CN210524457U - Positioner is used in aircraft model processing - Google Patents

Positioner is used in aircraft model processing Download PDF

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Publication number
CN210524457U
CN210524457U CN201921472337.7U CN201921472337U CN210524457U CN 210524457 U CN210524457 U CN 210524457U CN 201921472337 U CN201921472337 U CN 201921472337U CN 210524457 U CN210524457 U CN 210524457U
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CN
China
Prior art keywords
fixed pipe
aircraft model
permanent magnet
fixed
plate
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Expired - Fee Related
Application number
CN201921472337.7U
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Chinese (zh)
Inventor
曹自荣
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Chengdu Hangmai Technology Co ltd
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Chengdu Hangmai Technology 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.)
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Publication date
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Priority to CN201921472337.7U priority Critical patent/CN210524457U/en
Application granted granted Critical
Publication of CN210524457U publication Critical patent/CN210524457U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model relates to a machine model processing technology field just discloses a positioner is used in aircraft model processing, comprising a base plate, the left and right sides of bottom plate bottom all sets up threaded hole, the top fixed mounting of bottom plate has fixed pipe, the inside movable mounting of fixed pipe has the stopper, fixed mounting has the permanent magnet on the interior roof of fixed pipe, peg graft in the front of fixed pipe and have the collecting plate that is located the permanent magnet top, the inside fixed mounting of collecting plate has the filter screen, fixed mounting has the intubate that is located the permanent magnet left and right sides on the interior diapire of fixed pipe. This positioner is used in aircraft model processing adds man-hour to aircraft model through setting up the hole that leaks, has reached the effect of being convenient for clear up the metal piece that produces, and labour saving and time saving has reduced the cost of labor, and it is more convenient to use, simultaneously through setting up the spring, can slow down the impact force that stopper and workstation received to make the workstation more reliable and more stable.

Description

Positioner is used in aircraft model processing
Technical Field
The utility model relates to an aircraft model processing technology field specifically is a positioner is used in aircraft model processing.
Background
The model is an object (the object is not equal to an object, is not limited to a solid body and a virtual body, and is not limited to a plane and a solid body) which forms an expression purpose of objectively describing a morphological structure through subjective consciousness by means of a solid body or a virtual body, and in a broad sense: if one thing can be changed along with the change of another thing, then this thing is the model of another thing, and the effect of model is the nature of expressing different concepts, and a concept can make many models change to different extents, but can express the nature of a concept as long as few models, so a concept can change the expression form of nature through referring to different models, and of course, the aircraft model is only one of them, and is also more common simultaneously, has collection value.
At present, because the airplane models of metal are machined by using machine tools mostly, metal scraps generated in machining are inconvenient to remove, time and labor are wasted when manual work is carried out for cleaning, the manual cost is improved, and the airplane models are inconvenient to use, so that the positioning device for machining the airplane models is provided to solve the problems.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model provides a be not enough to prior art, the utility model provides a positioner is used in aircraft model processing possesses the advantage such as being convenient for clear away the piece, has solved positioner is used in aircraft model processing on the present market, because the aircraft model that uses the lathe to come the metal now mostly processes, and the metal piece that produces in the processing is detached very inconveniently, and the manual work is not only time-wasting but also more power consuming when clearing up, has improved artificial cost, uses very inconvenient problem.
(II) technical scheme
In order to realize the above-mentioned piece purpose of being convenient for clear away, the utility model provides a following technical scheme: a positioning device for processing an airplane model comprises a bottom plate, wherein threaded holes are respectively formed in the left side and the right side of the bottom plate, a fixed pipe is fixedly installed at the top of the bottom plate, a limiting block is movably installed in the fixed pipe, a permanent magnet is fixedly installed on the inner top wall of the fixed pipe, a collecting plate positioned at the top of the permanent magnet is inserted in the front of the fixed pipe, a filter screen is fixedly installed in the collecting plate, insertion pipes positioned at the left side and the right side of the permanent magnet are fixedly installed on the inner bottom wall of the fixed pipe, a movable plate fixedly installed at the bottom of the limiting block is movably installed in the insertion pipes, a spring is fixedly installed at the bottom of the movable plate, water leakage holes are respectively formed in the left side and the right side of the fixed pipe, a workbench is fixedly installed at the top, the top of the supporting rod is fixedly provided with a fixed block, and the top of the workbench, which is positioned at the opposite side of the supporting rod, is provided with a material leaking hole.
Preferably, the through hole is opened to the inside of stopper, and the through hole is hourglass hopper-shaped and is linked together with the hole that leaks the material.
Preferably, the connecting part of the fixed pipe and the collecting plate is provided with a sliding chute, and the collecting plate is movably connected with the fixed pipe through the sliding chute.
Preferably, the inner wall of the insertion tube is provided with a movable groove, and the movable plate is movably connected with the insertion tube through the movable groove.
Preferably, the number of the springs is two, and the springs are distributed in a left-right symmetrical mode.
Preferably, the number of the water leakage holes is two, and the water leakage holes are distributed in a bilateral symmetry mode.
(III) advantageous effects
Compared with the prior art, the utility model provides a positioner is used in aircraft model processing possesses following beneficial effect:
the positioning device for processing the airplane model is provided with the material leaking hole, when the airplane model is processed, the generated metal scraps and water are discharged from the material leaking hole together, then the metal scraps and water pass through the limiting block and enter the fixed pipe, the mixture formed by the metal scraps and the water is filtered by the filter screen, solid and liquid are separated, the water flows out of the water leakage holes, the metal scraps are separated on the filter screen, and the permanent magnet can generate adsorption force to the metal debris by arranging the permanent magnet, so that the metal debris can be attached to the filter screen, then the collecting plate is drawn out to recycle the collected metal scraps, thereby achieving the effect of conveniently cleaning the generated metal scraps, saving time and labor, reducing the labor cost, being more convenient to use, simultaneously, the impact force received by the limiting block and the workbench can be reduced by arranging the spring, so that the workbench is more stable and reliable.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is an enlarged schematic view of a position a of the present invention.
In the figure: the device comprises a base plate 1, threaded holes 2, fixed pipes 3, limiting blocks 4, permanent magnets 5, a collecting plate 6, a filter screen 7, an insertion pipe 8, a movable plate 9, springs 10, water leakage holes 11, a workbench 12, supporting rods 13, fixing blocks 14 and material leakage holes 15.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-2, a positioning device for processing an airplane model comprises a base plate 1, threaded holes 2 are respectively formed on the left side and the right side of the bottom of the base plate 1, a fixed tube 3 is fixedly installed on the top of the base plate 1, a sliding groove is formed at the joint of the fixed tube 3 and a collecting plate 6, the collecting plate 6 is movably connected with the fixed tube 3 through the sliding groove, a limiting block 4 is movably installed inside the fixed tube 3, a through hole is formed inside the limiting block 4, the through hole is funnel-shaped and is communicated with a material leaking hole 15, a permanent magnet 5 is fixedly installed on the inner top wall of the fixed tube 3, the collecting plate 6 positioned on the top of the permanent magnet 5 is inserted into the front surface of the fixed tube 3, a filter screen 7 is fixedly installed inside the collecting plate 6, insertion tubes 8 positioned on the left side and the right side of the permanent magnet 5 are fixedly installed on the inner bottom wall of the fixed tube, the inside movable mounting of intubate 8 has the fly leaf 9 with the bottom fixed mounting of stopper 4, the bottom fixed mounting of fly leaf 9 has spring 10, the quantity of spring 10 is two, and spring 10 is bilateral symmetry and distributes, the left and right sides of fixed pipe 3 has all seted up the hole of leaking 11, the quantity of hole of leaking 11 is two, and the hole of leaking 11 is bilateral symmetry and distributes, the top fixed mounting of stopper 4 has workstation 12, the left and right sides at workstation 12 top all fixed mounting has bracing piece 13, the top fixed mounting of bracing piece 13 has fixed block 14, the top of workstation 12 is located the opposite side of bracing piece 13 and has seted up the hole of leaking 15, through setting up the hole of leaking 15, when processing the aircraft model, the metal piece that produces is with water from the hole of leaking 15 together, then pass stopper 4 to fixed pipe 3, the mixture that metal piece and water formed can pass through the filtering action of filter screen 7, solid-liquid can take place the separation, water can flow from leaking hole 11, the metal piece is separated on filter screen 7, and through setting up permanent magnet 5, permanent magnet 5 can produce the adsorption affinity to the metal piece, it depends on filter screen 7 to enable the metal piece, then take collecting plate 6 out and can carry out recycle with the metal piece of collecting, the effect of being convenient for clear up the metal piece that produces has been reached, time saving and labor saving, the cost of labor has been reduced, it is more convenient to use, simultaneously through setting up spring 10, can slow down the impact force that stopper 4 and workstation 12 received, thereby make workstation 12 more reliable and more stable.
In conclusion, the positioning device for machining the airplane model is provided with the material leakage hole 15, when the airplane model is machined, the generated metal scraps and water are together discharged from the material leakage hole 15 and then pass through the limiting block 4 to the fixed pipe 3, a mixture formed by the metal scraps and the water is subjected to the filtering action of the filter screen 7, solid and liquid can be separated, the water can flow out from the water leakage hole 11, the metal scraps are separated on the filter screen 7, and the permanent magnet 5 is arranged to generate adsorption force on the metal scraps, so that the metal scraps can be attached to the filter screen 7, the collecting plate 6 is drawn out to recycle the collected metal scraps, the effect of conveniently cleaning the generated metal scraps is achieved, time and labor are saved, the labor cost is reduced, the positioning device is convenient to use, and meanwhile, by arranging the spring 10, the impact force on the limiting block 4 and the workbench 12 can be relieved, thereby make workstation 12 more reliable and more stable, solved aircraft model processing on the market at present and used positioner, because the aircraft model that uses the lathe to come the metal now mostly processes, the metal piece that produces is detached very inconveniently in the processing, and the manual work is not only time-wasting but also more power when clearing up, has improved artificial cost, uses very inconvenient problem.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The utility model provides a positioner is used in aircraft model processing, includes bottom plate (1), its characterized in that: the novel water-saving filter is characterized in that threaded holes (2) are formed in the left side and the right side of the bottom plate (1), a fixed pipe (3) is fixedly mounted at the top of the bottom plate (1), a limiting block (4) is movably mounted inside the fixed pipe (3), a permanent magnet (5) is fixedly mounted on the inner top wall of the fixed pipe (3), a collecting plate (6) located at the top of the permanent magnet (5) is inserted into the front of the fixed pipe (3), a filter screen (7) is fixedly mounted inside the collecting plate (6), insertion pipes (8) located at the left side and the right side of the permanent magnet (5) are fixedly mounted on the inner bottom wall of the fixed pipe (3), a movable plate (9) fixedly mounted at the bottom of the limiting block (4) is movably mounted inside the insertion pipes (8), a spring (10) is fixedly mounted at the bottom of the movable plate (9), and water leakage holes, the top fixed mounting of stopper (4) has workstation (12), the equal fixed mounting in the left and right sides at workstation (12) top has bracing piece (13), the top fixed mounting of bracing piece (13) has fixed block (14), the top of workstation (12) is located the opposite side of bracing piece (13) and has been seted up hourglass material hole (15).
2. The positioning device for machining an aircraft model according to claim 1, wherein: the through hole is opened to the inside of stopper (4), and the through hole is hourglass hopper-shaped and is linked together with hourglass material hole (15).
3. The positioning device for machining an aircraft model according to claim 1, wherein: the connecting part of the fixed pipe (3) and the collecting plate (6) is provided with a chute, and the collecting plate (6) is movably connected with the fixed pipe (3) through the chute.
4. The positioning device for machining an aircraft model according to claim 1, wherein: a movable groove is formed in the inner wall of the insertion pipe (8), and the movable plate (9) is movably connected with the insertion pipe (8) through the movable groove.
5. The positioning device for machining an aircraft model according to claim 1, wherein: the number of the springs (10) is two, and the springs (10) are distributed in a bilateral symmetry mode.
6. The positioning device for machining an aircraft model according to claim 1, wherein: the number of the water leakage holes (11) is two, and the water leakage holes (11) are distributed in a bilateral symmetry manner.
CN201921472337.7U 2019-09-05 2019-09-05 Positioner is used in aircraft model processing Expired - Fee Related CN210524457U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921472337.7U CN210524457U (en) 2019-09-05 2019-09-05 Positioner is used in aircraft model processing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921472337.7U CN210524457U (en) 2019-09-05 2019-09-05 Positioner is used in aircraft model processing

Publications (1)

Publication Number Publication Date
CN210524457U true CN210524457U (en) 2020-05-15

Family

ID=70604332

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201921472337.7U Expired - Fee Related CN210524457U (en) 2019-09-05 2019-09-05 Positioner is used in aircraft model processing

Country Status (1)

Country Link
CN (1) CN210524457U (en)

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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: 20200515

Termination date: 20200905

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