CN213200165U - Single rotor unmanned aerial vehicle test platform - Google Patents
Single rotor unmanned aerial vehicle test platform Download PDFInfo
- Publication number
- CN213200165U CN213200165U CN202022118904.8U CN202022118904U CN213200165U CN 213200165 U CN213200165 U CN 213200165U CN 202022118904 U CN202022118904 U CN 202022118904U CN 213200165 U CN213200165 U CN 213200165U
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- test platform
- aerial vehicle
- unmanned aerial
- rotor unmanned
- single rotor
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Abstract
The utility model discloses a single rotor unmanned aerial vehicle test platform relates to the unmanned air vehicle technique field, including single rotor unmanned aerial vehicle organism, cupboard and test platform, last photoelectric revolution speed sensor and the force sensor of being equipped with of test platform, the inside of cupboard is equipped with the hydraulic pump. The utility model discloses a photoelectric speed sensor passes through infrared inductor response main rotor and whether passes through, again with information transfer for the tachometer through back infrared inductor, the number of times that the tachometer redisplayed passes through, single rotor unmanned aerial vehicle test platform has installed force sensor additional, be used for measuring and show the ascending production pulling force of single rotor unmanned aerial vehicle, the single rotor unmanned aerial vehicle who adorns can go up and down in test platform, driftage, whether the rudder volume of throttle and every steering wheel matches, whether the transmission can go on test such as between each gear.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a single rotor unmanned aerial vehicle test platform.
Background
The single-rotor unmanned aerial vehicle testing platform has no special structure principle, working principle, flight test and data statistics for testing the single-rotor unmanned aerial vehicle, can clearly understand the working principle and the construction principle of the single-rotor unmanned aerial vehicle through the single-rotor unmanned aerial vehicle testing platform, and can also safely and effectively carry out rotation speed test, flight test and tension test.
At present, single rotor unmanned aerial vehicle needs spacious and the less flight place of personnel of a slice at the test, need indoor and outdoor run back and forth when carrying out the flight test like this moreover, and is troublesome again time-consuming promptly.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a single rotor unmanned aerial vehicle test platform, give the tachometer with information transfer again through back infrared inductor, the number of times that the tachometer redisplayed passes through, single rotor unmanned aerial vehicle test platform has installed force sensor additional, be used for measuring and show the ascending production pulling force of single rotor unmanned aerial vehicle, the single rotor unmanned aerial vehicle that adorns can go up and down in test platform, driftage, whether the rudder volume of throttle and every steering wheel matches, whether the transmission can go on test such as go on between each gear, with the problem of proposing in solving above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a single-rotor unmanned aerial vehicle test platform comprises a single-rotor unmanned aerial vehicle body, a cabinet and a test platform, wherein the test platform is provided with a photoelectric rotating speed sensor and a tension sensor, and a hydraulic pump is arranged inside the cabinet;
the photoelectric rotation speed sensor comprises a rotation speed display meter and an infrared sensor, the rotation speed display meter is electrically connected with the infrared sensor, and the infrared sensor is arranged at the top of the test platform;
the tension sensor comprises a tension display meter and a tension rod, the upper end of the tension rod is connected to the bottom of the single-rotor unmanned aerial vehicle body, and the lower end of the tension rod is connected to the output end of the hydraulic pump.
Preferably, a display is mounted on the edge of the test platform.
Preferably, the top of the cabinet is provided with a frame through bolts, and the edge of the frame is provided with a protective net.
Preferably, an alarm is mounted on the photoelectric rotating speed sensor.
Preferably, a net door is installed on one side of the frame through a hinge, and a lock catch is installed on the net door.
Preferably, a reinforcing plate is welded between one side of the cabinet and the bottom of the test platform.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model discloses a photoelectric speed sensor passes through infrared inductor response main rotor and whether passes through, again with information transfer for the tachometer through back infrared inductor, the number of times that the tachometer redisplayed passes through, single rotor unmanned aerial vehicle test platform has installed force sensor additional, be used for measuring and show the ascending production pulling force of single rotor unmanned aerial vehicle, the single rotor unmanned aerial vehicle who adorns can go up and down in test platform, driftage, whether the rudder volume of throttle and every steering wheel matches, whether the transmission can go on test such as between each gear.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic side view of the cabinet of the present invention.
In the figure: 1. a cabinet; 2. a test platform; 3. a photoelectric rotation speed sensor; 4. a tension sensor; 5. a rotating speed display meter; 6. an infrared sensor; 7. a tension display meter; 8. a tension bar; 9. a hydraulic pump; 10. a single rotor unmanned aerial vehicle body; 11. a frame; 12. a protective net; 13. a display; 14. an alarm; 15. a net door; 16. a reinforcing plate.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-2, the present invention provides a technical solution: a single-rotor unmanned aerial vehicle test platform comprises a single-rotor unmanned aerial vehicle body 10, a cabinet 1 and a test platform 2, wherein a photoelectric rotating speed sensor 3 and a tension sensor 4 are arranged on the test platform 2, a hydraulic pump 9 is arranged inside the cabinet 1, and a reinforcing plate 16 is welded between one side of the cabinet 1 and the bottom of the test platform 2, so that the stability of the test platform 2 is improved;
the photoelectric rotating speed sensor 3 is divided into two parts, one is a rotating speed display meter 5, the other is an infrared sensor 6, the model is QT30CM, the high and low levels are output, a relay can be directly driven, a 1K pull-up resistor is added between a positive electrode and a signal, the IO port of a singlechip can be directly connected, the technical parameters comprise 1, voltage, DC5V and 2, current, 20mA and 3, effective distance, 2-30CM and 5, and size, 20 x 10 x 8MM, the infrared sensor 6 can sense whether a main rotor passes through or not, the infrared sensor feeds back to the rotating speed display meter 5 once, the rotating speed display meter 5 records average passing times per second or per minute, then the display 13 displays numbers, the display 13 is installed on the side part of the test platform 2, in addition, the photoelectric rotating speed sensor 3 is provided with an alarm 14, and alarms can be set when the rotating speed is lower than or higher than the rotating speed, the revolution indicator 5 is electrically connected with the infrared sensor 6, and the infrared sensor 6 is arranged at the top of the test platform 2.
The working principle is as follows: during the use, install single rotor unmanned aerial vehicle organism 10 at the output of hydraulic pump 9 through tension bar 8, infrared sensor 6 is through whether the response main rotor passes through, just feeds back to tachograph 5 once every time, and tachograph 5 notes on average how many times each second or minute passes through, then shows the figure on display 13, passes through back infrared sensor 6 again with information transfer to tachograph 5, and tachograph 5 shows the number of times that passes through again;
the tensile force that single rotor unmanned aerial vehicle ascended the production passes to tensile force display table 7 through the pull rod, and tensile force display table 7 is again with data conversion on display 13. The single-rotor unmanned aerial vehicle is used for measuring and displaying the lifting force generated by the single-rotor unmanned aerial vehicle.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a single rotor unmanned aerial vehicle test platform, includes single rotor unmanned aerial vehicle organism (10), cupboard (1) and test platform (2), its characterized in that: the test platform (2) is provided with a photoelectric rotating speed sensor (3) and a tension sensor (4), and a hydraulic pump (9) is arranged in the cabinet (1);
the photoelectric rotation speed sensor (3) comprises a rotation speed display meter (5) and an infrared sensor (6), the rotation speed display meter (5) is electrically connected with the infrared sensor (6), and the infrared sensor (6) is installed at the top of the test platform (2);
tension sensor (4) include that pulling force shows table (7) and pull rod (8), the upper end of pull rod (8) is connected in the bottom of single rotor unmanned aerial vehicle organism (10), the lower extreme of pull rod (8) is connected in the output of hydraulic pump (9).
2. The single-rotor drone test platform of claim 1, wherein: and a display (13) is arranged on the edge of the test platform (2).
3. The single-rotor drone test platform of claim 1, wherein: a frame (11) is installed at the top of the cabinet (1) through bolts, and a protective net (12) is installed at the edge of the frame (11).
4. The single-rotor drone test platform of claim 1, wherein: and an alarm (14) is arranged on the photoelectric rotating speed sensor (3).
5. A single-rotor drone test platform according to claim 3, wherein: one side of the frame (11) is provided with a net door (15) through a hinge, and the net door (15) is provided with a lock catch.
6. The single-rotor drone test platform of claim 1, wherein: a reinforcing plate (16) is welded between one side of the cabinet (1) and the bottom of the test platform (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022118904.8U CN213200165U (en) | 2020-09-24 | 2020-09-24 | Single rotor unmanned aerial vehicle test platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022118904.8U CN213200165U (en) | 2020-09-24 | 2020-09-24 | Single rotor unmanned aerial vehicle test platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213200165U true CN213200165U (en) | 2021-05-14 |
Family
ID=75822566
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022118904.8U Expired - Fee Related CN213200165U (en) | 2020-09-24 | 2020-09-24 | Single rotor unmanned aerial vehicle test platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213200165U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113716073A (en) * | 2021-11-02 | 2021-11-30 | 西安迈远科技有限公司 | Multi freedom unmanned aerial vehicle power test device |
-
2020
- 2020-09-24 CN CN202022118904.8U patent/CN213200165U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113716073A (en) * | 2021-11-02 | 2021-11-30 | 西安迈远科技有限公司 | Multi freedom unmanned aerial vehicle power test device |
| CN113716073B (en) * | 2021-11-02 | 2022-08-12 | 西安迈远科技有限公司 | Multi freedom unmanned aerial vehicle power test device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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: 20210514 Termination date: 20210924 |