CN205186536U - Four shaft air vehicle's motor mounting structure - Google Patents
Four shaft air vehicle's motor mounting structure Download PDFInfo
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- CN205186536U CN205186536U CN201520866541.2U CN201520866541U CN205186536U CN 205186536 U CN205186536 U CN 205186536U CN 201520866541 U CN201520866541 U CN 201520866541U CN 205186536 U CN205186536 U CN 205186536U
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- China
- Prior art keywords
- motor
- mounting structure
- axle aircraft
- keysets
- structure according
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- 210000000078 claw Anatomy 0.000 claims description 5
- 229910000831 Steel Inorganic materials 0.000 claims description 4
- 239000010959 steel Substances 0.000 claims description 4
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 abstract 1
- 239000000463 material Substances 0.000 description 2
- 239000006185 dispersion Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
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Abstract
The utility model discloses a four shaft air vehicle's motor mounting structure, a serial communication port, motor on installing the end at four arms of four shaft air vehicle respectively, the motor is located respectively four shaft air vehicle's fan blade below is used for separately -driven the fan blade rotates, the lead wire of motor is connected on the keysets respectively, the keysets respectively with the follow the connector lug interconnect that the inside circuit board of four shaft air vehicle was drawn forth through such structure, can make things convenient for the change of corresponding motor.
Description
Technical field
The utility model relates to a kind of four-axle aircraft, particularly a kind of electric motor mounting structure of four-axle aircraft.
Background technology
Common four-axle aircraft, general is all be connected on the circuit card of the central part enclosure being positioned at four-axle aircraft by the lead-in wire of the motor on four arms, if a certain or some motor damage, then must remove whole shell (being also the panel of four-axle aircraft), the motor damaged could be changed, such process bothers and time-consuming very much, sometimes can owing to having removed whole shell, and cannot reduce the original-shape of four-axle aircraft and structure.
Utility model content
Main purpose of the present utility model is to provide a kind of electric motor mounting structure of four-axle aircraft, and it can facilitate the replacing of motor.
In order to achieve the above object, the utility model proposes a kind of electric motor mounting structure of four-axle aircraft, it is characterized in that, comprise the motor on the end of four arms being arranged on four-axle aircraft respectively, below the fan blade that described motor lays respectively at described four-axle aircraft and for driving described fan blade to rotate respectively, the lead-in wire of described motor is connected on keysets, and the connector lug that described keysets is drawn with the circuit card from described four-axle aircraft inside is respectively interconnected.
According to an embodiment of the present disclosure, described motor is arranged on motor cabinet, and described motor and described motor cabinet are coated with motor cover.
According to an embodiment of the present disclosure, the output driven gear of described motor rotates, and described gear driven is arranged with the axis of rotation of steel pipe socket, and described rotating shaft drives hexagonal axle sleeve to rotate, and described hexagonal axis cover drives described fan blade to rotate.
According to an embodiment of the present disclosure, the sidewall of described motor cabinet is provided with the bracing frame for installing described keysets.
According to an embodiment of the present disclosure, support frame as described above is provided with draw-in groove, and described keysets snaps in described draw-in groove.
According to an embodiment of the present disclosure, described motor cover is also provided with the fender bracket for the protection of described fan blade.
According to an embodiment of the present disclosure, described fender bracket comprises the projection snapped onto in described motor cover, three guard bars in claw type and connects the end of described three guard bars and the cross bar in circular arc.
According to an embodiment of the present disclosure, the end of four arms of described four-axle aircraft is respectively equipped with holding tank, described motor cover and described holding tank mutually fasten and described motor and described motor cabinet are contained in wherein.
According to an embodiment of the present disclosure, the end of four arms of described four-axle aircraft is respectively equipped with holding tank, and described motor cover and described holding tank mutually fasten and described motor, described motor cabinet, the described keysets snapped in described draw-in groove are contained in wherein.
According to an embodiment of the present disclosure, four connector lugs are drawn respectively from the circuit card of described four-axle aircraft inside, described four connector lugs are contained in the holding tank on the end of four arms of described four-axle aircraft respectively, and are connected with described keysets is detachable respectively.
Compared with prior art, the utility model has the following advantages: because motor is arranged on the end of four arms of four-axle aircraft respectively, and the lead-in wire of motor is connected on keysets, the connector lug that described keysets is drawn with the circuit card from described four-axle aircraft inside is respectively interconnected, therefore the shell shell of mounted motor (on the end of such as respective arms) dismantling respective arms is now only needed, and without the need to dismantling the shell of whole four-axle aircraft, thus facilitate the replacing of motor.
Accompanying drawing explanation
In order to clearer explanation the technical solution of the utility model, below the accompanying drawing used required in describing embodiment is briefly described, apparent, accompanying drawing in the following describes is only embodiments more of the present utility model, 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 structural representation of the four-axle aircraft of the utility model embodiment;
Fig. 2 is the structural representation of electric motor mounting structure in Fig. 1;
Fig. 3 is the structural representation of motor before being installed to motor cabinet in Fig. 1; And
Fig. 4 is the structural representation of motor after being installed to motor cabinet in Fig. 1.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment; clear, complete description is carried out to the technical scheme in the utility model embodiment; obviously described embodiment is only a part of embodiment of the present utility model; it not whole embodiments; based on the embodiment in the utility model; those of ordinary skill in the art are not paying the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
As Figure 1-Figure 4, the utility model embodiment provides a kind of electric motor mounting structure of four-axle aircraft, comprise the motor 2 on the end of four arms 1 being arranged on four-axle aircraft respectively, below the fan blade 3 that described motor 2 lays respectively at described four-axle aircraft and for driving described fan blade to rotate respectively, the lead-in wire 4 of described motor is connected on keysets 5, and the connector lug 6 that described keysets 5 is drawn with the circuit card from described four-axle aircraft inside is respectively interconnected.
Such as, because motor is arranged on the end of four arms of four-axle aircraft respectively, and the lead-in wire of motor is connected on keysets, the connector lug that described keysets is drawn with the circuit card from described four-axle aircraft inside is respectively interconnected, therefore the shell (end of such as respective arms being installed the detouchable shell of corresponding motor by screw) dismantling respective arms is now only needed, and without the need to dismantling the shell of whole four-axle aircraft, thus facilitate the replacing of motor.
According to an embodiment of the present disclosure, described motor 2 is arranged on motor cabinet 7, and described motor 2 and described motor cabinet 7 are coated with motor cover 8.
Such as, motor cabinet can play effect that is fixing and protection to the motor held within it, motor can cover motor cover after being contained in motor cabinet again, then such motor cover is arranged on the corresponding arm of four-axle aircraft.
According to an embodiment of the present disclosure, the output driven gear 9 of described motor 2 rotates, and described gear 9 drives the rotating shaft 11 being arranged with steel pipe socket 10 to rotate, and described rotating shaft 11 drives hexagonal axle sleeve 12 to rotate, and described hexagonal axle sleeve 12 drives described fan blade 3 to rotate.
Such as, the fan blade on corresponding arm can be driven to rotate by gear, the rotating shaft being arranged with steel pipe socket and hexagonal axle sleeve, thus whole four-axle aircraft held stationary is flown, and the circuit card of described four-axle aircraft inside can also control the motor on each arm respectively, thus control corresponding fan blade, realize the heading of four-axle aircraft and/or the adjustment of flying speed.
According to an embodiment of the present disclosure, the sidewall of described motor cabinet 7 is provided with the bracing frame 13 for installing described keysets.
Such as, the sidewall of motor cabinet can be arranged the bracing frame installing described keysets, bracing frame can be one-body molded with motor cabinet, thus convenient processing, also can integral replacing when changing motor, easy to use.
According to an embodiment of the present disclosure, support frame as described above 13 is provided with draw-in groove 14, and described keysets 5 snaps in described draw-in groove 14.
Such as, keysets can directly engage within it by the draw-in groove that bracing frame is provided with, thus is conveniently fixed keysets and locates, thus convenient after being installed on corresponding arm, is connected with corresponding connector lug; Such as described keysets 5 is installed in described draw-in groove 14 by engaging.
According to an embodiment of the present disclosure, described motor cover 8 is also provided with the fender bracket 15 for the protection of described fan blade.
Such as, the material of fender bracket can be plastics or other suitable materials, and the function of fender bracket prevents the rotation of fan blade from causing damage to other people or article, also protects the infringement that fan blade is not impacted etc.
According to an embodiment of the present disclosure, described fender bracket 15 comprises the projection 16 snapped onto in described motor cover, three guard bars 17 in claw type and connects the end of described three guard bars and the cross bar 18 in circular arc.
Such as, fender bracket can to snap onto in motor cover in corresponding hole by two projections, and its entirety is fixed in motor cover.Three guard bars in claw type are dispersion shape; and be certain radian in space; fan blade can be encompassed within its scope; in addition; cross bar in circular arc can connect the end of described three guard bars; further fixation is played to three guard bars in claw type, also more firm and safety.
According to an embodiment of the present disclosure, the end of four arms of described four-axle aircraft is respectively equipped with holding tank 19, described motor cover 8 mutually fastens with described holding tank 19 and described motor and described motor cabinet is contained in wherein.
Such as, holding tank can be a part for four own inner hollow of arm of four-axle aircraft, such as can be roughly cylindrical, can be used for jointly forming with motor cover the space holding motor and described motor cabinet, thus make four-axle aircraft more attractive in appearance on the whole.And mutually fasten the replacing that the motor cover of (being such as screwed) and described holding tank also facilitate motor, when needing to change the motor such as damaged, only need to take motor cover and described holding tank apart, then keysets and corresponding connector lug are taken apart, the integral replacing of motor and described motor cabinet can be realized, easy to use.
According to an embodiment of the present disclosure, the end of four arms of described four-axle aircraft is respectively equipped with holding tank 19, and described motor cover 8 mutually fastens with described holding tank 19 and described motor, described motor cabinet, the described keysets snapped in described draw-in groove is contained in wherein.
Such as, holding tank can be a part for four own inner hollow of arm of four-axle aircraft, such as can be roughly cylindrical, can be used for jointly forming the space holding motor, described motor cabinet and snap in the described keysets in described draw-in groove with motor cover, thus make four-axle aircraft more attractive in appearance on the whole.And mutually fasten the replacing that the motor cover of (being such as screwed) and described holding tank also facilitate motor, when needing to change the motor such as damaged, only need to take motor cover and described holding tank apart, then keysets and corresponding connector lug are taken apart, the integral replacing of motor and described motor cabinet can be realized, easy to use.
According to an embodiment of the present disclosure, four connector lugs are drawn respectively from the circuit card of described four-axle aircraft inside, described four connector lugs are contained in the holding tank 19 on the end of four arms of described four-axle aircraft respectively, and are connected with described keysets is detachable respectively.
Such as, the circuit card of described four-axle aircraft inside can draw four connector lugs respectively, respectively to the detachable connection of corresponding keysets that the end of four arms of described four-axle aircraft is installed, such as can by the connection of the form realizing circuit of engaging mutually, can connection on cut off when being separated from each other, such as general battery is arranged on the circuit card (in the shell of the medium position of such as four-axle aircraft) near four-axle aircraft inside, now the connector lug on the end of four of four-axle aircraft arms and keysets are separated from each other (such as extracting connector lug), corresponding motor cut off just can be made to connect, convenient directly replacing.
Through the above description of the embodiments, those skilled in the art can be well understood to the utility model and can also be realized by other structures, and feature of the present utility model is not limited to above-mentioned preferred embodiment.Any personnel being familiar with this technology are in technical field of the present utility model, and the change that can expect easily or modification, all should be encompassed within scope of patent protection of the present utility model.
Claims (10)
1. the electric motor mounting structure of a four-axle aircraft, it is characterized in that, comprise the motor on the end of four arms being arranged on four-axle aircraft respectively, below the fan blade that described motor lays respectively at described four-axle aircraft and for driving described fan blade to rotate respectively, the lead-in wire of described motor is connected on keysets, and the connector lug that described keysets is drawn with the circuit card from described four-axle aircraft inside is respectively interconnected.
2. electric motor mounting structure according to claim 1, is characterized in that, described motor is arranged on motor cabinet, and described motor and described motor cabinet are coated with motor cover.
3. electric motor mounting structure according to claim 2, it is characterized in that, the output driven gear of described motor rotates, and described gear driven is arranged with the axis of rotation of steel pipe socket, described rotating shaft drives hexagonal axle sleeve to rotate, and described hexagonal axis cover drives described fan blade to rotate.
4. electric motor mounting structure according to claim 2, is characterized in that, the sidewall of described motor cabinet is provided with the bracing frame for installing described keysets.
5. electric motor mounting structure according to claim 4, is characterized in that, support frame as described above is provided with draw-in groove, and described keysets snaps in described draw-in groove.
6. electric motor mounting structure according to claim 2, is characterized in that, described motor cover is also provided with the fender bracket for the protection of described fan blade.
7. electric motor mounting structure according to claim 6, is characterized in that, described fender bracket comprises the projection snapped onto in described motor cover, three guard bars in claw type and connects the end of described three guard bars and the cross bar in circular arc.
8. electric motor mounting structure according to claim 2, is characterized in that, the end of four arms of described four-axle aircraft is respectively equipped with holding tank, and described motor cover and described holding tank mutually fasten and described motor and described motor cabinet be contained in wherein.
9. electric motor mounting structure according to claim 5, it is characterized in that, the end of four arms of described four-axle aircraft is respectively equipped with holding tank, and described motor cover and described holding tank mutually fasten and described motor, described motor cabinet, the described keysets snapped in described draw-in groove are contained in wherein.
10. electric motor mounting structure according to claim 1, it is characterized in that, four connector lugs are drawn respectively from the circuit card of described four-axle aircraft inside, described four connector lugs are contained in the holding tank on the end of four arms of described four-axle aircraft respectively, and are connected with described keysets is detachable respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520866541.2U CN205186536U (en) | 2015-11-03 | 2015-11-03 | Four shaft air vehicle's motor mounting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520866541.2U CN205186536U (en) | 2015-11-03 | 2015-11-03 | Four shaft air vehicle's motor mounting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205186536U true CN205186536U (en) | 2016-04-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520866541.2U Expired - Fee Related CN205186536U (en) | 2015-11-03 | 2015-11-03 | Four shaft air vehicle's motor mounting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205186536U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018086227A1 (en) * | 2016-11-09 | 2018-05-17 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
-
2015
- 2015-11-03 CN CN201520866541.2U patent/CN205186536U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018086227A1 (en) * | 2016-11-09 | 2018-05-17 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
| US10538336B2 (en) | 2016-11-09 | 2020-01-21 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle |
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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 |
Granted publication date: 20160427 Termination date: 20161103 |
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| CF01 | Termination of patent right due to non-payment of annual fee |