CN211193130U - Maintenance device for avionic parts - Google Patents

Maintenance device for avionic parts Download PDF

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Publication number
CN211193130U
CN211193130U CN201922164380.3U CN201922164380U CN211193130U CN 211193130 U CN211193130 U CN 211193130U CN 201922164380 U CN201922164380 U CN 201922164380U CN 211193130 U CN211193130 U CN 211193130U
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CN
China
Prior art keywords
shell
workbench
fixed seat
magnet strip
electric telescopic
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
CN201922164380.3U
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Chinese (zh)
Inventor
牛武
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.)
Changsha Aeronautical Vocational and Technical College
Original Assignee
Changsha Aeronautical Vocational and Technical College
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 Changsha Aeronautical Vocational and Technical College filed Critical Changsha Aeronautical Vocational and Technical College
Priority to CN201922164380.3U priority Critical patent/CN211193130U/en
Application granted granted Critical
Publication of CN211193130U publication Critical patent/CN211193130U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a maintenance device of avionic parts, which comprises a base, a shell positioned at the top of the base and an operation door positioned in the middle of the shell, wherein the inside of the shell is fixedly connected with a fixed seat, the top of the fixed seat is movably connected with a workbench, one side of the workbench is positioned on the inner wall of the shell and is fixedly connected with an electric telescopic rod, the workbench and the fixed seat are connected through a connecting column, a positioning block is fixedly connected in the middle of the bottom of the connecting column, and a positioning groove matched with the positioning block for use is formed in the top of the fixed seat; through the setting of electric telescopic handle, workstation, very big increase the practicality of maintaining the device, the article of processing, maintenance can be placed in the top of workstation, uses through the cooperation of electric telescopic handle, workstation, places the article in the inside of shell, easy operation is convenient, and degree of automation is higher, has reduced the condition that the user's head deepened the device inside.

Description

Maintenance device for avionic parts
Technical Field
The utility model belongs to the technical field of maintain the device, concretely relates to avionics parts's maintenance device.
Background
The avionic device is a device of an electronic system on an airplane, internal facilities are often damaged or cannot operate along with the long-term use of electronic parts, the economic cost is increased by discarding the whole electronic parts or equipment and replacing the whole electronic parts or equipment with new equipment, and the electronic parts can be maintained and repaired by the maintenance device.
The existing maintenance device has certain problems in use, and due to the fact that the objects are processed and maintained inside the device, a user needs to put the head of the user into the device to correctly place and fix the processed and maintained objects, the head of the user collides with the device for many times, internal light is dim, the bulb is mounted, resources are wasted, certain potential safety hazards exist simultaneously, and the problem of working difficulty is increased.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a maintenance device of avionics parts to the current maintenance device that provides in solving above-mentioned background art has certain problem when using, because the processing of article with maintain all inside the device, lead to in the user of service need deepening the head into the device, just can correctly put and fix the article of processing, maintenance, appear the condition scheduling problem that collision appears with the device in user of service head many times.
In order to achieve the above object, the utility model provides a following technical scheme: a maintenance device for avionic parts comprises a base, a shell positioned at the top of the base and an operation door positioned in the middle of the shell, wherein a fixed seat is fixedly connected inside the shell, the top of the fixed seat is movably connected with a workbench, an electric telescopic rod is fixedly connected to one side of the workbench, which is positioned on the inner wall of the shell, the workbench and the fixed seat are connected through a connecting column, a positioning block is fixedly connected to the middle of the bottom of the connecting column, and a positioning groove matched with the positioning block is formed in the top of the fixed seat;
the lateral wall that the workstation is close to the operation door is equipped with first magnet strip, the inner wall of operation door is equipped with the second magnet strip that uses with first magnet strip cooperation.
Furthermore, the shape and size of the positioning block are consistent with those of the positioning groove, and the positioning block and the positioning groove are in clearance fit.
Further, the length of the electric telescopic rod is one half of the width of the shell.
Furthermore, after the workbench slides out of the inner part of the shell through the electric telescopic rod, part of the positioning blocks at the bottom of the workbench are positioned in the fixed seat.
Furthermore, the first magnetic stone strip and the second magnetic stone strip are located at the same height, and one surface, opposite to the first magnetic stone strip and the second magnetic stone strip, is an S pole or an N pole.
Furthermore, an operation table is embedded on the surface of the shell on one side of the operation door.
Compared with the prior art, the beneficial effects of the utility model are that:
1. through the setting of electric telescopic handle, workstation, very big increase the practicality of maintaining the device, the article of processing, maintenance can be placed in the top of workstation, uses through the cooperation of electric telescopic handle, workstation, places the article in the inside of shell, easy operation is convenient, and degree of automation is higher, has reduced the condition that the user's head gos deep into the device inside, has reduced the condition that the collision appears with the device in user's head, has improved the practicality.
2. Through the setting of first magnet strip, second magnet strip, very big increase the functional of workstation, use through the cooperation of first magnet strip, second magnet strip, can make the workstation when sliding, through the homopolar repellent's of first magnet strip, second magnet strip nature, open the operating door is automatic, increased the convenience, improved work efficiency.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a side sectional view of the base, the operation table, the electric telescopic rod, the working table, the fixing base and the connecting column of the present invention;
FIG. 3 is a cross-sectional view of the working table, the fixing base, the connecting column, the positioning block and the positioning groove of the present invention;
fig. 4 is a top cross-sectional view of the housing, the operation door, the table, the first magnetic stone strip and the second magnetic stone strip of the present invention;
fig. 5 is an enlarged view of a portion a in fig. 4 according to the present invention.
In the figure: 1. a housing; 2. an operating door; 3. a base; 4. an operation table; 5. an electric telescopic rod; 6. a work table; 7. a fixed seat; 8. connecting columns; 9. positioning blocks; 10. positioning a groove; 11. a first magnet bar; 12. a second magnet strip.
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 to 5, the present invention provides a technical solution: a maintenance device for avionic parts comprises a base 3, a shell 1 positioned at the top of the base 3 and an operation door 2 positioned in the middle of the shell 1, wherein an operation table 4 is embedded on the surface of the shell 1 on one side of the operation door 2, the operation door 2 is opened, an object needing to be processed and maintained is placed on a workbench 6 inside the shell 1, then the operation door 2 is closed, a button on the operation table 4 is operated, the maintenance device can be operated, and the workbench 6, the shell 1 and the operation table 4 are public knowledge of technical personnel in the field.
The inner part of the shell 1 is fixedly connected with a fixed seat 7, the top of the fixed seat 7 is movably connected with a workbench 6, one side of the workbench 6 is positioned on the inner wall of the shell 1 and is fixedly connected with an electric telescopic rod 5, the electric telescopic rod 5 is in the prior art and can have two states of contraction and expansion, the workbench 6 can slide to the outer part of the shell 1 through the expansion of the electric telescopic rod 5, the workbench 6 and the fixed seat 7 are connected through a connecting column 8, a positioning block 9 is fixedly connected in the middle of the bottom of the connecting column 8 of the workbench 6, a positioning groove 10 matched with the positioning block 9 is formed in the top of the fixed seat 7, the shape and size of the positioning block 9 are consistent with that of the positioning groove 10, the positioning block 9 and the positioning groove 10 are in clearance fit for use, and;
the lateral wall that workstation 6 is close to operation door 2 is equipped with first magnet strip 11, the inner wall of operation door 2 is equipped with the second magnet strip 12 of using with the cooperation of first magnet strip 11, second magnet strip 12 is in same height, first magnet strip 11, the relative one side of second magnet strip 12 is the S utmost point or the N utmost point, first magnet strip 11, second magnet strip 12 has homopolar repulsion, heteropolar attraction' S nature, when the relative face of first magnet strip 11 and second magnet strip 12 is the homopolar, first magnet strip 11 accessible workstation 6 slides to the outside of shell 1, when first magnet strip 11 is close to second magnet strip 12, accessible magnet nature, with the automatic opening of operation door 2.
Electric telescopic handle 5's length is the half of the width of shell 1, workstation 6 slides out the inside back of shell 1 through electric telescopic handle 5, and the part locating piece 9 of workstation 6 bottom is located the inside of fixing base 7 for workstation 6 slides the back through electric telescopic handle 5, and the locating piece 9 of workstation 6 bottom has the part still to stay in constant head tank 10, and locating piece 9 and constant head tank 10 are only partial separation, have increased workstation 6's stability.
The utility model discloses a theory of operation and use flow: only the electric telescopic rod 5 needs to be adjusted, so that the electric telescopic rod 5 is slowly unfolded, the electric telescopic rod 5 can slide the workbench 6 to the outside of the shell 1 while being unfolded, so that the positioning block 9 at the bottom of the working platform 6 slides in the positioning groove 10, the stability of the working platform 6 is increased, when the first magnet strip 11 on the side wall of the workbench 6 is close to the second magnet strip 12, the like poles of the first magnet strip 11 and the second magnet strip 12 repel each other, thereby opening the operation door 2, enabling the electric telescopic rod 5 to continuously slide the workbench 6, enabling the workbench 6 to slide to the outside of the shell 1, and the user only needs to place the processed and maintained objects on the top of the workbench 6, then, the electric telescopic rod 5 is operated, so that the workbench 6 slides to the inside of the shell 1 and is positioned right above the fixed seat 7 through the contraction of the electric telescopic rod 5, and finally, the operation door 2 is manually closed.
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. A maintenance device of avionic components, comprising a base (3), a casing (1) positioned at the top of the base (3) and an operating door (2) positioned in the middle of the casing (1), characterized in that: a fixed seat (7) is fixedly connected inside the shell (1), the top of the fixed seat (7) is movably connected with a workbench (6), one side of the workbench (6) is positioned on the inner wall of the shell (1) and is fixedly connected with an electric telescopic rod (5), the workbench (6) and the fixed seat (7) are connected through a connecting column (8), a positioning block (9) is fixedly connected in the middle of the bottom of the connecting column (8), and a positioning groove (10) matched with the positioning block (9) for use is formed in the top of the fixed seat (7);
the lateral wall that workstation (6) are close to operation door (2) is equipped with first magnet strip (11), the inner wall of operation door (2) is equipped with second magnet strip (12) that use with first magnet strip (11) cooperation.
2. A maintenance device for avionics components, according to claim 1, characterized in that: the shape and size of the positioning block (9) are consistent with those of the positioning groove (10), and the positioning block and the positioning groove are in clearance fit.
3. A maintenance device for avionics components, according to claim 1, characterized in that: the length of the electric telescopic rod (5) is one half of the width of the shell (1).
4. A maintenance device for avionics components, according to claim 1, characterized in that: after the workbench (6) slides out of the interior of the shell (1) through the electric telescopic rod (5), part of the positioning blocks (9) at the bottom of the workbench (6) are positioned in the fixed seat (7).
5. A maintenance device for avionics components, according to claim 1, characterized in that: the first magnet strip (11) and the second magnet strip (12) are located at the same height, and the opposite surfaces of the first magnet strip (11) and the second magnet strip (12) are S poles or N poles.
6. A maintenance device for avionics components, according to claim 1, characterized in that: an operation table (4) is embedded in the surface of the shell (1) on one side of the operation door (2).
CN201922164380.3U 2019-12-05 2019-12-05 Maintenance device for avionic parts Expired - Fee Related CN211193130U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201922164380.3U CN211193130U (en) 2019-12-05 2019-12-05 Maintenance device for avionic parts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201922164380.3U CN211193130U (en) 2019-12-05 2019-12-05 Maintenance device for avionic parts

Publications (1)

Publication Number Publication Date
CN211193130U true CN211193130U (en) 2020-08-07

Family

ID=71853455

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201922164380.3U Expired - Fee Related CN211193130U (en) 2019-12-05 2019-12-05 Maintenance device for avionic parts

Country Status (1)

Country Link
CN (1) CN211193130U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114290309A (en) * 2022-01-26 2022-04-08 滨州学院 Maintenance device for avionic parts

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114290309A (en) * 2022-01-26 2022-04-08 滨州学院 Maintenance device for avionic parts

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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: 20200807

Termination date: 20201205