CN218819587U - Oil ejector of airplane lubricating oil system - Google Patents
Oil ejector of airplane lubricating oil system Download PDFInfo
- Publication number
- CN218819587U CN218819587U CN202222960819.5U CN202222960819U CN218819587U CN 218819587 U CN218819587 U CN 218819587U CN 202222960819 U CN202222960819 U CN 202222960819U CN 218819587 U CN218819587 U CN 218819587U
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- China
- Prior art keywords
- oiling
- box
- lubricating oil
- grease squirt
- switch
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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
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model provides an aircraft lubricating oil system grease squirt, including the grease squirt box, the handle, the oil filler hole, the switch board, the oiling switch, the oiling pump, the oiling pipe, a flow sensor, the checkpost, pressure sensor, oiling nozzle and controller, the handle sets up on grease squirt box upper portion, the oil filler hole sets up on grease squirt box upper portion, the switch board sets up on the grease squirt box openly, oiling switch and circular telegram switch set up on the switch board, the oiling pump sets up lower part in the grease squirt box, the checkpost sets up on grease squirt box side, oiling pipe one end is connected with the oiling pump, its other end stretches out outside the grease squirt box and is provided with the oiling nozzle, flow sensor and pressure sensor set up inside the oiling pipe, the controller sets up on the grease squirt box openly. The aircraft lubricating oil system oil injector is simple in structure and convenient to operate and use, lubricating oil can be automatically injected into an aircraft lubricating oil system, the accuracy of the oil filling amount is ensured, the oil filling efficiency is improved, and the daily maintenance work of an aircraft is ensured.
Description
Technical Field
The utility model relates to an aircraft lubricating oil system technical field, in particular to aircraft lubricating oil system grease squirt.
Background
The aircraft lubricating oil system is one of important aircraft systems, lubricating oil in the system effectively lubricates a lubricating part of an aircraft engine through the lubricating system, and simultaneously takes away a large amount of heat generated by burning fuel oil and absorbed by a lubricated part, so that the engine can stably work at a certain working temperature, the safety and the stability of the aircraft engine are well guaranteed, and the flight safety of the aircraft is also guaranteed. The aircraft lubricating oil system is used for providing lubricating oil for lubricating, cooling and cleaning engine bearings and gears and mainly comprises a storage system, a distribution system, an indication system and the like, wherein the storage system is mainly used for keeping the lubricating oil and mainly comprises a lubricating oil tank. The currently used oil injector comprises an oil injection cavity, an oil pressing rod, a lubricating oil tank, an oil injection amount indicator and the like, and the oil injection rod is manually pushed to enable the lubricating oil to finish the oil injection process from the lubricating oil tank to the oil tank of the aircraft lubricating oil system. The mode mainly controls the oil filling amount through manual work, so that the oil filling amount is difficult to control, the oil filling time is long, the oil filling efficiency is low, and the normal maintenance work of the airplane is influenced.
SUMMERY OF THE UTILITY MODEL
The utility model discloses it is not enough above the solution to main objective, provides one kind can accurately provide aircraft lubricating system oil filler volume, improves the aircraft lubricating oil system oil ejector who refuels efficiency.
The utility model provides an aircraft lubricating oil system grease squirt, including the grease squirt box, the handle, the oil filler hole, the switch board, the oiling switch, the circular telegram switch, the oiling pump, the oiling pipe, a flow sensor, the checkpost, pressure sensor, oiling nozzle and controller, the handle sets up on grease squirt box upper portion, the oil filler hole sets up on grease squirt box upper portion, the switch board sets up on the grease squirt box openly, oiling switch and circular telegram switch set up on the switch board, the oiling pump sets up lower part in the grease squirt box, the checkpost sets up on grease squirt box side, oiling pipe one end is connected with the oiling pump, its other end stretches out outside the grease squirt box and is provided with the oiling nozzle, flow sensor and pressure sensor set up inside the oiling pipe, the controller sets up on the grease squirt box openly, the oiling switch, the circular telegram switch, the oiling pump, a flow sensor, pressure sensor and oiling nozzle pass through cable and controller electric connection.
Further, this aircraft lubricating oil system oil squirt still includes temperature sensor, and temperature sensor sets up on the oil squirt box inner wall, and temperature sensor passes through cable and controller electric connection.
Further, this aircraft lubricating oil system oil squirt still includes the display, and the display setting is on the right side of oil squirt box, and the display passes through cable and controller electric connection.
Further, this aircraft lubricating oil system oil squirt still includes level sensor, and level sensor sets up, and level sensor passes through cable and controller electric connection.
Further, the controller of the aircraft lubricating oil system oil injector is a single chip processor, an MCU processor or a PLC processor.
Compared with the prior art, the utility model discloses the beneficial technological effect who gains does: the oil injector for the aircraft lubricating oil system is simple in structure and convenient to operate and use, lubricating oil can be automatically injected into the aircraft lubricating oil system, the accuracy of the oil filling amount is ensured, the oil filling efficiency is improved, and the daily maintenance work of an aircraft is guaranteed. Moreover, the oiling pressure can be better monitored, the phenomenon that the oiling pressure is too high is avoided, the safety of the lubricating oil tank of the airplane is guaranteed, and the device is suitable for popularization and use.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a logic diagram of the present invention.
In the figure, 1, an oil lubricator tank; 2. a handle; 3. a display; 4. an oil filler; 5. a liquid level sensor; 6. a switch plate; 7. an oil filling switch; 8. a power-on switch; 9. an oil filling pump; 10. an oil filling pipe; 11. a flow sensor; 12. a temperature sensor; 13. a clip; 14. a pressure sensor; 15. an oil injection nozzle; 16. and a controller.
Detailed Description
The principles and features of the present invention are described below in conjunction with the following drawings, the examples given are only for explaining the present invention and are not intended to limit the scope of the present invention.
The utility model provides an aircraft lubricating oil system grease squirt, including grease squirt box 1, handle 2, oil filler hole 4, switch board 6, oiling switch 7, circular telegram switch 8, oiling pump 9, oiling pipe 10, flow sensor 11, checkpost 13, pressure sensor 14, oiling nozzle 15 and controller 16, handle 2 sets up on 1 upper portion of grease squirt box, oiling hole 4 sets up on 1 upper portion of grease squirt box, switch board 6 sets up on the grease squirt box 1 openly, oiling switch 7 and circular telegram switch 8 set up on switch board 6, oiling pump 9 sets up lower part in grease squirt box 1, checkpost 13 sets up on 1 side of grease squirt box, oiling pipe 10 one end is connected with oiling pump 9, its other end stretches out outside grease squirt box 1 and is provided with oiling nozzle 15, flow sensor 11 and pressure sensor 14 set up inside grease squirt pipe 10, controller 16 sets up on grease squirt box 1 openly, oiling switch 7, circular telegram switch 8, oiling pump 9, flow sensor 11, pressure sensor 14 and oiling nozzle 15 pass through cable and 16 electric connection with controller.
In order to monitor the temperature in the oil injector box body 1 in real time and improve the use reliability. The aircraft lubricating oil system lubricator further comprises a temperature sensor 12, the temperature sensor 12 is arranged on the inner wall of the lubricator box body 1, and the temperature sensor 12 is electrically connected with a controller 16 through a cable.
In order to observe the temperature and the oil injection flow and pressure in the oil injector box body 1 in real time, the service performance of the oil injector is improved. The aircraft lubricating oil system lubricator further comprises a display 3, the display 3 is arranged on the front face of the lubricator box body 1, and the display 3 is electrically connected with the controller 16 through a cable.
In order to monitor the oil amount in the oil injector box body 1 in real time and improve the applicability of the oil injector. The aircraft lubricating oil system oil injector further comprises a liquid level sensor 5, wherein the liquid level sensor 5 is arranged, and the liquid level sensor 5 is electrically connected with the controller 16 through a cable.
In order to satisfy various processors, the versatility is improved. The controller 16 of the aircraft lubricating oil system lubricator is a single chip processor, an MCU processor or a PLC processor.
The above description is only for the preferred embodiment of the present invention, and is not intended to limit the present invention, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention should be included within the protection scope of the present invention.
Claims (5)
1. An aircraft lubricating oil system grease squirt which characterized in that: aircraft lubricating oil system grease squirt includes grease squirt box (1), handle (2), oil filler hole (4), switch board (6), oiling switch (7), circular telegram switch (8), oiling pump (9), oiling pipe (10), flow sensor (11), checkpost (13), pressure sensor (14), pump nipple (15) and controller (16), handle (2) set up on grease squirt box (1) upper portion, oil filler hole (4) set up on grease squirt box (1) upper portion, switch board (6) set up on grease squirt box (1) openly, oiling switch (7) and circular telegram switch (8) set up on switch board (6), oiling pump (9) set up lower part in grease squirt box (1), checkpost (13) set up on grease squirt box (1) side, oiling pipe (10) one end is connected with oiling pump (9), and its other end stretches out outside grease squirt box (1) and is provided with pump nipple (15), flow sensor (11) and pressure sensor (14) set up in grease squirt box (10) inside electric switch (7), pump (8) control switch (7), pump (7) openly, the oil injection pump (9), the flow sensor (11), the pressure sensor (14) and the oil injection nozzle (15) are electrically connected with the controller (16) through cables.
2. An aircraft lubricating oil system lubricator as claimed in claim 1, wherein: the aircraft lubricating oil system lubricator further comprises a temperature sensor (12), the temperature sensor (12) is arranged on the inner wall of the lubricator box body (1), and the temperature sensor (12) is electrically connected with the controller (16) through a cable.
3. An aircraft lubrication oil system lubricator according to claim 1 or claim 2, wherein: the aircraft lubricating oil system lubricator further comprises a display (3), the display (3) is arranged on the front face of the lubricator box body (1), and the display (3) is electrically connected with the controller (16) through a cable.
4. An aircraft lubricating oil system lubricator according to claim 3, wherein: the aircraft lubricating oil system lubricator further comprises a liquid level sensor (5), wherein the liquid level sensor (5) is arranged, and the liquid level sensor (5) is electrically connected with the controller (16) through a cable.
5. An aircraft lubricating oil system lubricator according to claim 4, wherein: the controller (16) is a single chip processor, an MCU processor or a PLC processor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222960819.5U CN218819587U (en) | 2022-11-08 | 2022-11-08 | Oil ejector of airplane lubricating oil system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222960819.5U CN218819587U (en) | 2022-11-08 | 2022-11-08 | Oil ejector of airplane lubricating oil system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218819587U true CN218819587U (en) | 2023-04-07 |
Family
ID=87256133
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222960819.5U Active CN218819587U (en) | 2022-11-08 | 2022-11-08 | Oil ejector of airplane lubricating oil system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218819587U (en) |
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2022
- 2022-11-08 CN CN202222960819.5U patent/CN218819587U/en active Active
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