CN112268790A - Multi-shot continuous launching test platform - Google Patents
Multi-shot continuous launching test platform Download PDFInfo
- Publication number
- CN112268790A CN112268790A CN202011356192.1A CN202011356192A CN112268790A CN 112268790 A CN112268790 A CN 112268790A CN 202011356192 A CN202011356192 A CN 202011356192A CN 112268790 A CN112268790 A CN 112268790A
- Authority
- CN
- China
- Prior art keywords
- projectile
- shot
- permanent magnet
- test platform
- tube
- 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.)
- Pending
Links
- 230000001133 acceleration Effects 0.000 claims 4
- 229920001296 polysiloxane Polymers 0.000 claims 1
- 238000005480 shot peening Methods 0.000 abstract description 8
- 238000005422 blasting Methods 0.000 abstract description 7
- 239000000463 material Substances 0.000 abstract description 7
- 230000007547 defect Effects 0.000 abstract 1
- 238000009434 installation Methods 0.000 abstract 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 5
- 239000000741 silica gel Substances 0.000 description 5
- 229910002027 silica gel Inorganic materials 0.000 description 5
- 239000006187 pill Substances 0.000 description 4
- 239000010410 layer Substances 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- 239000008188 pellet Substances 0.000 description 2
- 239000004484 Briquette Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005489 elastic deformation Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/02—Details
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N3/30—Investigating strength properties of solid materials by application of mechanical stress by applying a single impulsive force, e.g. by falling weight
- G01N3/317—Investigating strength properties of solid materials by application of mechanical stress by applying a single impulsive force, e.g. by falling weight generated by electromagnetic means
Landscapes
- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Biochemistry (AREA)
- General Health & Medical Sciences (AREA)
- General Physics & Mathematics (AREA)
- Immunology (AREA)
- Pathology (AREA)
- Electromagnetism (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The invention provides a multi-shot continuous emission test platform, belongs to the field of shot peening, and solves the defects that shot peening equipment in a laboratory cannot meet the requirement of small material peening and the shot peening speed is not adjustable. The multi-shot continuous launching test platform comprises a shot filling device, a shot driving device and a shot launching device. The projectile is continuously provided by an open type projectile bin, the initial speed is provided by the projectile driving friction wheel, the electromagnetic accelerating coil is electrified when the projectile touches the pressure sensor, and the projectile is accelerated by forward thrust and then is shot on a sample by a magnetic field generated instantly. The initial speed of the projectile can be calculated by a related formula through the rotating speed of the driving friction wheel. The speed of the projectile exiting the launch tube can be measured by a laser speed measuring device. The angle of the sample is controlled to achieve the effect that the shot launching directions are different. The test platform can be used for shot blasting tests in laboratories and has the advantages of simplicity in installation, convenience in operation, good reliability and the like.
Description
Technical Field
The invention relates to the field of shot peening, in particular to a test platform capable of realizing continuous emission of multiple shots and controllable speed and striking angle.
Background
Shot peening is a relatively traditional surface strengthening technology, and utilizes high-speed shots to continuously impact the surface of a material to enable the material to generate elastic-plastic deformation, the hardness and the wear resistance of the surface of the material are improved due to work hardening and grain refinement of a plastic deformation layer, and beneficial residual compressive stress can be formed on the surface layer and the subsurface layer of the material through resilience of elastic deformation. The surface hardness of the material is improved, and the injection of the residual compressive stress can effectively inhibit and hinder the initiation and the propagation of surface cracks.
Currently, many shot blasting devices exist in the market, and the structure of the shot blasting devices is relatively complex, so that the shot blasting devices are mostly suitable for shot blasting and strengthening of large equipment materials. The invention provides a shot peening machine which is simple in structure, small in size and capable of being used for shot peening strengthening of a small sample in a laboratory and further researching relevant changes of the sample after shot peening.
Disclosure of Invention
As described above, the blasting equipment required in the laboratory is required to be simple in structure, easy to operate, small in size and low in cost.
The technical scheme adopted by the invention for solving the technical problems is as follows:
a multi-projectile continuous launching test platform comprises a projectile filling device, a projectile driving device and a projectile launching device. The device is fixed on a truss to form a multi-projectile continuous launching test platform, four support legs of the truss can be fixed on a test bed through bolts, and a laser speed measuring device for projectiles is also fixed on a truss rod.
The bullet filling device comprises a bullet cabin, a variable speed motor, an output shaft, a bullet drive plate, a plastic buckle and a cylindrical table. The plastic button is arranged in the front of the six antennae of the pill driving plate, so that the pills can be prevented from flowing randomly to ensure accurate entering into the pill driving device. The bullet storehouse and the bullet driver plate are all installed on the cylinder table, and the rotation of bullet driver plate is realized by variable speed motor.
The projectile driving device comprises a plastic launching tube and a projectile driving friction wheel. The plastic launching tube consists of a bent tube and a long straight tube, and the bent rod plays a role in guiding and is responsible for accurately entering the projectile driving friction wheel after the projectile falls down. The left side and the right side of the long straight pipe are respectively provided with a driving friction wheel to provide initial speed for the projectile. The pill driving friction wheel consists of a silica gel wheel, a permanent magnet coil rack and a rotor shaft. The rotor shaft is used as the center, the permanent magnet coil is wound on the permanent magnet coil rack, the permanent magnet ring is wound on the permanent magnet coil, and the outermost layer is the silica gel wheel.
The projectile launching device comprises a plastic launching tube, a pressure sensor, an electromagnetic accelerating coil and an infrared generator. The accelerating coil is assembled on a long straight pipe of a plastic launching tube at the front part of the projectile driving device, and the principle of the electromagnetic accelerating coil for accelerating the projectiles is that the energizing coil generates a magnetic field to generate force action on a moving conductive object. The electromagnetic accelerating coil is not always electrified, and the electromagnetic accelerating coil is electrified to launch the projectile only when the projectile with a certain initial speed touches the bottom pressure sensor. The infrared generator can aim at the sample to achieve the purpose of hitting the sample at a fixed point.
The invention provides a miniaturized shot blasting device, the speed of the shot can be controlled by a shot driving device, and the open type magazine provides great convenience for filling the shot. The combination of the friction wheel and the electromagnetic accelerating coil is utilized to solve the problems that the power of the friction wheel is insufficient and the projectile needs a certain initial speed when passing through the electromagnetic accelerating coil. An infrared generator is added in front of the transmitting tube to play a role in auxiliary aiming, and the projectile cannot deviate when striking a sample.
Drawings
The invention will be further described with reference to the accompanying drawings.
FIG. 1 is a perspective view of the present projectile charging, driving and launching apparatus;
FIG. 2 is a top view of FIG. 1;
FIG. 3 is a perspective view of a projectile actuation friction wheel;
FIG. 4 is a top view of the projectile drive friction wheel;
fig. 5 is a perspective view of an open magazine;
FIG. 6 is a perspective view of the projectile charging, driving, launching device and open magazine;
FIG. 7 is a perspective view of a truss;
FIG. 8 is a perspective view of a multiple shot continuous launch test platform;
FIG. 9 is a top view of a multiple shot continuous launch test platform.
Referring to fig. 1 and 8: 1. shot, 2, shot driver plate, 3, plastic button, 4, bolt, 5 variable speed motor and output shaft, 6, cylinder platform, 7 silica gel friction wheel, 8, permanent magnet, 9, permanent magnet coil, 10, permanent magnet coil rack, 11, rotor shaft, 12, pressure sensor 13, electromagnetic accelerating coil, 14, plastic transmitting tube, 15, laser velocimeter, 16, infrared generator, 17, infrared generator outer frame, 18, laser velocimeter, 19, truss rod, 20, magazine, 21, fixed panel.
Detailed Description
The invention is further described below with reference to the accompanying drawings.
As shown in fig. 8, the pellet driver plate 2 and the cylindrical table 6 are mounted on the output shaft of the motor in a base hole system, and the output shaft is driven by the variable speed motor to rotate at a proper speed. The projectile rolls down the ramp of the magazine 20 and falls through the projectile catch plate 2 into the curved tube of the plastic launch tube. Wherein the magazine and the variable speed motor are welded on the fixed panel 21 of the truss.
The projectile falls into the curved tube and is given an initial velocity by the projectile drive means. As shown in fig. 3, the rotor shaft 11 of the drive unit is made in a honeycomb briquette shape to reduce its weight to ensure a quick start when energized. The permanent magnet coil rack 10 is matched with the rotor shaft 11 through a base hole, the permanent magnet coil 9 is wound on the permanent magnet coil rack 10, and the permanent magnet 8 rotates along with the rotation of the silica gel friction wheel 7. As shown in figure 1, two pellet driving friction wheels are arranged in parallel and are assembled at the opening groove of the long straight pipe. As shown in fig. 9, the rotor shaft 11 is fixed to the truss arms 19 at the lower part of the truss.
As shown in fig. 1, the pressure sensor 12 is attached to the long straight tube of the plastic launch tube and does not affect the speed of the projectile advance. The electromagnetic accelerating coil 13 is assembled in the front of the pressure sensor, and after being electrified, the bullet is forced to roll forwards quickly. The infrared generator 16 and the infrared generator outer frame 17 at the left end of the long straight pipe can be freely disassembled or assembled.
The detailed protocol is as follows: see figure 1, the projectile 1 flows out from the magazine, the variable speed motor and the output shaft 5 make the projectile drive plate 2 rotate at a set speed, the plastic buckle 3 can prevent the projectile from running out of the cylindrical table 6, so that the projectile accurately enters the launching tube 14, the projectile drive friction wheel is composed of a silica gel wheel 7, a permanent magnet 8, a permanent magnet coil 9, a permanent magnet coil rack 10 and a rotor shaft 11, the rotor friction wheel can be set to a specific rotating speed to give a certain initial speed to the projectile 1, when the projectile 1 touches the pressure sensor 12, the electromagnetic accelerating coil 13 is instantly electrified to generate a strong magnetic field, so that the projectile 1 receives thrust and then is launched at a high speed to hit the model. Wherein, the infrared generator 16 can mark the position to be hit by the sample, and the laser velometer 18 is arranged on the truss rod 19 and emits laser which passes through the laser velometer hole 15, so that the speed of the projectile which is emitted out of the launching tube can be measured.
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011356192.1A CN112268790A (en) | 2020-11-26 | 2020-11-26 | Multi-shot continuous launching test platform |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011356192.1A CN112268790A (en) | 2020-11-26 | 2020-11-26 | Multi-shot continuous launching test platform |
Publications (1)
Publication Number | Publication Date |
---|---|
CN112268790A true CN112268790A (en) | 2021-01-26 |
Family
ID=74340515
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202011356192.1A Pending CN112268790A (en) | 2020-11-26 | 2020-11-26 | Multi-shot continuous launching test platform |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN112268790A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113091532A (en) * | 2021-03-11 | 2021-07-09 | 哈尔滨工程大学 | Compound driven second grade projectile body accelerating device and experiment platform |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT8920333A0 (en) * | 1988-05-02 | 1989-04-28 | Gen Electric | SYSTEM AND METHOD FOR DETECTING THE CAPACITY AND SPEED OF PARTICLES IN SHOT SHOT PELLING. |
RU2406279C1 (en) * | 2009-06-09 | 2010-12-10 | Федеральное государственное учреждение Российский научный центр "Курчатовский институт" | Coaxial electromagnetic accelerator |
CN106370383A (en) * | 2016-11-29 | 2017-02-01 | 浙江工业大学 | Multistage accelerating shot blasting device |
CN213842839U (en) * | 2020-11-26 | 2021-07-30 | 安徽理工大学 | Multi-shot continuous launching test platform |
-
2020
- 2020-11-26 CN CN202011356192.1A patent/CN112268790A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT8920333A0 (en) * | 1988-05-02 | 1989-04-28 | Gen Electric | SYSTEM AND METHOD FOR DETECTING THE CAPACITY AND SPEED OF PARTICLES IN SHOT SHOT PELLING. |
RU2406279C1 (en) * | 2009-06-09 | 2010-12-10 | Федеральное государственное учреждение Российский научный центр "Курчатовский институт" | Coaxial electromagnetic accelerator |
CN106370383A (en) * | 2016-11-29 | 2017-02-01 | 浙江工业大学 | Multistage accelerating shot blasting device |
CN213842839U (en) * | 2020-11-26 | 2021-07-30 | 安徽理工大学 | Multi-shot continuous launching test platform |
Non-Patent Citations (1)
Title |
---|
张国安;余明友;朱忠尼;夏敏学;: "三相异步感应线圈发射器适用的高功率脉冲电源性能分析", 电气技术, no. 1, 15 April 2010 (2010-04-15) * |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113091532A (en) * | 2021-03-11 | 2021-07-09 | 哈尔滨工程大学 | Compound driven second grade projectile body accelerating device and experiment platform |
CN113091532B (en) * | 2021-03-11 | 2021-09-21 | 哈尔滨工程大学 | Compound driven second grade projectile body accelerating device and experiment platform |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104780985B (en) | Position adjusting device, shooting game device using same, and shooting method thereof | |
CN111579190B (en) | A horizontal ejection-impact type blade cutting bird test device and test method | |
WO2019148829A1 (en) | Device and system for launching projectile, and launcher robot | |
CN106501013A (en) | A kind of equivalent scale model collision test device of train and method | |
CN213842839U (en) | Multi-shot continuous launching test platform | |
CN115541418B (en) | Rock emission device for impact test and application method | |
KR101418077B1 (en) | Apparatus for launching shuttlecock | |
CN112268790A (en) | Multi-shot continuous launching test platform | |
CN106908618A (en) | A kind of micro- Pellet Injection System | |
CN117554017A (en) | Bird strike test device based on electromagnetic loading and test method thereof | |
CN102393163B (en) | Quick-response linked target system | |
CN209809463U (en) | Belt-driven ball training machine | |
CN111111131B (en) | A straight line high throw frisbee device | |
CN108543295B (en) | An intelligent serving device suitable for tennis | |
CN111195427B (en) | Belt-driven ball training machine | |
JP2013106892A (en) | Ball tossing device | |
US3517656A (en) | Centrifugal type projecting device | |
RU2008960C1 (en) | Device for throwing balls out | |
CN109540534B (en) | Continuous Projectile Launching Device and Method for Aeroengine Blade FOD Model | |
AU2016100226B4 (en) | A projectile firing apparatus | |
US6923039B2 (en) | Method and apparatus for testing golf balls | |
CN209809465U (en) | Ball launching device for dog training | |
CN116222945A (en) | A kind of hail launching device and launching method thereof | |
GB2110351A (en) | Rocket launcher simulator | |
CN210131350U (en) | Multipurpose baseball robot |
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 |