CN204330275U - A kind of air pressure drives ejection type horizontal impact platform - Google Patents

A kind of air pressure drives ejection type horizontal impact platform Download PDF

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Publication number
CN204330275U
CN204330275U CN201420838928.2U CN201420838928U CN204330275U CN 204330275 U CN204330275 U CN 204330275U CN 201420838928 U CN201420838928 U CN 201420838928U CN 204330275 U CN204330275 U CN 204330275U
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China
Prior art keywords
worktable
air pressure
type horizontal
guide rail
ejection type
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Expired - Fee Related
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CN201420838928.2U
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Chinese (zh)
Inventor
尹辉俊
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Guangxi University of Science and Technology
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Guangxi University of Science and Technology
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Abstract

The utility model discloses a kind of air pressure and drive ejection type horizontal impact platform, comprise base, worktable, two-way cylinder, guide rail, waveform generator and latch mechanism; The side of described base is provided with front apron, and opposite side is provided with backboard; Described front apron is provided with waveform generator, for gathering hitting information; Described guide rail is arranged along the axis of worktable, is located between front apron and backboard; Described worktable is installed on guide rail, can do feed motion along guide rail, installation testing part on it; The piston rod of described two-way cylinder is fixed on backboard, and its cylinder body is fixing on the table; Described latch mechanism is used for pinning worktable at homeposition.The utility model solves the complicated operation that existing air pressure level shock testing machine exists, and the problem of poor stability, has the features such as structure is concise and to the point, simple to operate, stationarity is good.<b/>

Description

A kind of air pressure drives ejection type horizontal impact platform
Technical field
The utility model relates to a kind of horizontal impact experiment table, and particularly air pressure drives ejection type horizontal impact platform.
Background technology
In engineering practice, usually shock problem can be run into.Generally speaking, when the object (alluvium) with certain speed collides a static object (by alluvium), the motion of alluvium will be obstructed and in moment stop motion, at this moment just received percussive action by alluvium.In this process, alluvium obtains great backward acceleration, applies very large inertial force by by alluvium.The experiment of simulating this process is called impact acceleration test.In impact acceleration test, external general employing horizontal impact or inclined impact method, the domestic impact test method making still vertical impact testing equipment and inclination with the most use, greatly limit the accuracy of China's impact acceleration test.
At present, elastic string is adopted to be that power (horizontal impact tester as MTS company) produces the impact initial velocity needed from the horizontal impact tester of external import, the pulling force produced due to elastic string is limited, therefore need longer accelerator, require that slideway is longer, ground area of standing is large, and owing to requiring slideway precision higher, cost is also very expensive.Although inclined impact method does not need additionaling power, testing equipment is simple, and because angle of inclination can not be too large, the weight component by generation of tilting is less, also need the slideway grown very much could produce needed for impact initial velocity, floor area is also larger.For the experiment product that length is longer, during test, also produce difficulty very, even cannot reach the impact velocity needed for test.
In China, also there has been the production of relevant research and shaped article in some research institution, as western work large impact test technology investigation the SPT-600 two-way horizontal shock testing machine researched and produced, SPT-1000 horizontal impact platform, SPT-50 horizontal impact platform, SPT-200 horizontal impact platform and 200Kg horizontal impact platform, adopt expansion cylinder as power, use a low-pressure cylinder as worktable return power, corresponding brake gear is used in shock testing machine, but be the increase in the complicacy of equipment, be unfavorable for the maintenance of system, further increase operation easier simultaneously, and the shock testing machine weight ratio of design is larger, be not easy carrying.
Summary of the invention
The purpose of this utility model solves the problem, and provides the air pressure that a kind of structure is concise and to the point, simple to operate, stationarity is good to drive ejection type horizontal impact platform.
Air pressure of the present utility model drives ejection type horizontal impact platform, comprises base, worktable, two-way cylinder, guide rail, waveform generator and latch mechanism; The side of described base is provided with front apron, and opposite side is provided with backboard; Described front apron is provided with waveform generator, for gathering hitting information; Described guide rail is arranged along the axis of worktable, is located between front apron and backboard; Described worktable is installed on guide rail, can do feed motion along guide rail, installation testing part on it; The piston rod of described two-way cylinder is fixed on backboard, and its cylinder body is fixing on the table; Described latch mechanism is used for pinning worktable at homeposition.
Further illustrate as of the present utility model: the piston rod of described two-way cylinder is fixed on backboard by the dish that is connected.
Further illustrate as of the present utility model: the table top of described worktable is fixedly installed fixture, for fixedly mounting test block
Further illustrate as of the present utility model: air pressure drives ejection type horizontal impact platform also to comprise latch mechanism, and described latch mechanism comprises bearing, cylindrical shell, electromagnet, sucker, top board, connecting rod, spring, dead bolt; Described bearing is fixedly installed on base, and described cylindrical shell is fixed on bearing; Described electromagnet is fixedly installed in the bottom in cylindrical shell; Described sucker is positioned at the top of cylindrical shell electromagnet, and leaves space between electromagnet; Described top board is provided with hole; Described connecting rod one end is connected with sucker, and the other end is connected with dead bolt through after the hole on top board; Described spring housing is on the connecting rod between top board and dead bolt, and its diameter is greater than the diameter in hole.
Further illustrate as of the present utility model: described dead bolt is cambered surface near the side of waveform generator, and opposite side is vertical plane.
Further illustrate as of the present utility model: described waveform generator is columniform rubber blanket.
Further illustrate as of the present utility model: the end face of the worktable that described waveform generator is corresponding is provided with TR thin rubber pad.
Air pressure of the present utility model drives ejection type horizontal impact platform to solve the shortcoming and defect of prior art, compared with prior art has following progress:
1, the cylinder of the utility model scheme is two-way cylinder, is cushioned after impact by cylinder back pressure, and simultaneously reference position got back to by the reverse ventilating control worktable of cylinder, compares reset cylinder assembly, equipment more simple, operates more easy.
2, waveform generator is that supporting rubber blanket is advantageously accurate in data, because the hard nonlinear characteristic of rubber tool, if used according to designing and calculating numerical value out, the test bit obtained is not accurate enough, waveform generator needs to add TR thin rubber pad in use and suitably regulates, or suitably can reduce impact velocity, can also obtain data more accurately like this.
3, adopt cylinder as driving mechanism, as long as regulate charge pressure, different impact initial velocities can be obtained, thus obtain different impact acceleration values; And change the rigidity of waveform generator, can obtain different pulse width values, both cooperation, can be met the various impulse test waveforms of design objective requirement, operation is very easy.
Accompanying drawing explanation
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
Fig. 1 is the A-A figure that the utility model air pressure drives ejection type horizontal impact platform.
Fig. 2 is the vertical view figure that the utility model air pressure drives ejection type horizontal impact platform.
Fig. 3 is the A-A figure that the utility model air pressure drives the worktable of ejection type horizontal impact platform.
Fig. 4 is the vertical view that the utility model air pressure drives the worktable of ejection type horizontal impact platform.
In figure, 1-base; 2-worktable; 3-two-way cylinder; 4-guide rail; 5-waveform generator; 6-latch mechanism; 61-cylindrical shell; 62-electromagnet; 63-sucker; 64-top board; 65-connecting rod; 66-spring; 67-dead bolt; 68-bearing; 7-front apron; 8-backboard; 9-TR thin rubber pad; 10-fixture.
Embodiment
See Fig. 1 to Fig. 4, air pressure of the present utility model drives ejection type horizontal impact platform, comprises base 1, worktable 2, two-way cylinder 3, guide rail 4, waveform generator 5 and latch mechanism 6; The side of described base 1 is provided with front apron 7, and opposite side is provided with backboard 8; Described front apron 7 is provided with waveform generator 5, for gathering hitting information; Described guide rail 4 is arranged along the axis of worktable, is located between front apron 7 and backboard 8; Described worktable 2 is installed on guide rail 4, can do feed motion along guide rail 4, installation testing part on it; The piston rod of described two-way cylinder 3 is fixed on backboard 8, and its cylinder body is fixed on worktable 2; Described latch mechanism 6 is for pinning worktable 2 at homeposition.
Latch mechanism 6 is a very important mechanism driving in ejection type horizontal impact platform at air pressure, and make to launch when cylinder launches has enough ejection forces, first cylinder locking, then must pressurize to launching cylinder 3.
The model of cylinder and the selection of parameter, the maximum impact speed preset by shock testing machine, worktable weight, shock waveform generator distance determines, preferentially selects QGBM Ф 100-1000-MF2 to launch cylinder.
Also comprise latch mechanism 6, described latch mechanism 6 comprises bearing 68, cylindrical shell 61, electromagnet 62, sucker 63, top board 64, connecting rod 65, spring 66, dead bolt 67; Described bearing 68 is fixedly installed on base 1, and described cylindrical shell 61 is fixed on bearing 68; Described electromagnet 62 is fixedly installed in the bottom in cylindrical shell 61; Described sucker 63 is positioned at the top of cylindrical shell 61 electromagnet 62, and leaves space between electromagnet 62; Described top board 64 is provided with hole; Described connecting rod 65 one end is connected with sucker 63, and the other end is connected with dead bolt 67 through after the hole on top board 64; Described spring 66 is enclosed within the connecting rod 65 between top board 64 and dead bolt 67, and its diameter is greater than the diameter in hole.Produce magnetic force after electromagnet energising to be got off by sucker suction, drive dead bolt to move downward, after electromagnet dead electricity, sucker toward pull-up, drives dead bolt to move upward by spring.In actual use procedure, electromagnet can select commonplace on market and low-cost coiled electrical magnet.
When selecting spring, the elasticity coefficient of spring can be determined like this: latch mechanism 6 just works in the course of the work after compression cylinder quits work, so the friction force that latch mechanism overcomes is smaller, the force of compression just overcoming the gravity of sucker 63 and dead bolt 67 self and spring is just passable.According to measure sucker and locking block general assembly (TW) be M, determine its weight by formula G=Mg, the rigidity of getting holddown spring is K, and the displacement of permission is D, then the elasticity coefficient of spring is K=G/D.
Electromagnet model and specification select aspect: can according to sucker weight and the actual Mo Chali be subject to, consult coiled electrical magnet model in industry and parameter form is selected.
Guide rail is crucial parts in this design.Shock testing machine instantaneous velocity is operationally very large, so require that guide rail has very little friction force and high precision.Therefore the guide rail preferentially selected is high-precision rolling linear guide, and its advantage is: precision is high, friction force is little, stable working.
Described waveform generator 5 is provided with TR thin rubber pad 9 with front apron 7.Because the hard nonlinear characteristic of rubber tool, suitably regulate so semisinusoidal waveform generator can add TR thin rubber pad 9 in use, or suitably can reduce impact velocity, so just can obtain correct data.
Described positive stop 7 and backboard 8 trapezoidal buffer stopper is all installed.The infringement that the powerful impulsive force produced in minimizing shock process causes baffle plate and base 1, strengthens being fixedly connected with of cylinder, to produce larger acceleration simultaneously.
Described dead bolt 67 is cambered surface near the side of waveform generator 5, and opposite side is vertical plane.
Described waveform generator 5 is columniform rubber blanket.
The end face of the worktable of described waveform generator 5 correspondence is provided with TR thin rubber pad 9.
The piston rod of described two-way cylinder 3 is fixed on backboard 8 by the dish that is connected.
The table top of described worktable 2 is fixedly installed fixture 10, for fixedly mounting test block.
In use procedure: first guarantee that cylinder 3 and worktable 2 can be free to slide on linear motion guide 4, test specimen is arranged on the fixture 10 of work top.Electromagnet 62 power-off, mechanical interlock mechanism dead bolt 67 stretches out, locking worktable 2, then cylinder 3 is inflated, pressure in adjusting cylinders is after setting value, coiled electrical magnet 62 in latch mechanism is energized, produce attractive force, adhesive sucker 63 drives dead bolt 67 to move down, worktable 2 is impacted in release, the accelerated motion on guide rail 4 under the effect of gaseous tension of cylinder and worktable 2, clash into the waveform generator 5 of front apron 7, produce corresponding surge waveform, impact completes exhaust hood 3 and oppositely inflates, control worktable 2 and get back to reference position, coiled electrical magnet 62 dead electricity in latch mechanism 6, attractive force disappears, dead bolt 67 stretches out locking worktable 2, complete one-shot process.As can be seen from above impact process, regulate charge pressure, different impact initial velocities can be obtained, thus obtain different impact acceleration values; And change the rigidity of waveform generator, different pulse width values can be obtained, both cooperation, the various impulse test waveforms of design objective requirement can be met.

Claims (7)

1. air pressure drives an ejection type horizontal impact platform, comprises base (1), worktable (2), two-way cylinder (3), guide rail (4), waveform generator (5) and latch mechanism (6); It is characterized in that: the side of described base (1) is provided with front apron (7), and opposite side is provided with backboard (8); Described front apron (7) is provided with waveform generator (5), for gathering hitting information; Described guide rail (4) is arranged along the axis of worktable, is located between front apron (7) and backboard (8); Described worktable (2) is installed on guide rail (4), can do feed motion, installation testing part on it along guide rail (4); The piston rod of described two-way cylinder (3) is fixed on backboard (8), and its cylinder body is fixed on worktable (2); Described latch mechanism (6) is for pinning worktable (2) at homeposition.
2. air pressure according to claim 1 drives ejection type horizontal impact platform, it is characterized in that: the piston rod of described two-way cylinder (3) is fixed on backboard (8) by the dish that is connected.
3. air pressure according to claim 1 drives ejection type horizontal impact platform, it is characterized in that: the table top of described worktable (2) is fixedly installed fixture (10), for fixedly mounting test block.
4. air pressure according to claim 1 drives ejection type horizontal impact platform, it is characterized in that: also comprise latch mechanism (6), described latch mechanism (6) comprises bearing (68), cylindrical shell (61), electromagnet (62), sucker (63), top board (64), connecting rod (65), spring (66), dead bolt (67); Described bearing (68) is fixedly installed on base (1), and described cylindrical shell (61) is fixed on bearing (68); Described electromagnet (62) is fixedly installed in the bottom in cylindrical shell (61); Described sucker (63) is positioned at the top of cylindrical shell (61) electromagnet (62), and leaves space between electromagnet (62); Described top board (64) is provided with hole; Described connecting rod (65) one end is connected with sucker (63), and the other end is connected with dead bolt (67) through after the hole on top board (64); Described spring (66) is enclosed within the connecting rod (65) that is positioned between top board (64) and dead bolt (67), and its diameter is greater than the diameter in hole.
5. air pressure as claimed in claim 4 drives ejection type horizontal impact platform, it is characterized in that: described dead bolt (67) is cambered surface near the side of waveform generator (5), and opposite side is vertical plane.
6. air pressure according to claim 1 drives ejection type horizontal impact platform, it is characterized in that: described waveform generator (5) is columniform rubber blanket.
7. air pressure according to claim 6 drives ejection type horizontal impact platform, it is characterized in that: the end face of the worktable that described waveform generator (5) is corresponding is provided with TR thin rubber pad (9).
CN201420838928.2U 2014-12-26 2014-12-26 A kind of air pressure drives ejection type horizontal impact platform Expired - Fee Related CN204330275U (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104515668A (en) * 2014-12-26 2015-04-15 广西科技大学 Ejection-type horizontal impact platform driven by air pressure
CN106768782A (en) * 2017-01-10 2017-05-31 北京强度环境研究所 One kind blocks impact test apparatus
CN108088641A (en) * 2018-01-16 2018-05-29 南京航空航天大学 A kind of sand dust collision reaction testing stand and test method
CN108181074A (en) * 2018-01-25 2018-06-19 中北大学 A kind of lightweight Pneumatic horizontal shock testing machine with horizontal shock-absorbing structure
KR20220153318A (en) * 2021-05-11 2022-11-18 한국항공우주산업 주식회사 A electro-mechanical actuator integration environment simulation device for flight control simulation of a rotorcraft and a flight control simulation system for a rotorcraft including the same

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104515668A (en) * 2014-12-26 2015-04-15 广西科技大学 Ejection-type horizontal impact platform driven by air pressure
CN106768782A (en) * 2017-01-10 2017-05-31 北京强度环境研究所 One kind blocks impact test apparatus
CN108088641A (en) * 2018-01-16 2018-05-29 南京航空航天大学 A kind of sand dust collision reaction testing stand and test method
CN108181074A (en) * 2018-01-25 2018-06-19 中北大学 A kind of lightweight Pneumatic horizontal shock testing machine with horizontal shock-absorbing structure
KR20220153318A (en) * 2021-05-11 2022-11-18 한국항공우주산업 주식회사 A electro-mechanical actuator integration environment simulation device for flight control simulation of a rotorcraft and a flight control simulation system for a rotorcraft including the same
KR102595516B1 (en) * 2021-05-11 2023-10-31 한국항공우주산업 주식회사 A electro-mechanical actuator integration environment simulation device for flight control simulation of a rotorcraft and a flight control simulation system for a rotorcraft including the same

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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150513

Termination date: 20171226

CF01 Termination of patent right due to non-payment of annual fee