620714U CN 202620714 U CN202620714 U CN 202620714U CN 201120523211 CN201120523211 CN 201120523211 CN 201120523211 U CN201120523211 U CN 201120523211U CN 202620714 U CN202620714 U CN 202620714U
- Authority
- CN
- China
- Prior art keywords
- handle
- rod
- reel cage
- king
- support
- 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.)
- Expired - Fee Related
Links
Images
Abstract
A dual-purpose handle mechanism for throttle control and attitude control in a model plane remote controller comprises a support, a first swing frame and a centering rod. The two ends of the first swing frame are connected with the support through shafts. One end face of the first swing frame is provided with two centering pins in an outward way. The centering rod abuts on the upper sides of the two centering pins. One end of the centering rod is connected with the support through a pin shaft. A spring is arranged between the other end of the centering rod and the support. A switch handle is arranged on the support. The switch handle has a first docking position and a second docking position on the support. When the switch handle lies on the second docking position, the switch handle supports the centering rod and makes the centering rod detached from the centering pins. The dual-purpose handle mechanism provided in the utility model can get rid of the automatic centering function of the swing frame moving towards an Y direction as required and then make the swing frame moving towards the Y direction serve as a throttle signal control mechanism of a fixed-wing model plane or a propeller pitch signal control mechanism of a rotary-wing model plane. Furthermore, the dual-purpose handle mechanism facilitates left-and-right switches between a flight attitude control function and a throttle or propeller pitch control function of the remote controller for a person accustomed to using the left hand.
Description
Technical field:
The utility model relates to mechanical field, relates in particular to fly able model airplane, the particularly remote controller of model airplane, and concrete is a kind of dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control.
Background technology:
In the prior art, model plane are all realized control through remote controller.Model airplane for fixed-wing; Include flight attitude controlling organization and throttle signal controlling organization in the remote controller, the flight attitude controlling organization is made up of a rocking bar that can on directions X and Y direction, move, and rocking bar connects reel cage and the reel cage on directions X on the Y direction; Reel cage on the Y direction is through signal of telecommunication device output elevator control signal; Reel cage on the directions X is through signal of telecommunication device output aileron control signal, and the throttle signal controlling organization is made up of the signal of telecommunication device of another rocking bar that can on the Y direction, move and connection thereof, in order to simulate the true control action of fixed wing aircraft; Reel cage on the Y direction is provided with go back to middle mechanism; When the external force on being carried in reel cage disappeared, the centre position can be got back to by elevator signal controlling mechanism, and the throttle signal controlling organization is not established go back to middle mechanism; When the external force on being carried in the throttle reel cage disappeared, the throttle signal controlling organization stopped at current location.Model airplane for the rotation wing; Include flight attitude controlling organization and pitch signal controlling mechanism in its remote controller; The flight attitude controlling organization is made up of a rocking bar that can on directions X and Y direction, move, and produces the incline direction signal of rotor, and pitch signal controlling mechanism is made up of the signal of telecommunication device of reel cage on another Y direction and connection thereof; The up-down signal of control model airplane, pitch signal controlling mechanism does not establish go back to middle mechanism.The throttle signal controlling organization is used as pitch signal controlling mechanism; Same remote controller just can be used for handling the model airplane of the rotation wing; Usually; Throttle signal controlling organization or pitch signal controlling mechanism are arranged on the left half side of remote controller housing, and the flight attitude controlling organization is arranged on the right half side of housing.But for the personage of custom with the left-handed operation flight attitude, this set mode uses inconvenience.Although can the circuit signal that the reel cage on the Y direction connects be exchanged the redetermination of laying equal stress on the circuit signal that the throttle signal controlling organization is connected; Make the flight attitude controlling organization be set to the left half side of housing; The needs that are fit to the lefthanded personage; But the reel cage on the right half side former Y direction of housing then can not be used as throttle signal control or pitch signal controlling because middle mechanism is arranged back.
Summary of the invention:
The purpose of the utility model is to provide a kind of dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control, and the rocking bar that the described this dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control will solve model plane remote controller in the prior art is not suitable for the technical problem that the lefthanded personage handles.
This dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control of the utility model comprises support, first reel cage and time king-rod, and the two ends of described first reel cage are provided with one first separately, and described two first is positioned on the same axis; The two ends of first reel cage are connected with described support through first; To being outside equipped with pin in two times, described two are gone back to the both sides that middle pin is distributed in first in the one end end face of first reel cage, and described time king-rod rests in the upsides of pin in two times; The length direction that returns king-rod is perpendicular to first; An end that returns king-rod is connected with support through bearing pin, is provided with a spring between the other end of time king-rod and the support, wherein; Described support is provided with one and switches handle; Described switching handle has one first stop position and one second stop position in support, switch handle when described first stop position, switch that handle separates with described time king-rod or with return king-rod and keep zero active force; Switch handle when described second stop position, switch handle and supports back king-rod and return king-rod and return the middle disengaging of selling with described two.
Further, include one in the described support and switch handle set, be provided with a through hole in the described switching handle set; Described switching handle passes described through hole; Be provided with sliding pair between switching handle and the through hole, the front end that switches handle is adjacent with described time king-rod, and the rear portion outer wall that switches handle is outside equipped with radially boss; Described radially boss is connected with elastic cantilever, and an end of described elastic cantilever is connected and switches on the handle.
Further; Be provided with one second reel cage in described first reel cage; The two ends of described second reel cage are provided with one second separately; Described two second is positioned on the same axis and vertical with first, and the two ends of second reel cage are connected with first reel cage through second, are connected with a rocking bar on second reel cage.
Further; Be provided with a rectangular slot in the end face of described first reel cage; The length direction of described rectangular slot is parallel to first; Described rocking bar is to the upside extension and pass rectangular slot, and the length of rectangular slot is greater than the diameter of rocking bar, and the width of rectangular slot equals or be slightly larger than the diameter of rocking bar.
Further, the external diameter of described radially boss is greater than the internal diameter of described through hole.
The operation principle of the utility model is: first reel cage is done the action on the Y direction.First reel cage is used for operating the elevator of fixed-wing model airplane, when perhaps operating the pitching of rotor in the rotation wing model airplane, is placed on first stop position in the support with switching handle, and the switching handle separates perhaps with described time king-rod and keeps zero active force with time king-rod; When first reel cage rotates under external force; Pin promotes back king-rod and rotates around bearing pin in outer the returning of connecting of first reel cage, one end end face, returns spring that king-rod one end connects and produces and be out of shape, when acting on the external force disappearance on first reel cage; Spring recovers; Drive back king-rod and reset, return king-rod and promote back middle pin, first reel cage is turned to original position.With first reel cage be used for operating the throttle of fixed-wing model airplane, or when rotating the pitch in the wing model airplane; Be placed on second stop position in the support with switching handle; Switch handle and overcome spring returning the active force of king-rod; To return that king-rod pin from two are returned lifts and return with two in pin keep gaps, when first reel cage rotates under external force, sell in outer the returning of connecting of first reel cage, one end end face and break away from back king-rod all the time; When acting on the external force disappearance on first reel cage, first reel cage rests on current location.The radially boss that switches on the handle can be retreated by restriction switching handle after passing the through hole that switches handle set, remains on second stop position thereby will switch handle, defeats in addition to make radially can return to first stop position with switching handle behind the boss.
The utility model and prior art are compared, and its effect is actively with tangible.The utility model is provided with clutch in the flight attitude controlling organization of model plane remote controller; Can cut off acting on the spring reset power of Y on the action reel cage; Thereby remove Y function in automatic the returning of action reel cage; Y is used as the throttle signal controlling organization of fixed-wing model plane or the pitch signal controlling mechanism of rotating wing model plane to the action reel cage, makes things convenient for lefthanded personage exchange about realization flight attitude control function and throttle or pitch control function on the remote controller.
Description of drawings:
Fig. 1 be return in the dual-purpose handle mechanism that is used for the control of model plane remote controller throttle and attitude of the utility model king-rod rest in two return in sketch mapes on the pin.
Fig. 2 be return in the dual-purpose handle mechanism that is used for the control of model plane remote controller throttle and attitude of the utility model king-rod break away from two return in the sketch mapes of pin.
Fig. 3 is the plan structure sketch map of the dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control of the utility model.
Fig. 4 is the side direction structural representation of the dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control of the utility model.
The specific embodiment:
Embodiment 1:
Like Fig. 1, Fig. 2, Fig. 3 and shown in Figure 4, the dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control of the utility model comprises support 1, first reel cage 2 and returns king-rod 3; The two ends of described first reel cage 2 are provided with one first separately; Described two first is positioned on the same axis, and the two ends of first reel cage 2 are connected with described support 1 through first, sells 5 to being outside equipped with in two times in the end end face of first reel cage 2; Described two are gone back to the both sides that middle pin 5 is distributed in first; Described time king-rod 3 rests in two upsides that return middle pin 5, and the length direction that returns king-rod 3 is perpendicular to first, and an end that returns king-rod 3 is connected with support 1 through bearing pin; Return between the other end and the support 1 of king-rod 3 and be provided with a spring 4; Wherein, described support 1 is provided with one and switches handle 6, and described switching handle 6 has one first stop position and one second stop position in support 1; Switch handle 6 when described first stop position; Switch that handle 6 separates with described time king-rod 3 or with return king-rod 3 and keep zero active force, switch handle 6 when described second stop position, switch handle 6 and support back king-rod 3 and return king-rod 3 and sell 5 disengagings in returning with described two.
Further, include one in the described support 1 and switch handle set, be provided with a through hole in the described switching handle set; Described switching handle 6 passes described through hole; Be provided with sliding pair between switching handle 6 and the through hole, the front end that switches handle 6 is adjacent with described time king-rod 3, and the rear portion outer wall that switches handle 6 is outside equipped with radially boss 8; Described radially boss 8 is connected with elastic cantilever 9, and an end of described elastic cantilever 9 is connected and switches on the handle 6.
Further; Be provided with one second reel cage 10 in described first reel cage 2; The two ends of described second reel cage 10 are provided with one second separately; Described two second is positioned on the same axis and vertical with first, and the two ends of second reel cage 10 are connected with first reel cage 2 through second, are connected with a rocking bar 11 on second reel cage 10.
Further; Be provided with a rectangular slot in the end face of described first reel cage 2; The length direction of described rectangular slot is parallel to first; Described rocking bar 11 is to the upside extension and pass rectangular slot, and the length of rectangular slot is greater than the diameter of rocking bar 11, and the width of rectangular slot equals or be slightly larger than the diameter of rocking bar 11.
Further, the external diameter of described radially boss 8 is greater than the internal diameter of described through hole.
Further, support 1 all is set directly in the housing of model plane remote controller with the switching handle set.
The course of work of present embodiment is: first reel cage 2 is done the action on the Y direction.First reel cage 2 is used for operating the elevator of fixed-wing model airplane, when perhaps operating the pitching of rotor in the rotation wing model airplane, is placed on first stop position in the support 1 with switching handle 6, and switching handle 6 separates perhaps with described time king-rod 3 and keeps zero active force with time king-rod 3; When first reel cage 2 rotates under external force; The middle pin 5 that returns that first reel cage, 2 one end end faces connect outward promotes back king-rod 3 around the bearing pin rotation, returns the spring 4 generation distortion that king-rod 3 one ends connect, when acting on the external force disappearance on first reel cage 2; Spring 4 recovers; Drive back king-rod 3 and reset, return king-rod 3 and promote pin 5 in time, first reel cage 2 is turned to original position.With first reel cage 2 be used for operating the throttle of fixed-wing model airplane, or when rotating the pitch in the wing model airplane; Be placed on second stop position in the support 1 with switching handle 6; Switch handle 6 and overcome 4 pairs of active forces that return king-rod 3 of spring; To return that king-rod 3 pin 5 from two are returned lifts and return with two in pin 5 maintenance gaps, when first reel cage 2 rotates under external force, sell 5 in outer the returning of connecting of first reel cage, 2 one end end faces and break away from back king-rod 3 all the time; When acting on the external force disappearance on first reel cage 2, first reel cage 2 rests on current location.The radially boss 8 that switches on the handle 6 can be retreated by restriction switching handle 6 after passing the through hole that switches handle set; Remain on second stop position thereby will switch handle 6, defeat in addition and can return to first stop position with switching handle 6 after making radially boss 8.
Claims (5)
1. a dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control comprises support, first reel cage and returns king-rod, and the two ends of described first reel cage are provided with one first separately; Described two first is positioned on the same axis; The two ends of first reel cage are connected with described support through first, and to being outside equipped with pin in two times, described two are gone back to the both sides that middle pin is distributed in first in the end end face of first reel cage; Described time king-rod rests in two upsides of selling in returning; The length direction that returns king-rod is perpendicular to first, and an end that returns king-rod is connected with support through bearing pin, is provided with a spring between the other end of time king-rod and the support; It is characterized in that: described support is provided with one and switches handle; Described switching handle has one first stop position and one second stop position in support, switch handle when described first stop position, switch that handle separates with described time king-rod or with return king-rod and keep zero active force; Switch handle when described second stop position, switch handle and supports back king-rod and return king-rod and return the middle disengaging of selling with described two.
2. the dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control as claimed in claim 1; It is characterized in that: include one in the described support and switch handle set; Be provided with a through hole in the described switching handle set, described switching handle passes described through hole, switches between handle and the through hole to be provided with sliding pair; The front end that switches handle is adjacent with described time king-rod; The rear portion outer wall that switches handle is outside equipped with radially boss, and described radially boss is connected with elastic cantilever, and an end of described elastic cantilever is connected and switches on the handle.
3. the dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control as claimed in claim 1; It is characterized in that: be provided with one second reel cage in described first reel cage; The two ends of described second reel cage are provided with one second separately; Described two second is positioned on the same axis and vertical with first, and the two ends of second reel cage are connected with first reel cage through second, are connected with a rocking bar on second reel cage.
4. the dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control as claimed in claim 3; It is characterized in that: be provided with a rectangular slot in the end face of described first reel cage; The length direction of described rectangular slot is parallel to first; Described rocking bar is to the upside extension and pass rectangular slot, and the length of rectangular slot is greater than the diameter of rocking bar, and the width of rectangular slot equals or be slightly larger than the diameter of rocking bar.
5. the dual-purpose handle mechanism that is used for model plane remote controller throttle and attitude control as claimed in claim 2, it is characterized in that: the external diameter of described radially boss is greater than the internal diameter of described through hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120523211 CN202620714U (en) | 2011-12-14 | 2011-12-14 | Dual-purpose handle mechanism for throttle control and attitude control in model plane remote controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120523211 CN202620714U (en) | 2011-12-14 | 2011-12-14 | Dual-purpose handle mechanism for throttle control and attitude control in model plane remote controller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202620714U true CN202620714U (en) | 2012-12-26 |
Family
ID=47373962
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201120523211 Expired - Fee Related CN202620714U (en) | 2011-12-14 | 2011-12-14 | Dual-purpose handle mechanism for throttle control and attitude control in model plane remote controller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202620714U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014205885A1 (en) * | 2013-06-25 | 2014-12-31 | 深圳市大疆创新科技有限公司 | Control device, control system, and control method of aircraft |
| US10717525B2 (en) | 2013-06-25 | 2020-07-21 | SZ DJI Technology Co., Ltd. | Aircraft control apparatus, control system and control method |
-
2011
- 2011-12-14 CN CN 201120523211 patent/CN202620714U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014205885A1 (en) * | 2013-06-25 | 2014-12-31 | 深圳市大疆创新科技有限公司 | Control device, control system, and control method of aircraft |
| CN105938369A (en) * | 2013-06-25 | 2016-09-14 | 深圳市大疆创新科技有限公司 | Control system and control method of aircraft |
| US10717525B2 (en) | 2013-06-25 | 2020-07-21 | SZ DJI Technology Co., Ltd. | Aircraft control apparatus, control system and control method |
| US11260973B2 (en) | 2013-06-25 | 2022-03-01 | SZ DJI Technology Co., Ltd. | Aircraft control apparatus, control system and control method |
| US11801938B2 (en) | 2013-06-25 | 2023-10-31 | SZ DJI Technology Co., Ltd | Aircraft control apparatus, control system and control method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204310038U (en) | A kind of pilotless helicopter | |
| CN202620714U (en) | Dual-purpose handle mechanism for throttle control and attitude control in model plane remote controller | |
| CN104943862B (en) | Under-actuated flexible flat wing flapping wing flying robot | |
| CN103157288A (en) | Handle function switching method and mechanism of model airplane remote controller | |
| CN208915439U (en) | Adjustable wing swallow shape simulation type unmanned plane | |
| CN204998770U (en) | But folding frame | |
| CN108750105B (en) | System and method for realizing multi-angle accurate conversion of flapping-fixed wing structure | |
| CN105059525A (en) | Aerodynamic layout of small-sized vertical takeoff and landing aircraft | |
| CN204134213U (en) | Aeromodelling airplane VTOL power rack | |
| CN110767027A (en) | Pilot space situation perception auxiliary training system | |
| CN201678042U (en) | Rotary flapping wing aerocraft | |
| CN201235225Y (en) | Dicladispa armigera helicopter | |
| CN103386197B (en) | Amusement device | |
| CN210244696U (en) | Double-control central rod mechanism of flight simulator | |
| CN201737157U (en) | Mini-type aircraft with two parallel rotary wings | |
| CN107380426A (en) | A kind of compound unmanned plane of rotary shaft | |
| CN204895837U (en) | Small -size VTOL aircraft aerodynamic layout | |
| CN207157500U (en) | A kind of unmanned plane protects chassis | |
| CN208722460U (en) | A kind of manipulation coupling device for Helicopter Simulator emulation cycle Adjustable length rod | |
| CN209936905U (en) | Head moving mechanism and robot | |
| CN202538354U (en) | Operation mechanism of balance weight and CCPM (collective cyclic pitch mixing) control mode of model and helicopter model | |
| CN205248147U (en) | Two switching of power mechanisms and automatic change -over | |
| CN202285202U (en) | Automatic changeover switch device | |
| CN104354861B (en) | A kind of flat-type flapping wing aircraft of band servomotor | |
| CN217740056U (en) | Structure for simulating pitching of airplane rocker |
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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121226 Termination date: 20181214 |