CN214065577U - Aviation spare part drying device - Google Patents

Aviation spare part drying device Download PDF

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Publication number
CN214065577U
CN214065577U CN202022854282.5U CN202022854282U CN214065577U CN 214065577 U CN214065577 U CN 214065577U CN 202022854282 U CN202022854282 U CN 202022854282U CN 214065577 U CN214065577 U CN 214065577U
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fixedly connected
drying
box body
slide
drying box
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CN202022854282.5U
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Chinese (zh)
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付官菊
伍朝华
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Guizhou Hongting Standard Parts Manufacturing Co ltd
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Guizhou Hongting Standard Parts Manufacturing Co ltd
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Abstract

The utility model discloses an aviation spare part drying device relates to aviation spare part production technical field, including the drying cabinet, a set of support column of bottom surface fixedly connected with of drying cabinet, the front of drying cabinet articulates through the hinge has a set of switch door, the last fixed surface of drying cabinet is connected with the heating cabinet, the through-hole has been seted up to the upper surface of drying cabinet, and the drying cabinet is linked together through-hole and heating cabinet. The utility model relates to a rational in infrastructure, it can set up through the cooperation between a joint section of thick bamboo, the sliding frame, the driving lever, the slide, the joint pole, spacing hole, a spring, first air filter screen and the second air filter screen, upwards stimulate the driving lever, can drive slide and joint pole rebound under the effect of driving lever, can make the bottom of joint pole break away from the inside in spacing hole to can be with the quick dismantlement of first air filter screen or second air filter screen, dismantle convenient and fast in-process, the effectual practicality that has improved the device.

Description

Aviation spare part drying device
Technical Field
The utility model relates to an aviation spare part production technical field specifically is an aviation spare part drying device.
Background
The aviation part manufacturing industry mainly refers to manufacturing of various parts of an aviation airplane, and the manufacturing comprises manufacturing of airplane body parts, manufacturing of parts of an aero-engine, manufacturing of instruments, airborne equipment, hydraulic systems, accessories and the like.
Most of current drying device can install air filter screen at air intake and air outlet, in order to reach the inside dirt-proof effect of device, but air filter screen just need dismantle the washing after using a period, current drying device is very inconvenient when installing and dismantling air filter screen, drying device's practicality has been reduced, in addition, current drying device is when carrying out the drying to aviation spare part, can not make aviation spare part reach fine stoving effect, it is inhomogeneous to lead to spare part surface drying easily, influence the production quality of part. Therefore, the aviation part drying device is provided to solve the problems.
SUMMERY OF THE UTILITY MODEL
One) technical problem to be solved
The utility model aims at providing an aviation spare part drying device in order to remedy prior art not enough.
II) technical scheme
In order to achieve the above object, the utility model provides a following technical scheme: the aviation part drying device comprises a drying box, wherein the bottom surface of the drying box is fixedly connected with a group of supporting columns, the front surface of the drying box is hinged with a group of switch doors through hinges, the upper surface of the drying box is fixedly connected with a heating box, the upper surface of the drying box is provided with a through hole, the drying box is communicated with the heating box through the through hole, an aluminum alloy heater is installed on the inner top wall of the heating box, the inner side wall of the heating box is fixedly connected with a first supporting strip, an air feeder is fixedly embedded in the first supporting strip, the left side surface and the right side surface of the heating box are respectively provided with an air inlet, the lower parts of the left side surface and the right side surface of the drying box are respectively provided with an air outlet, the inner walls of the two air inlets and the inner walls of the air outlet are respectively and fixedly connected with a stop block, the inner walls of the two air inlets are respectively and slidably connected with a first fixing frame, and a first air filter screen is installed on the inner wall of the first fixing frame, the inner walls of the two air outlets are connected with a second fixed frame in a sliding manner, a second air filter screen is installed on the inner wall of the second fixed frame, limiting holes are formed in the upper surface of each first fixed frame and the upper surface of the second fixed frame, clamping cylinders are fixedly embedded in the heating box and the drying box and correspond to the limiting holes, the outer surface of each clamping cylinder is fixedly communicated with a sliding frame, a clamping assembly is installed between each clamping cylinder and the sliding frame, a second supporting bar is fixedly connected to the inner side wall of the drying box, the inner bottom wall of the drying box is rotatably connected with a rotating bar through a first bearing, the top end of the rotating bar is rotatably connected with the bottom surface of the second supporting bar through a second bearing, a motor is fixedly connected to the bottom surface of the drying box, and the output end of the motor is fixedly connected with the bottom end of the rotating bar, the surface fixedly connected with of dwang is a set of loading board, every the spacing frame of the equal fixedly connected with in upper surface of loading board, the last fixed surface of loading board is connected with the rubber pad, the ventilation hole that a set of equidistance was arranged is all seted up to the bottom surface of loading board and the bottom surface of rubber pad.
Further, the joint subassembly includes the slide, slide sliding connection is in the inner wall of a joint section of thick bamboo, the bottom surface fixedly connected with joint rod of slide, the bottom of joint rod runs through the bottom surface of slide and extends to the inside in spacing hole, the last fixed surface of slide is connected with the spring, the top of spring and the interior roof fixed connection of slide, the outer fixed surface of slide is connected with the driving lever, the one end that the slide was kept away from to the driving lever runs through the sliding frame and extends to the outside of sliding frame.
Furthermore, the outer surface of the driving lever is fixedly connected with a rubber sleeve, and the outer surface of the rubber sleeve is provided with anti-skid grains.
Furthermore, a group of heat dissipation fins are arranged inside the heating box, and the top end of each heat dissipation fin is fixedly connected with the bottom surface of the aluminum alloy heater.
Further, the bottom surface fixed connection mount of motor, the top of mount and the bottom surface fixed connection of drying cabinet.
Furthermore, every the below of support column all is equipped with the base, every the upper surface of base respectively with the bottom fixed connection of every support column.
Thirdly), the beneficial effects are as follows:
compared with the prior art, this aviation spare part drying device possesses following beneficial effect:
the utility model discloses a joint section of thick bamboo, sliding frame, driving lever, slide, joint pole, spacing hole, spring, first air filter screen and the cooperation setting between the second air filter screen, upwards stimulate the driving lever, can drive slide rebound under the effect of driving lever to can drive joint pole rebound, can make the bottom of joint pole break away from the inside in spacing hole, and then can be with the quick dismantlement of first air filter screen or second air filter screen, dismantle convenient and fast in-process, the effectual practicality that has improved the device.
Two, the utility model discloses a loading board, spacing frame, the rubber pad, the aluminum alloy heater, the heating cabinet, the forced draught blower, cooperation setting between motor and the dwang, place aviation spare part at the upper surface of loading board, motor work can drive the dwang and rotate, thereby can drive loading board and spacing frame and rotate, aviation spare part that can make the loading board upper surface place rotates around the dwang, the effect of cooperation forced draught blower, can carry out even blowing to aviation spare part's surface, can make aviation spare part reach fine stoving effect, it is more even to make the stoving on spare part surface, guarantee the production quality of part.
Drawings
Fig. 1 is a schematic perspective view of the present invention;
fig. 2 is a cross-sectional view of a front view of the present invention;
fig. 3 is a schematic perspective view of the limiting frame of the present invention;
FIG. 4 is an enlarged schematic view of the structure at A in FIG. 2 according to the present invention;
fig. 5 is an enlarged schematic view of the structure at B in fig. 2 according to the present invention.
In the figure: 1. a drying oven; 2. a support pillar; 3. opening and closing the door; 4. a heating box; 5. an aluminum alloy heater; 6. an air inlet; 7. an air outlet; 8. a stopper; 9. a first fixed frame; 10. a second fixed frame; 11. A first air screen; 12. a second air screen; 13. a limiting hole; 14. a clamping cylinder; 15. a sliding frame; 16. a clamping assembly; 161. a slide plate; 162. a clamping and connecting rod; 163. a spring; 164. a deflector rod; 165. a rubber sleeve; 17. a first support bar; 18. a through hole; 19. a blower; 20. rotating the rod; 21. a carrier plate; 22. a limiting frame; 23. a rubber pad; 24. a vent hole; 25. a second supporting strip; 26. heat dissipation fins; 27. A base; 28. a fixed mount; 29. an electric motor.
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.
As shown in fig. 1-5, the utility model provides a technical solution: an aviation part drying device comprises a drying box 1, a group of supporting columns 2 are fixedly connected to the bottom surface of the drying box 1, a group of switch doors 3 are hinged to the front surface of the drying box 1 through hinges, a heating box 4 is fixedly connected to the upper surface of the drying box 1, a through hole 18 is formed in the upper surface of the drying box 1, the drying box 1 is communicated with the heating box 4 through the through hole 18, an aluminum alloy heater 5 is installed on the inner top wall of the heating box 4, the type of the aluminum alloy heater 5 is DJR, a first supporting strip 17 is fixedly connected to the inner side wall of the heating box 4, an air feeder 19 is fixedly embedded inside the first supporting strip 17, the type of the air feeder 19 is SF3-2, air inlets 6 are formed in the left side surface and the right side surface of the heating box 4, air outlets 7 are formed in the lower portions of the left side surface and the right side surface of the, the inner walls of the two air inlets 6 are respectively connected with a first fixed frame 9 in a sliding manner, the inner wall of the first fixed frame 9 is provided with a first air filter screen 11, the inner walls of the two air outlets 7 are respectively connected with a second fixed frame 10 in a sliding manner, the inner wall of the second fixed frame 10 is provided with a second air filter screen 12, the upper surface of each first fixed frame 9 and the upper surface of the second fixed frame 10 are respectively provided with a limiting hole 13, the inside of the heating box 4 and the inside of the drying box 1 are respectively fixedly embedded with a clamping cylinder 14, the clamping cylinder 14 corresponds to the limiting hole 13, the outer surface of each clamping cylinder 14 is respectively fixedly communicated with a sliding frame 15, a clamping assembly 16 is respectively arranged between each clamping cylinder 14 and the sliding frame 15, the inner side wall of the drying box 1 is fixedly connected with a second supporting bar 25, the inner bottom wall of the drying box 1 is rotatably connected with a rotating bar 20 through a first bearing, the top end of the rotating bar 20 is rotatably connected with the bottom surface of the second supporting bar 25 through a second bearing, the bottom surface fixedly connected with motor 29 of drying cabinet 1, and the output of motor 29 and the bottom fixed connection of dwang 20, the brand model of this motor 29 is the loose MQMA04ZP1U, the external surface fixed connection of dwang 20 has a set of loading board 21, the equal fixedly connected with spacing frame 22 of upper surface of every loading board 21, the upper surface fixed connection of loading board 21 has a rubber pad 23, a set of ventilation hole 24 that the equidistance was arranged is all seted up to the bottom surface of loading board 21 and the bottom surface of rubber pad 23.
Further, the clamping assembly 16 includes a sliding plate 161, the sliding plate 161 is slidably connected to the inner wall of the clamping cylinder 14, a clamping rod 162 is fixedly connected to the bottom surface of the sliding plate 161, the bottom end of the clamping rod 162 penetrates through the bottom surface of the sliding plate 161 and extends to the inside of the limiting hole 13, a spring 163 is fixedly connected to the upper surface of the sliding plate 161, the top end of the spring 163 is fixedly connected to the inner top wall of the sliding plate 161, a shift lever 164 is fixedly connected to the outer surface of the sliding plate 161, and one end, away from the sliding plate 161, of the shift lever 164 penetrates through the sliding frame 15 and extends to the outside of the sliding frame 15. Through the cooperation setting between the above structure, can make the device convenient and fast more when dismantling first air filter 11 and second air filter 12, the effectual practicality that has improved the device.
Further, the outer surface of the driving lever 164 is fixedly connected with a rubber sleeve 165, and the outer surface of the rubber sleeve 165 is provided with anti-slip threads. By the scheme, the comfort when the poking rod 164 is poked can be improved.
Further, a group of radiating fins 26 are arranged inside the heating box 4, and the top end of each radiating fin 26 is fixedly connected with the bottom surface of the aluminum alloy heater 5. Through this scheme, can increase the area of contact with the air, improve the heating effect of aluminum alloy heater 5 to the air.
Further, the bottom surface of the motor 29 is fixedly connected with a fixing frame 28, and the top end of the fixing frame 28 is fixedly connected with the bottom surface of the drying box 1. Through this scheme, can carry out effectual fixed to motor 29, increase the stability of motor 29 during operation.
Further, all be equipped with base 27 below every support column 2, the upper surface of every base 27 respectively with the bottom fixed connection of every support column 2. Through this scheme, can increase the area of contact between support column 2 and the ground, make the device more stable at the during operation.
The working principle is as follows: when the device is used, firstly, two switch doors 3 are opened, then the aviation parts are placed on the upper surface of the bearing plate 21, the aviation parts can be limited through the limiting frame 22 and the rubber pad 23, then the aluminum alloy heater 5 and the blower 19 are started, the aluminum alloy heater 5 can heat the air in the heating box 4 when working, the blower 19 can blow the hot air in the heating box 4 to the inside of the drying box 1 when working, the aviation parts are dried, the motor 29 is started, the motor 29 can drive the rotating rod 20 to rotate when working, so that the bearing plate 21 and the limiting frame 22 can be driven to rotate, the aviation parts placed on the upper surface of the bearing plate 21 can rotate around the rotating rod 20, and the outer surfaces of the aviation parts can be uniformly blown by matching with the action of the blower 19, so that the aviation parts can achieve a good drying effect, make the stoving on spare part surface more even, guarantee the production quality of part, when needs are dismantled first air filter screen 11 or second air filter screen 12 and are washd, at first upwards spur driving lever 164, can drive slide 161 rebound under driving lever 164's effect, thereby can drive joint bar 162 rebound, can make the bottom of joint bar 162 break away from the inside of spacing hole 13, and then can be with the quick dismantlement of first air filter screen 11 or second air filter screen 12, dismantle in-process convenient and fast, the effectual practicality that has improved the device.
It should be noted that, in this document, the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "fixedly," "mounted," "connected," and "connected" are to be construed broadly, e.g., "mounted" may be fixedly connected, or detachably connected, or integrally connected; "connected" may be mechanically or electrically connected; "connected" may be directly connected or indirectly connected through an intermediate member, or may be internal or external to two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
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 an aviation spare part drying device, includes drying cabinet (1), its characterized in that: the drying box comprises a drying box body and is characterized in that a group of supporting columns (2) are fixedly connected to the bottom surface of the drying box body (1), a group of switch doors (3) are hinged to the front surface of the drying box body (1) through hinges, a heating box (4) is fixedly connected to the upper surface of the drying box body (1), a through hole (18) is formed in the upper surface of the drying box body (1), the drying box body (1) is communicated with the heating box body (4) through the through hole (18), an aluminum alloy heater (5) is installed on the inner top wall of the heating box body (4), a first supporting column (17) is fixedly connected to the inner side wall of the heating box body (4), an air feeder (19) is fixedly inlaid in the first supporting column (17), air inlets (6) are formed in the left side face and the right side face of the heating box body (4), air outlets (7) are formed in the lower portions of the left side face and the right side face of the drying box body (1), and check blocks (8) are fixedly connected to the inner walls of the air inlets (6) and the air outlets (7), the inner wall of the two air inlets (6) is connected with a first fixed frame (9) in a sliding manner, a first air filter screen (11) is installed on the inner wall of the first fixed frame (9), the inner wall of the two air outlets (7) is connected with a second fixed frame (10) in a sliding manner, a second air filter screen (12) is installed on the inner wall of the second fixed frame (10), each clamping cylinder (14) corresponds to the corresponding limiting hole (13), the outer surface of each clamping cylinder (14) is fixedly communicated with a sliding frame (15), each clamping assembly (16) is installed between each clamping cylinder (14) and the corresponding sliding frame (15), a second supporting strip (25) is fixedly connected to the inner side wall of the drying box (1), the interior diapire of drying cabinet (1) is connected with dwang (20) through first bearing rotation, the top of dwang (20) is passed through the second bearing and is connected with the bottom surface rotation of second support bar (25), the bottom surface fixedly connected with motor (29) of drying cabinet (1), and the output of motor (29) and the bottom fixed connection of dwang (20), the outer fixed surface of dwang (20) is connected with a set of loading board (21), every the equal fixedly connected with spacing frame (22) of upper surface of loading board (21), the upper fixed surface of loading board (21) is connected with rubber pad (23), ventilation hole (24) that a set of equidistance was arranged are all seted up to the bottom surface of loading board (21) and the bottom surface of rubber pad (23).
2. The aircraft component drying device of claim 1, wherein: joint subassembly (16) include slide (161), slide (161) sliding connection is in the inner wall of joint section of thick bamboo (14), the bottom surface fixedly connected with joint pole (162) of slide (161), the bottom of joint pole (162) runs through the bottom surface of slide (161) and extends to the inside of spacing hole (13), the last fixed surface of slide (161) is connected with spring (163), the top of spring (163) and the interior roof fixed connection of slide (161), the outer fixed surface of slide (161) is connected with driving lever (164), sliding frame (15) are run through and extend to the outside of sliding frame (15) to the one end that slide (161) were kept away from to driving lever (164).
3. The aviation component drying device of claim 2, wherein: the outer surface of the shifting lever (164) is fixedly connected with a rubber sleeve (165), and anti-skid grains are arranged on the outer surface of the rubber sleeve (165).
4. The aircraft component drying device of claim 1, wherein: a group of heat dissipation fins (26) are arranged inside the heating box (4), and the top end of each heat dissipation fin (26) is fixedly connected with the bottom surface of the aluminum alloy heater (5).
5. The aircraft component drying device of claim 1, wherein: the bottom surface of the motor (29) is fixedly connected with a fixing frame (28), and the top end of the fixing frame (28) is fixedly connected with the bottom surface of the drying box (1).
6. The aircraft component drying device of claim 1, wherein: every the below of support column (2) all is equipped with base (27), every the upper surface of base (27) respectively with the bottom fixed connection of every support column (2).
CN202022854282.5U 2020-12-02 2020-12-02 Aviation spare part drying device Active CN214065577U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202022854282.5U CN214065577U (en) 2020-12-02 2020-12-02 Aviation spare part drying device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202022854282.5U CN214065577U (en) 2020-12-02 2020-12-02 Aviation spare part drying device

Publications (1)

Publication Number Publication Date
CN214065577U true CN214065577U (en) 2021-08-27

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Application Number Title Priority Date Filing Date
CN202022854282.5U Active CN214065577U (en) 2020-12-02 2020-12-02 Aviation spare part drying device

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CN (1) CN214065577U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114524068A (en) * 2022-02-23 2022-05-24 中国人民解放军海军潜艇学院 High-safety underwater training device recovery system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114524068A (en) * 2022-02-23 2022-05-24 中国人民解放军海军潜艇学院 High-safety underwater training device recovery system
CN114524068B (en) * 2022-02-23 2023-02-24 中国人民解放军海军潜艇学院 High-safety underwater training device recovery system

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