CN202860117U - Model plane dynamic vector and pneumatic steerage combined type manipulation device - Google Patents
Model plane dynamic vector and pneumatic steerage combined type manipulation device Download PDFInfo
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- CN202860117U CN202860117U CN 201220527787 CN201220527787U CN202860117U CN 202860117 U CN202860117 U CN 202860117U CN 201220527787 CN201220527787 CN 201220527787 CN 201220527787 U CN201220527787 U CN 201220527787U CN 202860117 U CN202860117 U CN 202860117U
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Abstract
The utility model discloses model plane dynamic vector and pneumatic steerage combined type manipulation device. The model plane dynamic vector and pneumatic steerage combined type manipulation device comprises a left-dynamic duct, a right-dynamic duct and an elevator which are respectively connected with a control plate. The left-dynamic duct is arranged on a left wing of the model plane, the right-dynamic duct is arranged on a right wing of the model plane, and the elevator is arranged on a horizontal tail of the model plane. A left-dynamic increasing and decreasing operation module connected with the left-dynamic duct, a right-dynamic increasing and decreasing operation module connected with the right-dynamic duct, and a lifting operation module connected with the elevator are arranged on the control plate, and a dynamic gear grade operation unit is further arranged on the control plate. By combining pneumatic steerage effect and dynamic vector control, the model plane achieves controlling flight through dynamic, lifting and course channels, and meanwhile the flexibility of the dynamic vector control and the accuracy of pneumatic steerage control in flight can be provided. In addition, the operation is simple, and the structure is reliable.
Description
Technical field
The utility model relates to the operating means of model of an airplane flight, in particular a kind of power vector of the model of an airplane and pneumatic steerage combined type actuation means.
Background technology
Remote-controlled model aircraft all adopts pneumatic steerage or power vector controlled flight attitude in flight control now.
Pneumatic steerage control model belongs to conventional control model, needs assisting to control about aileron, lifting, direction and the wing flap rudder face, swinging of Servo-controller, and is so not only complicated in the operation, and brings expensive cost to the model of an airplane.
Power vector controlled pattern is relatively used less on the model of an airplane, mainly on two motive model of an airplanes by the differential course of controlling of power vector, and on the end models aircraft by rear motive force vector controlled course.The former tends to toy this operator scheme, and control mode is single, just course, the left and right sides is controlled, so flight control precision is poor; The latter is in structure and control all too complicatedly, is unsuitable for common remote-controlled model aircraft operator.
Therefore, there is defective in prior art, needs to improve.
The utility model content
Technical problem to be solved in the utility model is: provide a kind of pneumatic steerage effect and power vector controlled are combined, possess simultaneously the flexible of power vector controlled, when possessing again pneumatic steerage control flight accurately, and, simple to operate, the power vector of reliable in structure and pneumatic steerage combined type actuation means.
The technical solution of the utility model is as follows: a kind of power vector of the model of an airplane and pneumatic steerage combined type actuation means comprise the left power duct that is connected with control panel respectively, right power duct and elevator; Described left power duct is installed on the port wing of the model of an airplane, and described right power duct is installed on the starboard wing of the described model of an airplane, and described elevator is installed on the horizontal tail of the described model of an airplane; The left power increase and decrease operational module that is connected with described left power duct, the right power increase and decrease operational module that is connected with described right power duct, the descending operation module that is connected with described elevator are set on the described control panel; And, a power shelves level operating unit also is set on the described control panel.
Be applied to technique scheme, in described power vector and the pneumatic steerage combined type actuation means, described power shelves level operating unit arranges respectively 0-15% power operation module, 15%-85% power operation module and 85%-100% power operation module.
Be applied to each technique scheme, in described power vector and the pneumatic steerage combined type actuation means, described control panel also arranges a remote control control module, and described remote control control module is connected with described left power increase and decrease operational module, described right power increase and decrease operational module and the power shelves level operating unit of being connected respectively.
Be applied to each technique scheme, in described power vector and the pneumatic steerage combined type actuation means, the infrared detection module that described control panel also arranges an intelligent automatic operation module and is connected with described intelligent automatic operation module, and described intelligent automatic operation module is connected with described remote control control module, described left power increase and decrease operational module, described right power increase and decrease operational module and the power shelves level operating unit of being connected respectively.
Adopt such scheme, the utility model is by arranging left power duct and right power duct at wing, and corresponding left power increase and decrease operational module and right power increase and decrease operational module, and power shelves level operating unit is set, the model of an airplane adopts two duct power, so, and by control, when different power shelves level operations is set, produce the control course that left and right moving force vector differential change is come the flexible model of an airplane; And, by elevator and corresponding descending operation module are set, control flying height by the pneumatic steerage that controllable elevator produce.Like this, this model of an airplane is realized control flight by power, lifting, course triple channel.Vast model of an airplane operator like this can control course and flying height by triple channel when flight operation, control model of an airplane flight accuracy is high, operation in simply, and the model of an airplane structurally relative general models aircraft is simple and reliable.
Description of drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is structure connection diagram of the present utility model.
The specific embodiment
Below in conjunction with the drawings and specific embodiments, the utility model is elaborated.
Present embodiment provides a kind of power vector and pneumatic steerage combined type actuation means of the model of an airplane, when controlling course, the model of an airplane left and right sides by the differential of control power vector, control the flying height of the model of an airplane by the pneumatic steerage of the model of an airplane, thereby realize the flight attitude of the control model of an airplane by power, lifting, course triple channel, make the model of an airplane possess simultaneously the power vector controlled flexibly, when possessing again pneumatic steerage control flight accurately.
Wherein, as shown in Figure 1, described power vector and pneumatic steerage combined type actuation means comprise control panel 103, left power duct 102, right power duct 104 and elevator 107, left power duct 102, right power duct 104 are connected with elevator and are connected with control panel 103 respectively, send control instruction by control panel 103 and control.
And, described left power duct 102 is installed on the port wing of the model of an airplane, described right power duct 104 is installed on the starboard wing of the described model of an airplane, described elevator 107 is installed on the horizontal tail of the described model of an airplane, by control panel 103 sending controling instructions, control respectively the power size of left power duct 102 and right power duct 104, make the power of left power duct 102 and right power duct 104 produce difference, thereby make the left and right sides wing of the model of an airplane produce differential, reach the purpose in the course, the left and right sides that changes the model of an airplane.
And elevator 107 is connected with control panel by Servo-controller 106, thereby pass through control panel 103 sending controling instructions to Servo-controller 106, by Servo-controller 106 control elevators 107, thereby reaches the purpose of controlling model of an airplane height.
And, the left and right sides wing of the model of an airplane also arranges respectively the true duct 101 of picture and the true duct 105 of picture, by as true duct 101 with profile and the mounting means of duct are set as true duct 105, can simulate real manned aircraft, make the outward appearance of the model of an airplane more as real manned aircraft, the true duct 101 of picture and the true duct 105 of picture be mounted motor not, does not play duct.
And, as shown in Figure 2, left power increase and decrease operational module, right power increase and decrease operational module and descending operation module also are set on the described control panel, wherein, left power increase and decrease operational module is connected with described left power duct, right power increase and decrease operational module is connected with described right power duct, and the descending operation module is connected with described elevator 107; Can change the power vector of left power duct by left power increase and decrease operational module, can change the power vector of right power duct by right power increase and decrease operational module, thereby change the course, the left and right sides of the model of an airplane, and, make elevator produce pneumatic steerage by the descending operation module simultaneously, thereby change the flying height of the model of an airplane.
And, a power shelves level operating unit also is set on the described control panel, for example, described power shelves level operating unit arranges respectively 0-15% power operation module, 15%-85% power operation module and 85%-100% power operation module.
For example, making the described model of an airplane by described 0-15% power operation module is the 0-15% dynamic regime, and namely the described model of an airplane is when zero throttle, and by strengthening the power vector of left power duct, the model of an airplane is turned right; Perhaps, by strengthening the power vector of right power duct, the model of an airplane turns left.
And for example, making the described model of an airplane by described 15%-85% power operation module is the 15%-85% dynamic regime, and namely the described model of an airplane is when middle throttle, by strengthening the power vector of left power duct, weaken the power vector of right power duct, the model of an airplane is turned right; Perhaps, by strengthening the power vector of right power duct, weaken the power vector of left power duct, the model of an airplane turns left.
For another example, making the described model of an airplane by 85%-100% power operation module is the 85%-100% dynamic regime, and namely the described model of an airplane is at the full throttle state, by weakening the power vector of left power duct, the power vector of right power duct remains unchanged, and the model of an airplane turns left; Perhaps, by weakening the power vector of right power duct, the power vector of left power duct remains unchanged, and the model of an airplane is turned right.
So, at the normal flat state that flies, control its effect course by the power vector generation power differential vector of control left and right sides power duct at the model of an airplane; And control flying height by the lifting controllable rudder: the elevator rudder face upwards swings, and aircraft upwards climbs; The elevator rudder face is to lower swing, the aircraft falling head.Cooperate by aforesaid operations, just can well control model of an airplane flight attitude.
Perhaps, can also one remote control control module also be set at described control panel, described remote control control module is connected with described left power increase and decrease operational module, described right power increase and decrease operational module and the power shelves level operating unit of being connected respectively; Receive outside remote signal by described remote control control module, control described left power increase and decrease operational module, described right power increase and decrease operational module and described power shelves level operating unit according to remote signal.
Or, the infrared detection module that described control panel also arranges an intelligent automatic operation module and is connected with described intelligent automatic operation module, and described intelligent automatic operation module is connected with described remote control control module, described left power increase and decrease operational module, described right power increase and decrease operational module and the power shelves level operating unit of being connected respectively; When described remote control control module is not received remote signal in Preset Time, then automatically start described intelligent automatic operation module, by described intelligent automatic operation module according to the control model that presets, control respectively described remote control control module, described left power increase and decrease operational module, described right power increase and decrease operational module and described power shelves level operating unit, thereby course, the left and right sides and the flying height of automatic control model aircraft, and, whether be stored in infrared ray in the setpoint distance around the described infrared detection module detection model aircraft, and notify described intelligent automatic operation module, avoid the described model of an airplane and people or biology to bump, security performance is good.
Be preferred embodiment of the present utility model only below, be not limited to the utility model, all any modifications of within spirit of the present utility model and principle, doing, be equal to and replace and improvement etc., all should be included within the protection domain of the present utility model.
Claims (4)
1. the power vector of a model of an airplane and pneumatic steerage combined type actuation means is characterized in that,
Comprise the left power duct that is connected with control panel respectively, right power duct and elevator;
Described left power duct is installed on the port wing of the model of an airplane, and described right power duct is installed on the starboard wing of the described model of an airplane, and described elevator is installed on the horizontal tail of the described model of an airplane;
The left power increase and decrease operational module that is connected with described left power duct, the right power increase and decrease operational module that is connected with described right power duct, the descending operation module that is connected with described elevator are set on the described control panel;
And, a power shelves level operating unit also is set on the described control panel.
2. power vector according to claim 1 and pneumatic steerage combined type actuation means is characterized in that, described power shelves level operating unit arranges respectively 0-15% power operation module, 15%-85% power operation module and 85%-100% power operation module.
3. power vector according to claim 1 and pneumatic steerage combined type actuation means, it is characterized in that, described control panel also arranges a remote control control module, and described remote control control module is connected with described left power increase and decrease operational module, described right power increase and decrease operational module and the power shelves level operating unit of being connected respectively.
4. power vector according to claim 3 and pneumatic steerage combined type actuation means, it is characterized in that, the infrared detection module that described control panel also arranges an intelligent automatic operation module and is connected with described intelligent automatic operation module, and described intelligent automatic operation module is connected with described remote control control module, described left power increase and decrease operational module, described right power increase and decrease operational module and the power shelves level operating unit of being connected respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220527787 CN202860117U (en) | 2012-10-16 | 2012-10-16 | Model plane dynamic vector and pneumatic steerage combined type manipulation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220527787 CN202860117U (en) | 2012-10-16 | 2012-10-16 | Model plane dynamic vector and pneumatic steerage combined type manipulation device |
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| Publication Number | Publication Date |
|---|---|
| CN202860117U true CN202860117U (en) | 2013-04-10 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220527787 Withdrawn - After Issue CN202860117U (en) | 2012-10-16 | 2012-10-16 | Model plane dynamic vector and pneumatic steerage combined type manipulation device |
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| CN (1) | CN202860117U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102949849A (en) * | 2012-10-16 | 2013-03-06 | 深圳市艾特航模股份有限公司 | Power vector and pneumatic steerage combined control device of model aircraft |
-
2012
- 2012-10-16 CN CN 201220527787 patent/CN202860117U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102949849A (en) * | 2012-10-16 | 2013-03-06 | 深圳市艾特航模股份有限公司 | Power vector and pneumatic steerage combined control device of model aircraft |
| CN102949849B (en) * | 2012-10-16 | 2015-02-25 | 深圳市艾特航空科技股份有限公司 | Power vector and pneumatic steerage combined control device of model aircraft |
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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 |
Owner name: SHENZHEN ART AVIATION TECHNOLOGY CO., LTD. Free format text: FORMER NAME: SHENZHEN ART-TECH R/C HOBBY CO., LTD. |
|
| CP01 | Change in the name or title of a patent holder |
Address after: Two or three, 1, four floor, D4 building, Liyuan Industrial Estate, Shiyan community, Shiyan street, Shiyan City, Shenzhen, Guangdong, Baoan District 518000, China Patentee after: Shenzhen Art Aviation Technology Co., Ltd. Address before: Two or three, 1, four floor, D4 building, Liyuan Industrial Estate, Shiyan community, Shiyan street, Shiyan City, Shenzhen, Guangdong, Baoan District 518000, China Patentee before: Shenzhen Art-Tech R/C Hobby Co., Ltd. |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20130410 Effective date of abandoning: 20150225 |
|
| RGAV | Abandon patent right to avoid regrant |