CN219134531U - Unmanned aerial vehicle power device detecting system - Google Patents
Unmanned aerial vehicle power device detecting system Download PDFInfo
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- CN219134531U CN219134531U CN202320446571.2U CN202320446571U CN219134531U CN 219134531 U CN219134531 U CN 219134531U CN 202320446571 U CN202320446571 U CN 202320446571U CN 219134531 U CN219134531 U CN 219134531U
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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
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- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
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- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/40—Engine management systems
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Abstract
The utility model discloses a detection system of an unmanned aerial vehicle power device, which comprises an engine and an onboard oil tank, wherein the unmanned aerial vehicle power device comprises power device detection equipment and an oil circuit test board, the power device detection equipment is connected with the engine, the oil circuit test board is provided with an oil circuit input end and an oil circuit output end, the oil circuit input end is connected with the onboard oil tank, the oil circuit output end is connected with the engine, an oil circuit sensor assembly is arranged on a pipeline between the oil circuit input end and the oil circuit output end, and the oil circuit sensor assembly is connected with the power device detection equipment. According to the utility model, the power device detection equipment and the oil way test bench are configured to perform data detection, data transmission and visualization on the engine and the airborne oil tank of the unmanned aerial vehicle power device, so that the technical problem that a plurality of detection items are often independently performed in the detection means of the existing unmanned aerial vehicle power device, and the detection results cannot be summarized and checked quickly and conveniently is solved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle measurement and control, in particular to a detection system of an unmanned aerial vehicle power device.
Background
The power plant detector has the functions of full authority digital control and system detection of an aircraft power plant system and is used for detecting, controlling, debugging, fault positioning and isolating state parameters of the aircraft power plant system.
The detection means of the existing unmanned aerial vehicle power device often carries out a plurality of detection items independently, and the detection results cannot be summarized and checked rapidly and conveniently.
Disclosure of Invention
The utility model mainly aims to provide a detection system of an unmanned aerial vehicle power device, and aims to solve the technical problems that a plurality of detection items are often carried out independently in the detection means of the existing unmanned aerial vehicle power device, and the detection results cannot be summarized and checked quickly and conveniently.
In order to achieve the above purpose, the utility model provides a detection system of an unmanned aerial vehicle power device, wherein the unmanned aerial vehicle power device comprises an engine and an onboard oil tank, and the detection system of the unmanned aerial vehicle power device comprises power device detection equipment and an oil circuit test bench; wherein:
the power device detection equipment is connected with the engine and is used for sending a detection driving instruction to the engine so as to enable the engine to execute detection action;
the oil circuit test board is provided with an oil circuit input end and an oil circuit output end, the oil circuit input end is connected with the airborne oil tank, the oil circuit output end is connected with the engine, and an oil circuit sensor assembly is arranged on a pipeline between the oil circuit input end and the oil circuit output end and used for collecting oil circuit state information when the engine executes detection action;
the oil circuit sensor assembly is connected with the power device detection equipment and is used for sending the oil circuit state information to the power device detection equipment, so that the power device detection equipment can visualize the oil circuit state information when receiving the oil circuit state information.
Optionally, the unmanned aerial vehicle power device is still equipped with air flue steering wheel and/or air door steering wheel, when the engine carries out the detection action, drive air flue steering wheel and/or air door steering wheel operation.
Optionally, the power device detection equipment is connected with the air passage steering engine and/or the air door steering engine and is used for collecting the running state information of the air passage steering engine and/or the air door steering engine when the engine executes detection actions.
Optionally, the unmanned aerial vehicle power device is further provided with a cylinder temperature sensor, and the cylinder temperature sensor is connected with the power device detection equipment and is used for transmitting engine cylinder temperature information when the engine executes detection action to the power device detection equipment.
Optionally, the unmanned aerial vehicle power device is still equipped with the start-stop switch, start-stop switch connect the engine with power device check out test set for receive the start-stop instruction that power device check out test set sent, control start-stop when the engine carried out the detection action.
Optionally, a first oil pump is arranged on a pipeline between the onboard oil tank and the engine, and the first oil pump is connected with the power device detection equipment and is used for receiving a control instruction sent by the power device detection equipment and controlling the oil inlet amount when the engine executes the detection action.
Optionally, the oil circuit sensor assembly includes a first flow sensor and a first oil pressure sensor.
Optionally, the oil way test bench is further provided with a reserve oil tank, and the reserve oil tank is connected with the engine and is used for providing oil way input for the engine to execute ex-situ detection.
Optionally, a second oil pump, a second flow sensor and a second oil pressure sensor are sequentially arranged on a pipeline between the reserve oil tank and the engine; wherein:
the second oil pump is connected with the power device detection equipment and is used for receiving a control instruction sent by the power device detection equipment and controlling the oil inlet amount when the engine executes detection action;
the second flow sensor and the second oil pressure sensor are connected with the power device detection equipment and are used for sending oil path state information acquired by the second flow sensor and the second oil pressure sensor to the power device detection equipment, so that the power device detection equipment visualizes the oil path state information when receiving the oil path state information.
Optionally, the power device detection device further comprises an endoscope and a tachometer, wherein the endoscope and the tachometer are connected with the power device detection device, and are used for acquiring fault information when an engine fails and sending the fault information to the power device detection device.
The utility model provides a detection system of an unmanned aerial vehicle power device, which comprises an engine and an onboard oil tank, wherein the unmanned aerial vehicle power device comprises power device detection equipment and an oil circuit test board, the power device detection equipment is connected with the engine, the oil circuit test board is provided with an oil circuit input end and an oil circuit output end, the oil circuit input end is connected with the onboard oil tank, the oil circuit output end is connected with the engine, an oil circuit sensor assembly is arranged on a pipeline between the oil circuit input end and the oil circuit output end, and the oil circuit sensor assembly is connected with the power device detection equipment. According to the utility model, the power device detection equipment and the oil way test bench are configured to perform data detection, data transmission and visualization on the engine and the airborne oil tank of the unmanned aerial vehicle power device, so that the technical problem that a plurality of detection items are often independently performed in the detection means of the existing unmanned aerial vehicle power device, and the detection results cannot be summarized and checked quickly and conveniently is solved.
Drawings
FIG. 1 is a schematic diagram of a detection system for an unmanned aerial vehicle power device according to an embodiment of the present utility model;
fig. 2 is a schematic diagram of two configurations of a detection system for an unmanned aerial vehicle power device according to an embodiment of the present utility model.
Reference numerals illustrate:
10-an unmanned aerial vehicle power device; 101-an engine; 102-an onboard oil tank; 103-an airway steering engine; 104-an air door steering engine; 105-cylinder temperature sensor; 106-a start-stop switch; 20-power plant detection equipment; 30-an oil way test board; 301-an oil circuit input end; 302-an oil circuit output end; 303—an oil circuit sensor assembly; 304-a spare oil tank; 40-an endoscope; 50-tachometer.
The achievement of the objects, functional features and advantages of the present utility model will be further described with reference to the accompanying drawings, in conjunction with the embodiments.
Detailed Description
It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the scope of the utility model.
The technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are only some embodiments of the present utility model, not all embodiments. All other embodiments, based on the embodiments of the utility model, which would be apparent to one of ordinary skill in the art without inventive effort are within the scope of the utility model.
It should be noted that all directional indicators (such as up, down, left, right, front, and rear … …) in the embodiments of the utility model are merely used to explain the relative positional relationship, movement, etc. between the components in a particular posture (as shown in the drawings), and if the particular posture is changed, the directional indicators are changed accordingly.
In addition, the technical solutions of the embodiments may be combined with each other, but it is necessary that the technical solutions are based on the fact that the technical solutions can be realized by those skilled in the art, and when the technical solutions are contradictory or cannot be realized, the technical solutions should be considered that the combination does not exist and is not within the scope of protection claimed by the utility model.
Referring to fig. 1, fig. 1 is a schematic structural diagram of a detection system for an unmanned aerial vehicle power device according to an embodiment of the present utility model.
The embodiment provides an unmanned aerial vehicle power device detecting system, unmanned aerial vehicle power device 10 includes engine 101 and airborne oil tank 102, unmanned aerial vehicle power device detecting system includes power device check out test set 20 and oil circuit testboard 30.
In the present embodiment, the power plant detecting apparatus 20 is connected to the engine 101 for sending a detection driving instruction to the engine 101 to cause the engine 101 to perform a detection action; the oil circuit test board 30 is provided with an oil circuit input end 301 and an oil circuit output end 302, the oil circuit input end 301 is connected with the on-board oil tank, the oil circuit output end 302 is connected with the engine 101, and an oil circuit sensor assembly 303 is arranged on a pipeline between the oil circuit input end 301 and the oil circuit output end 302 and is used for collecting oil circuit state information when the engine 101 executes detection actions. The oil circuit sensor assembly 303 is connected to the power plant detection apparatus 20, and is configured to send the oil circuit state information to the power plant detection apparatus 20, so that the power plant detection apparatus 20 can visualize the oil circuit state information when receiving the oil circuit state information.
Further, the unmanned aerial vehicle power device 10 is further provided with an air passage steering engine 103 and/or an air door steering engine 104, and when the engine 101 executes the detection action, the air passage steering engine 103 and/or the air door steering engine 104 are driven to operate; the power device detection equipment 20 is connected with the air passage steering engine 103 and/or the air door steering engine 104, and is used for acquiring running state information of the air passage steering engine 103 and/or the air door steering engine 104 when the engine 101 executes detection actions.
Further, the unmanned aerial vehicle power device 10 is further provided with a cylinder temperature sensor 105, and the cylinder temperature sensor 105 is connected with the power device detecting apparatus 20 and is used for transmitting cylinder temperature information of the engine 101 to the power device detecting apparatus 20 when the engine 101 performs a detecting action.
Furthermore, the unmanned aerial vehicle power device 10 is further provided with a start-stop switch 106, and the start-stop switch 106 is connected with the engine 101 and the power device detection apparatus 20, and is configured to receive a start-stop instruction sent by the power device detection apparatus 20, and control start-stop of the engine 101 when executing a detection action.
Referring to fig. 2, fig. 2 is a schematic diagram of two configurations of a detection system for an unmanned aerial vehicle power device according to an embodiment of the present utility model.
In the present embodiment, the power plant detecting apparatus 20 is connected to the engine 101 for sending a detection driving instruction to the engine 101 to cause the engine 101 to perform a detection action; the oil circuit test board 30 is provided with an oil circuit input end 301 and an oil circuit output end 302, the oil circuit input end 301 is connected with the on-board oil tank, the oil circuit output end 302 is connected with the engine 101, and an oil circuit sensor assembly 303 is arranged on a pipeline between the oil circuit input end 301 and the oil circuit output end 302 and is used for collecting oil circuit state information when the engine 101 executes detection actions. The oil circuit sensor assembly 303 is connected to the power plant detection apparatus 20, and is configured to send the oil circuit state information to the power plant detection apparatus 20, so that the power plant detection apparatus 20 can visualize the oil circuit state information when receiving the oil circuit state information.
In comparison with the above embodiment, in this embodiment, a first oil pump is disposed in a pipeline between the on-board oil tank 102 and the engine 101, and the first oil pump is connected to the power plant detection device 20 and is configured to receive a control instruction sent by the power plant detection device 20, and control an oil intake amount when the engine performs a detection action.
Wherein the oil passage sensor assembly 303 includes a first flow sensor and a first oil pressure sensor; the oil path test bench 30 is further provided with a reserve oil tank 304, and the reserve oil tank 304 is connected with the engine 101 and is used for providing oil path input for the engine 101 to execute ex-situ detection.
In this embodiment, a second oil pump, a second flow sensor, and a second oil pressure sensor are sequentially provided in the line between the reserve tank 304 and the engine 101.
The second oil pump is connected to the power device detection apparatus 20, and is configured to receive a control instruction sent by the power device detection apparatus 20, and control an oil inlet amount when the engine 101 performs a detection action; the second flow sensor and the second oil pressure sensor are connected to the power unit detection device 20, and are configured to send the oil path status information collected by the second flow sensor and the second oil pressure sensor to the power unit detection device 20, so that the power unit detection device 20 visualizes the oil path status information when receiving the oil path status information.
In another embodiment, the system further comprises an endoscope 40 and a tachometer 50, wherein the endoscope 40 and the tachometer 50 are connected to the power plant detecting device 20 for acquiring fault information when the engine 101 fails and transmitting the fault information to the power plant detecting device 20.
The embodiment provides an unmanned aerial vehicle power device detecting system, through configuration power device check out test set 20 and oil circuit testboard 30, carries out data detection, data transmission and visualization to the engine 101 and the on-board oil tank 102 of unmanned aerial vehicle power device 10, has solved the detection means of current unmanned aerial vehicle power device 10 and often independently goes on with a plurality of detection items, and the detection result can not be swift, convenient gathers and looks over technical problem.
The foregoing description is only of the preferred embodiments of the utility model, and is not intended to limit the scope of the utility model, but rather is intended to cover any equivalent structure or equivalent flow scheme disclosed in the specification and drawings, or any other related art, directly or indirectly, as desired.
Claims (9)
1. The detection system of the unmanned aerial vehicle power device is characterized in that the unmanned aerial vehicle power device comprises an engine and an onboard oil tank, the unmanned aerial vehicle power device is also provided with an air passage steering engine and/or an air door steering engine, and when the engine executes detection action, the air passage steering engine and/or the air door steering engine are driven to run; the unmanned aerial vehicle power device detection system comprises power device detection equipment and an oil circuit test board; wherein:
the power device detection equipment is connected with the engine and is used for sending a detection driving instruction to the engine so as to enable the engine to execute detection action;
the oil circuit test board is provided with an oil circuit input end and an oil circuit output end, the oil circuit input end is connected with the airborne oil tank, the oil circuit output end is connected with the engine, and an oil circuit sensor assembly is arranged on a pipeline between the oil circuit input end and the oil circuit output end and used for collecting oil circuit state information when the engine executes detection action;
the oil circuit sensor assembly is connected with the power device detection equipment and is used for sending the oil circuit state information to the power device detection equipment, so that the power device detection equipment can visualize the oil circuit state information when receiving the oil circuit state information.
2. The unmanned aerial vehicle power device detection system of claim 1, wherein the power device detection apparatus is coupled to the airway steering engine and/or the damper steering engine for collecting operational status information of the airway steering engine and/or the damper steering engine when the engine performs the detection action.
3. The unmanned aerial vehicle power plant detection system of claim 1, wherein the unmanned aerial vehicle power plant is further provided with a cylinder temperature sensor, the cylinder temperature sensor being connected to the power plant detection apparatus for transmitting engine cylinder temperature information when the engine performs a detection action to the power plant detection apparatus.
4. The unmanned aerial vehicle power plant detection system of claim 1, wherein the unmanned aerial vehicle power plant is further provided with a start-stop switch, and the start-stop switch is connected with the engine and the power plant detection equipment and is used for receiving a start-stop instruction sent by the power plant detection equipment and controlling the start-stop of the engine when the engine executes the detection action.
5. The unmanned aerial vehicle power plant detection system of claim 1, wherein a first oil pump is arranged in a pipeline between the onboard oil tank and the engine, and the first oil pump is connected with the power plant detection equipment and is used for receiving a control instruction sent by the power plant detection equipment and controlling the oil inlet amount when the engine performs a detection action.
6. The unmanned aerial vehicle power device detection system of claim 1, wherein the oil circuit sensor assembly comprises a first flow sensor and a first oil pressure sensor.
7. The unmanned aerial vehicle power device inspection system of claim 1, wherein the oil circuit test stand is further provided with a reserve oil tank coupled to the engine for providing oil circuit input for the engine to perform ex-situ inspection.
8. The unmanned aerial vehicle power device detection system of claim 7, wherein a second oil pump, a second flow sensor, and a second oil pressure sensor are sequentially provided in the line between the reserve oil tank and the engine; wherein:
the second oil pump is connected with the power device detection equipment and is used for receiving a control instruction sent by the power device detection equipment and controlling the oil inlet amount when the engine executes detection action;
the second flow sensor and the second oil pressure sensor are connected with the power device detection equipment and are used for sending oil path state information acquired by the second flow sensor and the second oil pressure sensor to the power device detection equipment, so that the power device detection equipment visualizes the oil path state information when receiving the oil path state information.
9. The unmanned aerial vehicle power plant inspection system of claim 1, further comprising an endoscope and a tachometer coupled to the power plant inspection apparatus for obtaining fault information when an engine fails and transmitting the fault information to the power plant inspection apparatus.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320446571.2U CN219134531U (en) | 2023-03-10 | 2023-03-10 | Unmanned aerial vehicle power device detecting system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320446571.2U CN219134531U (en) | 2023-03-10 | 2023-03-10 | Unmanned aerial vehicle power device detecting system |
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| CN219134531U true CN219134531U (en) | 2023-06-06 |
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| CN202320446571.2U Active CN219134531U (en) | 2023-03-10 | 2023-03-10 | Unmanned aerial vehicle power device detecting system |
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| CN (1) | CN219134531U (en) |
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- 2023-03-10 CN CN202320446571.2U patent/CN219134531U/en active Active
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