CN206430999U - A kind of full-automatic fixed load impact fatigue testing machine - Google Patents
A kind of full-automatic fixed load impact fatigue testing machine Download PDFInfo
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- CN206430999U CN206430999U CN201621416513.1U CN201621416513U CN206430999U CN 206430999 U CN206430999 U CN 206430999U CN 201621416513 U CN201621416513 U CN 201621416513U CN 206430999 U CN206430999 U CN 206430999U
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- guide rod
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- testing machine
- fixed load
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Abstract
The utility model discloses a kind of full-automatic fixed load impact fatigue testing machine, including base, the entablature being connected to by two guide rods on base and the specimen holder being slidably connected between two guide rods, base is provided with one speed reducer, the decelerator is connected with a motor, the decelerator wherein side is connected with eccentric wheel transmission, the eccentric wheel is connected by a connecting rod with an oscillating bearing, the oscillating bearing is installed on specimen holder bottom surface, it is connected on entablature by a load guide rod with a counterweight, buffer is respectively equipped with the load guide rod both sides, the load guide rod upper end is arranged with a crash panel, the crash panel bottom surface is in contact with each buffer, the utility model realize high speed impact remain constant load not with tested sample be recessed and reduce impulsive force, improve the stability of fixed load impact, reduce fault rate, reduction is safeguarded and after cost, so that fixed load impact becomes more practical, fast, efficiently, it is more extensive using scope.
Description
Technical field
The utility model is related to the technical field of test equipment, refers in particular to a kind of full-automatic fixed load impact fatigue testing machine.
Background technology
Fixed load impact fatigue testing machine is a to foam implementation high speed fixed load Impacting endurance testing equipment, is showed
Some fixed load impact fatigue testing machines are usually to fix an eccentric throw to realize quick percussion action using eccentric wheel, are led to
One strength inductor of increase is crossed to control fixed load to impact strength, after test is started, because impacted using eccentric wheel
Stroke is constant all the time in testing, and tested sample foam can be with being recessed soon after repeated stock, therefore sample and punching
Gap between tapping the head is increasing to cause strength suffered by impact head just to become less and less, and fixed load punching is not met increasingly
The sample conditions of experiment are hit, later tests person closed-down manual must adjust the eccentric throw of eccentric wheel to offset the depression of sample repeatedly
Degree maintains constant impact forces as far as possible, and this manual regulation is not only wasted time and energy also very not precisely, and sample is recessed
Sunken speed does not have a rule, and laboratory technician can not analyze when assurance can manually adjust eccentric throw, therefore, in the market this
Kind of phase kind equipment does not reach holding constant load impulsive force this test request, also consumes and take often an experiment work
Journey Shi Quantian most of working time has a strong impact on the operating efficiency of test engineer, meanwhile, regulation also can manually for not timing
The operating efficiency and precision of testing equipment is set to have a greatly reduced quality.
The content of the invention
The purpose of this utility model is to overcome weak point of the prior art and provide a kind of full-automatic fixed load punching
Fatigue tester is hit, the testing machine realizes high speed impact all the time by fixed load load mode optimization transmission driving principle and device
Keep constant load not with tested sample be recessed and reduce impulsive force, improve fixed load impact stability, reduction failure
Rate, reduction are safeguarded and after cost so that fixed load impact becomes more practical, quick, efficient, more extensive using scope.
To achieve the above object, the utility model is adopted the following technical scheme that:
A kind of full-automatic fixed load impact fatigue testing machine, including base, be connected on base by two guide rods
Entablature and the specimen holder being slidably connected between two guide rods, the base be provided with one speed reducer, the decelerator with
One motor is connected, and the decelerator wherein side is connected with eccentric wheel transmission, and the eccentric wheel is closed by a connecting rod with one
Bearings are connected, and the oscillating bearing is installed on specimen holder bottom surface, the entablature by a load guide rod and a counterweight phase
Connection, is respectively equipped with buffer, the load guide rod upper end is arranged with a crash panel, the crash panel bottom surface in the load guide rod both sides
It is in contact with each buffer.
Described four angles of base end face are respectively equipped with a foot pad.
Each seat guide rod is vertically mounted on base two ends, respectively this guide rod upper end be respectively cooperating with a fixed seat with it is upper
Crossbeam corresponding end is connected.
The specimen holder two ends are slidably connected on corresponding seat guide rod by a linear bearing respectively, on the specimen holder
Provided with a sample setting area, the sample setting area is enclosed to set by some fixed blocks to be formed.
Described connecting rod one end is hinged with oscillating bearing, and the connecting rod other end is hinged with deviation wheel.
The crash panel coordinates a connection piece to be sheathed on load guide rod upper end.
The beneficial effects of the utility model are:Its motor via reducer band movable eccentric wheel rotates, and eccentric wheel passes through even
Extension bar promotes the upper and lower motion of specimen holder, when specimen holder is moved upwards, sample will be promoted to impact on counterweight, Ran Hou
Under the guiding of seat guide rod, counterweight drives buffer shock plate to move upwards by load guide rod, adjusts the position of entablature,
Specimen holder is set crash panel is departed from buffer when moving to peak, impact strength now is just equal to the lotus of counterweight
Weight, and then fixed load impact fatigue test is carried out to sample;The load mode generation that the utility model passes through the counterweight of fixed heavy burden
The side that the fixed load for having replaced conventional test device to be combined using actuator (making moving cell), strength sensor and capture card is impacted
Method, realize high speed impact remain constant load not with tested sample be recessed and reduce impulsive force, improve fixed load
The stability of impact, reduction fault rate, reduction are safeguarded and after cost so that fixed load impact becomes more practical, quick, height
Effect;The utility model can be used for the fixed load shock-testing of the multi-class products such as foam, spring bag, seat, using scope more
To be extensive.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is front view of the present utility model.
Drawing reference numeral explanation:
1- bases;11- foots pad;2- guide rods;3- entablatures;4- specimen holders;5- decelerators;6- motors;7- is eccentric
Wheel;8- connecting rods;9- oscillating bearings;E- load guide rods;F- counterweights;G- buffers;H- crash panels;K- connectors;M- fixed seats;
N- linear bearings;P- fixed blocks;Q- samples.
Embodiment
Below in conjunction with Figure of description, the utility model is described in further detail:
As shown in Figure 1-2, the utility model is on a kind of full-automatic fixed load impact fatigue testing machine, including base 1, logical
Cross the entablature 3 that two guide rods 2 are connected on base 1 and the specimen holder 4 being slidably connected between two guide rods 2, bottom
Seat 1 is provided with one speed reducer 5, and the decelerator 5 is connected with a motor 6, and the wherein side of decelerator 5 is driven with an eccentric wheel 7
It is connected, the eccentric wheel 7 is connected by a connecting rod 8 with an oscillating bearing 9, the oscillating bearing 9 is installed on the bottom of specimen holder 4
It is connected on face, entablature 3 by a load guide rod E with a counterweight F, buffer G is respectively equipped with load guide rod E both sides,
Load guide rod E upper ends are arranged with a crash panel H, and crash panel H bottom surfaces are in contact with each buffer G, wherein, the bottom surface of base 1
Four angles are respectively equipped with a foot pad 11, and crash panel H coordinates a connection piece K to be sheathed on load guide rod E upper ends.
As shown in Figure 1-2, each seat guide rod 2 is vertically mounted on the two ends of base 1, and respectively the upper end of this guide rod 2 is respectively cooperating with
One fixed seat M is connected with the corresponding end of entablature 3.
As shown in Figure 1-2, the two ends of specimen holder 4 are slidably connected at corresponding seat guide rod 2 by a linear bearing N respectively
On, the specimen holder 4 be provided with a sample setting area, the sample setting area is enclosed to set by some fixed block P to be formed, each fixed block P it
Between spacing it is consistent.
As shown in Figure 1-2, the one end of connecting rod 8 is hinged with oscillating bearing 9, and the other end of connecting rod 8 is mutually cut with scissors with deviation wheel
Connect.
Before use, sample Q to be tested to be first placed on to the sample deposition of specimen holder 4;In use, motor via reducer
Band movable eccentric wheel 7 rotates, and eccentric wheel 7 promotes the upper and lower motion of specimen holder 4 by connecting rod 8, when specimen holder 4 is moved upwards,
Sample Q will be promoted to impact on counterweight F, be then present under the guiding of guide rod 2, counterweight F is driven by load guide rod
Buffer G shock plates are moved upwards, are adjusted the position of entablature 3, specimen holder 4 is just made crash panel H when moving to peak
Depart from buffer G, the loading of impact strength just equal to counterweight F now.
A kind of full-automatic fixed load impact fatigue testing machine disclosed in the utility model, it passes through the counterweight of fixed heavy burden
F load mode instead of what conventional test device was combined using actuator (making moving cell), strength sensor and capture card
The method of fixed load impact, realizes stable fixed load depression and is automatically replenished loading constant impact forces, fast linked is fixed negative
Carry fatigue loading device, it can be ensured that on the sample for all loading fixed load strength per Secondary Shocks, and as sample difference is impacted
It is tired to be recessed and the corresponding fatigue loading impact stroke of automatic relative adjust automatically automatically, realize high speed impact and remain permanent
Fixed load not with tested sample be recessed and reduce impulsive force, improve fixed load impact stability, reduction fault rate, reduction
Safeguard and after cost so that fixed load impact becomes more practical, quick, efficient;The utility model can be used for foam, bullet
The fixed load shock-testing of the multi-class product such as spring bag, seat is more extensive using scope.
Described above is only, to preferred embodiment of the present utility model, not scope of the present utility model to be defined,
Therefore on the premise of the utility model design spirit is not departed from, this area ordinary skill technical staff is to described in the utility model
In equivalence changes or decoration that construction, feature and principle are made, the protection domain that present utility model application patent all should be fallen into.
Claims (6)
1. a kind of full-automatic fixed load impact fatigue testing machine, including base, be connected to by two guide rods it is upper on base
Crossbeam and the specimen holder being slidably connected between two guide rods, it is characterised in that:The base is provided with one speed reducer, should
Decelerator is connected with a motor, and the decelerator wherein side is connected with eccentric wheel transmission, and the eccentric wheel passes through a connection
Bar is connected with an oscillating bearing, the oscillating bearing be installed on specimen holder bottom surface, the entablature by a load guide rod with
One counterweight is connected, and buffer is respectively equipped with the load guide rod both sides, and the load guide rod upper end is arranged with a crash panel, and this hits
Plate bottom surface is hit to be in contact with each buffer.
2. a kind of full-automatic fixed load impact fatigue testing machine according to claim 1, it is characterised in that:The base bottom
Four, face angle is respectively equipped with a foot pad.
3. a kind of full-automatic fixed load impact fatigue testing machine according to claim 1, it is characterised in that:Each seat is led
Base two ends are vertically mounted on to bar, respectively this guide rod upper end is respectively cooperating with a fixed seat and is connected with entablature corresponding end.
4. a kind of full-automatic fixed load impact fatigue testing machine according to claim 1, it is characterised in that:The specimen holder
Two ends are slidably connected on corresponding seat guide rod by a linear bearing respectively, and the specimen holder is provided with a sample setting area,
The sample setting area is enclosed to set by some fixed blocks to be formed.
5. a kind of full-automatic fixed load impact fatigue testing machine according to claim 1, it is characterised in that:The connecting rod
One end is hinged with oscillating bearing, and the connecting rod other end is hinged with deviation wheel.
6. a kind of full-automatic fixed load impact fatigue testing machine according to claim 1, it is characterised in that:The crash panel
A connection piece is coordinated to be sheathed on load guide rod upper end.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201621416513.1U CN206430999U (en) | 2016-12-22 | 2016-12-22 | A kind of full-automatic fixed load impact fatigue testing machine |
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Application Number | Priority Date | Filing Date | Title |
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CN201621416513.1U CN206430999U (en) | 2016-12-22 | 2016-12-22 | A kind of full-automatic fixed load impact fatigue testing machine |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110375940A (en) * | 2019-08-16 | 2019-10-25 | 西北工业大学 | A kind of low frequency vibration isolation testboard and vibration detecting system |
CN113008658A (en) * | 2021-02-02 | 2021-06-22 | 广州城建职业学院 | Two-wavelength decomposition self-balancing supporting device based on biaxial SHPB experiment |
CN114166667A (en) * | 2021-11-19 | 2022-03-11 | 广东石油化工学院 | Multidirectional physical impact test equipment for testing fatigue of metal material |
-
2016
- 2016-12-22 CN CN201621416513.1U patent/CN206430999U/en not_active Expired - Fee Related
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110375940A (en) * | 2019-08-16 | 2019-10-25 | 西北工业大学 | A kind of low frequency vibration isolation testboard and vibration detecting system |
CN113008658A (en) * | 2021-02-02 | 2021-06-22 | 广州城建职业学院 | Two-wavelength decomposition self-balancing supporting device based on biaxial SHPB experiment |
CN113008658B (en) * | 2021-02-02 | 2024-05-03 | 广州城建职业学院 | Two ripples decompose self-balancing strutting arrangement based on biax SHPB experiment |
CN114166667A (en) * | 2021-11-19 | 2022-03-11 | 广东石油化工学院 | Multidirectional physical impact test equipment for testing fatigue of metal material |
CN114166667B (en) * | 2021-11-19 | 2023-09-29 | 广东石油化工学院 | Multidirectional physical impact test equipment for testing fatigue degree of metal material |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170822 Termination date: 20181222 |
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CF01 | Termination of patent right due to non-payment of annual fee |