CN206410933U - A kind of pressure testing machine - Google Patents

A kind of pressure testing machine Download PDF

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Publication number
CN206410933U
CN206410933U CN201720095193.2U CN201720095193U CN206410933U CN 206410933 U CN206410933 U CN 206410933U CN 201720095193 U CN201720095193 U CN 201720095193U CN 206410933 U CN206410933 U CN 206410933U
Authority
CN
China
Prior art keywords
fuselage
entablature
testing machine
pressure testing
bearing 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.)
Expired - Fee Related
Application number
CN201720095193.2U
Other languages
Chinese (zh)
Inventor
林耀棋
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.)
Zhejiang Giant Pipe Co Ltd
Original Assignee
Zhejiang Giant Pipe 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 Zhejiang Giant Pipe Co Ltd filed Critical Zhejiang Giant Pipe Co Ltd
Priority to CN201720095193.2U priority Critical patent/CN206410933U/en
Application granted granted Critical
Publication of CN206410933U publication Critical patent/CN206410933U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

Utility model is related to field of test instrument, specially a kind of pressure testing machine.It includes main frame and control slave, described main frame includes fuselage, column, equipment, and equipment includes oil cylinder, upper bearing plate, lower bearing plate, screw mandrel, fixing device, and control slave is located at the side of main frame, including controlling switch, handwheel, display screen, it is each provided on control slave fuselage.A kind of pressure testing machine that the utility model is provided, advantage is:Strengthen fixed effect by adding fixing device, it is ensured that measured object is difficult skew in test process, improves measuring accuracy;The design that entablature is connected by nut, realizes the detachable of entablature, is easy to entablature and is connected to the screw mandrel of entablature to be changed at any time.

Description

A kind of pressure testing machine
Technical field
Utility model is related to field of test instrument, specially a kind of pressure testing machine.
Background technology
Pressure testing machine is also referred to as electron pressure testing machine, is primarily adapted for use in rubber, plastic plate, tubing, profile shapes, plastics The various physical and mechanical properties test of the materials such as film, electric wire, waterproof roll, wire, carton.Pressure testing machine works During there are problems that indicating value mostly, this be due to dynamometry piston with jacking block position misalignment or column Under nut do not tighten and cause, the fixed effect difference of pressure testing machine turns into one of big factors of influence test effect, and pressure Force tester frequent operation is easily caused screw mandrel damage mostly, changes inconvenience, is unfavorable for permanent work.
The content of the invention
The purpose of utility model is in view of the above-mentioned problems, there is provided a kind of good fixing effect, detachable screw mandrel and entablature Pressure testing machine.
To reach above-mentioned purpose, utility model employs following technical proposal:A kind of pressure testing machine, including main frame and control Slave processed, described main frame includes fuselage, column, equipment, and described column is located on fuselage, connects the upper of fuselage upper end Crossbeam and the sill of lower end, described equipment include oil cylinder, upper bearing plate, lower bearing plate, screw mandrel, fixing device, work Plug, described oil cylinder is located at below fuselage, and lower bearing plate is provided with above oil cylinder, and described fixing device is located at lower bearing plate upper table Face, described screw mandrel is connected to the lower section of the entablature, positioned at the surface of oil cylinder, twist, is connected with below screw mandrel Upper bearing plate;Described control slave is located at the side of main frame, including controlling switch, handwheel, display screen, is each provided at control slave On fuselage.
In a kind of pressure testing machine described above, described fixing device is made up of two intersecting hold-down bars.Phase The fixed side design of friendship enhances the fixed effect of measured object, improves measurement accuracy.
In a kind of pressure testing machine described above, described control slave lower end is provided with roller mount.Roller mount makes control Slave processed may move, and enhance the mobility of control slave.
In a kind of pressure testing machine described above, described entablature is connected by nut with fuselage.Pass through nut Connected mode realize entablature and be connected to the dismounting of the screw mandrel of entablature, be easy to the part replacement after wear damage.
Compared with prior art, the advantage of utility model is, pressure testing machine is consolidated by two intersecting hold-down bars Determine device enhancing fixed effect, it is ensured that measured object is difficult skew in test process, prevent test indicating value from swinging back and forth, improve The experiment accuracy of complete machine;The design that entablature is connected by nut, realizes the detachable of entablature, is easy to entablature and company The screw mandrel for being connected on entablature is changed at any time, extends the service life of complete machine;Control the design of slave bottom roller seat just In closely moving for control slave, strengthen mobility.
Brief description of the drawings
In order to illustrate more clearly of inventive embodiments or technical scheme of the prior art, below to by embodiment or existing The accompanying drawing used required in technology description is briefly described, it is therefore apparent that drawings in the following description are only invention Some embodiments, for those of ordinary skill in the art, without having to pay creative labor, can also basis These accompanying drawings obtain other accompanying drawings.
Fig. 1 is intended to for diagram of the present utility model.
Embodiment
Below in conjunction with the accompanying drawing in utility model embodiment, the technical scheme in utility model embodiment is carried out clear Remove, complete description, it is clear that described embodiment is only a part of embodiment of utility model, rather than whole implementation Example, based on the embodiment in utility model, for the those of ordinary skill of field, is obtained on the premise of not paying creative work The every other embodiment obtained, belongs to the scope of utility model protection.
As shown in figure 1, a kind of pressure testing machine, including main frame 1 and control slave 2, described main frame 1 includes fuselage 3, vertical Post 4, equipment 5, described column 4 are located on fuselage 3, the entablature 6 of connection fuselage 3 upper end and the sill 7 of lower end, institute The equipment 5 stated includes oil cylinder 8, upper bearing plate 9, lower bearing plate 10, screw mandrel 11, fixing device 12, piston 13, described oil Cylinder 8 is located at the lower section of fuselage 3, and the top of oil cylinder 8 is provided with lower bearing plate 10, and described fixing device 12 is located at the lower upper table of bearing plate 10 Face, described screw mandrel 11 is connected to the lower section of the entablature 6, positioned at the surface of oil cylinder 8, twist, the lower section of screw mandrel 11 It is connected with bearing plate 9;Described control slave 2 is located at the side of main frame 1, including controlling switch 14, handwheel 15, display screen 16, it is each provided on the control fuselage of slave 2.
Main frame 1 includes fuselage 3, column 4, equipment 5, and described column 4 is located on fuselage 3, connection fuselage 3 upper end Entablature 6 and the sill of lower end 7, entablature 6 are connected by nut with fuselage 3, and upper horizontal stroke is realized by the connected mode of nut The replacing at any time of beam 6, is easy to entablature 6 and is connected to the replacement after the screw mandrel 11 of entablature 6 is damaged;Equipment 5 includes oil Cylinder 8, upper bearing plate 9, lower bearing plate 10, screw mandrel 11, fixing device 12, piston 13, described oil cylinder 8 are located at the lower section of fuselage 3, oil The top of cylinder 8 is provided with lower bearing plate 10, and lower bearing plate 10 is moved upwards by the effect of oil cylinder 8, applies larger pressure, fixed dress Put 12 and be located at the lower upper surface of bearing plate 10, fixing device 12 is made up of two intersecting hold-down bars, regulation is easy in intersecting shape design Fixation, enhances the fixed effect of measured object, prevents the measurement influence caused by the skew of object;Control slave 2 is set In the side of main frame 1, including controlling switch 14, handwheel 15, display screen 16, it is each provided on the control fuselage of slave 2, controls slave 2 Bottom is provided with roller mount 17, is easy to control closely moving for slave 2, enhances mobility.
Utility model preferred embodiment is the foregoing is only, not to limit essence of the utility model in utility model Within refreshing and principle, any modification made, equivalent substitution, improve etc., it should be included within the protection domain of utility model.

Claims (4)

1. a kind of pressure testing machine, including main frame (1) and control slave (2), it is characterised in that described main frame (1) includes machine Body (3), column (4), equipment (5), described column (4) are located on fuselage (3), connect the entablature of fuselage (3) upper end (6) and lower end sill (7), described equipment (5) includes oil cylinder (8), upper bearing plate (9), lower bearing plate (10), silk Bar (11), fixing device (12), piston (13), described oil cylinder (8) are located at below fuselage (3), are provided with down and are held above oil cylinder (8) Pressing plate (10), described fixing device (12) is located at lower bearing plate (10) upper surface, and described screw mandrel (11) is connected on described The lower section of crossbeam (6), the surface positioned at oil cylinder (8) twist, bearing plate (9) is connected with below screw mandrel (11);It is described Control slave (2) be located at the side of main frame (1), including controlling switch (14), handwheel (15), display screen (16), be each provided at control On slave (2) fuselage processed.
2. a kind of pressure testing machine according to claim 1, it is characterised in that described fixing device (12) is by two phases The hold-down bars composition of friendship.
3. a kind of pressure testing machine according to claim 1, it is characterised in that described control slave (2) lower end is provided with Roller mount (18).
4. a kind of pressure testing machine according to claim 1, it is characterised in that described entablature (6) by nut with Fuselage (3) is connected.
CN201720095193.2U 2017-01-19 2017-01-19 A kind of pressure testing machine Expired - Fee Related CN206410933U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720095193.2U CN206410933U (en) 2017-01-19 2017-01-19 A kind of pressure testing machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720095193.2U CN206410933U (en) 2017-01-19 2017-01-19 A kind of pressure testing machine

Publications (1)

Publication Number Publication Date
CN206410933U true CN206410933U (en) 2017-08-15

Family

ID=59557436

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720095193.2U Expired - Fee Related CN206410933U (en) 2017-01-19 2017-01-19 A kind of pressure testing machine

Country Status (1)

Country Link
CN (1) CN206410933U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107560947A (en) * 2017-10-10 2018-01-09 河南省产品质量监督检验院 Assembly type smoke evacuation discharge duct pressure testing machine and its application method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107560947A (en) * 2017-10-10 2018-01-09 河南省产品质量监督检验院 Assembly type smoke evacuation discharge duct pressure testing machine and its application method

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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: 20170815

Termination date: 20200119

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