CN112683565A - High-temperature working state test system for fuel test piece - Google Patents

High-temperature working state test system for fuel test piece Download PDF

Info

Publication number
CN112683565A
CN112683565A CN202011602018.0A CN202011602018A CN112683565A CN 112683565 A CN112683565 A CN 112683565A CN 202011602018 A CN202011602018 A CN 202011602018A CN 112683565 A CN112683565 A CN 112683565A
Authority
CN
China
Prior art keywords
fuel
test piece
inlet
outlet
oil
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN202011602018.0A
Other languages
Chinese (zh)
Other versions
CN112683565B (en
Inventor
孙立明
刘化天
王新
祝济之
严鲁涛
刘兆旭
王有杰
张宁宁
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Beijing Institute of Structure and Environment Engineering
Tianjin Aerospace Ruilai Technology Co Ltd
Original Assignee
Beijing Institute of Structure and Environment Engineering
Tianjin Aerospace Ruilai Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Beijing Institute of Structure and Environment Engineering, Tianjin Aerospace Ruilai Technology Co Ltd filed Critical Beijing Institute of Structure and Environment Engineering
Priority to CN202011602018.0A priority Critical patent/CN112683565B/en
Publication of CN112683565A publication Critical patent/CN112683565A/en
Application granted granted Critical
Publication of CN112683565B publication Critical patent/CN112683565B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Testing Resistance To Weather, Investigating Materials By Mechanical Methods (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

The invention discloses a high-temperature working state test system for a fuel test piece, which comprises a main fuel tank; a first oil outlet of the main fuel tank is connected with an inlet end of a first three-way conversion valve through a first stop valve; the first outlet end of the first three-way conversion valve is connected with the inlet end of the plunger booster pump; the second outlet end of the first three-way conversion valve is connected with the inlet end of the gear booster pump; the outlet end of the gear booster pump is connected with the inlet end of the second three-way conversion valve; the second outlet end of the second three-way conversion valve is connected with the first oil inlet of the pressure-resistant oil tank; an oil outlet of the pressure-resistant oil tank is connected with one end of the second cut-off valve; the other end of the second cut-off valve is connected with the inlet end of the fuel filter; the outlet end of the fuel filter is connected with the fuel inlet of a test piece in the environmental test box; and the fuel outlet of the test piece is connected with the inlet end of the third three-way conversion valve. The invention can be used for test pieces of different types and technical conditions, and reliably simulating the normal working state of the test piece.

Description

High-temperature working state test system for fuel test piece
Technical Field
The invention relates to the technical field of hydraulic pressure and hydraulic transmission tests, in particular to a high-temperature working state test system for a fuel test piece.
Background
Because aviation fuel oil products are various in types and have harsh working environment, in order to ensure that the aviation fuel oil products have higher reliability, the comprehensive environment test demand is larger in the research and production processes. The test system of the aviation fuel test piece (such as an aviation engine control accessory, a fuel pump test piece) is complex, the test environment is more, the high and low temperature environment is guaranteed, meanwhile, indexes such as fuel pressure and flow of the working environment are required to be provided, the normal working state of the test piece is simulated, and for different types and models of test pieces, the difference of various technical indexes is large.
At present, most of existing equipment is low in compatibility degree of test pieces of different types, the construction cost of products in the research and development process is high, and the manual operation cost is high.
Therefore, a novel test system which has a wide coverage and is fully compatible with different types of test pieces and technical conditions is urgently needed.
Disclosure of Invention
The invention aims to provide a high-temperature working state test system for a fuel test piece, aiming at the technical defects in the prior art.
Therefore, the invention provides a high-temperature working state test system for a fuel test piece, which comprises a main fuel tank;
the first oil outlet at the upper part of the right side of the main fuel tank is connected with the inlet end of the first three-way change-over valve through a first stop valve;
the first outlet end of the first three-way conversion valve is connected with the inlet end of the plunger booster pump;
the second outlet end of the first three-way conversion valve is connected with the inlet end of the gear booster pump;
the outlet end of the gear booster pump is connected with the inlet end of the second three-way conversion valve;
the second outlet end of the second three-way conversion valve is connected with a first oil inlet at the top of a pressure-resistant oil tank;
an oil outlet on the right side of the pressure-resistant oil tank is connected with one end of the second cut-off valve;
the other end of the second cut-off valve is converged and intersected with the outlet end of the plunger booster pump and the first outlet end of the second three-way change-over valve through a pipeline, and then is respectively connected with one end of a second pneumatic reducing valve, the inlet end of the high-temperature energy accumulator and the inlet end of the fuel filter;
the other end of the second pneumatic reducing valve is connected with a first oil inlet at the bottom of the main fuel tank;
the outlet end of the fuel filter is connected with the fuel inlet of a test piece in the environmental test box through a connecting pipeline;
the fuel outlet of the test piece is connected with the inlet end of the third three-way conversion valve through a connecting pipeline which is sequentially provided with a flowmeter and a fourth pneumatic pressure regulating valve;
the second oil outlet at the upper part of the left side of the main fuel tank is connected with an oil inlet at the upper part of a fuel oil heating tank;
the oil outlet at the lower part of the fuel oil heating box is connected with the first inlet end of the first heat exchanger;
the first outlet end of the first heat exchanger is connected with a second oil inlet at the lower part of the left side of the main fuel tank;
the second inlet end of the first heat exchanger is connected with the first water outlet of the external circulating cooling water supply device through a third pneumatic pressure regulating valve;
and the first water inlet of the external circulation cooling water supply device is connected with the second outlet end of the first heat exchanger.
Preferably, the outer wall of the pipeline connected with the inlet end of the fuel filter is provided with a pipe wall heating device.
Preferably, the second oil inlet on the left side of the pressure-resistant oil tank is connected with the air outlet of the nitrogen pressurizing device through a first pneumatic pressure regulating valve.
Preferably, a connecting pipeline between the outlet end of the fuel filter and the fuel inlet of the test piece in the environmental test chamber penetrates through a central through hole of a flange on the side wall of the environmental test chamber.
Preferably, a first pressure sensor and a first temperature sensor are sequentially arranged on a connecting pipeline between the outlet end of the fuel filter and the fuel inlet of the test piece;
and a second temperature sensor and a second pressure sensor are arranged on a connecting pipeline between the fuel outlet of the test piece and the flowmeter.
Preferably, the lubricating oil inlet on the test piece is connected with the oil outlet end of the lubricating oil supply system;
the oil inlet end of the lubricating oil supply system is connected with the first outlet end of the second heat exchanger;
the first inlet end of the second heat exchanger is connected with a lubricating oil outlet on the test piece;
the second inlet end of the second heat exchanger is connected with the second water outlet of the external circulating cooling water supply device;
and the second outlet end of the second heat exchanger is connected with a second water inlet of the external circulating cooling water supply device.
Preferably, the first outlet end of the third three-way conversion valve is connected with a third oil inlet at the bottom of the main fuel tank;
and a second outlet end of the third three-way conversion valve is connected with a third oil inlet at the bottom of the pressure-resistant oil tank.
Preferably, a fourth temperature sensor is arranged on the main fuel tank;
and a third temperature sensor is arranged on the heating box.
Preferably, the device also comprises a driving motor and a rotating speed sensor;
the test piece is connected with the power output end of the driving motor;
and the rotating speed sensor is used for measuring the rotating speed of the test piece.
Compared with the prior art, the high-temperature working state test system for the fuel test piece can provide indexes such as fuel pressure, fuel flow and the like of a working environment while ensuring environments such as high temperature and low temperature and the like for test pieces of different types and technical conditions, realizes reliable simulation of the normal working state of the test piece, and has great practical significance.
Drawings
FIG. 1 is a block diagram of a high-temperature working state test system for a fuel test piece according to the present invention;
FIG. 2 is a diagram of a specific connection mode of a high-temperature working state test system for a fuel test piece according to the present invention;
in the figure: 1 is a main fuel tank; 2 is a first cut-off valve; 3 is a first three-way change-over valve; 4 is a plunger piston booster pump; 5 is a gear booster pump;
6 is a second three-way change-over valve; 7 is a pressure-resistant oil tank; 8 is a nitrogen pressurizing device; 9 is a first pneumatic pressure regulating valve; 10 is a second pneumatic pressure regulating valve;
11 is a pipe wall heating device; 12 is a fuel oil filter; 13 is a first pressure sensor; 14 is a first temperature sensor; 15 is a test piece;
16 is an environmental test chamber; 17 is a second temperature sensor; 18 is a second pressure sensor; 19 is a flow meter; 20 is a fuel heater;
21 is a third temperature sensor; 22 is a gear pump; 23 is a first heat exchanger; 24 is a device for providing external circulation cooling water; 25 is a fourth temperature sensor;
26 is a driving motor; 27 is a rotation speed sensor; 28 is a lubricating oil supply system; 29 is a second heat exchanger; 30 is a third three-way change-over valve;
31 is a high temperature accumulator; 32 is a third pneumatic pressure regulating valve, 33 is a fourth pneumatic pressure regulating valve;
and 34 is a second stop valve.
Detailed Description
In order to make the technical means for realizing the invention easier to understand, the following detailed description of the present application is made in conjunction with the accompanying drawings and embodiments. It is to be understood that the specific embodiments described herein are merely illustrative of the relevant application and are not limiting of the application. It should be noted that, for convenience of description, only the portions related to the present application are shown in the drawings.
It should be noted that the embodiments and features of the embodiments in the present application may be combined with each other without conflict. The present application will be described in detail below with reference to the embodiments with reference to the attached drawings.
It should be noted that in the description of the present application, the terms of direction or positional relationship indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. are based on the directions or positional relationships shown in the drawings, which are merely for convenience of description, and do not indicate or imply that the device or element must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present application.
In addition, it should be noted that, in the description of the present application, unless otherwise explicitly specified and limited, the term "mounted" and the like should be interpreted broadly, and may be, for example, either fixedly mounted or detachably mounted.
The specific meaning of the above terms in the present application can be understood by those skilled in the art as the case may be.
Referring to fig. 1 and 2, the invention provides a high-temperature working state test system for a fuel test piece, which comprises a main fuel tank 1;
wherein, the first oil outlet of the upper portion of the right side of the main fuel tank 1 is connected with the inlet end of the first three-way change-over valve 3 through the first cut-off valve 2;
the first outlet end of the first three-way change-over valve 3 is connected with the inlet end of the plunger booster pump 4;
the second outlet end of the first three-way conversion valve 3 is connected with the inlet end of the gear booster pump 5;
the outlet end of the gear booster pump 5 is connected with the inlet end of the second three-way conversion valve 6;
the second outlet end of the second three-way conversion valve 6 is connected with a first oil inlet at the top of a pressure-resistant oil tank 7;
an oil outlet at the right side of the pressure-resistant oil tank 7 is connected with one end of a second cut-off valve 34;
the other end of the second cut-off valve 34 is converged and intersected with the outlet end of the plunger booster pump 4 and the first outlet end of the second three-way change-over valve 6 through pipelines, and then is respectively connected with one end of the second pneumatic reducing valve 10, the inlet end of the high-temperature accumulator and the inlet end of the fuel filter 12;
the other end of the second pneumatic reducing valve 10 is connected with a first oil inlet at the bottom of the main fuel tank 1;
the outlet end of the fuel filter 12 is connected with the fuel inlet of a test piece 15 positioned in the environment test box 16 through a connecting pipeline;
the fuel outlet of the test piece 15 is connected to the inlet end of the third three-way switching valve 30 through a connecting pipe provided with a flow meter 33 and a fourth pneumatic pressure regulating valve 33 in this order;
the second oil outlet at the upper part of the left side of the main fuel tank 1 is connected with an oil inlet at the upper part of a fuel oil heating tank 20;
an oil outlet at the lower part of the fuel oil heating box 20 is connected with a first inlet end of the first heat exchanger 23;
a first outlet end of the first heat exchanger 23 is connected with a second oil inlet at the lower part of the left side of the main fuel tank 1;
the second inlet end of the first heat exchanger 23 is connected with the first water outlet of the external circulation cooling water supply device 24 through a third pneumatic pressure regulating valve 32;
the first inlet of the external circulation cooling water supply device 24 is connected with the second outlet end of the first heat exchanger 23.
It should be noted that the first outlet end of the first heat exchanger 23 is communicated with the first inlet end, and the second inlet end is communicated with the second outlet end. The heat exchanger is the prior art equipment, and the heat exchange principle is not described herein again.
In the present invention, in a concrete implementation, a pipe wall heating device 11 is installed on the outer wall of the pipeline connected with the inlet end of the fuel filter 12.
In the invention, in concrete implementation, a second oil inlet on the left side of the pressure-resistant oil tank 7 is connected with an air outlet of the nitrogen pressurizing device 8 through a first pneumatic pressure regulating valve 9.
In the present invention, in a specific implementation, a connection pipe between the outlet end of the fuel filter 12 and the fuel inlet of the test piece 15 inside the environmental test chamber 16 penetrates through a central through hole of a flange on the side wall of the environmental test chamber 16.
In the present invention, in a concrete implementation, a first pressure sensor 13 and a first temperature sensor 14 are sequentially disposed on a connecting pipeline between the outlet end of the fuel filter 12 and the fuel inlet of the test piece 15.
In the present invention, in a concrete implementation, a second temperature sensor 17 and a second pressure sensor 18 are arranged on a connecting pipeline between the fuel outlet of the test piece 15 and the flowmeter 33.
In the present invention, in a specific implementation, the lubricating oil inlet on the test piece 15 is connected with the oil outlet end of the lubricating oil supply system 28;
the oil inlet end of the lubricating oil supply system 28 is connected with the first outlet end of the second heat exchanger 29;
a first inlet end of the second heat exchanger 29, connected to the lubricant outlet on the test piece 15;
a second inlet end of the second heat exchanger 29 is connected with a second water outlet of the external circulation cooling water supply device 24;
a second outlet end of the second heat exchanger 29 is connected to a second water inlet of the external circulation cooling water supply device 24;
it should be noted that the second heat exchanger 29 has a first outlet end communicating with the first inlet end and a second inlet end communicating with the second outlet end. The heat exchanger is the prior art equipment, and the heat exchange principle is not described herein again.
In the present invention, in a specific implementation, a first outlet end of the third three-way conversion valve 30 is connected to a third oil inlet at the bottom of the main fuel tank 1;
the second outlet end of the third three-way change-over valve 30 is connected to the third inlet port at the bottom of the pressure-resistant oil tank 7.
In the invention, in a concrete implementation, a fourth temperature sensor 25 is arranged on the main fuel tank 1;
a third temperature sensor 21 is attached to the heating box 20.
In the invention, in a concrete implementation, the test piece 15 is connected with a power output end of a driving motor 26 (through a coupler), and the driving motor is used for driving the test piece 15 to rotate and providing a corresponding rotating speed;
in a specific implementation, the system of the present invention further includes a rotation speed sensor 27, which is used for measuring the rotation speed of the test piece 15. The rotation speed sensor 27 is generally installed beside the output shaft of the driving motor 26.
In the present invention, the nitrogen pressurization device 8 may specifically include a nitrogen gas cylinder and a nitrogen gas pressure reducer (with a pressure gauge valve), the nitrogen gas cylinder is filled with high-pressure nitrogen gas, the nitrogen gas pressure reducer is connected to an outlet of the nitrogen gas cylinder, and the nitrogen gas pressure at the outlet of the nitrogen gas cylinder is controlled by the nitrogen gas pressure reducer.
In the present invention, in a specific implementation, the pipe wall heating device 11 is installed on the outer wall of the pipeline connected to the inlet end of the fuel filter 12, and an existing pipe wall heating device can be specifically adopted, and mainly comprises a heating wire. For example, the technical proposal of patent application No. CN202010328296.5 entitled "a silicone oil in-line type pipeline auxiliary heating device for fuel oil test system" can be adopted, the device can be installed on the outer wall of the pipeline, the silicone oil is heated by a heating wire, and then the medium flowing in the pipeline is heated by the heated silicone oil.
In the present invention, the environmental test chamber 16 is an existing test chamber, for example, an "explosion-proof environmental test chamber" manufactured by beijing space hill test technology ltd may be adopted, and the environmental test chamber is mainly used for providing a high-temperature or low-temperature environment required by the working condition of the test piece.
In the present invention, for a specific implementation, the external circulating cooling water supply device 24 may be an existing air-cooled water chiller, for example, a YSD series air-cooled water chiller manufactured by the refrigeration equipment ltd of yashidad, huizhou city, and is mainly used for supplying circulating cooling water.
In the present invention, for concrete implementation, the conventional lubricating oil supply system may be adopted as the lubricating oil supply system as long as it can ensure reliable improvement of the lubricating oil supply, and for example, a technical scheme of patent application No. CN202010346205.0 and patent name "a multi-channel lubricating oil station for an intelligent pump" may be adopted, in which the lubricating oil in the lubricating oil tank is mainly output by a booster pump, and an oil inlet end of the booster pump is connected to the lubricating oil tank.
Based on the technical scheme, the system mainly comprises a fuel oil supply system, a pressurization system, a temperature measurement control system, a product driving system, a lubricating oil supply system, control management software and an environmental test box. The system overcomes the problem that the traditional test bed has low compatibility with test technical indexes, has wide flow, pressure and temperature ranges, and can provide accurate control measurement of pressure, flow, rotating speed, ambient temperature and medium temperature for different types of test pieces.
For the present invention, the fuel supply system comprises a closed large-capacity main fuel tank 1 and a sealed pressure-resistant fuel tank 7. The two can be used separately or work simultaneously according to different test technical conditions. When the inlet flow of the test piece 15 is large or the inlet pressure is large and the inlet oil absorption of the test piece 15 is not unnecessarily increased or decreased, the sealed large-capacity main fuel tank is used for independently working; when the inlet (i.e. fuel inlet) of the test piece 15 has low pressure and small flow, the sealed pressure-resistant oil tank 7 is used for independent work; when the inlet oil suction of the test piece 15 is increased or decreased unnecessarily, the test piece and the test piece work simultaneously, and the sealed pressure-resistant oil tank 7 is a large-volume low-pressure accumulator. In this way, the wide coverage of the flow and pressure control measurement range of the system is realized.
For the invention, the pressurizing system mainly comprises a gear pressurizing pump 5, a plunger pressurizing pump 4, a nitrogen pressurizing device 8 and various measuring sensors at the inlet and the outlet of the test piece 15. The three supercharging devices are switched according to different test technical conditions. When the inlet pressure of the test piece 15 is small and the flow is large, the gear booster pump 5 and the corresponding pipeline thereof are controlled to work; when the inlet pressure of the test piece 15 is large and the flow rate is small, the plunger booster pump 4 and the corresponding pipeline thereof are controlled to work; and when the inlet pressure of the test piece 15 is small, the flow is small or the inlet flow fluctuation is large, controlling the nitrogen pressurizing device 8 and the corresponding pipeline to work.
For the present invention, the temperature measurement control system mainly includes a heating box 20, an external circulation cooling water supply device 24, a pipe wall heating device (i.e. pipe wall heater) 11, a first heat exchanger 23, a second heat exchanger 29 and corresponding measurement sensors. When the sealed large-capacity main fuel tank 1 is used for supplying fuel, the heating tank 20 and the external circulating water supply device 24 are used for controlling the temperature of a fuel medium, the fuel medium is enabled to circularly flow between the main fuel tank 1 and the heating tank 20 through the gear pump 22, the heating tank 20 heats the oil temperature, the external circulating cooling water is properly cooled through the first heat exchanger 23 between the heating tank 20 and the main fuel tank 1, the temperature of the fuel medium is measured through the fourth temperature sensor 24, and signals are acquired to the control system for PID control. When the sealed pressure-resistant fuel tank 7 is used, a low-power tube wall heating device (i.e., a tube wall heater) 11 is used for temperature control because of a small fuel medium capacity. When the ambient temperature is low, the temperature of the main fuel tank 1 flows to the front of the test piece 15, heat loss in a pipeline may exist, the pipe wall heating device (namely, the pipe wall heater) 1 is used for auxiliary heating, and the first temperature sensor 14 in front of the test piece is used for collecting temperature signals.
For the invention, the product driving system mainly comprises a driving motor 26, a rotating speed sensor 27, a corresponding transmission bearing and the like, wherein the driving motor 26 provides a corresponding rotating speed, and the rotating speed sensor 27 is used for measuring the rotating speed. Meanwhile, the lubricating oil supply system 28 provides lubrication and cooling for the product driving system, and the cooling is mainly completed by connecting the second heat exchanger 29 in the pipeline to the external circulating water.
It should be noted that, when the test piece 15 in the test process needs to provide the ambient temperature, the test piece may be placed in an explosion-proof environmental test chamber, and the pipeline is connected to the test piece through a flange hole of the environmental test chamber wall. The explosion-proof environmental test box is used for providing a high-temperature or low-temperature environment required by the working condition of the test piece.
The invention provides a working state comprehensive environment test system for an aviation fuel test piece. The invention mainly comprises a pressurization system, a temperature measurement control system, a lubricating oil supply system, a product driving system, a fuel oil supply system (namely an oil source system) and an environmental test box, can realize the pressure supply of the inlet of a test piece, control the rotating speed of the test piece, and can control the environmental temperature and control and measure the temperature of an oil medium, the pressure of an outlet and the flow of the oil medium for the test piece.
Compared with the traditional fuel oil test equipment, the test equipment can meet the requirements of different types of test pieces and different technical indexes, can realize multiple purposes, and has wide coverage for aviation fuel oil test pieces in different stages and types.
In order to more clearly understand the technical solution of the present invention, the following describes the working principle of the present invention.
According to the invention, when the inlet flow of the test piece 15 is large in the test technical conditions, the selection is carried out through control system software, the system controls the main fuel tank 1 to work, the first cut-off valve 2 is opened, and the second cut-off valve 34 is closed. The first three-way change-over valve 3 controls the fuel to flow to the gear booster pump 5, the gear booster pump 5 works, and the second three-way change-over valve 6 closes the inlet of the sealed pressure-resistant oil tank 7 and enters the fuel inlet of the test piece 15 through the fuel filter 12. The second pneumatic pressure regulating valve 10 is used for controlling the flow of the fuel inlet bypass circuit of the test piece 15 back to the main fuel tank 1, and thus the fuel inlet pressure of the test piece 15 is controlled.
A first pressure sensor 13 and a first temperature sensor 14 are arranged in front of a fuel inlet of the test piece 15 and used for monitoring and measuring the pressure and the temperature at the fuel inlet of the test piece 15, and the opening degree of the second pneumatic pressure regulating valve 10 is adjusted through data collected by the first pressure sensor 13, so that the fuel inlet pressure PID control of the test piece 15 is carried out.
After the fuel flows out from the fuel outlet of the test piece 15, the fuel passes through the second temperature sensor 17, the second pressure sensor 18 and the flowmeter 19 to measure the corresponding data of the fuel outlet of the test piece 15. The third three-way switching valve 30 closes the passage of the sealed pressure-resistant fuel tank 7, and allows the fuel to flow back to the main fuel tank 1 through a third pneumatic pressure-regulating valve 33, wherein the third pneumatic pressure-regulating valve 33 is used for regulating the fuel outlet pressure of the test piece 15 by controlling the opening degree. The high-temperature energy storage 31 in the pipeline is mainly used for eliminating the pressure pulse phenomenon in the system caused by unstable flow velocity and the like.
When the inlet pressure is higher in the technical conditions of the test piece, the control system software is used for selecting, the system controls the three-way change-over valve 3 to enable fuel to flow from the main oil tank to the plunger pump 4, and the plunger booster pump 4 works. The rest of the operation is the same as above.
For the invention, when the fuel inlet pressure and the flow of the test piece 15 are small or the flow increases or decreases excessively in the test technical conditions, the system controls the sealed pressure-resistant oil tank 7 to work, the first cut-off valve 2 is closed, and the second cut-off valve 34 is opened. The air pressure input by the nitrogen supercharging device 8 is controlled by the first pneumatic pressure regulating valve 9, and the pressure entering the test piece 15 is controlled by the bypass second pneumatic pressure regulating valve 10. In this mode, the system controls the third three-way switching valve 30 so that the fuel flowing out of the outlet of the test piece 15 flows back to the sealed pressure-resistant fuel tank 7.
For the present invention, when the test technical condition requires the temperature of the fuel medium, the selection can be made by the control system software, the system controls the gear pump 22 to work, so that the fuel circulates between the main fuel tank 1 and the heating tank 20, the heating tank 20 works at the same time, the fuel medium in the heating tank 20 is heated, the external circulation cold water provided by the external circulation cold water providing device 24 is cooled by the first heat exchanger 23. The third temperature sensor 21 and the fourth temperature sensor 25 monitor and measure the temperature of the two oil solutions and transmit the temperature to the control system, the control system controls the working power of the heater 20, and simultaneously controls the water flow rate of the external circulating water entering the radiator (i.e. the first heat exchanger 23) by controlling the opening degree of the third pneumatic pressure regulating valve 32, thereby completing the PID control of the fuel temperature. When a sealed pressure-resistant oil tank is used for supplying oil or the external environment has a large influence on the temperature in the test system, the pipe wall heating device 11 can be selectively opened according to actual conditions, and the first temperature sensor 14 is used for monitoring the temperature.
For the invention, when the test technical condition requires the rotating speed of the test piece, the selection can be carried out through the control system software, and the system controls the lubricating oil supply system 28 to work, so as to provide lubrication for the transmission system and reduce the temperature. The lubricating oil supply system 28 is connected with the external circulation cold water supply device 24 through a second heat exchanger 29 to cool the lubricating oil. Meanwhile, the system controls the driving motor 26 to work, and a rotating speed signal is acquired to the control system through the rotating speed sensor 27 to perform rotating speed PID control.
For the invention, when the test technical condition requires the environmental temperature of the test piece, the environmental test box 16 is controlled to work to provide the temperature and humidity environmental conditions, and the connecting pipeline of the test piece 15 enters the test box through the flange on the side wall of the environmental test box.
It should be noted that the system connection and the use or function of the different components shown in fig. 2 may be modified or finished according to different requirements of the test parameters of the test piece.
Compared with the prior art, the high-temperature working state test system for the fuel test piece provided by the invention can be used for different types and technical conditions of test pieces, can ensure high and low temperature and other environments, provides indexes such as fuel pressure, flow and the like of a working environment, realizes reliable simulation of the normal working state of the test piece, and has great practical significance.
The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, various modifications and decorations can be made without departing from the principle of the present invention, and these modifications and decorations should also be regarded as the protection scope of the present invention.

Claims (9)

1. A high-temperature working state test system for a fuel test piece is characterized by comprising a main fuel tank (1);
wherein, a first oil outlet at the upper part of the right side of the main fuel tank (1) is connected with the inlet end of a first three-way conversion valve (3) through a first cut-off valve (2);
the first outlet end of the first three-way change-over valve (3) is connected with the inlet end of the plunger booster pump (4);
the second outlet end of the first three-way conversion valve (3) is connected with the inlet end of the gear booster pump (5);
the outlet end of the gear booster pump (5) is connected with the inlet end of the second three-way change-over valve (6);
the second outlet end of the second three-way conversion valve (6) is connected with a first oil inlet at the top of a pressure-resistant oil tank (7);
an oil outlet at the right side of the pressure-resistant oil tank (7) is connected with one end of a second cut-off valve (34);
the other end of the second cut-off valve (34) is converged and intersected with the outlet end of the plunger booster pump (4) and the first outlet end of the second three-way change-over valve (6) through a pipeline, and then is respectively connected with one end of a second pneumatic reducing valve (10), the inlet end of a high-temperature energy accumulator and the inlet end of a fuel filter (12);
the other end of the second pneumatic reducing valve (10) is connected with a first oil inlet at the bottom of the main fuel tank (1);
the outlet end of the fuel filter (12) is connected with the fuel inlet of a test piece (15) in the environment test box (16) through a connecting pipeline;
the fuel outlet of the test piece (15) is connected with the inlet end of the third three-way change-over valve (30) through a connecting pipeline which is sequentially provided with a flowmeter (33) and a fourth pneumatic pressure regulating valve (33);
the second oil outlet at the upper part of the left side of the main fuel tank (1) is connected with an oil inlet at the upper part of a fuel heating tank (20);
an oil outlet at the lower part of the fuel oil heating box (20) is connected with a first inlet end of the first heat exchanger (23);
a first outlet end of the first heat exchanger (23) is connected with a second oil inlet at the lower part of the left side of the main fuel tank (1);
the second inlet end of the first heat exchanger (23) is connected with the first water outlet of the external circulating cooling water supply device (24) through a third pneumatic pressure regulating valve (32);
the first water inlet of the external circulation cooling water supply device (24) is connected with the second outlet end of the first heat exchanger (23).
2. The high-temperature working state test system of the fuel test piece according to claim 1, wherein a pipe wall heating device (11) is installed on the outer wall of the pipeline connected with the inlet end of the fuel filter (12).
3. The fuel test piece high-temperature working state test system as claimed in claim 1, wherein a second oil inlet on the left side of the pressure-resistant oil tank (7) is connected with an air outlet of the nitrogen pressurizing device (8) through a first pneumatic pressure regulating valve (9).
4. The fuel test piece high-temperature working state test system as claimed in claim 1, wherein a connecting pipeline between the outlet end of the fuel filter (12) and the fuel inlet of the test piece (15) in the environment test box (16) penetrates through a central through hole of a flange on the side wall of the environment test box (16).
5. The fuel test piece high-temperature working state test system as claimed in claim 1, wherein a first pressure sensor (13) and a first temperature sensor (14) are sequentially arranged on a connecting pipeline between the outlet end of the fuel filter (12) and the fuel inlet of the test piece (15);
and a second temperature sensor (17) and a second pressure sensor (18) are arranged on a connecting pipeline between the fuel outlet of the test piece (15) and the flowmeter (33).
6. The high-temperature working state test system of the fuel test piece according to claim 1, wherein a lubricating oil inlet on the test piece (15) is connected with an oil outlet end of a lubricating oil supply system (28);
the oil inlet end of the lubricating oil supply system (28) is connected with the first outlet end of the second heat exchanger (29);
the first inlet end of the second heat exchanger (29) is connected with a lubricating oil outlet on the test piece (15);
the second inlet end of the second heat exchanger (29) is connected with the second water outlet of the external circulating cooling water supply device (24);
and a second outlet end of the second heat exchanger (29) is connected with a second water inlet of the external circulating cooling water supply device (24).
7. The fuel test piece high-temperature working state test system as claimed in claim 1, wherein a first outlet end of the third three-way change-over valve (30) is connected with a third oil inlet at the bottom of the main fuel tank (1);
and a second outlet end of the third three-way change-over valve (30) is connected with a third oil inlet at the bottom of the pressure-resistant oil tank (7).
8. The high-temperature working state test system of the fuel test piece according to claim 1, characterized in that a fourth temperature sensor (25) is arranged on the main fuel tank (1);
a third temperature sensor (21) is mounted on the heating box (20).
9. The fuel test piece high-temperature working state testing system as claimed in any one of claims 1 to 8, characterized by further comprising a driving motor (26) and a rotating speed sensor (27);
the test piece (15) is connected with the power output end of the driving motor (26);
and the rotating speed sensor (27) is used for measuring the rotating speed of the test piece (15).
CN202011602018.0A 2020-12-29 2020-12-29 Fuel test piece high-temperature working state test system Active CN112683565B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202011602018.0A CN112683565B (en) 2020-12-29 2020-12-29 Fuel test piece high-temperature working state test system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202011602018.0A CN112683565B (en) 2020-12-29 2020-12-29 Fuel test piece high-temperature working state test system

Publications (2)

Publication Number Publication Date
CN112683565A true CN112683565A (en) 2021-04-20
CN112683565B CN112683565B (en) 2024-07-09

Family

ID=75454491

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202011602018.0A Active CN112683565B (en) 2020-12-29 2020-12-29 Fuel test piece high-temperature working state test system

Country Status (1)

Country Link
CN (1) CN112683565B (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2009148951A (en) * 2009-12-30 2011-07-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "СА EMERGENCY CONTROL DEVICE FOR FUEL SUPPLY TO THE MAIN COMBUSTION CHAMBER OF A GAS-TURBINE ENGINE
CN103149041A (en) * 2013-01-28 2013-06-12 南京航空航天大学 Accumulation type plane auxiliary fuel system air pressure transfusion fuel oil testing system and method
CN104074844A (en) * 2014-07-02 2014-10-01 北京机械设备研究所 Debuggable movable hydraulic oil source
KR20150015721A (en) * 2013-08-01 2015-02-11 한국항공우주산업 주식회사 Device for Engine Feed Performance Analysis and Its Comparison with Test Result of KC-100 Aircraft Fuel System and Controlling Method for the Same
CN104613476A (en) * 2015-01-12 2015-05-13 中国石油大学(华东) Multi-head self-adjusting oil-gas co-combusting device of offshore heavy oil platform
CN107144432A (en) * 2017-07-06 2017-09-08 中国船舶重工集团公司第七�三研究所 A kind of big-and-middle-sized gas turbine land experimental bench system
CN109580209A (en) * 2019-01-10 2019-04-05 贵州永红航空机械有限责任公司 A kind of alternating-current generator of airplane combustion oil cooler service life experimental testers
CN214224545U (en) * 2020-12-29 2021-09-17 天津航天瑞莱科技有限公司 High-temperature working state test system for fuel test piece

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2009148951A (en) * 2009-12-30 2011-07-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "СА EMERGENCY CONTROL DEVICE FOR FUEL SUPPLY TO THE MAIN COMBUSTION CHAMBER OF A GAS-TURBINE ENGINE
CN103149041A (en) * 2013-01-28 2013-06-12 南京航空航天大学 Accumulation type plane auxiliary fuel system air pressure transfusion fuel oil testing system and method
KR20150015721A (en) * 2013-08-01 2015-02-11 한국항공우주산업 주식회사 Device for Engine Feed Performance Analysis and Its Comparison with Test Result of KC-100 Aircraft Fuel System and Controlling Method for the Same
CN104074844A (en) * 2014-07-02 2014-10-01 北京机械设备研究所 Debuggable movable hydraulic oil source
CN104613476A (en) * 2015-01-12 2015-05-13 中国石油大学(华东) Multi-head self-adjusting oil-gas co-combusting device of offshore heavy oil platform
CN107144432A (en) * 2017-07-06 2017-09-08 中国船舶重工集团公司第七�三研究所 A kind of big-and-middle-sized gas turbine land experimental bench system
CN109580209A (en) * 2019-01-10 2019-04-05 贵州永红航空机械有限责任公司 A kind of alternating-current generator of airplane combustion oil cooler service life experimental testers
CN214224545U (en) * 2020-12-29 2021-09-17 天津航天瑞莱科技有限公司 High-temperature working state test system for fuel test piece

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
王野牧 等: "飞机发动机二工位燃油总管试验器液压控制原理及关键技术的实现方法", 《机床与液压》, 31 October 2013 (2013-10-31), pages 76 - 78 *

Also Published As

Publication number Publication date
CN112683565B (en) 2024-07-09

Similar Documents

Publication Publication Date Title
CN102354168B (en) Electro-hydraulic control system of high/ low temperature test stand of automobile automation transmission valve body
CN101587027B (en) System for testing heat-transfer performance of gas-water-oil heat interchanger
CN101793652B (en) Heat exchanger performance experiment device
CN201828400U (en) Electromagnetic valve and valve body performance detection device for automatic transmission
CN101655414B (en) Simulation test bench of automobile cooling system
CN103487269A (en) Capacity-variable water cooling unit test system
CN106198048A (en) Cooling system of vehicle cold collateral resistance simulation test experiment platform and method thereof
CN104316326A (en) Fuel-oil auxiliary system of diesel engine laboratory
CN111811825A (en) Multifunctional engine cooling temperature control system and control method thereof
CN214224545U (en) High-temperature working state test system for fuel test piece
CN201212760Y (en) Liquid cooling temperature control device
CN110792586A (en) Intelligent compressor performance test and monitoring test bed
CN202102305U (en) Electrohydraulic control system of high/low-temperature test stand for valve body of automatic speed changer of automobile
CN112683565B (en) Fuel test piece high-temperature working state test system
CN201730900U (en) High-temperature hydraulic test system using normal temperature control valve
CN109974320B (en) High-temperature deionized water cooling device
CN207816531U (en) A kind of thermostat of automobile engine leakage amount detector
CN110454466A (en) Hydrostatic drive system combination property bench and method
CN205333454U (en) Liquid circulation cold and hot impact test case
CN205785843U (en) Cooling system of vehicle cold collateral resistance simulation test experiment platform
CN211176264U (en) Lubrication test system for oil flow test of heavy gearbox
CN210894621U (en) New forms of energy motor's test system
CN109425490A (en) New-energy automobile simulated testing system
CN207248541U (en) New-energy automobile simulated testing system
CN218995602U (en) Water supply device for portable new energy electric drive system water cooling experiment

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant