CN207746776U - A kind of frock clamp of aviation pipe fitting - Google Patents

A kind of frock clamp of aviation pipe fitting Download PDF

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Publication number
CN207746776U
CN207746776U CN201820145151.XU CN201820145151U CN207746776U CN 207746776 U CN207746776 U CN 207746776U CN 201820145151 U CN201820145151 U CN 201820145151U CN 207746776 U CN207746776 U CN 207746776U
Authority
CN
China
Prior art keywords
pipe fitting
fixing device
frock clamp
spanner
reverse
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
CN201820145151.XU
Other languages
Chinese (zh)
Inventor
陈庆东
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.)
Binzhou University
Original Assignee
Binzhou University
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 Binzhou University filed Critical Binzhou University
Priority to CN201820145151.XU priority Critical patent/CN207746776U/en
Application granted granted Critical
Publication of CN207746776U publication Critical patent/CN207746776U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of frock clamps of aviation pipe fitting,Its structure includes spanner,Fixing device,Button,Body,Stabilizer blade,Indicator light,Pipe fitting,Measuring rod,Pedestal,Radiator window,Switch,Cabinet door,Shaft,Spanner is threadedly coupled with fixing device,Button is electrically connected with body,It is mutually welded with the lower surface of body the upper surface of stabilizer blade,Pipe fitting is located at the upper end of pedestal,The lower surface of pedestal and the upper surface of body fit,Radiator window is integrated with body,A kind of frock clamp of aviation pipe fitting of the utility model,Structure is equipped with fixing device,Fixing device is mounted on body,Pipe fitting is put on protective pad,Reverse-flighted screw rotation is driven by rotating spanner,Stripper plate is driven to be moved on baffle by pulley,Reverse-flighted screw is fixed by bearing,When spanner rotation is motionless,Expression screws,Thereby guarantee that pipe fitting is securely seated between body,Prevent pipe fitting from falling damage,Injure staff by a crashing object.

Description

A kind of frock clamp of aviation pipe fitting
Technical field
The utility model is a kind of frock clamp of aviation pipe fitting, belongs to aviation pipe fitting field.
Background technology
Fixture refers to that machine-building is used for fixing processing object in the process, is allowed to occupy correct position, to receive construction Or the device of detection, also known as fixture, in a broad sense, any process in technical process, be used for it is rapid, it is convenient, safely The device for installing workpiece, all can be described as fixture.
Prior art discloses application No. is:201621026795.4 a kind of aviation pipe fitting frock clamp, structure Including a two-jaw self-centering chuck, two-jaw self-centering chuck includes chuck body, and claw driving mechanism is located in chuck body Two symmetrically arranged claw pedestals are equipped with symmetrically arranged left jamming claw, right jamming claw, left jamming claw and pipe on two claw pedestals It is provided with longitudinal arc groove and lateral arc groove on the right side of part contact, is provided on the left side that right jamming claw is contacted with pipe fitting Longitudinal arc groove and lateral arc groove, but the prior art fixed effect is poor, causes pipe fitting to fall damage, injures work by a crashing object Make personnel.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of frock clamp of aviation pipe fitting, with It is poor to solve prior art fixed effect, the problem of causing pipe fitting to fall damage, injure staff by a crashing object.
To achieve the goals above, the utility model is to realize by the following technical solutions:A kind of aviation pipe fitting Frock clamp, structure include spanner, fixing device, button, body, stabilizer blade, indicator light, pipe fitting, measuring rod, pedestal, heat dissipation Window, switch, cabinet door, shaft, the spanner are threadedly coupled with fixing device, and the button is electrically connected with body, the stabilizer blade Upper surface and the lower surface of body are mutually welded, and the pipe fitting is located at the upper end of pedestal, the lower surface of the pedestal and body it is upper Surface fits, and the radiator window is integrated with body, and the switch is integrated with cabinet door, the shaft with Cabinet door is threadedly coupled, and the shaft is threadedly coupled with body, and the fixing device includes shell, pulley, fixed plate, holder, double To screw rod, baffle, screw hole, sliding screw hole, protective pad, stripper plate, bearing, buffer spring, the pulley is located at the inside of shell, The pulley is connect with barrier slides, and the fixed plate is located at the left end of bearing, the holder and pulley axis connection, described two-way Screw rod is threadedly coupled with sliding screw hole, and the screw hole is integrated with reverse-flighted screw, the upper surface of the protective pad and crowded The lower surface of pressing plate fits, and the bearing and reverse-flighted screw axis connection, the buffer spring are located at the inside of shell.
Further, the indicator light is electrically connected with body.
Further, the lower surface of the measuring rod and the upper surface of body are mutually welded.
Further, the lower surface of the protective pad and the upper surface of pipe fitting fit.
Further, a length of 5cm of the stabilizer blade, width 7cm, a height of 9cm.
Further, the stabilizer blade is rectangular parallelepiped structure.
Further, the reverse-flighted screw is made of stainless steel, and hardness is high and is not easy to get rusty.
Advantageous effect
A kind of frock clamp of aviation pipe fitting of the utility model, structure are equipped with fixing device, fixing device are mounted on On body, pipe fitting is put on protective pad, reverse-flighted screw rotation is driven by rotating spanner, stripper plate is driven to be kept off by pulley It is moved on plate, reverse-flighted screw is fixed by bearing, when spanner rotates motionless, indicated to screw, thereby guarantee that pipe fitting is firmly solid It is scheduled on body, prevents pipe fitting from falling damage, injures staff by a crashing object.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model Sign, objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of the frock clamp of aviation pipe fitting of the utility model;
Fig. 2 is a kind of cross-sectional view of fixing device of the utility model.
In figure:Spanner -1, fixing device -2, button -3, body -4, stabilizer blade -5, indicator light -6, pipe fitting -7, measuring rod -8, Pedestal -9, radiator window -10, switch -11, cabinet door -12, shaft -13, shell -201, pulley -202, fixed plate -203, holder - 204, reverse-flighted screw -205, baffle -206, screw hole -207, sliding screw hole -208, protective pad -209, stripper plate -2010, bearing - 2011, buffer spring -2012.
Specific implementation mode
To make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, below In conjunction with specific implementation mode, the utility model is expanded on further.
It please refers to Fig.1, Fig. 2, the utility model provides a kind of frock clamp technical solution of aviation pipe fitting:Its structure includes Spanner 1, fixing device 2, button 3, body 4, stabilizer blade 5, indicator light 6, pipe fitting 7, measuring rod 8, pedestal 9, radiator window 10, switch 11, cabinet door 12, shaft 13, the spanner 1 are threadedly coupled with fixing device 2, and the button 3 is electrically connected with body 4, the stabilizer blade 5 upper surface and the lower surface of body 4 are mutually welded, and the pipe fitting 7 is located at the upper end of pedestal 9, the lower surface of the pedestal 9 and machine The upper surface of body 4 fits, and the radiator window 10 is integrated with body 4, and the switch 11 is integrated with cabinet door 12 Structure, the shaft 13 are threadedly coupled with cabinet door 12, and the shaft 13 is threadedly coupled with body 4, and the fixing device 2 includes outer Shell 201, pulley 202, fixed plate 203, holder 204, reverse-flighted screw 205, baffle 206, screw hole 207, sliding screw hole 208, protection Pad 209, stripper plate 2010, bearing 2011, buffer spring 2012, the pulley 202 are located at the inside of shell 201, the pulley 202 are slidably connected with baffle 206, and the fixed plate 203 is located at the left end of bearing 2011, and the holder 204 connects with 202 axis of pulley It connecing, the reverse-flighted screw 205 is threadedly coupled with sliding screw hole 208, and the screw hole 207 is integrated with reverse-flighted screw 205, The upper surface of the protective pad 209 and the lower surface of stripper plate 2010 fit, and the bearing 2011 connects with 205 axis of reverse-flighted screw It connects, the buffer spring 2012 is located at the inside of shell 201, and the indicator light 6 is electrically connected with body 4, under the measuring rod 8 Surface and the upper surface of body 4 are mutually welded, and the lower surface and the upper surface of pipe fitting 7 of the protective pad 209 fit, the stabilizer blade 5 a length of 5cm, width 7cm, a height of 9cm, the stabilizer blade 5 is rectangular parallelepiped structure, and the reverse-flighted screw 205 is made of stainless steel, Hardness is high and is not easy to get rusty.
The light monitoring circuit of indicator light 6 described in this patent and the device of electrical equipment work or location status, instruction The working condition that lamp is commonly used in reflection circuit has electricity or without electricity, the working condition operation of electrical equipment, stoppage in transit or experiment and position Set state closure or disconnect etc., the bearing 2011 is a kind of important spare part in contemporary mechanical equipment, its major function is The mechanical rotary body of support, reduces the friction coefficient in its motion process, and ensure its rotating accuracy.
Fixing device 2 is mounted on body 4 when being used, pipe fitting 7 is put on protective pad 209, rotation is passed through Spanner 1 drives reverse-flighted screw 205 to rotate, and drives stripper plate 2010 to be moved on baffle 206 by pulley 202, passes through bearing 2011 fix reverse-flighted screw 205, when spanner rotate it is motionless, indicate to screw, thereby guarantee that pipe fitting 7 is securely seated between body 4, It prevents pipe fitting from falling damage, injures staff by a crashing object.
It is poor that the utility model solves prior art fixed effect, causes pipe fitting to fall damage, injures staff's by a crashing object Problem, the utility model are combined with each other by above-mentioned component, and fixing device is mounted on body, pipe fitting is put into protective pad On, reverse-flighted screw rotation is driven by rotating spanner, drives stripper plate to be moved on baffle by pulley, is fixed by bearing Reverse-flighted screw, when spanner rotate it is motionless, indicate to screw, thereby guarantee that pipe fitting is securely seated between body, prevent pipe fitting from falling damage It is bad, injure staff by a crashing object.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above, for For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art The other embodiment being appreciated that.

Claims (5)

1. a kind of frock clamp of aviation pipe fitting, it is characterised in that:Its structure includes spanner (1), fixing device (2), button (3), body (4), stabilizer blade (5), indicator light (6), pipe fitting (7), measuring rod (8), pedestal (9), radiator window (10), switch (11), Cabinet door (12), shaft (13), the spanner (1) are threadedly coupled with fixing device (2), and the button (3) is electrically connected with body (4) It connects, the upper surface and the lower surface of body (4) of the stabilizer blade (5) are mutually welded, and the pipe fitting (7) is located at the upper end of pedestal (9), institute The lower surface and the upper surface of body (4) for stating pedestal (9) fit, and the radiator window (10) is integrated with body (4), The switch (11) is integrated with cabinet door (12), and the shaft (13) is threadedly coupled with cabinet door (12), the shaft (13) it is threadedly coupled with body (4), the fixing device (2) includes shell (201), pulley (202), fixed plate (203), holder (204), reverse-flighted screw (205), baffle (206), screw hole (207), sliding screw hole (208), protective pad (209), stripper plate (2010), bearing (2011), buffer spring (2012), the pulley (202) are located at the inside of shell (201), the pulley (202) be slidably connected with baffle (206), the fixed plate (203) is located at the left end of bearing (2011), the holder (204) with Pulley (202) axis connection, the reverse-flighted screw (205) with sliding screw hole (208) be threadedly coupled, the screw hole (207) with it is two-way Screw rod (205) is integrated, and the upper surface and the lower surface of stripper plate (2010) of the protective pad (209) fit, institute Bearing (2011) and reverse-flighted screw (205) axis connection are stated, the buffer spring (2012) is located at the inside of shell (201).
2. a kind of frock clamp of aviation pipe fitting according to claim 1, it is characterised in that:The indicator light (6) and machine Body (4) is electrically connected.
3. a kind of frock clamp of aviation pipe fitting according to claim 1, it is characterised in that:Under the measuring rod (8) Surface and the upper surface of body (4) are mutually welded.
4. a kind of frock clamp of aviation pipe fitting according to claim 1, it is characterised in that:The protective pad (209) The upper surface of lower surface and pipe fitting (7) fits.
5. a kind of frock clamp of aviation pipe fitting according to claim 1, it is characterised in that:The stabilizer blade (5) it is a length of 5cm, width 7cm, a height of 9cm.
CN201820145151.XU 2018-01-28 2018-01-28 A kind of frock clamp of aviation pipe fitting Expired - Fee Related CN207746776U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820145151.XU CN207746776U (en) 2018-01-28 2018-01-28 A kind of frock clamp of aviation pipe fitting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820145151.XU CN207746776U (en) 2018-01-28 2018-01-28 A kind of frock clamp of aviation pipe fitting

Publications (1)

Publication Number Publication Date
CN207746776U true CN207746776U (en) 2018-08-21

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820145151.XU Expired - Fee Related CN207746776U (en) 2018-01-28 2018-01-28 A kind of frock clamp of aviation pipe fitting

Country Status (1)

Country Link
CN (1) CN207746776U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109664132A (en) * 2018-11-22 2019-04-23 广州市昊志机电股份有限公司 One kind embracing clamp device and embraces clamping method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109664132A (en) * 2018-11-22 2019-04-23 广州市昊志机电股份有限公司 One kind embracing clamp device and embraces clamping method

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

Granted publication date: 20180821

Termination date: 20200128