Aero-engine test running lubricating oil filling device

By designing an oil filling device for aircraft engine test runs, a closed-loop transportation and filling system for oil was achieved, solving the problems of safety risks and low efficiency in the oil filling process and improving the production efficiency of the test stand.

CN119642069BActive Publication Date: 2025-12-26CHINA HANGFA SOUTH IND CO LTD
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Patent Information

Application Number
CN202411583414.1
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2024-11-07
Publication Date
2025-12-26
Estimated Expiration
2044-11-07

AI Technical Summary

Technical Problem

In the existing technology, there are safety risks, misoperation risks and low work efficiency problems when adding lubricating oil during the test of aero engines. In particular, when adding lubricating oil on the test stand, the lubricating oil is easy to splash and spill, which takes up space and takes a long time.

Method used

An oil filling device for aircraft engine test runs was designed, including an oil filtration cart, an oil filling mechanism, a mounting plate assembly under the test stand, an oil gun, a front gun holder mechanism, and a rear gun holder mechanism. The oil filtration cart filters the oil and delivers it to the oil gun through an oil supply pipe. The front and rear gun holder mechanisms support and limit the oil gun. The oil filling mechanism is integrated under the test stand to prevent the oil from being exposed to the external environment, thus achieving closed transportation and filling.

Benefits of technology

It eliminates splashing and spillage during lubricating oil transportation and filling, avoids safety risks, reduces the risk of misoperation, improves work efficiency, shortens working time, and enhances the production efficiency of the test bench.

✦ Generated by Eureka AI based on patent content.

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Abstract

The application discloses an aero-engine test running lubricating oil filling equipment, and belongs to the technical field of aero-engine test running, which comprises a lubricating oil filtering vehicle, the lubricating oil filtering vehicle comprises a lubricating oil tank and an oil conveying pipe, and the oil conveying pipe is used for connecting the lubricating oil filtering vehicle and an oil gun; the lubricating oil filling mechanism comprises a lower hanging bin, a curved vertical hose and a hard pipe, a front gun stock mechanism and a rear gun stock mechanism are used for supporting and limiting the oil gun, the oil gun is communicated with a first end of the curved vertical hose, and a second end of the curved vertical hose is communicated with the hard pipe. The lubricating oil filtering vehicle is used for filtering lubricating oil, the high-cleanliness lubricating oil is conveyed to the oil gun through the oil conveying pipe, the lubricating oil filling mechanism is used for supporting, limiting and storing the oil gun, the oil gun is convenient to take and use, the lubricating oil filling operation of the engine is facilitated, the limited operation space on the test bench is not occupied during the work of the test bench, the splashing and falling phenomenon of the lubricating oil during transportation and filling is eliminated, and the safety risk of the test bench caused by the lubricating oil filling is avoided.
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Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of aero-engine test running, in particular, to an aero-engine test running lubricating oil filling equipment. BACKGROUND

[0002] The information provided in this section is for the purpose of generally presenting the background of the application. To the extent that the descriptions in this section describe the work of the inventors, and to the extent that the descriptions in this section are not considered prior art by themselves or in combination with other prior art, they are not an admission that the work described belongs to the prior art.

[0003] When the aero-engine is tested on the test bed, the engine is first installed on the test bed of the test bed, and after the connection of various pipeline lines, the lubricating oil is filled.

[0004] The lubricating oil is a third-class flammable material, and for safety reasons, it is not allowed to directly store the oil tank containing lubricating oil and other containers on the test bed of the test bed. At the same time, due to the large number of test bed test related equipment and facilities on the test bed, the space on the test bed is usually not sufficient. Please refer to the attached drawings of the specification Figure 1 , which is a schematic diagram of the layout of the test bed in the prior art. At present, the lubricating oil is filled on the test bed, and the operator takes the lubricating oil from the test bed lubricating oil room, transports it to the outside of the test room, and then uses the manual oil tank to climb the test bed rack to fill the lubricating oil. Please refer to the attached drawings of the specification Figure 2 , which is a schematic diagram of the layout of the test bed in the prior art. The operator needs to climb the steel ladder of the test bed to operate.

[0005] At present, the lubricating oil is filled on the test bed, and the traditional manual lubricating oil tank is used to climb the test bed rack to fill the lubricating oil. There are several shortcomings:

[0006] 1. There is a safety risk. During the transportation and lubricating oil filling process, some lubricating oil will inevitably splash and fall on the test bed, and the lubricating oil remaining on the test bed will have a flammable safety risk;

[0007] 2. There is a risk of misoperation. When there is residual lubricating oil on the test bed, the operator may also fall due to the slippery surface of the test bed, and misoperate the equipment and facilities on the test bed;

[0008] 3. The working efficiency of lubricating oil filling is low. The operator needs to transport the lubricating oil from the test bed lubricating oil room to the test room door, and then lift it to the test bed to fill the lubricating oil. The operation time is long, the production efficiency is low, and the production efficiency of the test bed is restricted.

[0009] It should be noted that the information disclosed in the above background section is only used to enhance the understanding of the background of the present application, and therefore can include information that does not constitute prior art known to those skilled in the art. SUMMARY

[0010] In view of at least one of the above technical problems, the present application provides an aero-engine test run lubricating oil filling device, which can filter lubricating oil by a lubricating oil filtering vehicle, transport the lubricating oil with high cleanliness to an oil gun through an oil pipe, support and limit the oil gun by a lubricating oil filling mechanism, and conveniently take the oil gun to perform lubricating oil filling operation of the engine. The lubricating oil filling device does not occupy the limited working space on the test bench during the working period of the test bench, eliminates the splashing and falling phenomenon of the lubricating oil during transportation and filling, and avoids the safety risk caused by lubricating oil filling on the test bench.

[0011] According to an aspect of the present application, an aero-engine test run lubricating oil filling device is provided for transporting lubricating oil from a lubricating oil tank to a test room and filling the lubricating oil into an engine. The lubricating oil tank is isolated from the test room by a partition wall. The aero-engine test run lubricating oil filling device comprises a lubricating oil filtering vehicle, a lubricating oil filling mechanism, a test bench lower mounting plate assembly, an oil gun, a front gun stock mechanism, and a rear gun stock mechanism.

[0012] The lubricating oil filtering vehicle comprises a lubricating oil tank and an oil pipe. The oil pipe is used to connect the lubricating oil filtering vehicle and the oil gun. A coarse filter, a pump set, a three-stage fine filter, a pressure gauge, and an electromagnetic valve are sequentially arranged on the oil pipe. The coarse filter is used to coarsely filter the lubricating oil. The pump set is used to pressurize the lubricating oil in the oil pipe. The three-stage fine filter is used to perform three-stage filtration on the lubricating oil to improve the cleanliness of the lubricating oil.

[0013] The lubricating oil filling mechanism comprises a lower hanging bin, a curved soft tube, and a hard pipe. The lower hanging bin is arranged below the test bench surface. The lower hanging bin is used to mount the front gun stock mechanism and the rear gun stock mechanism. The front gun stock mechanism and the rear gun stock mechanism are used to support and limit the oil gun. The oil gun is connected with the first end of the curved soft tube. The second end of the curved soft tube is connected with the hard pipe. The hard pipe is arranged on the test bench lower mounting plate assembly. The other end of the hard pipe is connected with the oil pipe.

[0014] In some embodiments of the present application, the lubricating oil filling mechanism further comprises a cover plate. The cover plate is rotatably arranged on the test bench surface. The cover plate is used to shield the lower hanging bin. A limiting hole is arranged on the side wall of the lower hanging bin. The limiting hole is used to pass through the curved soft tube.

[0015] In some embodiments of the present application, the test bench lower mounting plate assembly comprises a mounting plate, a pipe joint, and a thin nut. The pipe joint is arranged on the mounting plate. The thin nut is used to cover the pipe joint and lock the pipe joint on the mounting plate. The mounting plate is arranged on the bottom of the test bench surface. An installation groove is arranged on the mounting plate. The installation groove is used to clamp and limit the pipe joint. The pipe joint is used to connect the curved soft tube and the hard pipe.

[0016] In some embodiments of the present application, the oil tank is provided with a filling port and a discharge port, and is provided with a liquid level gauge and a detection interface inside, the detection interface being used for externally connecting an online particle size detection device; the oil filter vehicle further comprises an overflow valve and a pressure regulating valve connected with the oil tank and the oil delivery pipe, the overflow valve being used for preventing overpressure of the oil delivery pipe, and the pressure regulating valve being used for regulating the output pressure by preset bypass pressure relief return through the oil delivery pipe.

[0017] In some embodiments of the present application, the front gun stock mechanism comprises a base, a telescopic rod assembly and a limiting support frame, the base being used for being mounted on the lower hanging bin bottom plate, the telescopic rod assembly being arranged on the base, and the limiting support frame being arranged on the top of the telescopic rod assembly, the telescopic rod assembly being used for driving the limiting support frame to lift and lower, and the limiting support frame being used for supporting the front barrel of the limiting oil gun.

[0018] In some embodiments of the present application, the front gun stock mechanism further comprises a clamping assembly, the limiting support frame comprises a limiting bottom plate and limiting side plates, the limiting side plates being arranged at both sides of the limiting bottom plate, and the clamping assembly comprising a clamping piece, the middle part of the clamping piece being hinged to the top of the inner wall of the limiting side plate, and the clamping pieces at both sides of the limiting bottom plate being used for clamping and limiting both sides of the front barrel of the oil gun.

[0019] In some embodiments of the present application, the front gun stock mechanism further comprises a pushing assembly, a rotating assembly, a first shielding piece and a second shielding piece, the rotating assembly being provided with two groups, the two groups of rotating assemblies being respectively hinged to the outer walls of the limiting side plates at both sides, the pushing assembly being movably arranged on the limiting side plate, the first end of the pushing assembly being hinged to the bottom of the clamping piece, the second end of the pushing assembly being hinged to the bottom of the rotating assembly, the first shielding piece being connected to the top of the rotating assembly at one side, the second shielding piece being connected to the top of the rotating assembly at the other side, and both sides of the clamping piece being used for being pressed downward by the front barrel to rotate, so as to drive both sides of the pushing assembly to move outward along the vertical direction of the limiting side plate synchronously, and then drive both sides of the rotating assembly to rotate to drive the first shielding piece and the second shielding piece to abut and close respectively and shield and protect the inlet of the front barrel.

[0020] In some embodiments of the present application, the pushing assembly comprises a pushing rod, a first compression spring and a spring connecting plate, the rotating assembly comprises a rotating plate and a supporting plate, the supporting plate being arranged on the top of the outer wall of the limiting side plate, the middle part of the rotating plate being hinged to the tail end of the supporting plate, the spring connecting plate being arranged on the bottom of the rotating plate, the pushing rod being movably arranged on the limiting side plate, the first compression spring being sleeved on the pushing rod, and the first end of the first compression spring being connected with the spring connecting plate and the second end of the first compression spring being connected with the side wall of the limiting side plate.

[0021] In some embodiments of the present application, the first shielding member and the second shielding member are both semicircular plate structures and are used to fold to form a circular shielding plate, the outer side of the first shielding member is provided with a first arc-shaped plate, the outer side of the second shielding member is provided with a second arc-shaped plate, the second arc-shaped plate is used to enclose the first arc-shaped plate and the shielding plate to form a limiting cavity, and the limiting cavity is used to shield and protect the front barrel of the oil gun.

[0022] In some embodiments of the present application, the rear stock mechanism includes a stock bottom plate, side support plates, a tail wall and a plurality of safety pins, the stock bottom plate is used to be fixed on the bottom plate of the lower hanging bin, the side support plates are arranged on both sides of the stock bottom plate, the tail wall is arranged on the stock bottom plate and has an included angle with the stock bottom plate, the tail wall is used to be connected with the bottom of the side support plates on both sides, a plurality of safety holes are arranged on the side support plates, and the plurality of safety pins are used to pass through the safety holes respectively to clamp the trigger of the oil gun.

[0023] The present application has the following beneficial effects:

[0024] The aero-engine test running oil filling equipment of the present application filters the oil through the oil filter vehicle to obtain high-cleanliness oil, which is transported to the oil gun through the oil conveying pipe, supports and installs the front stock mechanism and the rear stock mechanism through the lower hanging bin of the oil filling mechanism, supports and limits the oil gun through the front stock mechanism and the rear stock mechanism, and sets the lower hanging bin below the test bench platform to shield and protect the front stock mechanism and the rear stock mechanism and realize the storage of the oil gun, which is convenient for taking and using the oil gun to fill the oil of the engine. When the oil is not needed to be filled, i.e. during the operation of the test bench, the limited operation space on the platform is not occupied. The present application eliminates the splashing and falling phenomenon of the oil during transportation and filling, avoids the safety risk caused by the oil filling on the test bench, the oil transportation and filling are carried out in the closed pipeline and device, and the safety risk is not caused by the exposure to the external environment. The oil filling equipment is integrated in the test bench platform, does not occupy the limited space on the test bench, and does not cause the misoperation risk. The oil filling is convenient, fast and efficient, does not need to occupy too much test bench operation time, shortens the working time of the process, and improves the production efficiency of the test bench.

[0025] Of course, it is not necessary to achieve all the advantages described above when implementing any product of the present application. In addition to the purposes, features and advantages described above, the present application has other purposes, features and advantages. The present application will be further described below with reference to the drawings. BRIEF DESCRIPTION OF DRAWINGS

[0026] The drawings constituting a part of the present application are used to provide further understanding of the present application, the schematic embodiments of the present application and the description thereof are used to explain the present application and do not constitute improper limitations on the present application. In the drawings:

[0027] Figure 1 is a schematic diagram of a test bench layout in the prior art;

[0028] Figure 2 is a schematic diagram of a test bench layout in the prior art;

[0029] Figure 3 is a schematic diagram of the overall layout of the preferred embodiment of the application;

[0030] Figure 4 is a schematic diagram of the internal structure of the oil filter vehicle of the preferred embodiment of the application;

[0031] Figure 5 is a schematic diagram of the structure of the oil filling mechanism of the preferred embodiment of the application;

[0032] Figure 6 is a schematic diagram of the structure of the rear stock mechanism of the preferred embodiment of the application;

[0033] Figure 7 is a schematic diagram of the structure of the side support plate of the preferred embodiment of the application;

[0034] Figure 8 is a schematic diagram of the structure of the under bench mounting plate assembly of the preferred embodiment of the application;

[0035] Figure 9 is a schematic diagram of the structure of the mounting plate of the preferred embodiment of the application;

[0036] Figure 10 is a schematic diagram of the installation of the pipe joint of the preferred embodiment of the application;

[0037] Figure 11 is a schematic diagram of the structure of the front stock mechanism of the preferred embodiment of the application;

[0038] Figure 12 is a schematic diagram of the installation of the detent of the preferred embodiment of the application;

[0039] Figure 13 is a schematic diagram of the installation of the first and second shielding members of the preferred embodiment of the application;

[0040] Figure 14 is a schematic diagram of the structure of the pushing assembly of the preferred embodiment of the application;

[0041] Legend: 100, aero-engine; 101, oil port; 200, oil filter vehicle; 201, oil tank; 2011, oil filling port; 2012, blowdown port; 2013, liquid level gauge; 202, coarse filter; 203, pump group; 204, overflow valve; 205, pressure regulating valve; 206, three-stage fine filter; 207, pressure gauge; 208, flow meter; 209, solenoid valve; 210, oil delivery pipe; 300, oil filling mechanism; 301, lower hanging bin; 302, cover plate; 303, curved flexible hose; 304, rigid pipe; 305, wall penetrating connector; 400, under-rack mounting plate assembly; 401, mounting plate; 4011, mounting groove; 402, pipe connector; 403, thin nut; 1, oil gun; 2, front stock mechanism; 21, base; 22, telescopic rod assembly; 221, telescopic inner rod; 222, telescopic outer rod; 23, pushing assembly; 231, pushing rod; 232, first compression spring; 233, spring connecting plate; 24, limiting support frame; 241, limiting bottom plate; 242, limiting side plate; 25, clamping assembly; 251, clamping piece; 2511, limiting boss; 26, rotating assembly; 261, rotating plate; 262, support plate; 27, first shielding piece; 271, first arc-shaped plate; 272, shielding platform; 28, second shielding piece; 281, second arc-shaped plate; 29, second compression spring; 3, rear stock mechanism; 31, stock bottom plate; 32, side support plate; 33, tail wall; 34, safety hole; 35, safety pin. DETAILED DESCRIPTION

[0042] The embodiments of the present application are described in detail below with reference to the accompanying drawings, but the present application can be implemented in various different ways as defined and covered by the following.

[0043] Figure 1 is a schematic diagram of the layout of a test bench in the prior art; Figure 2 is a schematic diagram of the layout of a test bench in the prior art; Figure 3 is a schematic diagram of the overall layout of the preferred embodiment of the present application; Figure 4 is a schematic diagram of the internal structure of the oil filter vehicle of the preferred embodiment of the present application; Figure 5 is a schematic diagram of the structure of the oil filling mechanism of the preferred embodiment of the present application; Figure 6 is a schematic diagram of the structure of the rear stock mechanism of the preferred embodiment of the present application; Figure 7 is a schematic diagram of the structure of the side support plate of the preferred embodiment of the present application; Figure 8 is a schematic diagram of the structure of the under-rack mounting plate assembly of the preferred embodiment of the present application; Figure 9 is a schematic diagram of the structure of the mounting plate of the preferred embodiment of the present application;

[0044] Figure 10 is a schematic diagram of the installation of the pipe connector of the preferred embodiment of the present application; Figure 11is a structural schematic diagram of a front stock mechanism of a preferred embodiment of the present application; Figure 12 is an installation schematic diagram of a detent of a preferred embodiment of the present application;

[0045] Figure 13 is an installation schematic diagram of a first shielding member and a second shielding member of a preferred embodiment of the present application; Figure 14 is a structural schematic diagram of a pushing assembly of a preferred embodiment of the present application.

[0046] An aero-engine test run lubricating oil filling device is used for transporting lubricating oil between lubricating oil and filling into an engine 100, and the lubricating oil is isolated from the test run room by a partition wall. The aero-engine test run lubricating oil filling device comprises a lubricating oil filtering vehicle 200, a lubricating oil filling mechanism 300, a bench lower mounting plate assembly 400, an oil gun 1, a front stock mechanism 2 and a rear stock mechanism 3.

[0047] The lubricating oil filtering vehicle 200 comprises a lubricating oil tank 201 and an oil conveying pipe 210, the oil conveying pipe 210 is used for connecting the lubricating oil filtering vehicle 200 and the oil gun 1, and a coarse filter 202, a pump set 203, a three-stage fine filter 206, a pressure gauge 207 and a solenoid valve 209 are sequentially arranged on the oil conveying pipe 210. The coarse filter 202 is used for coarsely filtering the lubricating oil, the pump set 203 is used for pressurizing the lubricating oil in the oil conveying pipe 210, and the three-stage fine filter 206 is used for three-stage filtering the lubricating oil to improve the cleanliness of the lubricating oil.

[0048] The lubricating oil filling mechanism 300 comprises a lower hanging bin 301, a curved vertical hose 303 and a hard pipe 304. The lower hanging bin 301 is arranged below the test run bench surface, and is used for mounting the front stock mechanism 2 and the rear stock mechanism 3. The front stock mechanism 2 and the rear stock mechanism 3 are used for supporting and limiting the oil gun 1. The oil gun 1 is connected with the first end of the curved vertical hose 303, the second end of the curved vertical hose 303 is connected with the hard pipe 304, the hard pipe 304 is arranged on the bench lower mounting plate assembly 400, and the other end of the hard pipe 304 is connected with the oil conveying pipe 210.

[0049] Here, the oil conveying pipe 210 needs to pass through the partition wall to connect the lubricating oil filtering vehicle 200 and the oil gun 1. In some embodiments, a wall-penetrating connecting pipe 305 is arranged on the partition wall, one end of the wall-penetrating connecting pipe 305 is connected with the oil conveying pipe 210 and the other end is connected with the hard pipe 304, so as to realize the connection between the lubricating oil tank 201 and the oil gun 1.

[0050] Here, the flow meter 208 reflects the flow signal output at the end of the oil conveying pipe 210 to the test run bench control system, and the lubricating oil filtering vehicle 200 is controlled by the control system, so as to meet the quantitative filling of the lubricating oil of the engine 100 by the operator. The solenoid valve 209 at the end mainly plays a role of switching on and off. When the control system transmits a stop signal, the solenoid valve 209 acts together with the pump set 203 to close the oil conveying pipe 210.

[0051] The aero-engine test run lubricating oil filling equipment of the application filters the lubricating oil through the lubricating oil filtering vehicle 200 to obtain high-cleanliness lubricating oil, which is delivered to the oil gun 1 through the oil delivery pipe 210, and the front gun stock mechanism 2 and the rear gun stock mechanism 3 are supported and installed through the lower hanging bin 301 of the lubricating oil filling mechanism 300, the oil gun 1 is supported and limited by the front gun stock mechanism 2 and the rear gun stock mechanism 3, the lower hanging bin 301 is arranged below the test bench platform surface, the front gun stock mechanism 2 and the rear gun stock mechanism 3 can be shielded and protected, and the oil gun 1 can be stored, which is convenient for the lubricating oil filling operation of the engine 100, and the limited operation space on the platform is not occupied during the test bench operation when the lubricating oil is not needed to be filled. The application eliminates the splashing and falling phenomenon of the lubricating oil during transportation and filling, avoids the safety risk caused by the lubricating oil filling on the test bench, the lubricating oil transportation and filling are carried out in the closed pipeline and device, and the safety risk is not caused by being exposed to the external environment; the lubricating oil filling equipment is integrated in the test bench platform, the limited space on the test bench is not occupied, and the misoperation risk is not caused; the lubricating oil filling is convenient, fast and efficient, the test bench operation time is not occupied, the working time of the process is shortened, and the production efficiency of the test bench is improved.

[0052] Preferably, as shown in Figure 5 The lubricating oil filling mechanism 300 further includes a cover plate 302, which is rotatably arranged on the test bench platform surface, and is used for shielding the lower hanging bin 301. The sidewall of the lower hanging bin 301 is provided with a limiting perforation, and the curved and vertical hose 303 is arranged through the limiting perforation.

[0053] It can be understood that the lower hanging bin 301 can support and install the front gun stock mechanism 2 and the rear gun stock mechanism 3, and store and protect the oil gun 1. The lubricating oil filling mechanism 300 is integrated below the test bench platform surface of the test bench in the test bench, and the lubricating oil filling mechanism 300 and the oil gun 1 do not occupy the limited operation space on the platform during the test bench operation after the cover plate 302 is covered.

[0054] Preferably, as shown in Figure 8 , 9 , and 10, the platform lower mounting plate assembly 400 includes a mounting plate 401, a pipe joint 402 and a thin nut 403. The pipe joint 402 is arranged through the mounting plate 401, the thin nut 403 is used for sleeving the pipe joint 402 and locking and limiting the pipe joint 402 on the mounting plate 401, the mounting plate 401 is arranged on the bottom of the test bench platform surface, the mounting plate 401 is provided with a mounting groove 4011, the mounting groove 4011 is used for clamping and limiting the pipe joint 402, and the pipe joint 402 is used for connecting the curved and vertical hose 303 and the hard pipe 304.

[0055] It can be understood that the pipe joint 402 is communicated with the curved and vertical hose 303 at one end and communicated with the hard pipe 304 at the other end, plays a supporting role of connecting the upper and lower parts, is beneficial to disperse the pressure of the pipeline, and is convenient for maintenance and replacement of the pipeline. The pipe joint 402 can be limited through the mounting groove 4011, and the pipe joint 402 can be conveniently locked on the mounting plate 401 through the thin nut 403, so that the pipe joint 402 can be quickly disassembled and assembled through the thin nut 403.

[0056] Optionally, a flat square is provided on the pipe joint 402, which can be clamped into the mounting groove 4011 to play a role of strengthening the limiting effect.

[0057] Preferably, as shown in Figure 3 , 4 The oil tank 201 is provided with a filling port 2011 and a pollution discharge port 2012, and is provided with a liquid level gauge 2013 and a detection interface in the oil tank 201, and the detection interface is used for external connection of an online particle size detection device; the oil filter vehicle 200 further comprises an overflow valve 204 and a pressure regulating valve 205 connected with the oil tank 201 and the oil delivery pipe 210, the overflow valve 204 is used for preventing overpressure of the oil delivery pipe 210, and the pressure regulating valve 205 is used for preset bypass pressure relief return through the oil delivery pipe 210 to adjust the output pressure.

[0058] It can be understood that the oil tank 201 is provided with a filling port 2011, a liquid level gauge 2013, a pollution discharge port 2012 and an online particle size detection device interface, which can realize the functions of oil loading and discharging.

[0059] It should be noted that the oil filter vehicle 200 is designed as a vehicle-mounted structure, and the output end cooperates with the oil delivery pipe 210 to realize one machine with multiple uses, which can be placed in the oil tank of the test bench according to the demand and used for different test benches.

[0060] Preferably, as shown in Figures 11-14 The front gun stock mechanism 2 comprises a base 21, a telescopic rod assembly 22 and a limiting support frame 24, the base 21 is used for being arranged on the bottom plate of the lower hanging bin 301, the telescopic rod assembly 22 is arranged on the base 21, and the limiting support frame 24 is arranged on the top of the telescopic rod assembly 22. The telescopic rod assembly 22 is used for driving the limiting support frame 24 to ascend and descend, and the limiting support frame 24 is used for supporting the front barrel of the limiting oil gun 1.

[0061] Specifically, the front gun stock mechanism 2 further comprises a clamping assembly 25, the limiting support frame 24 comprises a limiting bottom plate 241 and limiting side plates 242, the limiting side plates 242 are arranged at two sides of the limiting bottom plate 241, and the clamping assembly 25 comprises a clamping piece 251, the middle part of the clamping piece 251 is hinged to the top of the inner wall of the limiting side plate 242, and the clamping pieces 251 at two sides of the limiting bottom plate 241 are used for clamping and limiting two sides of the front barrel of the oil gun 1.

[0062] It can be understood that the elevatable limiting support frame 24 can be used to support and limit the front barrel of the oil gun 1, facilitating the taking and storing of the oil gun 1. In order to enhance the limiting stability of the front barrel, the clamping members 251 hinged on the limiting side plates 242 are used to press and limit the front barrel, ensuring the stability of the limiting and avoiding the front barrel from falling off and other phenomena.

[0063] Optionally, the telescopic rod assembly 22 comprises a telescopic inner rod 221 and a telescopic outer rod 222, the telescopic outer rod 222 being telescopically sleeved outside the telescopic inner rod 221 and being lockable and fixed by a locking nut.

[0064] Optionally, the clamping member 251 is an arc-shaped plate structure, and the upper portion of the clamping member 251 is provided with a limiting boss 2511 for limiting the top of the front barrel after the front barrel is clamped into the middle of the clamping members 251 on both sides. The clamping member 251 is hinged to the limiting side plate 242 through a torsional spring.

[0065] Preferably, as shown in Figures 11-14 The front stock mechanism 2 further comprises a pushing assembly 23, two rotating assemblies 26, a first shielding member 27 and a second shielding member 28. The two rotating assemblies 26 are hinged to the outer walls of the limiting side plates 242 on both sides, respectively. The pushing assembly 23 is movably arranged on the limiting side plate 242. The first end of the pushing assembly 23 is hinged to the bottom of the clamping member 251, and the second end of the pushing assembly 23 is hinged to the bottom of the rotating assembly 26. The first shielding member 27 is connected to the top of the rotating assembly 26 on one side, and the second shielding member 28 is connected to the top of the rotating assembly 26 on the other side. The clamping members 251 on both sides are used to be pressed downward by the front barrel to rotate, so as to drive the pushing assemblies 23 on both sides to move outward along the vertical direction of the limiting side plate 242 synchronously, and then drive the rotating assemblies 26 on both sides to rotate, so as to drive the first shielding member 27 and the second shielding member 28 to abut and close, respectively, and shield and protect the inlet of the front barrel.

[0066] Specifically, the pushing assembly 23 comprises a pushing rod 231, a first compression spring 232 and a spring connecting plate 233. The rotating assembly 26 comprises a rotating plate 261 and a supporting plate 262. The supporting plate 262 is arranged on the top of the outer wall of the limiting side plate 242. The middle portion of the rotating plate 261 is hinged to the tail end of the supporting plate 262. The spring connecting plate 233 is arranged on the bottom of the rotating plate 261. The pushing rod 231 is movably arranged on the limiting side plate 242. The first compression spring 232 is sleeved on the pushing rod 231, and the first end of the first compression spring 232 is connected to the spring connecting plate 233. The second end of the first compression spring 232 is connected to the side wall of the limiting side plate 242.

[0067] It can be understood that when the front barrel is inserted into the middle of the clamping members 251 on both sides, the bottom of the clamping member 251 is pressed down to rotate around the hinge point, the bottom of the clamping member 251 drives the push rod 231 to move outward along the vertical direction of the limiting side plate 242, and then the bottom of the rotating plate 261 is driven to rotate, so that the first shielding member 27 and the second shielding member 28 are brought together to shield and protect the front barrel, prevent foreign matter from falling into the front barrel to affect the cleanliness of the oil, and avoid affecting the subsequent test run of the engine 100.

[0068] The first compression spring 232 sleeved on the push rod 231 is used to provide an elastic force for pulling the bottom of the rotating plate 261 close to the limiting side plate 242, that is, to reset the rotating plate 261 and the clamping member 251 after the front barrel is removed.

[0069] Optionally, the top of the rotating plate 261 on both sides is connected to the outside of the first shielding member 27 and the second shielding member 28 through the second compression spring 29, and the second compression spring 29 can play a role of elastic buffering to reduce the impact and damage between the first shielding member 27 and the second shielding member 28.

[0070] Preferably, as shown in Figure 13 , 14 The first shielding member 27 and the second shielding member 28 are both semicircular plate structures and are used to fold to form a circular shielding plate, the outside of the first shielding member 27 is provided with a first arc-shaped plate 271, and the outside of the second shielding member 28 is provided with a second arc-shaped plate 281, the second arc-shaped plate 281 is used to enclose a limiting cavity with the first arc-shaped plate 271 and the shielding plate, and the limiting cavity is used to shield and protect the front barrel of the oil gun 1.

[0071] It can be understood that the second arc-shaped plate 281, the first arc-shaped plate 271, and the first shielding member 27 and the second shielding member 28 that are brought together form a cylindrical structure and form a limiting cavity inside to shield and protect the front barrel. Because the clamping members 251 on both sides are symmetrically inclined, it is convenient to realize the clamping and limiting of the front barrel, the first shielding member 27 and the second shielding member 28 are in a state of moving away before the front barrel is placed, and after the front barrel is clamped into the clamping members 251 on both sides, the first shielding member 27 and the second shielding member 28 are brought together by the push assembly 23 and the rotating assembly 26, that is, the clamping and limiting of the front barrel and the shielding protection of the barrel port are realized at one time, and the operation is very simple and intuitive.

[0072] Optionally, the side wall of the first shielding member 27 is provided with a shielding platform 272, which is used to fit the side wall of the second shielding member 28 when the second shielding member 28 is butted with the first shielding member 27, so as to shield and seal the butt joint gap between the second shielding member 28 and the first shielding member 27, and reduce the dust impurities from entering the limiting cavity through the gap.

[0073] Preferably, as shown in Figure 6 、 7 The rear stock mechanism 3 includes a stock bottom plate 31, side support plates 32, a tail wall 33 and a plurality of safety pins 35. The stock bottom plate 31 is used to be fixed on the bottom plate of the lower hanging bin 301. The side support plates 32 are arranged on both sides of the stock bottom plate 31. The tail wall 33 is arranged on the stock bottom plate 31 and has an included angle with the stock bottom plate 31. The tail wall 33 is used to be connected with the bottom of the side support plates 32 on both sides. A plurality of safety holes 34 are arranged on the side support plates 32. The plurality of safety pins 35 are used to pass through the respective safety holes 34 to clamp the trigger of the oil gun 1.

[0074] It can be understood that the rear stock mechanism 3 cooperates with the front stock mechanism 2 to support and limit the oil gun 1, and keep the front barrel oriented and clamped. The stock bottom plate 31 is fixed in the lower hanging bin 301, and the inner side of the stock bottom plate 31 mainly plays a role in supporting the bottom of the oil gun 1. The distance between the side support plates 32 on both sides is set to be 2-3mm larger than the width of the oil gun 1, which facilitates the placement of the oil gun 1 and clamps the oil gun 1 through the side support plates 32 on both sides to prevent the oil gun 1 from tilting left and right. The side support plates 32 are provided with a plurality of safety holes 34. The safety pins 35 are inserted into the safety holes 34, which can lock the oil gun 1 and clamp the trigger of the oil gun 1 to avoid the risk of oil spouting caused by misoperation. The tail wall 33 supports the rear side of the protective edge of the oil gun trigger. The oil inlet hose of the oil gun 1 passes through the upper end of the tail wall 33 and is communicated with the vertically curved hose 303 through the limiting perforation of the lower hanging bin 301.

[0075] In summary, the device has strong practicability, simple and convenient operation and equipment management, and simple maintenance in the later period. When adding lubricating oil on the aero-engine test bench, the following beneficial effects can be achieved: the splashing and falling of lubricating oil during transportation and addition is eliminated, and the safety risk of the test bench caused by lubricating oil addition is avoided; the lubricating oil addition equipment is integrated in the test bench, which does not occupy the limited space on the test bench and does not produce misoperation risk; the lubricating oil addition is fast and efficient, which shortens the working time of the process and improves the production efficiency of the test bench.

[0076] In addition, the structure of the oil filling device of the present application is suitable for oil filling on an aero-engine test bed, and can also be popularized to oil and fuel filling of other types of aero-engine test devices. It is particularly suitable for scenarios where the oil filling end cannot be directly laid with a fixed conveying pipeline due to space, environment, device physical interference and other factors, and needs to maintain an oil-free clean working environment.

[0077] It should be noted that in this document, the terms "comprising", "including", or any other variant thereof are intended to cover non-exclusive inclusions, so that a process, method, article or device including a series of elements not only includes those elements, but also includes other elements not explicitly listed, or inherent to such a process, method, article or device.

[0078] The principles and implementation modes of the present application are described by applying specific examples in this document, and the above examples are only used to help understand the method of the present application and its core idea. The above description is only the preferred implementation mode of the present application. It should be noted that due to the limited nature of the language expression, there are objectively infinite specific structures, and for ordinary skilled persons in the technical field, some improvements, refinements or changes can be made without departing from the principles of the present application, and the above technical features can also be combined in an appropriate manner; these improvements, refinements, changes or combinations, or the direct application of the inventive concept and technical solution to other occasions without improvement, should be regarded as the protection of the present application.

Claims

1. An aeroengine test cell lubricating oil filling apparatus for transporting lubricating oil from a lubricating oil tank to a test cell and filling the lubricating oil into an engine (100), the lubricating oil tank being isolated from the test cell by a partition wall, characterized in that, The aero-engine test running lubricating oil filling equipment comprises a lubricating oil filtering vehicle (200), a lubricating oil filling mechanism (300), a bench lower mounting plate assembly (400), an oil gun (1), a front gun stock mechanism (2) and a rear gun stock mechanism (3): The lubricating oil filtering vehicle (200) comprises a loading vehicle, a lubricating oil tank (201) and an oil conveying pipe (210), the lubricating oil tank (201) is arranged on the loading vehicle, the oil conveying pipe (210) is used for connecting the lubricating oil filtering vehicle (200) and the oil gun (1), and a coarse filter (202), a pump set (203), a three-stage fine filter (206), a pressure gauge (207) and an electromagnetic valve (209) are sequentially arranged on the oil conveying pipe (210), the coarse filter (202) is used for coarsely filtering lubricating oil, the pump set (203) is used for pressurizing the lubricating oil in the oil conveying pipe (210), and the three-stage fine filter (206) is used for three-stage filtering of the lubricating oil to improve the cleanliness of the lubricating oil; The oil filling mechanism (300) comprises a lower hanging bin (301), a curved vertical hose (303) and a hard pipe (304), the lower hanging bin (301) is arranged below the test bench platform surface, the lower hanging bin (301) is used for mounting the front gun stock mechanism (2) and the rear gun stock mechanism (3), the front gun stock mechanism (2) and the rear gun stock mechanism (3) are used for supporting the limiting oil gun (1), the oil gun (1) is communicated with the first end of the curved vertical hose (303), the second end of the curved vertical hose (303) is communicated with the hard pipe (304), the hard pipe (304) is arranged on the bench lower installation plate assembly (400), and the other end of the hard pipe (304) is communicated with the oil conveying pipe (210); the front gun stock mechanism (2) comprises a base (21), a telescopic rod assembly (22) and a limiting support frame (24), the base (21) is used for being arranged on the bottom plate of the lower hanging bin (301), the telescopic rod assembly (22) is arranged on the base (21), and the limiting support frame (24) is arranged on the top of the telescopic rod assembly (22); the telescopic rod assembly (22) is used for driving the limiting support frame (24) to ascend and descend, and the limiting support frame (24) is used for supporting the front barrel of the limiting oil gun (1); the front gun stock mechanism (2) further comprises a clamping assembly (25), the limiting support frame (24) comprises a limiting bottom plate (241) and a limiting side plate (242), the limiting side plate (242) is arranged on the two sides of the limiting bottom plate (241) at intervals, the clamping assembly (25) comprises a clamping piece (251), the middle part of the clamping piece (251) is hinged to the top of the inner wall of the limiting side plate (242), and the clamping pieces (251) on the two sides of the limiting bottom plate (241) are used for clamping and limiting the two sides of the front barrel of the oil gun (1); the front gun stock mechanism (2) further comprises a pushing assembly (23), a rotating assembly (26), a first shielding piece (27) and a second shielding piece (28), the rotating assembly (26) is provided in two groups, the two groups of rotating assemblies (26) are respectively hinged to the outer walls of the limiting side plates (242) on the two sides, the pushing assembly (23) is movably arranged on the limiting side plate (242), the first end of the pushing assembly (23) is hinged to the bottom of the clamping piece (251), the second end of the pushing assembly (23) is hinged to the bottom of the rotating assembly (26), the first shielding piece (27) is connected with the top of the rotating assembly (26) on one side, the second shielding piece (28) is connected with the top of the rotating assembly (26) on the other side, the clamping pieces (251) on the two sides are used for being pressed downward by the front barrel to rotate, so as to drive the pushing assemblies (23) on the two sides to move outward along the vertical direction of the limiting side plate (242) synchronously, and then drive the rotating assemblies (26) on the two sides to rotate to drive the first shielding piece (27) and the second shielding piece (28) to abut and close and shield and protect the inlet of the front barrel.

2. An aircraft engine run-up oiling apparatus according to claim 1, wherein, The oil filling mechanism (300) further comprises a cover plate (302), the cover plate (302) is rotatably arranged on the test bench platform surface, and the cover plate (302) is used for shielding the lower hanging bin (301); a limiting through hole is formed in the side wall of the lower hanging bin (301), and the limiting through hole is used for allowing the curved vertical hose (303) to pass through.

3. An aircraft engine run-up oiling apparatus as claimed in claim 1, wherein, The gantry under mounting plate assembly (400) comprises a mounting plate (401), a pipe joint (402) and a thin nut (403), the pipe joint (402) is arranged on the mounting plate (401), the thin nut (403) is used for sleeving on the pipe joint (402) and locking the pipe joint (402) on the mounting plate (401), the mounting plate (401) is arranged on the bottom of the test bed gantry surface, the mounting plate (401) is provided with a mounting groove (4011), the mounting groove (4011) is used for clamping and limiting the pipe joint (402), and the pipe joint (402) is used for connecting the curved vertical hose (303) and the hard pipe (304).

4. An aircraft engine run-up oiling apparatus as claimed in claim 1, wherein, The oil tank (201) is provided with a filling port (2011) and a blowdown port (2012), and is provided with a liquid level gauge (2013) and a detection interface in the oil tank (201), the detection interface is used for external connection of an online particle size detection device; the oil filter vehicle (200) further comprises an overflow valve (204) and a pressure regulating valve (205) connected with the oil tank (201) and the oil delivery pipe (210), the overflow valve (204) is used for preventing overpressure of the oil delivery pipe (210), and the pressure regulating valve (205) is used for preset bypass pressure relief return through the oil delivery pipe (210) to adjust the output pressure.

5. An aircraft engine run-up oiling apparatus as claimed in claim 1, wherein, The pushing assembly (23) comprises a pushing rod (231), a first compression spring (232) and a spring connecting plate (233), the rotating assembly (26) comprises a rotating plate (261) and a supporting plate (262), the supporting plate (262) is arranged on the top of the outer wall of the limiting side plate (242), the middle part of the rotating plate (261) is hinged to the tail end of the supporting plate (262), the spring connecting plate (233) is arranged on the bottom of the rotating plate (261), the pushing rod (231) is movably arranged on the limiting side plate (242), the first compression spring (232) is sleeved on the pushing rod (231), and the first end of the first compression spring (232) is connected with the spring connecting plate (233), and the second end of the first compression spring (232) is connected with the side wall of the limiting side plate (242).

6. An aircraft engine run-up oiling apparatus as claimed in claim 1, wherein, The first shielding member (27) and the second shielding member (28) are both semicircular plate structures and are used for folding to form a circular shielding plate, the outer side of the first shielding member (27) is provided with a first arc-shaped plate (271), the outer side of the second shielding member (28) is provided with a second arc-shaped plate (281), the second arc-shaped plate (281) is used for surrounding the first arc-shaped plate (271) and the shielding plate to form a limiting cavity, and the limiting cavity is used for shielding and protecting the front barrel of the oil gun (1).

7. An aircraft engine run-up oiling apparatus as claimed in claim 1, wherein, The rear stock mechanism (3) comprises a stock bottom plate (31), side support plates (32), a tail wall (33) and a plurality of safety pins (35), the stock bottom plate (31) is used for being fixed on the bottom plate of the lower hanging bin (301), the side support plates (32) are arranged on both sides of the stock bottom plate (31), the tail wall (33) is arranged on the stock bottom plate (31) and has an included angle with the stock bottom plate (31), the tail wall (33) is used for being connected with the bottom of the side support plates (32) on both sides, a plurality of safety holes (34) are arranged on the side support plates (32), and the plurality of safety pins (35) are used for respectively penetrating through the safety holes (34) to clamp the trigger of the oil gun (1).

Citation Information

Patent Citations

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    CN206036602U

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