CN106762595B - Load sensitive pump pilot system - Google Patents

Load sensitive pump pilot system Download PDF

Info

Publication number
CN106762595B
CN106762595B CN201710107738.1A CN201710107738A CN106762595B CN 106762595 B CN106762595 B CN 106762595B CN 201710107738 A CN201710107738 A CN 201710107738A CN 106762595 B CN106762595 B CN 106762595B
Authority
CN
China
Prior art keywords
load sensitive
sensitive pump
cut
pump
subject
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.)
Active
Application number
CN201710107738.1A
Other languages
Chinese (zh)
Other versions
CN106762595A (en
Inventor
汪立平
曹海建
郭言
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.)
Jiangsu Hengli Hydraulic Co Ltd
Original Assignee
Jiangsu Hengli Hydraulic 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 Jiangsu Hengli Hydraulic Co Ltd filed Critical Jiangsu Hengli Hydraulic Co Ltd
Priority to CN201710107738.1A priority Critical patent/CN106762595B/en
Publication of CN106762595A publication Critical patent/CN106762595A/en
Application granted granted Critical
Publication of CN106762595B publication Critical patent/CN106762595B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B51/00Testing machines, pumps, or pumping installations

Abstract

The invention discloses a kind of load sensitive pump pilot systems, including fuel tank, the fuel tank is connected to subject load sensitive pump by pipeline, the torque speed sensor and motor for driving subject load sensitive pump output oil liquid are connected on the subject load sensitive pump, the first flowmeter for calculating subject load sensitive pump oil pump capacity is communicated on the subject load sensitive pump, by the first cut-off reversal valve, the first cut-off reversal valve makes to be tested the LS hydraulic fluid port that load sensitive pump output oil liquid is back to subject load sensitive pump after opening for connection in the first flowmeter.By the above-mentioned means, load sensitive pump pilot system of the present invention, it can be under conditions of being tested load sensitive pump LS hydraulic fluid port pressure adjustable section, the dredge oil amount of accurate measurement subject load sensitive pump, and realize the LS responsiveness test of subject load sensitive pump.

Description

Load sensitive pump pilot system
Technical field
The present invention relates to hydraulic test fields, more particularly to a kind of load sensitive pump pilot system.
Background technique
Existing load sensitive pump pilot system such as Fig. 2 controls subject load by proportional pressure control valve by external pilot pump Sensitive pump LS hydraulic fluid port pressure is to realize the subject variable control purpose of load sensitive pump LS hydraulic fluid port pressure.Due to drawing in the program The oil liquid of external pilot pump is entered, which generates internal leakage after entering the LS valve for being tested load sensitive pump, and Leakage Energy flows into Subject load sensitive pump flows away from drain tap, so the dredge oil amount tested is equal to the portion pumped by itself dredge oil amount+external pilot Divide draining.Calculate to obtain efficiency of pump inaccuracy.
It is negative to be introduced subject by another load sensitive pump pilot system such as Fig. 3 for subject pump load sensitivity pump discharge P hydraulic oil Sensitive pump itself LS hydraulic fluid port is carried, although the dredge oil amount of flowmeter detection is subject load sensitive pump itself dredge oil amount, is existed The nonadjustable disadvantage of LS hydraulic fluid port pressure.
Summary of the invention
The invention mainly solves the technical problem of providing a kind of load sensitive pump pilot systems, can be quick in subject load Under conditions of sense pump LS hydraulic fluid port pressure adjustable section, the dredge oil amount of accurate measurement subject load sensitive pump, and realize that subject load is quick The LS responsiveness test of sense pump.
In order to solve the above technical problems, one technical scheme adopted by the invention is that: a kind of load-sensitive pump testing is provided System, including fuel tank, the fuel tank are connected to subject load sensitive pump by pipeline, connect on the subject load sensitive pump useful It is communicated on the torque speed sensor and motor of driving subject load sensitive pump output oil liquid, the subject load sensitive pump For calculating the first flowmeter of subject load sensitive pump oil pump capacity, the first cut-off commutation is communicated in the first flowmeter Valve, the first cut-off reversal valve make to be tested the LS oil that load sensitive pump output oil liquid is back to subject load sensitive pump after opening Mouthful.
In a preferred embodiment of the present invention, proportional pressure control valve, the ratio are parallel on the first cut-off reversal valve Example overflow valve carries out electric proportional control load to pump.
In a preferred embodiment of the present invention, first cut-off reversal valve lower end has been sequentially communicated the second cut-off commutation Valve and operated proportional flow control valve, the other end of the operated proportional flow control valve are connected to fuel tank, and the operated proportional flow control valve is opened Degree is tested the LS hydraulic fluid port pressure of load sensitive pump to adjust.
In a preferred embodiment of the present invention, the first cut-off reversal valve, the second cut-off reversal valve and subject load Third cut-off reversal valve is communicated between the LS hydraulic fluid port of sensitive pump, the other end of third cut-off reversal valve is connected to fuel tank, described First cut-off reversal valve is opened, and the second cut-off reversal valve is closed, and the switch of control third cut-off reversal valve is to subject load-sensitive The LS hydraulic fluid port of pump carries out responsiveness test.
In a preferred embodiment of the present invention, described proportional pressure control valve one end is connected in parallel on the first shut-off valve, the other end It is connected in parallel on operated proportional flow control valve.
In a preferred embodiment of the present invention, it is successively linked between subject load sensitive pump and the first flowmeter Check valve and filter.
In a preferred embodiment of the present invention, gate valve is equipped between the fuel tank and subject load sensitive pump.
In a preferred embodiment of the present invention, the is connected between the S hydraulic fluid port and fuel tank of the subject load sensitive pump Two flowmeters.
In a preferred embodiment of the present invention, it is connected between the second cut-off reversal valve and fuel tank for cooling logical The cooler of oil liquid after crossing proportional pressure control valve load.
The beneficial effects of the present invention are: load sensitive pump pilot system of the present invention, it can be in subject load sensitive pump LS oil Under conditions of mouth pressure adjustable section, the dredge oil amount of accurate measurement subject load sensitive pump, and realize the LS of subject load sensitive pump Responsiveness test.
Detailed description of the invention
To describe the technical solutions in the embodiments of the present invention more clearly, make required in being described below to embodiment Attached drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the invention, for For those of ordinary skill in the art, without creative efforts, it can also be obtained according to these attached drawings other Attached drawing, in which:
Fig. 1 is the structural schematic diagram of one preferred embodiment of load sensitive pump pilot system of the present invention;
Fig. 2 is the structural schematic diagram of existing load sensitive pump pilot system;
Fig. 3 is the structural schematic diagram of existing another load sensitive pump pilot system;
The components in the drawings are labeled as follows: 1, gate valve, 2, subject load sensitive pump, 3, sensor, 4, motor, and 5, unidirectional Valve, 6, filter, 7, first flowmeter, the 8, first cut-off reversal valve, the 9, second cut-off reversal valve, 10, operated proportional flow control valve, 11, proportional pressure control valve, 12, third cut-off reversal valve, 13, cooler, 14, second flowmeter, 15, runner.
Specific embodiment
The technical scheme in the embodiments of the invention will be clearly and completely described below, it is clear that described implementation Example is only a part of the embodiments of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, this field is common Technical staff's all other embodiment obtained without making creative work belongs to the model that the present invention protects It encloses.
Referring to Fig. 1, a kind of load sensitive pump pilot system, including fuel tank 15, pass through pipeline connection subject on fuel tank 15 Load sensitive pump 2 is tested the sensor being connected on load sensitive pump 2 for driving subject load sensitive pump 2 to export oil liquid 3 and motor 4, the revolving speed and torque of the detection subject load sensitive pump 2 of sensor 3 are tested on load sensitive pump 2 and are communicated with based on The first flowmeter 7 of subject 2 oil pump capacity of load sensitive pump is calculated, the first cut-off of connection oil reversal valve 8 in first flowmeter 7, first Cut-off reversal valve 8 makes to be tested the LS hydraulic fluid port that the output oil liquid of load sensitive pump 2 is back to subject load sensitive pump 2 after opening.
In addition, being parallel with proportional pressure control valve 11 on the first cut-off reversal valve 8,11 pairs of pumps of proportional pressure control valve carry out electric ratio control System load.
In addition, the first cut-off 8 lower end of reversal valve has been sequentially communicated the second cut-off reversal valve 9 and operated proportional flow control valve 10, The other end of operated proportional flow control valve 10 is connected to fuel tank 15, and 10 aperture of operated proportional flow control valve is to adjust subject load sensitive pump 2 LS hydraulic fluid port pressure.
It is connected between reversal valve 9 and the LS hydraulic fluid port for being tested load sensitive pump 1 in addition, the first cut-off reversal valve 8, second ends There is third to end reversal valve 12, the other end of third cut-off reversal valve 12 is connected to fuel tank 15, and the first cut-off reversal valve 8 is opened, Second cut-off reversal valve 9 is closed, and the switch of control third cut-off reversal valve 12 rings the LS hydraulic fluid port of subject load sensitive pump Answering property is tested.
In addition, 11 one end of proportional pressure control valve is connected in parallel on the first shut-off valve 8, the other end is connected in parallel on operated proportional flow control valve 10 On.
In addition, being successively linked with check valve 5 and filter 6 between subject load sensitive pump 1 and first flowmeter 7.
In addition, being equipped with gate valve 1 between fuel tank 15 and subject load sensitive pump 2.
In addition, being connected with second flowmeter 14, second flowmeter between the S hydraulic fluid port and fuel tank 15 of subject load sensitive pump 2 14 for detecting the draining flow of subject load sensitive pump, to calculate the volumetric efficiency of subject load sensitive pump.
In addition, being connected between the second cut-off reversal valve 9 and fuel tank 15 for after the cooling load by proportional pressure control valve 11 Oil liquid cooler 13.
The specific working principle is as follows for load sensitive pump pilot system of the present invention: the driving subject load sensitive pump 2 of variable-frequency motor 4 Oil liquid is exported through check valve 5 after the filtering of filter 6, subject 2 output stream of load sensitive pump is detected by first flowmeter 7 Amount, is loaded by proportional pressure control valve 11, is realized by command signal to pump electric proportional control load.It is tested load sensitive pump 2 The high pressure oil of output can enter the LS hydraulic fluid port of subject load sensitive pump 2 after opening by bypass the first cut-off reversal valve 8, realize LS Hydraulic fluid port control oil is introduced by subject load sensitive pump itself.The second cut-off reversal valve 9 is opened, operated proportional flow control valve 10 is adjusted Aperture solves subject 2 draining of load sensitive pump to realize the function of the LS hydraulic fluid port pressure adjustable of subject load sensitive pump 2 Flow inaccuracy and nonadjustable two problems of LS hydraulic fluid port pressure.The first cut-off reversal valve 8 is opened, the second cut-off reversal valve is closed 9, the switch of reversal valve 12 is ended by control third, it can be achieved that the LS responsiveness of subject load sensitive pump 2 is tested.
It is different from the prior art, load sensitive pump pilot system of the present invention, it can be in subject load sensitive pump LS hydraulic fluid port pressure Under the conditions of power is adjustable, the dredge oil amount of accurate measurement subject load sensitive pump, and realize the LS response of subject load sensitive pump Property test.
The above description is only an embodiment of the present invention, is not intended to limit the scope of the invention, all to utilize this hair Equivalent structure or equivalent flow shift made by bright description is applied directly or indirectly in other relevant technology necks Domain is included within the scope of the present invention.

Claims (9)

1. a kind of load sensitive pump pilot system, which is characterized in that including fuel tank, the fuel tank is connected to subject load by pipeline Sensitive pump, it is described to be tested the torque revolution speed sensing being connected on load sensitive pump for driving subject load sensitive pump output oil liquid Device and motor, it is described to be tested the first flowmeter being communicated on load sensitive pump for calculating subject load sensitive pump oil pump capacity, The first cut-off reversal valve is communicated in the first flowmeter, the first cut-off reversal valve makes to be tested load sensitive pump after opening Output oil liquid is back to the LS hydraulic fluid port of subject load sensitive pump.
2. load sensitive pump pilot system according to claim 1, which is characterized in that on the first cut-off reversal valve simultaneously It is associated with proportional pressure control valve, the proportional pressure control valve carries out electric proportional control load to subject load sensitive pump.
3. load sensitive pump pilot system according to claim 2, which is characterized in that first cut-off reversal valve lower end It is sequentially communicated the second cut-off reversal valve and operated proportional flow control valve, the other end of the operated proportional flow control valve is connected to oil Case, the operated proportional flow control valve aperture are tested the LS hydraulic fluid port pressure of load sensitive pump to adjust.
4. load sensitive pump pilot system according to claim 3, which is characterized in that the first cut-off reversal valve, the Third cut-off reversal valve is communicated between two cut-off reversal valves and the LS hydraulic fluid port for being tested load sensitive pump, third ends reversal valve The other end is connected to fuel tank, and the first cut-off reversal valve is opened, and the second cut-off reversal valve is closed, and control third ends reversal valve Switch to subject load sensitive pump LS hydraulic fluid port carry out responsiveness test.
5. load sensitive pump pilot system according to claim 4, which is characterized in that described proportional pressure control valve one end is in parallel On the first shut-off valve, the other end is connected in parallel on operated proportional flow control valve.
6. -5 any load sensitive pump pilot system according to claim 1, which is characterized in that the subject load-sensitive Check valve and filter are successively linked between pump and first flowmeter.
7. load sensitive pump pilot system according to claim 6, which is characterized in that the fuel tank and subject load-sensitive Gate valve is equipped between pump.
8. load sensitive pump pilot system according to claim 7, which is characterized in that the S of the subject load sensitive pump Second flowmeter is connected between hydraulic fluid port and fuel tank.
9. load sensitive pump pilot system according to claim 3, which is characterized in that the second cut-off reversal valve and oil The cooler for the oil liquid after the cooling load by proportional pressure control valve is connected between case.
CN201710107738.1A 2017-02-27 2017-02-27 Load sensitive pump pilot system Active CN106762595B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710107738.1A CN106762595B (en) 2017-02-27 2017-02-27 Load sensitive pump pilot system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710107738.1A CN106762595B (en) 2017-02-27 2017-02-27 Load sensitive pump pilot system

Publications (2)

Publication Number Publication Date
CN106762595A CN106762595A (en) 2017-05-31
CN106762595B true CN106762595B (en) 2019-03-05

Family

ID=58960830

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710107738.1A Active CN106762595B (en) 2017-02-27 2017-02-27 Load sensitive pump pilot system

Country Status (1)

Country Link
CN (1) CN106762595B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108760321B (en) * 2018-05-23 2024-01-02 杭州良丰动力设备有限公司 Engine power loading test system
CN109185275B (en) * 2018-10-26 2024-01-09 华南理工大学 Load-sensing constant-pressure variable pump test device, use method and detection method thereof
CN114321108B (en) * 2021-12-29 2023-06-13 湖南三一中型起重机械有限公司 Electrohydraulic composite control system and method and working machine
CN115059606B (en) * 2022-06-21 2023-03-07 重庆大学 Load-sensitive pump control loop simulation test system

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103738396A (en) * 2013-12-27 2014-04-23 三一汽车起重机械有限公司 Constant flow steering system and engineering machinery
CN105221506A (en) * 2015-09-18 2016-01-06 徐州工业职业技术学院 A kind of load-sensitive valve and load-sensitive hydraulic system
CN206917836U (en) * 2017-02-27 2018-01-23 江苏恒立液压科技有限公司 Load sensitive pump pilot system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3694355B2 (en) * 1996-02-09 2005-09-14 日立建機株式会社 Hydraulic drive unit with load sensing control
JP2012122590A (en) * 2010-12-10 2012-06-28 Daikin Industries Ltd Hydraulic unit

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103738396A (en) * 2013-12-27 2014-04-23 三一汽车起重机械有限公司 Constant flow steering system and engineering machinery
CN105221506A (en) * 2015-09-18 2016-01-06 徐州工业职业技术学院 A kind of load-sensitive valve and load-sensitive hydraulic system
CN206917836U (en) * 2017-02-27 2018-01-23 江苏恒立液压科技有限公司 Load sensitive pump pilot system

Also Published As

Publication number Publication date
CN106762595A (en) 2017-05-31

Similar Documents

Publication Publication Date Title
CN106762595B (en) Load sensitive pump pilot system
CN103335834B (en) A kind of throttle valve port performance test device
CN104454748B (en) Reliable comprehensive energy-saving hydraulic test device for gear pumps, overflow valves and one-way valves
WO2018041257A1 (en) Hydraulic system of device for testing comprehensive performance of high-pressure gear flowmeter and testing method
CN103471829A (en) Test stand of multi-way valve of hydraulic excavator
CN103511397A (en) Reliability test method and device for axial plunger pump and axial plunger motor
CN107781155B (en) Test macro, durability test method and performance test methods
CN105181355A (en) Multifunctional testing device of air brake system of tractor transportation unit
CN103343742B (en) Testing system and testing method for characteristics of plunger pump
CN206917836U (en) Load sensitive pump pilot system
CN202370940U (en) Hydraulic oil way suitable for various hydraulic element tests
CN111043105A (en) High-power hydraulic comprehensive test bed and test method thereof
CN205808480U (en) A kind of check valve type metering control
CN205861174U (en) A kind of pipeline liquid sealing and circulating device of intelligence piston volume tube assay device
CN102213635B (en) Testing system for main valve leakage of hydraulic excavator
CN205002971U (en) Many functional test of tractor transportation unit gas braking system device
CN209513290U (en) The test mechanism of simulation test is carried out for exchanging flow control water installations
CN213838891U (en) Flow pressure testing device for vane pump
CN203116821U (en) Manual and automatic calibrating device of liquidometer
CN211449273U (en) Hydraulic motor loading test system
CN207231535U (en) Water-cooling system factory testing system
CN103728138B (en) gear motor performance test method
RU149336U1 (en) DEVICE FOR DETERMINING THE TECHNICAL CONDITION OF THE PUMP
CN201513718U (en) Pipeline structure for quickly and accurately metering liquid capacity
RU2612684C1 (en) Device for determining technical state of pump

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
GR01 Patent grant