CN105221318A - A kind of unmanned plane with remote activating device - Google Patents
A kind of unmanned plane with remote activating device Download PDFInfo
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- CN105221318A CN105221318A CN201510700744.9A CN201510700744A CN105221318A CN 105221318 A CN105221318 A CN 105221318A CN 201510700744 A CN201510700744 A CN 201510700744A CN 105221318 A CN105221318 A CN 105221318A
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- electric device
- starting motor
- suav
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Abstract
The invention provides a kind of unmanned plane with remote activating device, solve the SUAV of the prior art motor technical problem of easily stopping working awing, its structure comprises: internal-combustion engine, electric device and starting motor; Electric device is electrically connected with starting motor; The output shaft of starting motor is in transmission connection by the rotation output terminal of transmission device and internal-combustion engine; Electric device is provided with the wireless signal send receive module running for remote control starting motor and cut out; Electric device is electrically connected with the internal power supply system of SUAV.The present invention is by arranging remote activating device for SUAV, overcome the flame-out technological deficiency that easily to meet accident when SUAV flies in rugged environment, be arranged on wireless signal send receive module in electric device by being connected with control base station or remote controller signal, realize the open and close of remote wireless controlled starting motor, and then provide strong technical support for the internal-combustion engine of wireless startup SUAV.
Description
Technical field
The present invention relates to SUAV technical field, particularly a kind of unmanned plane with remote activating device.
Background technique
The unmanned plane internal-combustion engine used as motor in prior art is mainly large-scale model plane and researches and develops, due to the more complete safety installations of the usual proportioning of large-scale model plane, the latent defect of motor can be made up, and then can the relatively severe flight environment of adaptive temperature, humidity and air pressure.But above-mentioned safety installations are due to physical dimension and weight issue, usually be rejected when SUAV structural design, therefore subtract the flight safety aspect of the vibrational power flow after joining to SUAV and bring certain potential safety hazard, particularly SUAV fly under the rugged environment of mountain area High aititude operation time, very easily cause the technical failure of engine misses.
Therefore, research and develop a kind of unmanned plane with remote activating device, to overcome above-mentioned technological deficiency, the flight safety increasing SUAV becomes a kind of required.
Summary of the invention
For this reason, the invention provides a kind of unmanned plane with remote activating device, solve the SUAV of the prior art motor technical problem of easily stopping working awing.
For this reason, the invention provides a kind of SUAV with remote activating device, comprise internal-combustion engine, comprising: electric device and starting motor; Described electric device is electrically connected with described starting motor; The output shaft of described starting motor is in transmission connection by the rotation output terminal of transmission device and described internal-combustion engine; Described electric device is provided with the wireless signal send receive module running for starting motor described in remote control and cut out; Described electric device is electrically connected with the internal power supply system of described SUAV.
According to an embodiment of the invention, wherein, the form be in transmission connection described in comprises: V belt translation or Chain conveyer.
According to an embodiment of the invention, wherein, described transmission device is unidirectional transmission.
According to an embodiment of the invention, wherein, described unidirectional transmission is provided with unilateral bearing.
According to an embodiment of the invention, wherein, also comprise: startup power supply for subsequent use, described startup power supply for subsequent use and the electrical connection of described electric device.
The present invention is by arranging remote activating device for SUAV, overcome the flame-out technological deficiency that easily to meet accident when SUAV flies in rugged environment, be arranged on wireless signal send receive module in electric device by being connected with control base station or remote controller signal, realize the open and close of remote wireless controlled starting motor, and then provide strong technical support for the internal-combustion engine of wireless startup SUAV.
Further, the present invention, by arranging unilateral bearing for transmission device, continues after avoiding internal combustion engine start to drive starting motor running, reduces flight energy consumption.
Further, the present invention is by arranging startup power supply for subsequent use for SUAV, further safety guarantee is provided for SUAV power supply circuits break down, when SUAV power supply line breaks down, startup power supply for subsequent use can be the startup energy that starting motor provides sufficient, and then be again that starting apparatus combustion engine provides strong technical support, guarantee the flight safety of SUAV.
Accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present invention or technological scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the unmanned plane structural representation in the embodiment of the present invention 1 with remote activating device;
Fig. 2 is a kind of structural representation of connecting plate in the embodiment of the present invention 1;
Fig. 3 is the another kind of structural representation of connecting plate in the embodiment of the present invention 1.
Embodiment
Below in conjunction with embodiment, the specific embodiment of the present invention is described in further detail.Following examples only for illustration of the present invention, but can not be used for limiting the scope of the invention.
Embodiment 1:
Without loss of generality, as shown in Figure 1, the invention provides a kind of unmanned plane with remote activating device, comprise internal-combustion engine 300, it is characterized in that, comprising: electric device 100 and starting motor 200; Described electric device 100 is electrically connected with described starting motor 200; The output shaft of described starting motor 200 is in transmission connection by the rotation output terminal of transmission device and described internal-combustion engine 300; Described electric device 100 is provided with the wireless signal send receive module 101 running for starting motor described in remote control 200 and cut out; Described electric device 100 is electrically connected with the internal power supply system of described unmanned plane.
When SUAV occurs flame-out in-flight, only need send to electric device the startup again that enabled instruction can realize SUAV.It should be noted that, the internal structure due to electric device is prior art, therefore its specific structural details does not repeat them here.
Further, in an optimal technical scheme of the present embodiment, described in the form that is in transmission connection comprise: V belt translation or Chain conveyer.As shown in figures 2 and 3, starting motor and internal-combustion engine are fastenedly connected by connecting plate shown in figure by the present invention, and the output terminal of starting motor and internal-combustion engine is fastenedly connected respectively on the corresponding attachment hole shown in Fig. 2 or 3.
Further, in an optimal technical scheme of the present embodiment, described transmission device is unidirectional transmission.Single-direction transmission continues the running of traction starting motor after helping avoid engine starts, expend the energy.
Further, in an optimal technical scheme of the present embodiment, described unidirectional transmission is provided with unilateral bearing.
Embodiment 2:
The present embodiment, on the basis of embodiment 1, also comprises further: startup power supply for subsequent use, described startup power supply for subsequent use and the electrical connection of described electric device.Startup power supply for subsequent use, further safety guarantee is provided for SUAV power supply circuits break down, when SUAV power supply line breaks down, startup power supply for subsequent use can be the startup energy that starting motor provides sufficient, and then be again that starting apparatus combustion engine provides strong technical support, guarantee the flight safety of SUAV.
More than inventing is only the preferred embodiment of the present invention; it should be pointed out that for those skilled in the art, under the prerequisite not departing from the technology of the present invention principle; can also make some improvement and modification, these improve and modification also should be considered as protection scope of the present invention.
It should be noted, the present invention will be described instead of limit the invention for above-described embodiment, and those skilled in the art can design alternative embodiment when not departing from the scope of claims.In the claims, any reference symbol between bracket should be configured to limitations on claims.Word " comprises " not to be got rid of existence and does not arrange element in the claims or step.Word "a" or "an" before being positioned at element is not got rid of and be there is multiple such element.The present invention can by means of including the hardware of some different elements and realizing by means of the computer of suitably programming.In the unit claim listing some devices, several in these devices can be carry out imbody by same hardware branch.Word first, second and third-class use do not represent any order.
Claims (5)
1. there is a unmanned plane for remote activating device, comprise internal-combustion engine, it is characterized in that, comprising: electric device and starting motor; Described electric device is electrically connected with described starting motor; The output shaft of described starting motor is in transmission connection by the rotation output terminal of transmission device and described internal-combustion engine; Described electric device is provided with the wireless signal send receive module running for starting motor described in remote control and cut out; Described electric device is electrically connected with the internal power supply system of described unmanned plane.
2. unmanned plane according to claim 1, wherein, described in the form that is in transmission connection comprise: V belt translation or Chain conveyer.
3. unmanned plane according to claim 1, wherein, described transmission device is unidirectional transmission.
4. unmanned plane according to claim 3, wherein, described unidirectional transmission is provided with unilateral bearing.
5. unmanned plane according to claim 1, wherein, also comprises: startup power supply for subsequent use, described startup power supply for subsequent use and the electrical connection of described electric device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510700744.9A CN105221318A (en) | 2015-10-23 | 2015-10-23 | A kind of unmanned plane with remote activating device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510700744.9A CN105221318A (en) | 2015-10-23 | 2015-10-23 | A kind of unmanned plane with remote activating device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105221318A true CN105221318A (en) | 2016-01-06 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510700744.9A Pending CN105221318A (en) | 2015-10-23 | 2015-10-23 | A kind of unmanned plane with remote activating device |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106043715A (en) * | 2016-05-27 | 2016-10-26 | 襄阳宏伟航空器有限责任公司 | In-flight auto-ignition control method of engine of unmanned aerial vehicle |
| CN106774358A (en) * | 2016-11-17 | 2017-05-31 | 广州极飞科技有限公司 | Unmanned plane intelligent battery and its control method, device and unmanned plane |
| CN107191306A (en) * | 2017-01-25 | 2017-09-22 | 浙江白马实业有限公司 | A kind of gasoline engine starting transponder and its method for starting gasoline engine |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1193812A (en) * | 1997-09-25 | 1999-04-06 | Yamaha Motor Co Ltd | Engine starter of unmanned helicopter |
| CN101482082A (en) * | 2008-08-28 | 2009-07-15 | 杨东 | Remote control starting method and apparatus for internal combustion engine |
| CN203879670U (en) * | 2014-03-26 | 2014-10-15 | 沈阳天之翼航空科技有限公司 | Remote control electric starting device |
| CN203996906U (en) * | 2014-08-21 | 2014-12-10 | 张曹勇 | The generating of model plane unmanned plane and the airborne starter gear of startup unification |
| CN204716443U (en) * | 2015-04-07 | 2015-10-21 | 安徽天马航空植保科技有限公司 | A kind of new oil moves the remote control electric starting system of agricultural plant protection unmanned plane |
| CN205225553U (en) * | 2015-10-23 | 2016-05-11 | 四川测绘地理信息局测绘技术服务中心 | Unmanned aerial vehicle with remote start up device |
-
2015
- 2015-10-23 CN CN201510700744.9A patent/CN105221318A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1193812A (en) * | 1997-09-25 | 1999-04-06 | Yamaha Motor Co Ltd | Engine starter of unmanned helicopter |
| CN101482082A (en) * | 2008-08-28 | 2009-07-15 | 杨东 | Remote control starting method and apparatus for internal combustion engine |
| CN203879670U (en) * | 2014-03-26 | 2014-10-15 | 沈阳天之翼航空科技有限公司 | Remote control electric starting device |
| CN203996906U (en) * | 2014-08-21 | 2014-12-10 | 张曹勇 | The generating of model plane unmanned plane and the airborne starter gear of startup unification |
| CN204716443U (en) * | 2015-04-07 | 2015-10-21 | 安徽天马航空植保科技有限公司 | A kind of new oil moves the remote control electric starting system of agricultural plant protection unmanned plane |
| CN205225553U (en) * | 2015-10-23 | 2016-05-11 | 四川测绘地理信息局测绘技术服务中心 | Unmanned aerial vehicle with remote start up device |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106043715A (en) * | 2016-05-27 | 2016-10-26 | 襄阳宏伟航空器有限责任公司 | In-flight auto-ignition control method of engine of unmanned aerial vehicle |
| CN106043715B (en) * | 2016-05-27 | 2018-03-27 | 襄阳宏伟航空器有限责任公司 | A kind of aerial method for controlling automatic ignition of unmanned vehicle engine |
| CN106774358A (en) * | 2016-11-17 | 2017-05-31 | 广州极飞科技有限公司 | Unmanned plane intelligent battery and its control method, device and unmanned plane |
| CN107191306A (en) * | 2017-01-25 | 2017-09-22 | 浙江白马实业有限公司 | A kind of gasoline engine starting transponder and its method for starting gasoline engine |
| CN107191306B (en) * | 2017-01-25 | 2024-01-05 | 浙江白马实业有限公司 | Gasoline engine starting transfer device and gasoline engine starting method thereof |
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Application publication date: 20160106 |