CN111921773A - Aircraft application stoving integration equipment - Google Patents

Aircraft application stoving integration equipment Download PDF

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Publication number
CN111921773A
CN111921773A CN202010828996.0A CN202010828996A CN111921773A CN 111921773 A CN111921773 A CN 111921773A CN 202010828996 A CN202010828996 A CN 202010828996A CN 111921773 A CN111921773 A CN 111921773A
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CN
China
Prior art keywords
filter screen
motor
lead screw
heating
aircraft
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.)
Pending
Application number
CN202010828996.0A
Other languages
Chinese (zh)
Inventor
金卫明
Original Assignee
金卫明
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 金卫明 filed Critical 金卫明
Priority to CN202010828996.0A priority Critical patent/CN111921773A/en
Publication of CN111921773A publication Critical patent/CN111921773A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B16/00Spray booths
    • B05B16/20Arrangements for spraying in combination with other operations, e.g. drying; Arrangements enabling a combination of spraying operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D50/00Combinations of methods or devices for separating particles from gases or vapours
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D53/00Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols
    • B01D53/02Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols by adsorption, e.g. preparative gas chromatography
    • B01D53/04Separation of gases or vapours; Recovering vapours of volatile solvents from gases; Chemical or biological purification of waste gases, e.g. engine exhaust gases, smoke, fumes, flue gases, aerosols by adsorption, e.g. preparative gas chromatography with stationary adsorbents
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B13/00Machines or plants for applying liquids or other fluent materials to surfaces of objects or other work by spraying, not covered by groups B05B1/00 - B05B11/00
    • B05B13/02Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work
    • B05B13/0221Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work characterised by the means for moving or conveying the objects or other work, e.g. conveyor belts
    • B05B13/0228Means for supporting work; Arrangement or mounting of spray heads; Adaptation or arrangement of means for feeding work characterised by the means for moving or conveying the objects or other work, e.g. conveyor belts the movement of the objects being rotative
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05BSPRAYING APPARATUS; ATOMISING APPARATUS; NOZZLES
    • B05B15/00Details of spraying plant or spraying apparatus not otherwise provided for; Accessories
    • B05B15/60Arrangements for mounting, supporting or holding spraying apparatus
    • B05B15/68Arrangements for adjusting the position of spray heads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B05SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05DPROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
    • B05D3/00Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
    • B05D3/04Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to gases
    • B05D3/0406Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by exposure to gases the gas being air
    • B05D3/0413Heating with air
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B01PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01DSEPARATION
    • B01D2253/00Adsorbents used in seperation treatment of gases and vapours
    • B01D2253/10Inorganic adsorbents
    • B01D2253/102Carbon

Abstract

The invention discloses an aircraft coating and drying integrated device which comprises a device body, a third motor, a heating box and a processing box, wherein the left side of the device body is fixedly provided with the first motor, the lower end of a second transmission shaft penetrates through the upper surface of the device body and is connected with a second lead screw, the lower end of the second lead screw penetrates through the upper end surface of a support frame and is rotatably connected to the inner side wall of the support frame, the support frame is fixedly arranged in the device body, the processing box is fixed on the upper end surface of the device body and is arranged on the right side of the heating box, the right side of the processing box is connected with a connecting pipe, and the connecting pipe is far away from the processing box and is connected with. This aircraft application stoving integration equipment, with the gas suction to the heating cabinet under the effect of first fan in, after the heating element heating, can carry out drying process to the aircraft after the application through first spray tube blowout, the second filter screen that sets up in the filter shell can filter the gas that enters into the heating cabinet, reduces dust impurity and gets into.

Description

Aircraft application stoving integration equipment
Technical Field
The invention relates to the technical field of aircraft processing, in particular to an aircraft coating and drying integrated device.
Background
The aircraft is an apparatus flying object which is manufactured by human beings, can fly off the ground, flies in space and is controlled by people to fly, the aircraft is easily influenced by external environments such as wind, rain, sunshine and the like in the flying use process, corrosion damage and other phenomena easily occur after long-time use, in order to reduce the influence of external environment factors on the aircraft, the surface of the aircraft can be coated during production and processing of the aircraft, the coated aircraft needs to be dried on the surface of the aircraft, and in order to improve the coating efficiency, the problem is solved by the aircraft coating and drying integrated equipment.
Disclosure of Invention
The invention aims to provide an aircraft coating and drying integrated device, which aims to solve the problems that in order to reduce the influence of external environmental factors on an aircraft, the surface of the aircraft is generally coated during production and processing of the aircraft, and the coated aircraft needs to be dried.
In order to achieve the purpose, the invention provides the following technical scheme: an aircraft coating and drying integrated device comprises a device body, a third motor, a heating box and a treatment box,
the device comprises a device body, wherein a first motor is fixedly mounted on the left side of the device body and is connected with a first lead screw through a bevel gear set, the left side wall of the device body is observed at the right end of the first lead screw, the left side wall of the device body is rotatably connected to the inner side wall of the device body, a first moving frame is arranged on the first lead screw in a penetrating manner, the upper end of the first moving frame is connected with a fixed frame, a second motor is mounted in the fixed frame and is connected with a first transmission shaft, and the upper end of the first transmission shaft is connected with a clamping table;
the third motor is arranged on the upper end face of the equipment body and is connected with the second transmission shaft, the lower end of the second transmission shaft penetrates through the upper surface of the equipment body and is connected with the second lead screw, the lower end of the second lead screw penetrates through the upper end face of the support frame and is rotatably connected to the inner side wall of the support frame, the support frame is fixedly arranged in the equipment body and is arranged behind the fixed frame, a second movable frame penetrates through the second lead screw, a spraying mechanism is arranged on the front side of the second movable frame, and the spraying mechanism is connected with the conveying pipe;
the heating box is fixed on the upper end face of the equipment body, a first fan is installed on the heating box, the first fan is connected with the filtering shell, the left side of the heating box is connected with a first spray pipe, and one end, far away from the heating box, of the first spray pipe penetrates through the left side wall of the equipment body;
handle the case, handle the case and fix the up end at the equipment body, and handle the right side that the case set up at the heating cabinet, handle the case setting simultaneously in the front side of third motor, it is provided with the second fan to handle case left side, and the second fan is connected with the straw, the straw is kept away from second fan one end and is run through the up end of the equipment body, and the straw setting is in the place ahead of mount, it is connected with the connecting pipe to handle the case right side, and the connecting pipe is kept away from and is handled the case and be connected with the storage water tank, and the storage water tank sets up the right side at the equipment body simultaneously.
Preferably, the equipment body comprises a through groove, a first filter screen and a first activated carbon adsorption net, the through groove is formed in the upper end face of the equipment body, the first filter screen is arranged in the through groove, and the upper end of the first filter screen is connected with the first activated carbon adsorption net.
Preferably, the first motor, the bevel gear set and the first lead screw form a rotating mechanism, and the first lead screw is in threaded connection with the first movable frame.
Preferably, the second motor, the first transmission shaft and the clamping table form a rotating mechanism, and the clamping table is in sliding connection with the fixing frame.
Preferably, the third motor, the second transmission shaft and the second lead screw form a rotating mechanism, and the second lead screw is in threaded connection with the second movable frame.
Preferably, the heating box comprises a partition plate, a heating element, a first guide plate and a second guide plate, the partition plate is arranged on the inner side wall of the heating box, the heating element is embedded into the side face of the partition plate, the first guide plate and the second guide plate are arranged in the heating box, and the first guide plate is arranged on the inner side of the second guide plate.
Preferably, filter the casing including the second filter screen, and filter the casing inner wall and be provided with the second filter screen, the second filter screen is provided with two, and the hole crisscross setting each other between two upper and lower second filter screens.
Preferably, handle the case including first connecting plate, third filter screen and second active carbon adsorption net, and handle case up end and be provided with first connecting plate, first connecting plate lower extreme is connected with third filter screen and second active carbon adsorption net, and the third filter screen setting is in the left side of second active carbon adsorption net, and third filter screen and second active carbon adsorption net lower extreme run through simultaneously and handle case upper surface setting in handling the incasement.
Preferably, the storage water tank is including second connecting plate, fourth filter screen, water pump and second spray tube, and the second connecting plate is installed on the storage water tank right side, second connecting plate left side is connected with the fourth filter screen, and the right side wall that runs through the storage water tank on the left of the fourth filter screen sets up in the storage water tank, the storage water tank front side is provided with the water pump, and the water pump is connected with the second spray tube, and the one end that the water pump was kept away from to the second spray tube simultaneously runs through the up end of handling the case.
Compared with the prior art, the invention has the beneficial effects that: the aircraft coating and drying integrated equipment comprises a coating machine,
(1) the aircraft is fixed on the clamping table, the surface of the aircraft is coated through the spraying mechanism, the vertical position of the spraying mechanism is adjusted under the action of a third motor, a second transmission shaft and a second lead screw, and the aircraft on the clamping table is driven to rotate under the action of the second motor and the first transmission shaft to uniformly coat the surface of the aircraft;
(2) the air is pumped into the heating box under the action of the first fan, and is heated by the heating element, and then is sprayed out through the first spray pipe to dry the coated aircraft, a second filter screen arranged in the filter shell can filter the air entering the heating box, so that the entering of dust and impurities is reduced, and in addition, the partition plates arranged in the heating box in a staggered manner and the first guide plate and the second guide plate arranged in the heating box can prolong the heating time of the air in the heating box, so that the air is fully heated;
(3) waste gas, dust and the like in the spraying process can be sucked into the treatment box under the action of the second fan, and are subjected to wet dust fall treatment through the third filter screen, the second active carbon adsorption net and the second spray pipe under the action of water spraying, so that the pollution of discharged gas to the environment is reduced;
(4) the storage water tank provides the water source for the second spray tube, and water after the dust fall is handled flows back to the storage water tank in through the connecting pipe, and the water source waste is reduced to the recyclable after the fourth filter screen filters, and the absorption can be filtered to the combustion gas to first filter screen and the first active carbon adsorption net that equipment body upper end set up in addition when drying process.
Drawings
FIG. 1 is a schematic front sectional view of the present invention;
FIG. 2 is a schematic front view of the present invention;
FIG. 3 is a schematic view of the internal structure of the filter housing according to the present invention;
FIG. 4 is a schematic view of the internal structure of the heating chamber of the present invention;
FIG. 5 is a schematic view showing the internal structure of the treatment tank of the present invention;
FIG. 6 is an enlarged view of the structure at A in FIG. 1 according to the present invention.
In the figure: 1. the device comprises a device body, 101, a through hole groove, 102, a first filter screen, 103, a first activated carbon adsorption screen, 2, a first motor, 3, a bevel gear group, 4, a first lead screw, 5, a first moving frame, 6, a fixed frame, 7, a second motor, 8, a first transmission shaft, 9, a clamping table, 10, a third motor, 11, a second transmission shaft, 12, a supporting frame, 13, a second lead screw, 14, a second moving frame, 15, a spraying mechanism, 16, a conveying pipe, 17, a heating box, 1701, a partition plate, 1702, a heating element, 1703, a first guide plate, 1704, a second guide plate, 18, a first fan, 19, a filtering shell, 1901, a second filter screen, 20, a first spray pipe, 21, a treatment box, 2101, a first connecting plate, 2102, a third filter screen, 2103, a second activated carbon adsorption screen, 22, a second fan, 23, a water storage tank, 24, a connecting pipe, 25, 2501, A second connecting plate, 2502, a fourth filter screen, 2503, a water pump, 2504 and a second spray pipe.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-6, the present invention provides a technical solution: an aircraft coating and drying integrated device is disclosed, as shown in fig. 1 and fig. 6, a first motor 2 is fixedly installed on the left side of a device body 1, the first motor 2 is connected with a first lead screw 4 through a bevel gear set 3, the device body 1 comprises an opening groove 101, a first filter screen 102 and a first activated carbon adsorption net 103, the opening groove 101 is formed in the upper end face of the device body 1, the first filter screen 102 is arranged in the opening groove 101, the upper end of the first filter screen 102 is connected with the first activated carbon adsorption net 103, during drying, the opening groove 101 keeps the interior of the device body 1 communicated with the outside, meanwhile, the first filter screen 102 and the first activated carbon adsorption net 103 filter and adsorb discharged gas to reduce pollution of the discharged gas to the environment, the first motor 2, the bevel gear set 3 and the first lead screw 4 form a rotating mechanism, the first lead screw 4 is in threaded connection with a first moving frame 5, the first lead screw 4 is driven to rotate through the bevel gear set 3 under the action of the first motor 2, the spraying device is characterized in that the first moving frame 5 can conveniently move left and right on the first lead screw 4, the right end of the first lead screw 4 is used for observing that the left side wall of the device body 1 is rotatably connected to the inner side wall of the device body 1, the first moving frame 5 penetrates through the first lead screw 4, the upper end of the first moving frame 5 is connected with the fixed frame 6, the fixed frame 6 is internally provided with a second motor 7, the second motor 7, a first transmission shaft 8 and a clamping table 9 form a rotating mechanism, the clamping table 9 is in sliding connection with the fixed frame 6, the second motor 7 drives an aircraft on the clamping table 9 to rotate through the first transmission shaft 8, so that omnibearing spraying is performed, the second motor 7 is connected with the first transmission shaft 8, the upper end of the first transmission shaft 8 is connected with the clamping table 9, the third motor 10 is arranged on the upper end face of the device body 1, the third motor 10 is connected with the second transmission shaft 11, and the third motor, Second transmission shaft 11 and second lead screw 13 constitute slewing mechanism, and be threaded connection between second lead screw 13 and the second removal frame 14, third motor 10 drives second lead screw 13 through second transmission shaft 11 and rotates, make second removal frame 14 reciprocate on second lead screw 13, the lower extreme of second transmission shaft 11 runs through the upper surface of equipment body 1 and is connected with second lead screw 13, and second lead screw 13 lower extreme runs through support frame 12 up end and rotates and connect on the inside wall of support frame 12, support frame 12 fixed mounting is in equipment body 1, and support frame 12 sets up at mount 6 rear, run through on the second lead screw 13 and be provided with second removal frame 14, and second removal frame 14 front side installs spraying mechanism 15, spraying mechanism 15 is connected with conveying pipeline 16 simultaneously.
As shown in fig. 1, 2, 3 and 4, a heating box 17 is fixed on the upper end surface of the apparatus body 1, and a first fan 18 is installed on the heating box 17, and the first fan 18 is connected with a filtering housing 19, the heating box 17 includes a partition 1701, a heating element 1702, a first guide plate 1703 and a second guide plate 1704, the inner side wall of the heating box 17 is provided with the partition 1701, and the heating element 1702 is embedded in the side surface of the partition 1701, a first guide plate 1703 and a second guide plate 1704 are arranged in the heating box 17, and the first guide plate 1703 is arranged inside the second guide plate 1704, the partition 1701 arranged alternately and the first guide plate 1703 and the second guide plate 1704 are arranged on the partition 1701 and the inner side wall of the heating box 17 to extend the heating time of the gas in the heating box 17, the first guide plate 1703 is arranged on the partition 1701, the second guide plate 1704 is arranged on the partition 1701 and the inner side wall of the heating box 17, the filtering housing 19 includes a second filter screen 1901, and the inner side wall of the filtering shell 19 is provided with a second filter screen 1901, the second filter screen 1901 is provided with two, and the holes between the upper and lower second filter screens 1901 are arranged in a staggered manner, the second filter screen 1901 reduces dust entering into the heating box 17, the left side of the heating box 17 is connected with a first spray pipe 20, one end of the first spray pipe 20 far away from the heating box 17 penetrates through the left side wall of the equipment body 1, the treatment box 21 is fixed on the upper end surface of the equipment body 1, the treatment box 21 is arranged on the right side of the heating box 17, the treatment box 21 is arranged on the front side of a third motor 10, the treatment box 21 comprises a first connecting plate 2101, a third filter screen 2102 and a second active carbon adsorption screen 2103, the upper end surface of the treatment box 21 is provided with a first connecting plate 2101, the lower end of the first connecting plate 2101 is connected with the third filter screen 2102 and the second active carbon adsorption screen 2103, and the third filter screen 2102102 is arranged on the left side, meanwhile, the lower ends of the third filter screen 2102 and the second activated carbon adsorption screen 2103 penetrate through the upper surface of the treatment box 21 and are arranged in the treatment box 21, and the discharged gas is filtered and adsorbed under the action of the third filter screen 2102 and the second activated carbon adsorption screen 2103.
As shown in fig. 1, 2 and 5, the left side of the treatment tank 21 is provided with a second fan 22, the second fan 22 is connected with a suction pipe 23, one end of the suction pipe 23 far away from the second fan 22 penetrates through the upper end face of the apparatus body 1, the suction pipe 23 is arranged in front of the fixing frame 6, the right side of the treatment tank 21 is connected with a connecting pipe 24, the connecting pipe 24 far away from the treatment tank 21 is connected with a water storage tank 25, the water storage tank 25 is arranged on the right side of the apparatus body 1, the water storage tank 25 comprises a second connecting plate 2501, a fourth filter screen 2502, a water pump 2503 and a second spray pipe 2504, the right side of the water storage tank 25 is provided with the second connecting plate 2501, the left side of the second connecting plate 2501 is connected with the fourth filter screen 2502, the left side of the fourth filter screen 2502 penetrates through the right side wall of the water storage tank 25 and is arranged in the water storage tank 25, the front side of the water storage tank 25 is provided with the water pump 2503, the fourth filter screen 2502 can be used after being used for filtering the treated water, two fourth filter screens 2502 are arranged, holes in the upper fourth filter screen 2502 and the lower fourth filter screen 2502 are arranged in a staggered mode, and a sealing piece is arranged between the water storage tank 25 and the second connecting plate 2501.
The working principle is as follows: when the aircraft coating and drying integrated equipment is used, a power supply is switched on, an aircraft is fixed on a clamping table 9, a conveying pipeline 16 is connected with an external coating supply device, the aircraft is subjected to spraying treatment under the action of a spraying mechanism 15, a first motor 7 drives a first transmission shaft 8 to rotate, the aircraft on the clamping table 9 is driven by the first transmission shaft 8 to rotate so as to be sprayed in all directions, a third motor 10 drives a second transmission shaft 11 to rotate, the second transmission shaft 11 drives a second lead screw 13 to rotate, a second movable frame 14 moves on the second lead screw 13 so as to change the spraying position, waste gas impurities and the like in the spraying process are sucked into a treatment box 21 through a suction pipe 23 under the action of a second fan 22, the waste gas impurities and the like are filtered and adsorbed through a third filter screen 2102 and a second active carbon adsorption screen 2103, water in a water storage tank 25 is sprayed out through a second spray pipe 2504 under the action of a water pump 2503 so as to carry out, the treated water flows back into the water storage tank 25 through the connecting pipe 24, can be recycled after being filtered by the fourth filter screen 2502, and after the spraying is finished, the first motor 2 drives the first screw rod 4 to rotate through the bevel gear set 3, so as to move the fixed frame 6 to the left, the air is pumped into the heating box 17 under the action of the first fan 18, heated by the heating element 1702 and sprayed out of the first spray pipe 20 to dry the aircraft, wherein the second filter screen 1901 disposed in the filter housing 19 can filter the air entering the heating box 17 to reduce the dust entering, the partition 1701, the first guide plate 1703 and the second guide plate 1704 disposed in the heating box 17 can prolong the heating time of the air in the heating box 17 to make the air heated more sufficiently, when drying, the first sieve 102 and the first activated carbon adsorption net 103 may filter and adsorb the exhaust gas, and the contents not described in detail in this specification belong to the prior art well known to those skilled in the art.
The terms "central," "longitudinal," "lateral," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientation or positional relationship indicated in the drawings for simplicity of description only and are not intended to indicate or imply that the referenced devices or elements must be in a particular orientation, constructed and operative in a particular orientation, and are not to be considered limiting of the claimed invention.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that various changes in the embodiments and/or modifications of the invention can be made, and equivalents and modifications of some features of the invention can be made without departing from the spirit and scope of the invention.

Claims (9)

1. The utility model provides an aircraft application stoving integration equipment, includes equipment body (1), third motor (10), heating cabinet (17) and handles case (21), its characterized in that:
the device comprises a device body (1), wherein a first motor (2) is fixedly mounted on the left side of the device body (1), the first motor (2) is connected with a first lead screw (4) through a bevel gear set (3), the left side wall of the device body (1) is observed at the right end of the first lead screw (4) and is rotatably connected to the inner side wall of the device body (1), a first movable frame (5) penetrates through the first lead screw (4), the upper end of the first movable frame (5) is connected with a fixed frame (6), a second motor (7) is mounted in the fixed frame (6), the second motor (7) is connected with a first transmission shaft (8), and the upper end of the first transmission shaft (8) is connected with a clamping table (9);
the device comprises a third motor (10), the third motor (10) is installed on the upper end face of the device body (1), the third motor (10) is connected with a second transmission shaft (11), the lower end of the second transmission shaft (11) penetrates through the upper surface of the device body (1) and is connected with a second lead screw (13), the lower end of the second lead screw (13) penetrates through the upper end face of a support frame (12) and is rotatably connected to the inner side wall of the support frame (12), the support frame (12) is fixedly installed in the device body (1), the support frame (12) is arranged behind a fixed frame (6), a second movable frame (14) penetrates through the second lead screw (13), a spraying mechanism (15) is installed on the front side of the second movable frame (14), and the spraying mechanism (15) is connected with a material conveying pipe (16);
the heating box (17) is fixed on the upper end face of the equipment body (1), a first fan (18) is installed on the heating box (17), meanwhile, the first fan (18) is connected with the filtering shell (19), the left side of the heating box (17) is connected with a first spray pipe (20), and one end, far away from the heating box (17), of the first spray pipe (20) penetrates through the left side wall of the equipment body (1);
handle case (21), handle case (21) and fix the up end at the equipment body (1), and handle case (21) and set up the right side at heating cabinet (17), handle case (21) simultaneously and set up the front side at third motor (10), handle case (21) left side and be provided with second fan (22), and second fan (22) are connected with straw (23), straw (23) are kept away from the up end that second fan (22) one end runs through equipment body (1), and straw (23) set up the place ahead at mount (6), handle case (21) right side and be connected with connecting pipe (24), and connecting pipe (24) keep away from and handle case (21) and be connected with storage water tank (25), and storage water tank (25) set up the right side at equipment body (1) simultaneously.
2. The aircraft coating and drying integrated device according to claim 1, characterized in that: the device comprises a device body (1) and is characterized in that the device body (1) comprises a through groove (101), a first filter screen (102) and a first activated carbon adsorption screen (103), the through groove (101) is formed in the upper end face of the device body (1), the first filter screen (102) is arranged in the through groove (101), and the upper end of the first filter screen (102) is connected with the first activated carbon adsorption screen (103).
3. The aircraft coating and drying integrated device according to claim 1, characterized in that: the first motor (2), the bevel gear set (3) and the first lead screw (4) form a rotating mechanism, and the first lead screw (4) is in threaded connection with the first movable frame (5).
4. The aircraft coating and drying integrated device according to claim 1, characterized in that: the second motor (7), the first transmission shaft (8) and the clamping table (9) form a rotating mechanism, and the clamping table (9) is in sliding connection with the fixing frame (6).
5. The aircraft coating and drying integrated device according to claim 1, characterized in that: and the third motor (10), the second transmission shaft (11) and the second lead screw (13) form a rotating mechanism, and the second lead screw (13) is in threaded connection with the second movable frame (14).
6. The aircraft coating and drying integrated device according to claim 1, characterized in that: the heating box (17) comprises a partition plate (1701), a heating element (1702), a first guide plate (1703) and a second guide plate (1704), wherein the partition plate (1701) is arranged on the inner side wall of the heating box (17), the heating element (1702) is embedded into the side face of the partition plate (1701), a first guide plate (1703) and a second guide plate (1704) are arranged in the heating box (17), and the first guide plate (1703) is arranged on the inner side of the second guide plate (1704).
7. The aircraft coating and drying integrated device according to claim 1, characterized in that: filter casing (19) including second filter screen (1901), and filter casing (19) inside wall and be provided with second filter screen (1901), second filter screen (1901) is provided with two, and the mutual staggered arrangement in hole between two upper and lower second filter screens (1901).
8. The aircraft coating and drying integrated device according to claim 1, characterized in that: the treatment box (21) comprises a first connecting plate (2101), a third filter screen (2102) and a second activated carbon adsorption net (2103), the upper end face of the treatment box (21) is provided with the first connecting plate (2101), the lower end of the first connecting plate (2101) is connected with the third filter screen (2102) and the second activated carbon adsorption net (2103), the third filter screen (2102) is arranged on the left side of the second activated carbon adsorption net (2103), and meanwhile the upper surface of the treatment box (21) is arranged at the lower ends of the third filter screen (2102) and the second activated carbon adsorption net (2103) in a penetrating mode.
9. The aircraft coating and drying integrated device according to claim 1, characterized in that: storage water tank (25) is including second connecting plate (2501), fourth filter screen (2502), water pump (2503) and second spray tube (2504), and storage water tank (25) right side installs second connecting plate (2501), second connecting plate (2501) left side is connected with fourth filter screen (2502), and the right lateral wall setting that storage water tank (25) were run through on fourth filter screen (2502) left side is in storage water tank (25), storage water tank (25) front side is provided with water pump (2503), and water pump (2503) are connected with second spray tube (2504), and the one end that water pump (2503) were kept away from in second spray tube (2504) simultaneously runs through the up end of handling case (21).
CN202010828996.0A 2020-08-18 2020-08-18 Aircraft application stoving integration equipment Pending CN111921773A (en)

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Publication number Priority date Publication date Assignee Title
CN112474229A (en) * 2020-12-14 2021-03-12 樊朝亮 Workpiece spraying auxiliary equipment for electrostatic spraying production line
CN113385348A (en) * 2021-08-17 2021-09-14 南通索星流体设备有限公司 Casing paint spraying equipment for power distribution cabinet

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EP2684613A1 (en) * 2012-07-09 2014-01-15 Zachodniopomorski Uniwersytet Technologiczny w Szczecinie Device for exchanging air with heat recovery, especially in spray booths
CN108636645A (en) * 2018-07-31 2018-10-12 江苏自强涂装机械有限公司 A kind of environment-friendly type gadget spray equipment
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CN208853084U (en) * 2018-08-02 2019-05-14 北川泰和新材料有限公司 A kind of spray equipment of sample
CN209205633U (en) * 2018-08-16 2019-08-06 安徽华灿彩钢薄板科技有限公司 A kind of color steel plate production painting installation with drying function
CN210279628U (en) * 2019-06-01 2020-04-10 邹春怡 Wallboard spraying device for building
CN210410084U (en) * 2019-07-29 2020-04-28 福建云驰智能装备制造有限公司 Activated carbon adsorption device of spray-baking paint room
CN211160406U (en) * 2019-11-01 2020-08-04 太仓汎亚涂装设备有限公司 Automatic reciprocating spraying machine

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KR100830228B1 (en) * 2007-04-03 2008-05-19 주식회사 에이,에스,텍 A combined painting booth of oil-paint and water-paint
EP2684613A1 (en) * 2012-07-09 2014-01-15 Zachodniopomorski Uniwersytet Technologiczny w Szczecinie Device for exchanging air with heat recovery, especially in spray booths
CN208661516U (en) * 2018-07-25 2019-03-29 德阳利源节能科技有限公司 A kind of paint spray booth spray piece heating, drying equipment
CN108636645A (en) * 2018-07-31 2018-10-12 江苏自强涂装机械有限公司 A kind of environment-friendly type gadget spray equipment
CN208853084U (en) * 2018-08-02 2019-05-14 北川泰和新材料有限公司 A kind of spray equipment of sample
CN209205633U (en) * 2018-08-16 2019-08-06 安徽华灿彩钢薄板科技有限公司 A kind of color steel plate production painting installation with drying function
CN210279628U (en) * 2019-06-01 2020-04-10 邹春怡 Wallboard spraying device for building
CN210410084U (en) * 2019-07-29 2020-04-28 福建云驰智能装备制造有限公司 Activated carbon adsorption device of spray-baking paint room
CN211160406U (en) * 2019-11-01 2020-08-04 太仓汎亚涂装设备有限公司 Automatic reciprocating spraying machine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112474229A (en) * 2020-12-14 2021-03-12 樊朝亮 Workpiece spraying auxiliary equipment for electrostatic spraying production line
CN113385348A (en) * 2021-08-17 2021-09-14 南通索星流体设备有限公司 Casing paint spraying equipment for power distribution cabinet

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