CN210230791U - A wash drying equipment for space flight and aviation part - Google Patents
A wash drying equipment for space flight and aviation part Download PDFInfo
- Publication number
- CN210230791U CN210230791U CN201920951488.4U CN201920951488U CN210230791U CN 210230791 U CN210230791 U CN 210230791U CN 201920951488 U CN201920951488 U CN 201920951488U CN 210230791 U CN210230791 U CN 210230791U
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- water
- frame plate
- water outlet
- pipe
- drying device
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- 238000001035 drying Methods 0.000 title claims abstract description 33
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 72
- 238000004140 cleaning Methods 0.000 claims description 20
- 239000007921 spray Substances 0.000 claims description 17
- 238000005192 partition Methods 0.000 claims description 10
- ZZUFCTLCJUWOSV-UHFFFAOYSA-N furosemide Chemical group C1=C(Cl)C(S(=O)(=O)N)=CC(C(O)=O)=C1NCC1=CC=CO1 ZZUFCTLCJUWOSV-UHFFFAOYSA-N 0.000 claims description 3
- 239000002699 waste material Substances 0.000 claims description 3
- 238000005406 washing Methods 0.000 abstract description 8
- 230000009977 dual effect Effects 0.000 abstract description 2
- 238000007605 air drying Methods 0.000 abstract 1
- 239000002351 wastewater Substances 0.000 description 6
- 238000005507 spraying Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
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- Cleaning By Liquid Or Steam (AREA)
Abstract
The utility model discloses a washing drying equipment for space flight and aviation part, there is the water tank including a box and a box side fixed mounting, motor and blast air drying device are still installed to the up end of box, and the baffle that the multiunit level set up is installed at even interval in the inner chamber of box, multiunit the up end one side of baffle is all installed through the pivot and is placed the deckle board, place the deckle board and be upper end open-ended cylindricality tubular structure, the lateral surface of placing the deckle board is all cup jointed the worm wheel, and the medial surface symmetry of placing the deckle board installs two sets of hydraulic cylinder, a worm wheel side all meshes and is connected with a set of worm, the top of worm and the coaxial fixed connection of spindle of motor, bottom are inserted and are established in the fixing base to rotate with the fixing base and be connected, hydraulic cylinder's the flexible. This a washing drying equipment for space flight and aviation part realizes rotating washing and stoving dual processing, and the efficiency of washing and stoving is faster, better.
Description
Technical Field
The utility model belongs to the technical field of the part washs, concretely relates to washing drying equipment for space flight and aviation part.
Background
In the field of aeronautical manufacturing, oil and impurities adhere to the surfaces of a plurality of aviation parts after the parts are machined, and the surfaces of the parts must be cleaned by a special cleaning machine in order to ensure the assembly quality of the parts.
However, in the cleaning process, the number of parts is small, and most of the parts can be cleaned only once, so that time is wasted due to repeated cleaning when the parts are more, most of the parts are directly washed by water, the cleaning efficiency is low, and after the parts are cleaned, the parts are mostly required to be taken out for drying treatment, the time is wasted, and the parts cannot be directly cleaned completely at one time.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a wash drying equipment for space flight and aviation part to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a cleaning and drying device for aerospace parts comprises a box body and a box body side face fixedly provided with a water tank, wherein a motor and a blast drying device are further mounted on the upper end face of the box body, a plurality of groups of horizontally arranged partition boards are mounted in an inner cavity of the box body at even intervals, a placing frame plate is mounted on one side of the upper end face of each partition board through a rotating shaft, the placing frame plate is of a cylindrical tubular structure with an opening at the upper end, a worm wheel is sleeved on the outer side face of the placing frame plate, two groups of hydraulic cylinders are symmetrically mounted on the inner side face of the placing frame plate, one side face of the worm wheel is meshed and connected with a group of worms, the top ends of the worms are coaxially and fixedly connected with a shaft of the motor, the bottom ends of the worms are inserted into a fixed seat and are rotatably connected with the fixed seat, push plates are bonded on the telescopic ends of the hydraulic cylinders, the push plates, the bottom of the water spray pipe is provided with a plurality of groups of spray heads in an annular array.
Preferably, the outer side of the bottom end face of the placing frame plate is provided with water leakage holes in an annular array mode, the two side faces of the partition plate are also symmetrically provided with water leakage holes, and a side face, back to the water tank, of the bottom end of the inner cavity of the box body is further connected with a waste water pipe.
Preferably, a group of connecting backing plates are further welded and fixed at one end, close to the inner wall of the frame plate, of the hydraulic cylinder, and the outer side faces of the connecting backing plates are fixed with the inner wall of the frame plate through threads of locking bolts arranged in an annular array.
Preferably, push pedal and clamp plate are discoid structure, and the clamp plate is the rubber slab, and the spring between clamp plate and the push pedal is the rectangle array and is provided with four groups, and the both ends of spring are embedded respectively to be fixed in clamp plate and rubber slab.
Preferably, the water tank is internally connected with a water pump, a water outlet of the water pump is connected with a water outlet pipe, the water outlet pipe is connected with four groups of water outlet branch pipes, the water outlet branch pipes extend into the inner layer of the tank body respectively and are communicated with the top end of the water spray pipe, and a control valve is arranged at the connection position of the water outlet of the water pump and the water outlet pipe.
Preferably, one end of the blast drying device is connected with an air outlet pipe, and the air outlet pipe is respectively communicated with the water outlet pipe and the group of water outlet branch pipes through a three-way valve.
The utility model discloses a technological effect and advantage: according to the cleaning and drying equipment for the aerospace parts, a plurality of groups of partition plates are arranged in the box body, the rotatable placing frame plate is mounted on the partition plates, the water spraying pipe and the spray head are mounted on the upper end face of the placing frame plate, the water spraying pipe and the spray head are connected with the water tank and are also connected with the blast drying device, and the placing frame plate can rotate through the transmission of the worm and the worm wheel, so that the dual treatment of rotating cleaning and drying can be realized, and the cleaning and drying efficiency is higher and better; in addition, different aviation parts can be placed in the placing frame plates by simultaneously applying the plurality of groups of placing frame plates, more parts can be cleaned and dried at one time, and the rapid cleaning and drying of the whole parts are improved; and place and be provided with hydraulic cylinder in the deckle board, can fix the part centre gripping by the extension of hydraulic cylinder in placing the deckle board, when can making rotatory washing stoving, reduce the rocking that rotates and arouse to avoid the wearing and tearing that the collision takes place as far as, and the cylinder can be installed by oneself according to the user demand, and practical function is better.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is an enlarged view of the structure a in fig. 1 according to the present invention;
fig. 3 is an enlarged view of the structure B in fig. 1 according to the present invention.
In the figure: the device comprises a box body 1, a water tank 2, a blast drying device 3, a motor 4, a partition plate 5, a placing frame plate 6, a rotating shaft 7, a worm 8, a worm wheel 9, a waste water pipe 10, a water leakage hole 11, a hydraulic cylinder 12, a water spray pipe 13, a spray nozzle 14, an air outlet pipe 15, a water outlet pipe 16, a three-way valve 17, a connecting base plate 18, a locking bolt 19, a push plate 20, a spring 21, a press plate 22 and a control valve 23.
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.
The utility model provides a cleaning and drying device for aerospace parts as shown in figures 1-3, which comprises a box body 1 and a side surface of the box body 1, a water tank 2 is fixedly arranged on the upper end surface of the box body 1, a motor 4 and a blast drying device 3 are also arranged on the upper end surface of the box body 1, a plurality of groups of horizontally arranged partition plates 5 are arranged in an inner cavity of the box body 1 at even intervals, a placing frame plate 6 is arranged on one side of the upper end surface of each group of partition plates 5 through a rotating shaft 7, the placing frame plate 6 is a cylindrical tubular structure with an open upper end, a worm wheel 9 is sleeved on the outer side surface of the placing frame plate 6, two groups of hydraulic cylinders 12 are symmetrically arranged on the inner side surface of the placing frame plate 6, a group of worms 8 are engaged and connected on one side surface of the worm wheel 9, the top ends of the worms 8 are, thereby accomplish a set of motor 4 and place the rotation of framed panel 6 in pivot 7 through driving the multiunit, hydraulic cylinder 12's flexible end all bonds has push pedal 20, push pedal 20 through spring 21 with bulldoze board 22 fixed connection, place the spray pipe 13 that the level set up still installed in framed panel 6's top, the bottom of spray pipe 13 all is annular array and installs multiunit shower nozzle 14, the setting of spray pipe 13 and shower nozzle 14 is similar with the water jet equipment that current shower used.
Specifically, the bottom face outside of placing frame plate 6 is annular array and has seted up hole 11 that leaks, hole 11 that leaks has also been seted up to the both sides face of baffle 5 symmetry, and the side that the inner chamber bottom of box 1 is in the place of water tank 2 dorsad still is connected with waste pipe 10, can discharge the waste water after the washing, and the valve also should be installed during the actual use on waste pipe 10.
Specifically, hydraulic cylinder 12 still welded fastening has a set of connecting pad 18 with the one end of placing the inner wall of framed panel 6 and hugging closely, the lateral surface of connecting pad 18 passes through the locking bolt 19 that the annular array set up and the inner wall thread tightening of placing framed panel 6 to conveniently dismantle hydraulic cylinder 12, install the hydraulic cylinder 12 of different models according to actual need.
Specifically, push pedal 20 and clamp plate 22 are discoid structure, and clamp plate 22 is the rubber slab, can provide the buffer capacity at the centre gripping in-process, makes the centre gripping more firm, and spring 21 between clamp plate 22 and the push pedal 20 is the rectangle array and is provided with four groups, and embedded the fixing respectively in clamp plate 22 and the rubber slab in the both ends of spring 21.
Specifically, the inside of the water tank 2 is connected with a water pump, the water outlet of the water pump is connected with a water outlet pipe 16, the water outlet pipe 16 is connected with four groups of water outlet branch pipes, the water outlet branch pipes extend into the inner layer of the tank body 1 respectively and are communicated with the top end of the water spraying pipe 13, and a control valve 23 is arranged at the connection position of the water outlet of the water pump and the water outlet pipe 16.
Specifically, the one end of air-blast drying device 3 is connected with 15 pipes of air-out, and air-blast drying device 3 can be electric fan or other drying-machine equipment, and 15 pipes of air-out are linked together with outlet pipe 16 and a set of outlet branch pipe respectively through three-way valve 17.
Specifically, the lateral surface of box 1 still should install the side door that is used for sealed box 1, opens when conveniently accomplishing the back when the part washs the stoving, and the during operation is closed, is common structure.
Specifically, the cleaning and drying equipment for aerospace parts comprises the steps of firstly putting parts into a placing frame plate 6, then controlling hydraulic cylinders 12 in different placing frame plates 6 to extend, clamping and fixing the parts in the placing frame plate 6, then sealing a box body 1, closing one end of a three-way valve 17 communicated with an air outlet pipe 15 when cleaning, opening a water pump in a water tank 2, opening a motor 4, spraying water in the water tank 2 from a water outlet pipe 16 and a water outlet branch pipe finally from a water spraying pipe 13 and a spray head 14 by the water pump, washing the surfaces of the parts in the placing frame plate 6, simultaneously rotating the motor 4 to drive a worm 8 to rotate, so as to drive a plurality of groups of worm wheels 9 to rotate, further rotating the placing frame plate 6 on a rotating shaft 7, driving the rotation of internal parts, cleaning the rotation, and having better cleaning efficiency, and dripping cleaned wastewater into the bottom end of the box body 1 from a water leakage hole 11, finally, the waste water is discharged from the waste water pipe 10, when the drying is carried out after the cleaning is finished, the control valve 23 is closed, the air outlet pipe 15 of the three-way valve 17 is opened, the air outlet pipe 15 is communicated with the water outlet pipe 16 and the water outlet branch pipe, then the blast drying device 3 is opened, hot air is sprayed out from the water spray pipe 13 and the spray head 14, the drying is carried out during the rotation, and the drying effect is better.
Finally, it should be noted that: 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 modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.
Claims (6)
1. The utility model provides a wash drying equipment for space flight and aviation part, includes that box (1) and box (1) a side fixed mounting have water tank (2), its characterized in that: the upper end face of the box body (1) is further provided with a motor (4) and a blast drying device (3), a plurality of groups of horizontally arranged partition plates (5) are uniformly arranged in an inner cavity of the box body (1) at intervals, one side of the upper end face of each group of partition plates (5) is provided with a placing frame plate (6) through a rotating shaft (7), the placing frame plate (6) is of a cylindrical tubular structure with an open upper end, the outer side face of the placing frame plate (6) is sleeved with a worm wheel (9), two groups of hydraulic cylinders (12) are symmetrically arranged on the inner side face of the placing frame plate (6), one side face of the worm wheel (9) is respectively connected with one group of worms (8) in a meshed manner, the top end of each worm (8) is coaxially and fixedly connected with a crankshaft of the motor (4), the bottom end of each worm is inserted into a fixed seat and is rotationally connected with the fixed, the push plate (20) is fixedly connected with the push plate (22) through a spring (21), a horizontally arranged water spray pipe (13) is further installed above the frame plate (6), and a plurality of groups of spray heads (14) are installed at the bottom ends of the water spray pipes (13) in an annular array mode.
2. The cleaning and drying device for aerospace parts according to claim 1, wherein: the bottom face outside of placing frame plate (6) is the annular array and has seted up hole (11) that leaks, hole (11) that leaks have also been seted up to the both sides face of baffle (5) symmetry, and the side at the inner chamber bottom dorsad water tank (2) place of box (1) still is connected with waste pipe (10).
3. The cleaning and drying device for aerospace parts according to claim 1, wherein: the hydraulic cylinder (12) and the end of placing the inner wall of the frame plate (6) to be attached are fixedly welded with a group of connecting base plates (18), and the outer side surfaces of the connecting base plates (18) are fixed with the inner wall of the frame plate (6) through threads of locking bolts (19) arranged in an annular array.
4. The cleaning and drying device for aerospace parts according to claim 1, wherein: push pedal (20) and clamp plate (22) are discoid structure, and clamp plate (22) are the rubber slab, and spring (21) between clamp plate (22) and push pedal (20) are the rectangle array and are provided with four groups, and the both ends of spring (21) are embedded respectively to be fixed in clamp plate (22) and rubber slab.
5. The cleaning and drying device for aerospace parts according to claim 1, wherein: the water tank (2) is internally connected with a water pump, a water outlet of the water pump is connected with a water outlet pipe (16), the water outlet pipe (16) is connected with four groups of water outlet branch pipes which respectively extend into the inner layer of the tank body (1) to be communicated with the top end of the water spray pipe (13), and a control valve (23) is arranged at the joint of the water outlet of the water pump and the water outlet pipe (16).
6. The cleaning and drying device for aerospace parts according to claim 1, wherein: one end of the blast drying device (3) is connected with an air outlet (15) pipe, and the air outlet (15) pipe is respectively communicated with a water outlet pipe (16) and a group of water outlet branch pipes through a three-way valve (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920951488.4U CN210230791U (en) | 2019-06-24 | 2019-06-24 | A wash drying equipment for space flight and aviation part |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920951488.4U CN210230791U (en) | 2019-06-24 | 2019-06-24 | A wash drying equipment for space flight and aviation part |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210230791U true CN210230791U (en) | 2020-04-03 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920951488.4U Expired - Fee Related CN210230791U (en) | 2019-06-24 | 2019-06-24 | A wash drying equipment for space flight and aviation part |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210230791U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111530830A (en) * | 2020-05-18 | 2020-08-14 | 江西弘珽金属制品有限公司 | Outer surface cleaning equipment for plastic product processing |
| CN114082697A (en) * | 2021-11-24 | 2022-02-25 | 中国机房设施工程有限公司 | Clean channel system for purifying large-scale component |
-
2019
- 2019-06-24 CN CN201920951488.4U patent/CN210230791U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111530830A (en) * | 2020-05-18 | 2020-08-14 | 江西弘珽金属制品有限公司 | Outer surface cleaning equipment for plastic product processing |
| CN114082697A (en) * | 2021-11-24 | 2022-02-25 | 中国机房设施工程有限公司 | Clean channel system for purifying large-scale component |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200403 |