CN205060005U - Empty energy -conserving unmanned aerial vehicle can stagnate - Google Patents
Empty energy -conserving unmanned aerial vehicle can stagnate Download PDFInfo
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- CN205060005U CN205060005U CN201520732693.3U CN201520732693U CN205060005U CN 205060005 U CN205060005 U CN 205060005U CN 201520732693 U CN201520732693 U CN 201520732693U CN 205060005 U CN205060005 U CN 205060005U
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- China
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- brushless
- electronic governor
- support
- holster shell
- oar
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Abstract
The utility model relates to an aircraft technical field, more specifically say and relate to an empty energy -conserving unmanned aerial vehicle can stagnate, has improved unmanned aerial vehicle's stagnant short side formula, king bolt oar, brushless big motor and the electronic governor I work when empty of stagnating, and electronic governor II, minor spiral oar and brushless small motor stop work, and unmanned aerial vehicle will consume less battery power when empty stagnating like this, reaches the long -time purpose empty and energy -conservation that stagnates. The battery is installed in the inside centre of frame shell, and the flight control board is installed in the inside upper end of frame shell. The king bolt oar is installed in the upper end of brushless big motor, and brushless big motor is installed in electronic governor I's upper end, and electronic governor I fixes the centre on frame shell top. The inner of support is fixed in the centre of frame shell, and electronic governor II installs in the centre of support, and the minor spiral oar is installed in the upper end of brushless small motor, and the outer end at the support is installed to brushless small motor. The bottom at the frame shell is fixed to the landing leg.
Description
Technical field
The utility model relates to vehicle technology field, more specifically to a kind of can the energy-conservation unmanned plane of stagnant sky.
Background technology
Unmanned plane is a kind of conventional aerial reconnaissance means.But the battery consumption of four of unmanned plane motors is also very fast, this just causes the stagnant empty flight time of unmanned plane greatly to be reduced, and needs repeatedly to charge, and causes waste to the energy.So design a kind of can being necessary by the energy-conservation unmanned plane of stagnant sky.
Summary of the invention
The technical matters that the utility model mainly solves is: provide a kind of can the energy-conservation unmanned plane of stagnant sky, improve the stagnant short side formula of unmanned plane, during stagnant sky, king bolt oar, brushless heavy motor and electronic governor I work, and electronic governor II, minor spiral oar and brushless small machine quit work, such unmanned plane will consume less battery electric quantity when stagnant sky, reaches long-time stagnant sky and energy-conservation object.
For solving the problems of the technologies described above, the utility model relates to vehicle technology field, more specifically to a kind of can the energy-conservation unmanned plane of stagnant sky, comprise holster shell, battery, flight control desk, king bolt oar, brushless heavy motor, electronic governor I, support, electronic governor II, minor spiral oar, brushless small machine and supporting leg, improve the stagnant short side formula of unmanned plane, king bolt oar during stagnant sky, brushless heavy motor and electronic governor I work, and electronic governor II, minor spiral oar and brushless small machine quit work, such unmanned plane will consume less battery electric quantity when stagnant sky, reach long-time stagnant sky and energy-conservation object.
Battery is arranged on the inside of holster shell, and is positioned at the centre of holster shell.Flight control desk is arranged on the inside of holster shell, and is positioned at the upper end of holster shell.King bolt oar is arranged on brushless heavy motor, and is positioned at the upper end of brushless heavy motor.Brushless heavy motor is arranged on electronic governor I, and is positioned at the upper end of electronic governor I.Electronic governor I is fixed on the top of holster shell, and is positioned at the centre of holster shell.The inner of support is fixed in holster shell, and is positioned at the centre of holster shell.Electronic governor II is rack-mount, and is positioned at the centre of support.Minor spiral oar is arranged on brushless small machine, and is positioned at the upper end of brushless small machine.Brushless small machine is rack-mount, and is positioned at the outer end of support.Supporting leg is fixed in holster shell, and is positioned at the bottom of holster shell.
As the further optimization of the technical program, the utility model is a kind of can the material of the energy-conservation holster shell described in unmanned plane of stagnant sky be PVC.
As the further optimization of the technical program, the utility model is a kind of the energy-conservation king bolt oar described in unmanned plane of stagnant sky and minor spiral oar can be two-bladed porpeller.
As the further optimization of the technical program, the utility model is a kind of can the material of the energy-conservation support described in unmanned plane of stagnant sky be aluminum alloy.
As the further optimization of the technical program, the utility model is a kind of can the material of the energy-conservation supporting leg described in unmanned plane of stagnant sky be nylon.
As the further optimization of the technical program, the utility model is a kind of can be provided with four by the energy-conservation support described in unmanned plane, electronic governor II, minor spiral oar and the brushless small machine of stagnant sky, and symmetrical distribution.
The utility model is a kind of can the beneficial effect of the energy-conservation unmanned plane of stagnant sky be:
The utility model is a kind of can the energy-conservation unmanned plane of stagnant sky, improve the stagnant short side formula of unmanned plane, during stagnant sky, king bolt oar, brushless heavy motor and electronic governor I work, and electronic governor II, minor spiral oar and brushless small machine quit work, such unmanned plane will consume less battery electric quantity when stagnant sky, reaches long-time stagnant sky and energy-conservation object.
Accompanying drawing explanation
Below in conjunction with accompanying drawing and specific implementation method, the utility model is described in further detail.
Fig. 1 is that the utility model is a kind of can the structural representation of the energy-conservation unmanned plane of stagnant sky.
In figure: holster shell 1; Battery 2; Flight control desk 3; King bolt oar 4; Brushless heavy motor 5; Electronic governor I6; Support 7; Electronic governor II8; Minor spiral oar 9; Brushless small machine 10; Supporting leg 11.
Detailed description of the invention
Detailed description of the invention one:
Below in conjunction with Fig. 1, present embodiment is described, the utility model relates to vehicle technology field, more specifically to a kind of can the energy-conservation unmanned plane of stagnant sky, comprise holster shell 1, battery 2, flight control desk 3, king bolt oar 4, brushless heavy motor 5, electronic governor I6, support 7, electronic governor II8, minor spiral oar 9, brushless small machine 10 and supporting leg 11, improve the stagnant short side formula of unmanned plane, king bolt oar during stagnant sky, brushless heavy motor and electronic governor I work, and electronic governor II, minor spiral oar and brushless small machine quit work, such unmanned plane will consume less battery electric quantity when stagnant sky, reach long-time stagnant sky and energy-conservation object.
Battery 2 is arranged on the inside of holster shell 1, and is positioned at the centre of holster shell 1, and battery 2 is for providing power supply for unmanned plane.Flight control desk 3 is arranged on the inside of holster shell 1, and is positioned at the upper end of holster shell 1, and flight control desk 3 is for controlling the state of flight adjusting unmanned plane.King bolt oar 4 is arranged on brushless heavy motor 5, and is positioned at the upper end of brushless heavy motor 5.Brushless heavy motor 5 is arranged on electronic governor I6, and is positioned at the upper end of electronic governor I6.Electronic governor I6 is fixed on the top of holster shell 1, and is positioned at the centre of holster shell 1.King bolt oar 4, brushless heavy motor 5 and electronic governor I6 are used for making the long-time stagnant sky of unmanned plane in same position, and can save the electricity of battery 2.The inner of support 7 is fixed in holster shell 1, and is positioned at the centre of holster shell 1, and support 7, for increasing the distance between minor spiral oar 9, reduces interacting between the air-flow that produces when minor spiral oar 9 rotates.Electronic governor II8 is arranged on support 7, and is positioned at the centre of support 7, and electronic governor II8 is used for the size control signal of flight control desk 3 being changed into electric current, to control the rotating speed of brushless small machine 10.Minor spiral oar 9 is arranged on brushless small machine 10, and is positioned at the upper end of brushless small machine 10, and minor spiral oar 9 is for generation of lift upwards.Brushless small machine 10 is arranged on support 7, and is positioned at the outer end of support 7, and brushless small machine 10 has the advantage that volume is little, quality is light and the life-span is long, and cleaning is convenient.Supporting leg 11 is fixed in holster shell 1, and is positioned at the bottom of holster shell 1, and supporting leg 11 can play a protective role when unmanned plane lands.
Detailed description of the invention two:
Below in conjunction with Fig. 1, present embodiment is described; present embodiment is described further embodiment one; the material of described holster shell 1 is PVC; the good toughness of PVC; intensity is high; can the inner structure of available protecting unmanned plane, and the quality of PVC is light, cause burden can not to taking off of unmanned plane.
Detailed description of the invention three:
Below in conjunction with Fig. 1, present embodiment is described, present embodiment is described further embodiment one, described king bolt oar 4 and minor spiral oar 9 are two-bladed porpeller, and the impact rotating the sinuous flow of generation because of king bolt oar 4 and minor spiral oar 9 can drop to minimum by two-bladed porpeller.
Detailed description of the invention four:
Below in conjunction with Fig. 1, present embodiment is described, present embodiment is described further embodiment one, and the material of described support 7 is aluminum alloy, and the intensity of aluminum alloy is high, hardness large, can not be out of shape easily or rupture, and the quality of aluminum alloy is light.
Detailed description of the invention five:
Below in conjunction with Fig. 1, present embodiment is described, present embodiment is described further embodiment one, and the material of described supporting leg 11 is nylon, the good springiness of the supporting leg 11 that nylon makes, and toughness is high, effectively can resist impact when landing, protection unmanned plane.
Detailed description of the invention six:
Below in conjunction with Fig. 1, present embodiment is described, present embodiment is described further embodiment one, described support 7, electronic governor II8, minor spiral oar 9 and brushless small machine 10 are provided with four, and symmetrical distribution, symmetrical structure can ensure that unmanned plane flies reposefully.
Certain above-mentioned explanation is not limitation of the utility model; the utility model is also not limited only to above-mentioned citing; the change that those skilled in the art make in essential scope of the present utility model, remodeling, interpolation or replacement, also belong to protection domain of the present utility model.
Claims (6)
1. one kind can the energy-conservation unmanned plane of stagnant sky, comprise holster shell (1), battery (2), flight control desk (3), king bolt oar (4), brushless heavy motor (5), electronic governor I (6), support (7), electronic governor II (8), minor spiral oar (9), brushless small machine (10) and supporting leg (11), it is characterized in that: battery (2) is arranged on the inside of holster shell (1), and is positioned at the centre of holster shell (1); Flight control desk (3) is arranged on the inside of holster shell (1), and is positioned at the upper end of holster shell (1); King bolt oar (4) is arranged on brushless heavy motor (5), and is positioned at the upper end of brushless heavy motor (5); Brushless heavy motor (5) is arranged on electronic governor I (6), and is positioned at the upper end of electronic governor I (6); Electronic governor I (6) is fixed on the top of holster shell (1), and is positioned at the centre of holster shell (1); The inner of support (7) is fixed in holster shell (1), and is positioned at the centre of holster shell (1); Electronic governor II (8) is arranged on support (7), and is positioned at the centre of support (7); Minor spiral oar (9) is arranged on brushless small machine (10), and is positioned at the upper end of brushless small machine (10); Brushless small machine (10) is arranged on support (7), and is positioned at the outer end of support (7); Supporting leg (11) is fixed in holster shell (1), and is positioned at the bottom of holster shell (1).
2. according to claim 1 a kind of can the energy-conservation unmanned plane of stagnant sky, it is characterized in that: the material of described holster shell (1) is PVC.
3. according to claim 1 a kind of can the energy-conservation unmanned plane of stagnant sky, it is characterized in that: described king bolt oar (4) and minor spiral oar (9) are two-bladed porpeller.
4. according to claim 1 a kind of can the energy-conservation unmanned plane of stagnant sky, it is characterized in that: the material of described support (7) is aluminum alloy.
5. according to claim 1 a kind of can the energy-conservation unmanned plane of stagnant sky, it is characterized in that: the material of described supporting leg (11) is nylon.
6. according to claim 1 a kind of can the energy-conservation unmanned plane of stagnant sky, it is characterized in that: described support (7), electronic governor II (8), minor spiral oar (9) and brushless small machine (10) are provided with four, and symmetrical distribution.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520732693.3U CN205060005U (en) | 2015-09-21 | 2015-09-21 | Empty energy -conserving unmanned aerial vehicle can stagnate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520732693.3U CN205060005U (en) | 2015-09-21 | 2015-09-21 | Empty energy -conserving unmanned aerial vehicle can stagnate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205060005U true CN205060005U (en) | 2016-03-02 |
Family
ID=55386592
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520732693.3U Expired - Fee Related CN205060005U (en) | 2015-09-21 | 2015-09-21 | Empty energy -conserving unmanned aerial vehicle can stagnate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205060005U (en) |
-
2015
- 2015-09-21 CN CN201520732693.3U patent/CN205060005U/en not_active Expired - Fee Related
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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: 20160302 Termination date: 20160921 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |