CN105136436B - Device and method for testing reliability of sealing ring of oil injector - Google Patents

Device and method for testing reliability of sealing ring of oil injector Download PDF

Info

Publication number
CN105136436B
CN105136436B CN201510452352.5A CN201510452352A CN105136436B CN 105136436 B CN105136436 B CN 105136436B CN 201510452352 A CN201510452352 A CN 201510452352A CN 105136436 B CN105136436 B CN 105136436B
Authority
CN
China
Prior art keywords
fuel injector
sealing ring
simulating piece
vibration
pressing plate
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
CN201510452352.5A
Other languages
Chinese (zh)
Other versions
CN105136436A (en
Inventor
任芸
余国强
贺亚玲
方劲松
邱高上
姚云伟
李捷
田浚廷
刘少云
李书伟
肖汉平
高昂
代超群
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.)
Dongfeng Automobile Co Ltd
Original Assignee
Dongfeng Automobile 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 Dongfeng Automobile Co Ltd filed Critical Dongfeng Automobile Co Ltd
Priority to CN201510452352.5A priority Critical patent/CN105136436B/en
Publication of CN105136436A publication Critical patent/CN105136436A/en
Application granted granted Critical
Publication of CN105136436B publication Critical patent/CN105136436B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Fuel-Injection Apparatus (AREA)

Abstract

The invention discloses a reliability testing device and method for a sealing ring of an oil sprayer. The method comprises a cold-hot alternating test method step and a high-temperature vibration durability test method step. The design of the invention with excellent price and simplification effectively simulates the high-temperature vibration and high-low temperature harsh environment conditions in complex working conditions after the fuel injector and the sealing ring are installed on the engine valve chamber, and simultaneously inspects the working performance adaptability of the test sample under the preset high-temperature vibration condition and high-low temperature condition.

Description

Fuel injector sealing ring RTA reliability test assembly and method
Technical field
The present invention relates to fuel injector sealing ring detection technique field, specially a kind of fuel injector sealing ring reliability testing dress Put and method.
Background technology
The effect of the sealing ring of external fuel injector is to realize the sealing between fuel injector and valve cage cover lid, and sealing ring leads to Pressing plate is crossed to be firmly attached on fuel injector form entirety with fuel injector.Pass through the compression of the one side vulcanised rubber layer of pressing plate The axial float of fuel injector is limited, the sealing ring compression inside sealing ring, is close to fuel injector axial plane and realizes radial seal. The fuel injector and its sealing ring used under engine complex working conditions is, it is necessary to examine sealing ring to the reliable of fuel injector simultaneously Property, is included under the conditions of high-temperature vibrating and alternating hot and cold, the installation function and sealing property of pressing plate and sealing ring to fuel injector. But existing test device is tested using actual fuel injector and sealing ring, method of testing also mostly using manually or Measurement condition environment is single, and not only testing cost is high, and it is not very high to test accurate rate.
The content of the invention
The invention aims to overcome above-mentioned deficiency to provide a kind of fuel injector sealing ring RTA reliability test assembly and side Method.
A kind of fuel injector sealing ring RTA reliability test assembly, including a pair of pressing plates, the fuel injector simulating piece for being provided with the shaft shoulder And the sealing ring of step mounting surface, thrust surface and mounting hole is provided with, the fuel injector simulating piece is located in mounting hole, described One end of pressing plate is fixed on step mounting surface by follower bolt, and the other end of the pressing plate is bonded with the upper surface of the shaft shoulder, The thrust surface is bonded with the lower surface of the shaft shoulder, and one side vulcanization rubber is provided between the other end of the pressing plate and the upper surface of the shaft shoulder Glue-line, the inner wall of the hole installing are provided with the sealing ring coordinated with fuel injector simulating piece, and the inside of the fuel injector simulating piece is real The heart, the top of the fuel injector simulating piece are provided with screwed hole.
A kind of alternating hot and cold method of testing of fuel injector sealing ring RTA reliability test assembly comprises the following steps:001st, spray This part of appearance and size being connected in oily device simulating piece with sealing ring is fabricated to the appearance and size of actual fuel injection device, makes oil spout The total length of device simulating piece is less than the total length of actual fuel injection device, the gross weight of fuel injector simulating piece is equal to actual fuel injection device Gross weight;002nd, described fuel injector sealing ring RTA reliability test assembly is placed horizontally at built in high low temperature cycles test case On pallet, pallet is placed horizontally to the center of high low temperature cycles test case, not accessible high low temperature cycles test case Surrounding;003rd, the power supply of high low temperature cycles test case is connected, the temperature inside the box is dropped to -40 DEG C from room temperature in 1min, it is small to stablize 1 Shi Hou, 100 DEG C are raised to from -40 DEG C in 1min, stablized 1 hour, so far complete a circulation, complete alternating hot and cold circulation 10 It is secondary.
A kind of high-temperature vibrating durability test method of fuel injector sealing ring RTA reliability test assembly comprises the following steps:011、 This part of appearance and size being connected in fuel injector simulating piece with sealing ring is fabricated to the appearance and size of actual fuel injection device, made The total length of fuel injector simulating piece is less than the total length of actual fuel injection device, the gross weight of fuel injector simulating piece is equal to actual fuel injection The gross weight of device;012nd, coordinated using the screwed hole at the top of tooling bracket fastening bolt and fuel injector simulating piece, by described spray Oily device sealing ring RTA reliability test assembly is arranged on fastening device support, records follower bolt torque;013rd, by step 012 Mounted fuel injector sealing ring RTA reliability test assembly and fastening device support are integrally placed in vibration rig and pass through work Dress support fastening bolt is fixed;014th, the power supply of vibration rig is connected, by temperature stabilization in vibration rig in 90 DEG C;015、 Four kinds of measurement conditions are set, carry out single sinusoidal vibration by above-below direction successively under every kind of measurement condition;016th, close and shake The power supply of dynamic test machine, injects kerosene into sealing ring, observe in sealing ring kerosene whether seepage, if seepage returns to upper one Step, if non-leakage turn of next step;017th, the torque of measuring pressure plate bolt, if the torque after high-temperature vibrating is original torque 60% or more than 60%, turn in next step, previous step is returned if less than 60%;018th, whether observation pressing plate is broken after cooling down, and sees Whether cracked examine one side vulcanised rubber layer.
The effective simulation of design of the excellent simplification of valency of the present invention is installed on engine air valve chamber when fuel injector and sealing ring High-temperature vibrating in complex working condition and high/low temperature harsh and unforgiving environments situation afterwards, while test sample is checked in predetermined height Service behaviour adaptability under warm vibration condition and high/low temperature condition.In addition, the present invention can reach following main purpose:1st, survey Test result instructs the design optimization of sealing ring mechanical structure;2nd, structural reliability binding test result, draws structural reliability Judge conclusion.This method can detect the parts of fuel injector sealing ring in high-temperature vibrating durable test and high and low temperature alternative bar Whether there is fracture under part, release or disabler situation, to ensure that its long-term normal table in actual applications works.
Brief description of the drawings
Fig. 1 is alternating hot and cold test mode schematic diagram of the present invention;
Fig. 2 is fuel injector sealing ring RTA reliability test assembly structural representation;
Fig. 3 is high-temperature vibrating durable test view;
Fig. 4 is the structural representation that fuel injector simulating piece is arranged on sealing ring in fastening mounting bracket.
Embodiment
Below in conjunction with the accompanying drawings and embodiment further illustrates the present invention.
Embodiment:A kind of fuel injector sealing ring RTA reliability test assembly of the present invention, including a pair of pressing plates 32, it is provided with the shaft shoulder 21 fuel injector simulating piece 2 and the sealing ring 3 for being provided with step mounting surface 33, thrust surface 35 and mounting hole 36, its feature exist In:The fuel injector simulating piece 2 is located in mounting hole 36, and step peace is fixed in one end of the pressing plate 32 by follower bolt 31 On dress face 33, the other end of the pressing plate 32 is bonded with the upper surface of the shaft shoulder 21, the lower surface of the thrust surface 35 and the shaft shoulder 21 Fitting, is provided with one side vulcanised rubber layer 37, the mounting hole 36 between the other end of the pressing plate 32 and the upper surface of the shaft shoulder 21 Inwall is provided with the sealing ring 34 coordinated with fuel injector simulating piece 2, and the inside of the fuel injector simulating piece 2 is solid, the oil spout The top of device simulating piece 2 is provided with screwed hole 22.
Alternating hot and cold method of testing of the present invention comprises the following steps:001st, being connected in fuel injector simulating piece 2 with sealing ring 3 This part of appearance and size be fabricated to the appearance and size of actual fuel injection device, make fuel injector simulating piece 2 total length be less than it is real The total length of border fuel injector, the gross weight of fuel injector simulating piece 2 is set to be equal to the gross weight of actual fuel injection device;002nd, by described spray Oily device sealing ring RTA reliability test assembly is placed horizontally on the pallet 11 built in high/low temperature alternation test box 1, by the water of pallet 11 The center for being placed in high/low temperature alternation test box 1 is kept flat, the surrounding of not accessible high/low temperature alternation test box 1;003rd, connect The power supply of high/low temperature alternation test box 1, makes the temperature inside the box drop to -40 DEG C from room temperature in 1min, after stablizing 1 hour, in 1min It is interior that 100 DEG C are raised to from -40 DEG C, stablize 1 hour, so far complete a circulation, complete alternating hot and cold and circulate 10 times.
Alternating hot and cold test purpose is installation and sealing work(of the examination sealing ring to fuel injector under high temperature and cryogenic conditions Energy.Fuel injector simulating piece 2 is process according to fuel injector actual outer dimensions, and the purpose for making fuel injector simulating piece 2 is section About testing cost, simplify processing.Therefore, the inside of fuel injector simulating piece 2 for solid construction the oil channel structure without fuel injector, it is outside Structure retains the coupling part of fuel injector and sealing ring, and the overall length of fuel injector simulating piece 2 is less than the physical length of fuel injector, But need to ensure that the simplified weight of fuel injector simulating piece 2 is suitable with the actual weight of fuel injector.The skill of high/low temperature alternation test box 1 Art parameter is as follows:Operating voltage:AC380V ± 10%, 50Hz;Rated power:12kW;Test box temperature range:- 40 DEG C~130 ℃;Temperature accuracy:±1℃.Test condition is as follows:Low temperature:-40℃×1hr;High temperature:100℃×1hr;Cycle-index:10 times, The equipment that the model HRT405E of Chongqing Weier Test Equipment Co., Ltd.'s production can be used.
High-temperature vibrating durability test method comprises the following steps:011st, being connected with sealing ring 3 in fuel injector simulating piece 2 This part of appearance and size is fabricated to the appearance and size of actual fuel injection device, the total length of fuel injector simulating piece 2 is less than reality The total length of fuel injector, the gross weight of fuel injector simulating piece 2 is set to be equal to the gross weight of actual fuel injection device;012nd, using tooling bracket Fastening bolt 5 and the screwed hole 22 at the top of fuel injector simulating piece 2 coordinate, by described fuel injector sealing ring RTA reliability test assembly On fastening device support 6, the torque of follower bolt 31 is recorded;013rd, by mounted fuel injector sealing ring in step 012 RTA reliability test assembly and fastening device support 6 are integrally placed in vibration testing machine 4 and solid by tooling bracket fastening bolt 7 It is fixed;014th, the power supply of vibration testing machine 4 is connected, by temperature stabilization in vibration testing machine 4 in 90 DEG C;The 015th, four kinds of test works are set Condition, carry out single sinusoidal vibration by above-below direction successively under every kind of measurement condition;016th, the electricity of vibration testing machine 4 is closed Source, injects kerosene into sealing ring 3, observe in sealing ring 3 kerosene whether seepage, if seepage returns to previous step, if not permeable Leakage turns in next step;017th, the torque of measuring pressure plate bolt 31, if torque after high-temperature vibrating for original torque 60% or More than 60%, turn in next step, previous step is returned if less than 60%;018th, whether observation pressing plate 32 is broken after cooling down, and observation is single Whether face vulcanised rubber layer 37 is cracked.
The purpose of high-temperature vibrating durable test is under high-temperature vibrating, loading condition, and (emphasis is pressing plate and close to examination sealing ring Seal) installation to fuel injector and sealing function.Fuel injector simulating piece 2 is process according to fuel injector actual outer dimensions, The purpose for making fuel injector simulating piece 2 is to save testing cost, simplifies processing.Therefore, the inside of fuel injector simulating piece 2 is solid knot Structure and the oil channel structure without fuel injector, external structure retain the coupling part of fuel injector and sealing ring, fuel injector simulating piece 2 it is total Body length is less than the physical length of fuel injector, but needs to ensure the actual heavy of the simplified weight of fuel injector simulating piece 2 and fuel injector Amount is suitable.The screwed hole 22 at the top of fuel injector simulating piece 2 is used to be fixed on fastening device support 6.The skill of vibration testing machine 4 Art parameter is as follows:Operating voltage:Three-phase 380V ± 10%, 50Hz;Rated power:16kW;Vibration-testing built-in temperature:90℃; Temperature fluctuation value:±1℃;Temperature accuracy:±1℃;Vibration frequency:1~2000Hz;Mode of vibration:Frequency sweep, it is at random, sinusoidal, it is fixed Frequently, the equipment that the model DC-1000-15 of Suzhou Sushi Testing Instrument Co., Ltd.'s production can be used.Fastening device Support 6 should have enough rigidity, to ensure that the motion of shake table is correctly transferred to the survey of fuel injector simulating piece and sealing ring Sample coupon.Installing plate quality is symmetrical, to reduce the unbalanced load of shake table.
Mode of vibration:According to fuel injector on the basis of the actual installation state of engine, carried out by above-below direction single Sinusoidal vibration.The present embodiment test shares the vibration parameters such as four kinds of measurement conditions, corresponding acceleration (load), frequency and number It is as follows:
The present embodiment test result is as follows:
1) kerosene is injected into sealing ring 3 in the condition of high temperature, is stored at room temperature 72 hours, ne-leakage.
2) torque of follower bolt 31:
3) bolt is disassembled, range estimation pressing plate 32 is intact without fracture, one side vulcanised rubber layer 37 and sealing ring 34.

Claims (1)

1. a kind of high-temperature vibrating durability test method of fuel injector sealing ring RTA reliability test assembly, described device includes a pair of pressures Plate (32), the fuel injector simulating piece (2) for being provided with the shaft shoulder (21) and be provided with step mounting surface (33), thrust surface (35) and peace The sealing ring (3) of hole (36) is filled, the fuel injector simulating piece (2) is located in mounting hole (36), and one end of the pressing plate (32) leads to Cross follower bolt (31) to be fixed on step mounting surface (33), the other end of the pressing plate (32) pastes with the upper surface of the shaft shoulder (21) Close, the thrust surface (35) is bonded with the lower surface of the shaft shoulder (21), the other end of the pressing plate (32) and the upper end of the shaft shoulder (21) One side vulcanised rubber layer (37) is provided between face, mounting hole (36) inwall is provided with close with fuel injector simulating piece (2) cooperation Seal (34), the inside of the fuel injector simulating piece (2) is solid, and the top of the fuel injector simulating piece (2) is provided with screwed hole (22);Characterized in that, the method for testing comprises the following steps:
011st, this part of appearance and size being connected in fuel injector simulating piece (2) with sealing ring (3) is fabricated to actual fuel injection The appearance and size of device, the total length of fuel injector simulating piece (2) is less than the total length of actual fuel injection device, make fuel injector simulating piece (2) gross weight is equal to the gross weight of actual fuel injection device;
012nd, coordinated using the screwed hole (22) at the top of the first tooling bracket fastening bolt (5) and fuel injector simulating piece (2), by institute The fuel injector sealing ring RTA reliability test assembly stated is arranged on fastening device support (6), records follower bolt (31) torque;
013rd, mounted fuel injector sealing ring RTA reliability test assembly in step 012 and fastening device support (6) are integrally put It is in vibration rig (4) and fixed by the second tooling bracket fastening bolt (7);
014th, the power supply of vibration rig (4) is connected, by vibration rig (4) interior temperature stabilization in 90 DEG C;
The 015th, four kinds of measurement conditions are set, carry out single sinusoidal vibration by above-below direction successively under every kind of measurement condition;
016th, the power supply of vibration rig (4) is closed, to the interior injection kerosene of sealing ring (3), whether is observation sealing ring (3) interior kerosene Seepage, if seepage returns to previous step, if non-leakage turn of next step;
017th, the torque of measuring pressure plate bolt (31), if torque after high-temperature vibrating for original torque 60% or 60% with On, turn in next step, previous step is returned if less than 60%;
018th, observe whether pressing plate (32) is broken after cooling down, whether observation one side vulcanised rubber layer (37) is cracked.
CN201510452352.5A 2015-07-29 2015-07-29 Device and method for testing reliability of sealing ring of oil injector Active CN105136436B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510452352.5A CN105136436B (en) 2015-07-29 2015-07-29 Device and method for testing reliability of sealing ring of oil injector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510452352.5A CN105136436B (en) 2015-07-29 2015-07-29 Device and method for testing reliability of sealing ring of oil injector

Publications (2)

Publication Number Publication Date
CN105136436A CN105136436A (en) 2015-12-09
CN105136436B true CN105136436B (en) 2018-01-16

Family

ID=54721867

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510452352.5A Active CN105136436B (en) 2015-07-29 2015-07-29 Device and method for testing reliability of sealing ring of oil injector

Country Status (1)

Country Link
CN (1) CN105136436B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109268183A (en) * 2018-11-20 2019-01-25 宁波裕隆汽车制泵有限公司 A kind of fuel injector installation latch closure and its processing method
CN114577463B (en) * 2022-05-05 2022-08-12 西安航天动力研究所 Reliability evaluation method of bolt injector

Citations (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1322943A (en) * 1970-08-11 1973-07-11 Barkas Werke Veb Fuel injectors for internal combustion engines
CN1546855A (en) * 2003-12-12 2004-11-17 上海交通大学 Sealing device for common rail Injector of diesel engine
CN101131339A (en) * 2007-10-09 2008-02-27 宁波摩士集团股份有限公司 High/low-temperature impact life testing device especially for bearing
CN201464164U (en) * 2009-07-22 2010-05-12 邵阳市通达汽车零部件制造有限公司 High-and-low temperature dynamic cyclic fatigue tester for air springs
CN201731974U (en) * 2010-03-17 2011-02-02 广西玉柴机器股份有限公司 Clamping device of O-shaped seal ring of leakage testing machine
CN102384820A (en) * 2010-09-03 2012-03-21 天津市泽宝水泥制品有限公司 Sealing test method for rubber sealing ring of prestressed concrete tube
CN102539257A (en) * 2011-11-15 2012-07-04 中国商用飞机有限责任公司 Device for measuring high-low temperature durability of sealing element
CN102564881A (en) * 2011-12-19 2012-07-11 北京矿冶研究总院 Titanium alloy anti-adhesion effect simulation test device
CN102607947A (en) * 2012-02-27 2012-07-25 北京工业大学 Nanoindentation test desk and experimental method for interfacial shear force of carbon fiber composite
CN102635475A (en) * 2012-05-05 2012-08-15 中国兵器工业集团第七〇研究所 Installation device of fuel injector with independent cooling space
CN202614472U (en) * 2012-05-14 2012-12-19 山东双环密封科技有限公司 Sealing performance testing machine for mechanical sealing component
CN202757757U (en) * 2012-06-30 2013-02-27 上海美钻设备成套有限公司 Device for testing rapid pressure release of rubber seal
CN202974628U (en) * 2012-10-26 2013-06-05 中国航空动力机械研究所 Elastic ring support stiffness measuring device
CN104175285A (en) * 2014-08-09 2014-12-03 广西玉柴机器股份有限公司 Mounting instrument and mounting method for cylinder cover oil injector hole sealing ring
CN104634529A (en) * 2015-02-13 2015-05-20 清华大学 Experiment table for measuring mounting rigidity and damping of sealing ring

Patent Citations (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1322943A (en) * 1970-08-11 1973-07-11 Barkas Werke Veb Fuel injectors for internal combustion engines
CN1546855A (en) * 2003-12-12 2004-11-17 上海交通大学 Sealing device for common rail Injector of diesel engine
CN101131339A (en) * 2007-10-09 2008-02-27 宁波摩士集团股份有限公司 High/low-temperature impact life testing device especially for bearing
CN201464164U (en) * 2009-07-22 2010-05-12 邵阳市通达汽车零部件制造有限公司 High-and-low temperature dynamic cyclic fatigue tester for air springs
CN201731974U (en) * 2010-03-17 2011-02-02 广西玉柴机器股份有限公司 Clamping device of O-shaped seal ring of leakage testing machine
CN102384820A (en) * 2010-09-03 2012-03-21 天津市泽宝水泥制品有限公司 Sealing test method for rubber sealing ring of prestressed concrete tube
CN102539257A (en) * 2011-11-15 2012-07-04 中国商用飞机有限责任公司 Device for measuring high-low temperature durability of sealing element
CN102564881A (en) * 2011-12-19 2012-07-11 北京矿冶研究总院 Titanium alloy anti-adhesion effect simulation test device
CN102607947A (en) * 2012-02-27 2012-07-25 北京工业大学 Nanoindentation test desk and experimental method for interfacial shear force of carbon fiber composite
CN102635475A (en) * 2012-05-05 2012-08-15 中国兵器工业集团第七〇研究所 Installation device of fuel injector with independent cooling space
CN202614472U (en) * 2012-05-14 2012-12-19 山东双环密封科技有限公司 Sealing performance testing machine for mechanical sealing component
CN202757757U (en) * 2012-06-30 2013-02-27 上海美钻设备成套有限公司 Device for testing rapid pressure release of rubber seal
CN202974628U (en) * 2012-10-26 2013-06-05 中国航空动力机械研究所 Elastic ring support stiffness measuring device
CN104175285A (en) * 2014-08-09 2014-12-03 广西玉柴机器股份有限公司 Mounting instrument and mounting method for cylinder cover oil injector hole sealing ring
CN104634529A (en) * 2015-02-13 2015-05-20 清华大学 Experiment table for measuring mounting rigidity and damping of sealing ring

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
一种新型金属弹性密封环的实验研究;方庆贤 等;《科学通报》;19801231(第5期);第206-209页 *
机械密封静环密封性试验工装设计;庞欣;《机械管理开发》;20110831(第4期);第37-38、40页 *

Also Published As

Publication number Publication date
CN105136436A (en) 2015-12-09

Similar Documents

Publication Publication Date Title
CN101387598B (en) Rock porosity real-time test device under action of Chemosmosis and creep coupling
CN204613077U (en) True triaxial Rock parameter measurement system
CN105020128B (en) Comprehensive performance test bed of fuel pumps
CN105116113A (en) Visualized evaluation device for pressure-bearing drilling fluid plugging and leaking stoppage material property
CN203404164U (en) Test equipment for testing durability of sealing element of hydraulic cylinder
CN105136436B (en) Device and method for testing reliability of sealing ring of oil injector
CN201803832U (en) Tester using acoustic emission signals to detect valve leakage
CN102735549A (en) Multifunctional true triaxial flow solid coupling pressure chamber
CN103939421B (en) A kind of method for testing fatigue for hydraulic cylinder and device
CN106556547B (en) A kind of full sea is deep to simulate friction-wear test platform and pilot system
CN105865874A (en) Sample preparing device suitable for sandy soil laboratory tests
CN102072326A (en) Magnetic liquid sealing process researching device
CN205483440U (en) Solenoid valve testing arrangement on nuclear power station main steam isolating valve
CN109975179B (en) Fission gas diffusion form test device and method during fuel rod breakage
CN106950043B (en) A kind of valve oil seal and oil leak amount detecting device and detection method
CN109060565A (en) A kind of small-sized high frequency and low stress width soil dynamic triaxial apparatus
CN208752001U (en) A kind of environmental protection insulating gas and metal phase capacitive experiment simulator
CN106017880A (en) Piston mechanical fatigue tester capable of applying side force
CN106124702A (en) Dynamic drilling fluid mud cake Simulation evaluation instrument under High Temperature High Pressure
RU123948U1 (en) LARGE VESSEL VESSEL TEST DEVICE
CN108254033B (en) A leak gas mass flow measuring device for aeroengine seal test
CN105628500B (en) A kind of temperature coefficient test system of rock thermal insulation STRESS VARIATION
CN104155187A (en) Closed container strength verification testing method
CN209656236U (en) A kind of automotive oil tank air-tightness detection device
CN105152070A (en) Integrated jack for static load test of building pile foundation

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant