CN207742086U - Building ground material is misfired performance aircraft - Google Patents

Building ground material is misfired performance aircraft Download PDF

Info

Publication number
CN207742086U
CN207742086U CN201820151121.XU CN201820151121U CN207742086U CN 207742086 U CN207742086 U CN 207742086U CN 201820151121 U CN201820151121 U CN 201820151121U CN 207742086 U CN207742086 U CN 207742086U
Authority
CN
China
Prior art keywords
misfired
ground material
building ground
performance aircraft
support element
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
CN201820151121.XU
Other languages
Chinese (zh)
Inventor
徐晓滨
刘虹
付永刚
贾海鑫
郭艳梅
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.)
Hohhot Sifang engineering quality testing Co.,Ltd.
Original Assignee
Hohhot Sifang Engineering Quality Testing And Testing Center
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 Hohhot Sifang Engineering Quality Testing And Testing Center filed Critical Hohhot Sifang Engineering Quality Testing And Testing Center
Priority to CN201820151121.XU priority Critical patent/CN207742086U/en
Application granted granted Critical
Publication of CN207742086U publication Critical patent/CN207742086U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Sampling And Sample Adjustment (AREA)

Abstract

Misfire performance aircraft, including the body of top end opening and the cover body at the top of body the utility model discloses building ground material, it is horizontal in body to be equipped with support element, offer pilot hole vertically on support element;Motor and horizontally disposed grinding wheel are equipped in the body of support element lower part, motor is sequentially connected with grinding wheel;It is arranged with guide rod vertically in pilot hole, guide rod lower end is pressed from both sides equipped with test specimen, and fixing sleeve is equipped with pallet on the guide rod on support element top.The utility model is simple in structure, easy to operate, by specimen holder on test specimen folder, and cover body is provided on body, and security risk and the stress for eliminating manual hand manipulation are uncertain, by placing counterweight on pallet, keeps test specimen stress accurate, uniform;It sets grinding wheel to liftable structure, is convenient for the experiment of different test specimens;And the utility model is equipped with dust-extraction unit, optimizes working environment, improves work efficiency.

Description

Building ground material is misfired performance aircraft
Technical field:
Misfire performance aircraft the utility model is related to a kind of testing machine more particularly to building ground material.
Background technology:
Common building earth material is concrete, and general concrete is being subjected to the mechanisms such as collision impact and friction Under be possible to generate spark, and building ground material of misfiring refer to use material and hardening after test specimen, with metal or stone The hard objects such as block are rubbed, impact or when the mechanical tests such as scouring abrasion, not will produce spark;In the row such as military project, chemical industry, oil Industry to the preventing fires of ground, explosion-proof has strict demand.
Existing building ground material misfires test instrument frequently with the hand-held grinding wheel of a diameter of 120mm, demarcates first, Then control starting rotating speed is 600-1200r/min, and the arbitrary portion of test specimen is contacted the grinding wheel of rotation and applies the pressure of 10-20N Power, the place for examining time and grinding wheel friction have no-spark, experiment that need to continue to that each test specimen is worn away and be not less than It could stop after 20g, such as in test without finding any moment spark, it is possible to determine that the material is material of misfiring.
Existing using the method that grinding wheel is tested is held, there are some potential safety problemss, and dust is larger during experiment, work It is poor to make environment, and test accuracy is difficult to control.
Utility model content:
Misfire performance aircraft the purpose of this utility model is to provide a kind of building ground material.
The utility model is implemented by following technical solution:Building ground material is misfired performance aircraft comprising top The body of opening and the cover body at the top of the body, it is horizontal in the body to be equipped with support element, in the support element On offer pilot hole vertically;Motor and horizontally disposed grinding wheel, the electricity are equipped in the body of the support element lower part Machine is sequentially connected with the grinding wheel;It is arranged with guide rod vertically in the pilot hole, the guide rod lower end is pressed from both sides equipped with test specimen, Fixing sleeve is equipped with pallet on the guide rod on the support element top.
Further, the test specimen folder is that inverted " Qian " type presss from both sides, the folder bottom outer wall and the guide rod of the test specimen folder It is fixedly connected, the side wall of the test specimen folder is bolted with puller bolt.
Further, the grinding wheel is connect with the motor coaxle.
Further, further include the screw rod, adjusting rod and pedestal being arranged in the body, the screw rod is vertically arranged In the body, the screw rod is rotatablely connected with the body;The motor is arranged on the base, the pedestal and institute Screw rod is stated to be spirally connected;The body is stretched out in one end of the adjusting rod, and the adjusting rod is rotatablely connected with the body, the adjusting Bar is connect with the screw drive.
Further, it is located at one end in the body in the adjusting rod and is equipped with first bevel gear, on the screw rod It is fixed with and bores tooth by described first with the matched second bevel gear of the first bevel gear, the adjusting rod and the screw rod Wheel and the second bevel gear are sequentially connected.
Further, it is located at described extra-organismal one end in the adjusting rod and is equipped with handwheel, can be realized by shaking handwheel The rotation of adjusting rod, and then the rotation of screw rod is driven, drive pedestal and motor to move up and down.
Further, transparent window is equipped on the side wall of the body.
Further, the cover body is transparent cover.
Further, further include dust removing tube, wind turbine and water tank, one end of the dust removing tube and the cover body or the machine The side wall of body is connected to, and the other end of the dust removing tube is passed through the water tank lower part, and the dust removing tube is equipped with the wind turbine.
The advantages of the utility model:
The utility model is simple in structure, easy to operate, by specimen holder on test specimen folder, and cover body is provided on body, Security risk and the stress for eliminating manual hand manipulation are uncertain, by placing counterweight on pallet, keep test specimen stress accurate Really, uniformly;It sets grinding wheel to liftable structure, is convenient for the experiment of different test specimens;And the utility model is equipped with dedusting dress It sets, optimizes working environment, improve work efficiency.
Description of the drawings:
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only It is some embodiments of the utility model, for those of ordinary skill in the art, in the premise not made the creative labor Under, other drawings may also be obtained based on these drawings.
FIG. 1 is a schematic structural view of the utility model;
Fig. 2 is the sectional view of the utility model.
In figure:Body 1, cover body 2, peep hole 3, support element 4, pilot hole 5, grinding wheel 6, guide rod 7, test specimen folder 8, pallet 9, Screw rod 10, adjusting rod 11, pedestal 12, first bevel gear 13, handwheel 14, second bevel gear 15, dust removing tube 16, wind turbine 17, water tank 18, motor 19, counterweight 20.
Specific implementation mode:
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without creative efforts The every other embodiment obtained, shall fall within the protection scope of the present invention.
Building ground material is misfired performance aircraft, including the body 1 of top end opening and set on the saturating of 1 top of body Bright cover body 2 is equipped with transparent peep hole 3 on the side wall of body 1, horizontal in body 1 to be equipped with support element 4, in support element 4 On offer pilot hole 5 vertically;Be equipped with motor 19 and horizontally disposed grinding wheel 6 in the body 1 of 4 lower part of support element, motor 19 with Grinding wheel 6 is coaxially connected;It is arranged with guide rod 7 vertically in pilot hole 5,7 lower end of guide rod is equipped with test specimen and presss from both sides 8, on the support 4 Fixing sleeve is equipped with pallet 9 on the guide rod 7 in portion.Screw rod 10, adjusting rod 11 and pedestal 12 are additionally provided in body 1, screw rod 10 is perpendicular Straight to be arranged in body 1, screw rod 10 is rotatablely connected with body 1;Motor 19 is arranged on pedestal 12, pedestal 12 and 10 spiral shell of screw rod It connects;Body 1 is stretched out in one end of adjusting rod 11, and adjusting rod 11 is rotatablely connected with body 1, is located at one in body 1 in adjusting rod 11 End be equipped with first bevel gear 13, adjusting rod 11 be located at one end outside body 1 be equipped with handwheel 14, be fixed on screw rod 10 and 13 matched second bevel gear 15 of first bevel gear, adjusting rod 11 and screw rod 10 pass through first bevel gear 13 and second bevel gear 15 It is sequentially connected.
As a kind of specific implementation mode, test specimen presss from both sides 8 and is pressed from both sides for inverted " Qian " type, folder bottom outer wall and the guiding of test specimen folder 8 Bar 7 is fixedly connected, and the side wall of test specimen folder 8 is bolted with puller bolt.
Further include dust removing tube 16, wind turbine 17 and water tank 18 as a kind of specific implementation mode, one end of dust removing tube 16 with The side wall of body 1 is connected to, and the other end of dust removing tube 16 is passed through 18 lower part of water tank, and dust removing tube 16 is equipped with wind turbine 17.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this Within the spirit and principle of utility model, any modification, equivalent replacement, improvement and so on should be included in the utility model Protection domain within.

Claims (9)

  1. The performance aircraft 1. building ground material is misfired, which is characterized in that it include top end opening body and be set to institute The cover body at the top of body is stated, it is horizontal in the body to be equipped with support element, pilot hole is offered vertically on the support element;Institute It states and is equipped with motor and horizontally disposed grinding wheel in the body of support element lower part, the motor is sequentially connected with the grinding wheel; It is arranged with guide rod vertically in the pilot hole, the guide rod lower end is pressed from both sides equipped with test specimen, the institute on the support element top It states fixing sleeve on guide rod and is equipped with pallet.
  2. The performance aircraft 2. building ground material according to claim 1 is misfired, which is characterized in that the test specimen, which presss from both sides, is The folder bottom outer wall of inverted " Qian " type folder, the test specimen folder is fixedly connected with the guide rod, and the side wall of the test specimen folder is spirally connected There is puller bolt.
  3. The performance aircraft 3. building ground material according to claim 1 is misfired, which is characterized in that the grinding wheel and institute State motor coaxle connection.
  4. The performance aircraft 4. building ground material according to claim 3 is misfired, which is characterized in that it further includes setting Screw rod, adjusting rod in the body and pedestal, the screw rod are vertically arranged in the body, the screw rod and the machine Body is rotatablely connected;On the base, the pedestal is spirally connected with the screw rod for the motor setting;It stretches one end of the adjusting rod Go out the body, the adjusting rod is rotatablely connected with the body, and the adjusting rod is connect with the screw drive.
  5. The performance aircraft 5. building ground material according to claim 4 is misfired, which is characterized in that in the adjusting rod One end in the body is equipped with first bevel gear, is fixed on the screw rod matched with the first bevel gear Second bevel gear, the adjusting rod and the screw rod are sequentially connected by the first bevel gear and the second bevel gear.
  6. The performance aircraft 6. building ground material according to claim 4 or 5 is misfired, which is characterized in that in the tune Pole is located at described extra-organismal one end and is equipped with handwheel.
  7. The performance aircraft 7. building ground material according to claim 1 is misfired, which is characterized in that in the body Side wall is equipped with transparent window.
  8. The performance aircraft 8. building ground material according to claim 1 is misfired, which is characterized in that the cover body is Bright cover body.
  9. The performance aircraft 9. building ground material according to claim 1 is misfired, which is characterized in that it further includes dedusting Pipe, wind turbine and water tank, one end of the dust removing tube are connected to the side wall of the cover body or the body, the dust removing tube it is another End is passed through the water tank lower part, and the dust removing tube is equipped with the wind turbine.
CN201820151121.XU 2018-01-29 2018-01-29 Building ground material is misfired performance aircraft Active CN207742086U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820151121.XU CN207742086U (en) 2018-01-29 2018-01-29 Building ground material is misfired performance aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820151121.XU CN207742086U (en) 2018-01-29 2018-01-29 Building ground material is misfired performance aircraft

Publications (1)

Publication Number Publication Date
CN207742086U true CN207742086U (en) 2018-08-17

Family

ID=63124414

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820151121.XU Active CN207742086U (en) 2018-01-29 2018-01-29 Building ground material is misfired performance aircraft

Country Status (1)

Country Link
CN (1) CN207742086U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112611712A (en) * 2020-04-30 2021-04-06 健研检测集团有限公司 Performance tester

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112611712A (en) * 2020-04-30 2021-04-06 健研检测集团有限公司 Performance tester
CN112611712B (en) * 2020-04-30 2022-05-17 健研检测集团有限公司 Material performance tester

Similar Documents

Publication Publication Date Title
CN102944512B (en) The end-surface twisting friction-wear testing machine of a kind of Real-time and Dynamic observation frictional interface and method
CN110987694B (en) Concrete strength monitoring system for engineering supervision
CN209043737U (en) A kind of falling sphere test device for mobile phone glass
CN207742086U (en) Building ground material is misfired performance aircraft
CN103353392B (en) A kind of Automated condtrol torsional bending testing machine
CN106680033A (en) Static cone penetration test type underground water sampling method
CN106353112A (en) Wheel impact fatigue testing machine for high-speed EMU
CN208223993U (en) A kind of electric plastic Rockwell apparatus
CN205148053U (en) Cylinder sample plane polishing device
CN208060249U (en) A kind of soybean detection lift riffle sampler
CN106289698A (en) Solar panel impact resistance detection device
CN210376013U (en) Impact testing machine for simply supported beam
CN213422658U (en) Concrete strength detection equipment convenient to operation
CN209820970U (en) Test equipment for testing torsion performance of metal wire
CN204074096U (en) A kind of ozone resistance test case
CN2525506Y (en) Rotary hydro-concrete water sand wearing machine
CN113390717A (en) Tensile detection device and detection method for rock-soil body
CN209416252U (en) A kind of Construction of Civil Engineering angle square
CN208860274U (en) A kind of concrete carburized depth meter
CN208937446U (en) A kind of engineering mechanics hardness tester
CN206523382U (en) A kind of hammer taps fatigue tester
CN206788007U (en) A kind of rock mechanics anisotropy measurement device
CN214224814U (en) Pendulum impact testing machine
CN108797659A (en) A kind of pile measurement device
CN219121740U (en) Hammering sinking cutter sampler

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CP03 Change of name, title or address

Address after: No.26 Saihan West Street, Saihan District, Hohhot, Inner Mongolia Autonomous Region

Patentee after: Hohhot Sifang engineering quality testing Co.,Ltd.

Address before: 010010 office area of Hohhot construction engineering test center, 26 Saihan West Street, Saihan District, Hohhot, Inner Mongolia Autonomous Region

Patentee before: HOHHOT SIFANG ENGINEERING QUALITY DETECTION AND TEST CENTER

CP03 Change of name, title or address