CN203669995U - Small engine supercharging device of unmanned aerial vehicle - Google Patents
Small engine supercharging device of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN203669995U CN203669995U CN201320769516.3U CN201320769516U CN203669995U CN 203669995 U CN203669995 U CN 203669995U CN 201320769516 U CN201320769516 U CN 201320769516U CN 203669995 U CN203669995 U CN 203669995U
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- CN
- China
- Prior art keywords
- supercharging device
- aerial vehicle
- unmanned aerial
- speed regulator
- engine supercharging
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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Abstract
The utility model discloses a small engine supercharging device of an unmanned aerial vehicle. The small engine supercharging device of the unmanned aerial vehicle mainly comprises five parts, namely a power source, a central controller, a speed regulator, a height sensor and an engine, wherein three lines are arranged on the central controller, the first line is connected with the power source, the second line is connected with the speed regulator, the third line is connected with the height sensor, and the line at the other end of the speed regulator is connected with the engine. The small engine supercharging device of the unmanned aerial vehicle is simple in structure, a CPU collects signals of the height sensor, the speed regulator is controlled to output current, so that the supercharging quantity of a turbocharger is controlled, and the power source is in charge of power supply of the entire system. The small engine supercharging device of the unmanned aerial vehicle has the advantages that when the small engine supercharging device is installed on a small aero-engine, the unmanned aerial vehicle can operate for a long time at high altitude and will not shut down after taking off at low altitude.
Description
Technical field
The utility model belongs to mechanical field, relates in particular to a kind of unmanned plane mini engine supercharging device.
Background technique
Motor applies to the every field such as aircraft, steamer, automobile, and it is most important for a national development, in China, the technology of motor need to improve, still exist some defects: such as, time service for a long time in the time of height operating mode frequent variations, fuel efficiency is not high, waste oil, and easily cause flame-outly, be in extreme danger, so, in order to make up these defects, motor is further carried out to technical improvement.
Model utility content
The purpose of this utility model is to overcome the deficiencies in the prior art, and a kind of fuelling rate that improves is provided, can be at high-altitude long-play but unmanned plane mini engine supercharging device that can be not flame-out.
The utility model takes following technological scheme to realize: a kind of unmanned plane mini engine supercharging device, it mainly comprises five parts, be respectively power supply, central control unit, speed regulator, height sensor and motor, on described central control unit, be provided with three-line, Article 1, connection power supply, Article 2 connection speed regulator, Article 3 connection height sensor, the other end connection motor of described speed regulator.
Brushless turbosupercharger is installed on described motor.
The utlity model has in sum following beneficial effect: the utility model system architecture is simple, CPU gathers height sensor signal, control speed regulator output current, thereby control the supercharging amount of turbosupercharger, power supply is responsible for the power supply of whole system, the utility model has the advantages that small aero aircraft is installed can be from low height above sea level takes off, at high-altitude long-play but can not stop working, better adapted to the variation of height height above sea level.
Accompanying drawing explanation
Fig. 1 is the utility model general structure schematic diagram.
Embodiment
As shown in Figure 1, a kind of unmanned plane mini engine supercharging device, it mainly comprises five parts, be respectively power supply, central control unit, speed regulator, height sensor and motor, on described central control unit, be provided with three-line, Article 1 connection power supply, Article 2 connection speed regulator, Article 3 connection height sensor, the other end connection motor of described speed regulator.
Embodiment: brushless turbosupercharger is installed on described motor, and CPU gathers height sensor signal, controls speed regulator output current, thereby controls the supercharging amount of turbosupercharger, and power supply is responsible for the power supply of whole system.
The above is embodiment of the present utility model, and the equivalence of doing according to structure, feature and principle described in the utility model application range therefore all changes or modifies, and is included in the utility model patent claim.
Claims (2)
1. a unmanned plane mini engine supercharging device, it mainly comprises five parts, be respectively power supply, central control unit, speed regulator, height sensor and motor, it is characterized in that: on described central control unit, be provided with three-line, Article 1, connection power supply, Article 2 connection speed regulator, Article 3 connection height sensor, the other end connection motor of described speed regulator.
2. unmanned plane mini engine supercharging device according to claim 1, is characterized in that: brushless turbosupercharger is installed on described motor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320769516.3U CN203669995U (en) | 2013-11-30 | 2013-11-30 | Small engine supercharging device of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320769516.3U CN203669995U (en) | 2013-11-30 | 2013-11-30 | Small engine supercharging device of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203669995U true CN203669995U (en) | 2014-06-25 |
Family
ID=50966304
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320769516.3U Expired - Fee Related CN203669995U (en) | 2013-11-30 | 2013-11-30 | Small engine supercharging device of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203669995U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107387232A (en) * | 2017-08-24 | 2017-11-24 | 武汉华伍航空科技有限公司 | A kind of electric duct supercharging device and boosting method for small-sized piston formula engine |
-
2013
- 2013-11-30 CN CN201320769516.3U patent/CN203669995U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107387232A (en) * | 2017-08-24 | 2017-11-24 | 武汉华伍航空科技有限公司 | A kind of electric duct supercharging device and boosting method for small-sized piston formula engine |
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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: ANHUI TIANLU AVIAT TECHNOLOGY CO., LTD. Free format text: FORMER NAME: HUAIBEI TIANLU AVIAT TECHNOLOGY CO., LTD. |
|
| CP01 | Change in the name or title of a patent holder |
Address after: 235000, F industrial building, Longhu Industrial Park, Huaibei Economic Development Zone, Anhui Province, No. 3, building 1-2 Patentee after: Anhui's aviation Polytron Technologies Inc Address before: 235000, F industrial building, Longhu Industrial Park, Huaibei Economic Development Zone, Anhui Province, No. 3, building 1-2 Patentee before: Huaibei City Tian Lu Aerotech Inc. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140625 Termination date: 20161130 |