CN104875876A - Dual-steering-engine output system - Google Patents
Dual-steering-engine output system Download PDFInfo
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- CN104875876A CN104875876A CN201510319080.1A CN201510319080A CN104875876A CN 104875876 A CN104875876 A CN 104875876A CN 201510319080 A CN201510319080 A CN 201510319080A CN 104875876 A CN104875876 A CN 104875876A
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Abstract
The invention provides a dual-steering-engine output system. The dual-steering-engine output system comprises a first steering engine, a second steering engine, a first output component and a second output component, wherein the first output component is mounted on an output shaft of the first steering engine, the second output component is mounted on an output shaft of the second steering engine, the first output component is connected with the second output component, and the second output component is applied to dual-steering-engine output. According to the dual-steering-engine output system provided by the invention, large thrust is provided by adopting the linkage of two small-thrust steering engines, so as to achieve control on a yaw rudder and a water rudder of an amphibious unmanned aerial vehicle.
Description
Technical field
The present invention relates to amphibious unmanned plane automation field, be specifically related to a kind of double steering engine output system.
Background technology
Amphibious unmanned plane refers to and can take off on the water, lands, again can the unmanned plane of field takeoff and landing by land.
When aloft flying, amphibious unmanned plane use yaw rudder controlling party to, and take off at the water surface, when landing, use water rudder controlling party to.
The thrust that the thrust that water rudder needs needs much larger than yaw rudder, such as: when aloft flying, the thrust that yaw rudder needs is 10 kilograms, and the thrust that water rudder needs is 0 kilogram; And take off at the water surface, when landing, the thrust that yaw rudder needs is still 10 kilograms, the thrust that water rudder needs is 160 kilograms.
And be difficult to the general steering wheel for unmanned plane finding high thrust at present, make to control yaw rudder and water rudder is very difficult simultaneously.
And general amphibian is manned, the autopilot be equipped with does not have the function of automatic takeoff, landing, therefore without the need to automatically controlling water rudder, the control of water rudder is completed by joystick by chaufeur, completes the control to yaw rudder and water rudder by the power applying different size on joystick.
Therefore, those skilled in the art are devoted to provide a kind of thrust output system, use the general steering wheel of the low thrust easily found, and realize the control of yaw rudder to amphibious unmanned plane and water rudder.
Summary of the invention
For problems of the prior art, the invention provides a kind of double steering engine output system, adopt the steering wheel interlock of two low thrusts, large thrust is provided, realizes the automatic control of yaw rudder to amphibious unmanned plane and water rudder.
The invention provides a kind of double steering engine output system, comprise the first steering wheel, the second steering wheel, the first output block and the second output block, first output block is installed on the output shaft of the first steering wheel, second output block is installed on the output shaft of the second steering wheel, first output block is connected with the second output block, and the second output block is used for double steering engine and exports.
Further, the first output block comprises output panel, the first connecting rod of rotarying connection with output panel and second connecting rod.
Further, the output panel of the first output block is ellipsoidal structure.
Further, the second output block comprises output panel, the first connecting rod of rotarying connection with output panel and second connecting rod, and output panel arranges output connecting bore.
Further, the output panel of the second output block is sector structure.
Further, the first connecting rod of the first output block and the first connecting rod of the second output block are rigidly connected.
Further, the second connecting rod of the first output block and the second connecting rod of the second output block are rigidly connected.
Compared with prior art, the invention provides a kind of double steering engine output system and there is following beneficial effect: the steering wheel interlock adopting two low thrusts, provides large thrust, realize the automatic control to yaw rudder and water rudder.
Accompanying drawing explanation
Fig. 1 is the constructional drawing of the double steering engine output system of one embodiment of the present of invention;
Fig. 2 is the output schematic diagram of the double steering engine output system shown in Fig. 1.
Detailed description of the invention
Be below specific embodiments of the invention and by reference to the accompanying drawings, technical scheme of the present invention is further described, but the present invention be not limited to following examples.
As shown in Figure 1, the double steering engine output system of one embodiment of the present of invention, comprise the first steering wheel 11, second steering wheel 12, first output block and the second output block, first output block is installed on the output shaft of the first steering wheel 11 by screw, and the second output block is installed on the output shaft of the second steering wheel 12 by screw
First output block comprises output panel 213, the first connecting rod 211 of rotarying connection with output panel 213 and second connecting rod 212.
In the present embodiment, the output panel 213 of the first output block is ellipsoidal structure, also can adopt other structures, such as rectangular configuration.
Second output block comprises output panel 223, the first connecting rod 221 of rotarying connection with output panel 223 and second connecting rod 222, output panel 223 arranges and exports connecting bore 224, second output block is used for thrust output, by connecting bore 224 and by the equipment connection of servos control.
In the present embodiment, output panel 223 is provided with three and exports connecting bore 224, different output connecting bores 224 can be used to connect by the equipment of servos control according to actual conditions.
In the present embodiment, the output panel 223 of the second output block is sector structure, also can adopt other structures, such as triangular structure.
The first connecting rod 211 of the first output block is connected with the first connecting rod 221 of the second output block.
The second connecting rod 212 of the first output block is connected with the second connecting rod 222 of the second output block.
As shown in Figure 2, according to control signal, the output shaft of the first steering wheel 11 and the output shaft of the second steering wheel 12 rotate an angle simultaneously, and the output panel 213 of the first steering wheel 11 also rotates corresponding angle to the output panel 223 of the second steering wheel 12; Because the first connecting rod of the first output block and the first connecting rod of the second output block are rigidly connected, the second connecting rod of the first output block and the second connecting rod of the second output block are rigidly connected, making the thrust that the first steering wheel 11 and the second steering wheel 12 export, can output to by the equipment connection of servos control by exporting connecting bore 224 simultaneously.
In the present embodiment, export yaw rudder and water rudder that connecting bore 224 connects amphibious unmanned plane, the less total thrust that when can either be provided in airflight, yaw rudder and water rudder need, such as 10 kilograms, also the larger total thrust that the water surface takes off, yaw rudder and water rudder need when landing can be provided in, such as 170 kilograms, thus realize the automatic control to yaw rudder and water rudder.
More than describe preferred embodiment of the present invention in detail.Should be appreciated that those of ordinary skill in the art just design according to the present invention can make many modifications and variations without the need to creative work.Therefore, all technical personnels in the art, all should by the determined protection domain of claims under this invention's idea on the basis of existing technology by the available technical scheme of logical analysis, reasoning, or a limited experiment.
Claims (7)
1. a double steering engine output system, it is characterized in that, described double steering engine output system comprises the first steering wheel, the second steering wheel, the first output block and the second output block, described first output block is installed on the output shaft of described first steering wheel, described second output block is installed on the output shaft of described second steering wheel, described first output block is connected with described second output block, and described second output block is used for double steering engine and exports.
2. double steering engine output system as claimed in claim 1, it is characterized in that, described first output block comprises output panel, the first connecting rod of rotarying connection with described output panel and second connecting rod.
3. double steering engine output system as claimed in claim 2, it is characterized in that, the output panel of described first output block is ellipsoidal structure.
4. double steering engine output system as claimed in claim 2, it is characterized in that, described second output block comprises output panel, the first connecting rod of rotarying connection with described output panel and second connecting rod, and described output panel arranges output connecting bore.
5. double steering engine output system as claimed in claim 4, it is characterized in that, the output panel of described second output block is sector structure.
6. double steering engine output system as claimed in claim 4, it is characterized in that, the described first connecting rod of described first output block and the described first connecting rod of described second output block are rigidly connected.
7. double steering engine output system as claimed in claim 4, it is characterized in that, the described second connecting rod of described first output block and the described second connecting rod of described second output block are rigidly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510319080.1A CN104875876B (en) | 2015-06-11 | 2015-06-11 | A kind of double steering engine output system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510319080.1A CN104875876B (en) | 2015-06-11 | 2015-06-11 | A kind of double steering engine output system |
Publications (2)
| Publication Number | Publication Date |
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| CN104875876A true CN104875876A (en) | 2015-09-02 |
| CN104875876B CN104875876B (en) | 2017-08-15 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510319080.1A Active CN104875876B (en) | 2015-06-11 | 2015-06-11 | A kind of double steering engine output system |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201419025Y (en) * | 2009-05-27 | 2010-03-10 | 罗之洪 | Model helicopter |
| CN202414162U (en) * | 2011-11-20 | 2012-09-05 | 西北工业大学 | Micro flapping-wing air vehicle with front horizontal swing and front vertical swing |
| CN103043208A (en) * | 2012-12-28 | 2013-04-17 | 天津曙光敬业科技有限公司 | Unmanned helicopter used in double-tail rotor steering engine aerial photographing |
| EP2631171A2 (en) * | 2012-02-27 | 2013-08-28 | Nabtesco Corporation | Aircraft actuator hydraulic system |
| CN103482059A (en) * | 2013-09-27 | 2014-01-01 | 中国航天科技集团公司烽火机械厂 | Electric steering engine |
-
2015
- 2015-06-11 CN CN201510319080.1A patent/CN104875876B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201419025Y (en) * | 2009-05-27 | 2010-03-10 | 罗之洪 | Model helicopter |
| CN202414162U (en) * | 2011-11-20 | 2012-09-05 | 西北工业大学 | Micro flapping-wing air vehicle with front horizontal swing and front vertical swing |
| EP2631171A2 (en) * | 2012-02-27 | 2013-08-28 | Nabtesco Corporation | Aircraft actuator hydraulic system |
| CN103043208A (en) * | 2012-12-28 | 2013-04-17 | 天津曙光敬业科技有限公司 | Unmanned helicopter used in double-tail rotor steering engine aerial photographing |
| CN103482059A (en) * | 2013-09-27 | 2014-01-01 | 中国航天科技集团公司烽火机械厂 | Electric steering engine |
Non-Patent Citations (1)
| Title |
|---|
| 王冈等: "《中小学生航空航天知识 航空模型的原理与制作（下册）》", 31 August 1998 * |
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| CN104875876B (en) | 2017-08-15 |
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Effective date of registration: 20200910 Address after: 610015 China (Sichuan) Free Trade Pilot Area, Chengdu City, Sichuan Province No. 1 Tianwei Road, Southwest Airport Economic Development Zone, Shuangliu District, Chengdu City Patentee after: Sichuan tengdun Kechuang Co., Ltd Address before: 201203 Shanghai Guo Shou Jing Road, Zhangjiang High Tech Park of Pudong New Area No. 351 Building No. 2 room A638-03 Patentee before: SHANGHAI UVS INTELLIGENT SYSTEM Co.,Ltd. |