CN102941474B - Casing of machining device - Google Patents
Casing of machining device Download PDFInfo
- Publication number
- CN102941474B CN102941474B CN201210359706.8A CN201210359706A CN102941474B CN 102941474 B CN102941474 B CN 102941474B CN 201210359706 A CN201210359706 A CN 201210359706A CN 102941474 B CN102941474 B CN 102941474B
- Authority
- CN
- China
- Prior art keywords
- fuselage
- panel
- connector
- cover
- lower panel
- 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
Links
Landscapes
- Auxiliary Devices For Machine Tools (AREA)
Abstract
The invention discloses a casing of a machining device. The casing comprises a machine body panel, and further comprises all-in-one sectional machine body connecting pieces arranged at four corners and provided with arc-shaped corners, wherein the machine body panel comprises a lower panel, or a lower panel and an upper panel; two lateral slots are molded on each machine body connecting piece; the opposite slots of the two machine body connecting pieces on the same side are internally fixed with the lower panel and detachably mounted with an upper panel, or the opposite two slots of the machine body connecting pieces on the same side are internally fixed with the lower panel and mounted with a door that is mounted on the machine body connecting pieces on the side; a bottom plate with a side connected with the lower panel is fixed at the bottom near the lower panel; a mounting plate is fixed above the bottom plate; an accommodation space is formed between the bottom plate and the mounting plate; a liquid collecting cavity for sealing liquid is formed above the mounting plate; liquid leakage holes are arranged in the mounting plate; a liquid collecting pool is arranged in the accommodation space; and the liquid leakage holes rightly face the liquid collecting pool. The casing has the advantages of convenience in installation, more beautiful appearance, low possibility of hurting a user and more safety in use.
Description
Technical field
The present invention relates to a kind of machining apparatus casing, particularly relate to the casing of the equipment such as a kind of blind rivet unit mahine, washer unit mahine, the blind rivet of loosing core, slotter, tail milling machine, thread rolling machine, thread rolling machine, brill tail forming machine, numerical control machine.
Background technology
The casing of existing equipment is to be all welded by panel beating.The shortcoming of this casing is that the corner of casing is wedge angle, cannot make fillet.Because equipment needs repairing and process operation, need to there is fluid collection chamber etc., so the panel of casing need be divided into top panel or lower panel, or lower panel and door, the existing mode by welding is fixed together lower panel and top panel, processing trouble, and outward appearance is not attractive in appearance, maintenance, debugging and the use of process equipment, wedge angle is easily damaged.
Application number is in 201020673576.1 utility model patent, a kind of angle syndeton of thermal insulation faceplates of air handling unit band collet is disclosed, at the angle steel at four jiaos of places, unit box body outer side covers panel, angle connector is located at corner, forms by decorating cover fillet, angle connector, collet and securing member, decorates cover fillet and comprises exterior finish and two hooks, exterior finish is circular arc, and both side edges is covered the outside at two panels; Two hooks are located at respectively the left and right sides of exterior finish inwall; Angle connector comprises joint face, two outer drag hooks and two interior drag hooks, and outer drag hook is located at the both sides of joint face, with corresponding the buckling of hook of decorating cover fillet; Interior drag hook is located at joint face both sides, with the corresponding slotting embedding of groove on panel lateral margin; Collet pads respectively the inside and outside both sides that are located at a joint face; Securing member is fixed the joint face of collet, angle connector and angle steel.In this utility model, on the one hand by angle connector, angle steel, the acting in conjunction of decoration cover fillet by orthogonal two erecting of panels together, structure is very complicated; This patent is only open is on the other hand installed together panel by connector.
Application number is in 02213466.2 utility model patent, a kind of dry-type transformer protective shell manufacturing with aluminium alloy special-shaped section.This dry-type transformer protective shell is by four sides and upper and lower bottom surface forms and with the rectangular box structure of opening the door, the column of this casing frame is to be all formed by fixedly connecting by two square aluminium alloy extrusions 6 with wing 3, two wings of this square aluminium alloy extrusions are on opposite flank, and mutually vertical; Form arrangements that meet at right angles of two square aluminium alloy extrusions of column, on its opposite flank, with groove type or boss shape connector, in two pawl Snap joint devices of backplate, make the structures such as turning formation circular arc, trapezoidal, many prismatics.This patent is only open to be only openly installed together panel by connector, and the connecting-piece structure of connection panel is very complicated.
Summary of the invention
The technical problem to be solved in the present invention be to provide a kind of very easily by the erecting of panel of casing together, appearance looks elegant, easily form the machining apparatus casing of fluid collection chamber, hydrops pond and accommodation space.
A kind of machining apparatus casing, comprises fuselage panel, also comprises the integrated section bar fuselage connector that is arranged on four angle positions, is provided with arc corner; Fuselage panel comprises lower panel or lower panel and top panel; On fuselage connector, form two side direction slots of setting angle; In being all fixed with lower panel and top panel or two slots relative at the same side fuselage connector are installed removably in the relative slot of two fuselage connectors of the same side, be fixed with lower panel and be arranged on the door on the fuselage connector of this side; Be fixed with in the bottom near lower panel the base plate that side is connected with lower panel, above base plate, be also fixed with installing plate that side is connected with lower panel, fitting machine process equipment main body, between base plate and installing plate, form accommodation space; Installing plate top forms the fluid collection chamber of liquid sealing; On installing plate, be provided with liquid-leaking nozzle; In accommodation space, be provided with hydrops pond; Liquid-leaking nozzle is just to hydrops pond.
As the improvement of scheme one, in the relative slot of two fuselage connectors of every side, be all fixed with lower panel and top panel is installed removably; Also comprise cover, cover comprises the cover connector that is arranged on four angle positions, coordinates with corresponding fuselage connector; Cover connector comprises the cover connector body of arc corner, sets the cover slot of angle for two; In two relative cover slots of cover connector, be all fixed with cover panel; Cover also comprises the top board of the end face that is fixed on cover connector and cover panel; Cover links together opening or closing with a corresponding top panel.Cover also adopts by cover connector by cover erecting of panel together, makes cover and fuselage perfect adaptation, and outward appearance is more attractive in appearance.
As the improvement of scheme two, also comprise cover, on fuselage connector, be also provided with fuselage locating hole; On cover connector, be also provided with the cover locating hole coordinating with fuselage locating hole; In relative fuselage locating hole or cover locating hole, be fixed with locating dowel.Coordinate by locating dowel and locating hole, cover is covered accurately on fuselage.
As the improvement of scheme two, the cover connector being installed together and the end face of cover panel are cascaded surface.Meet the use needs of the equipment such as heading machine, thread rolling machine.
As the improvement of scheme one, in relative two slots of two fuselage connectors more than a side, be fixed with lower panel and be arranged on the door more than fan on a fuselage connector of this side or be arranged on respectively the door more than fan on two fuselage connectors of this side, door is arranged on the fuselage connector of this side by hinge.By hinge, door is installed, simple in structure, easy to use.
As the improvement of scheme one, be more than two fans at a side door, corresponding fuselage connector also comprises locating slot, and positioning strip is installed in locating slot.Use positioning strip, the multiple leaf door of the same side is remained on same straight line.
As the improvement of scheme one, in the relative slot of two fuselage connectors of each side, be all fixed with lower panel and top panel is installed removably; The fuselage connector being installed together and the end face of top panel are cascaded surface; Also be provided with the cover that the top planes the highest with cascaded surface coordinates; Cover links together opening or closing with a corresponding top panel.The stepped use needs that meet the equipment such as heading machine, thread rolling machine.Machine semitight state, oil is difficult for running out of casing, and the operation of debugging machine, monitoring machine is convenient.
As the improvement of scheme one, fuselage panel comprises lower panel and top panel; On fuselage connector more than a side, extrusion modling has installing hole, also comprises with installing hole and is installed together the driving mechanism that drives top panel automatically to move up and down.When top panel is too large when inconvenient with manpower dismounting, when use, promotes top panel formation action pane by driving mechanism, easy to use, laborsaving.
As the common improvement of such scheme, in two relative slots of each side fuselage connector, be all fixed with lower panel and top panel is installed removably; Plate is provided with to block near the position of corresponding fuselage connector and is provided with the lower baffle plate blocking with the seam of corresponding lower panel with the slanting baffle of the seam of this fuselage connector, near bottom position in the above.Slanting baffle avoids oil, cooling fluid etc. to overflow fuselage outside from the junction of fuselage connector and top panel, lower baffle plate avoids oil, cooling fluid etc. to overflow from the junction of top panel and lower panel outside fuselage.
As the common improvement of such scheme, be equipped with both sides and adjacent lower panel engages, bottom surface engages with installing plate sealing plate four corners; Lower panel, installing plate, sealing plate form the fluid collection chamber that is positioned at installing plate top.Adopt sealing plate, the easier liquid sealing of fluid collection chamber, sealing effectiveness is better.
The invention has the beneficial effects as follows, because panel, door are installed together formation casing by the fuselage connector that adopts extrusion modling, easy for installation; Four corner rounding ofves, make casing outward appearance more attractive in appearance, are difficult for being bruised when use, use safer.Particularly lower panel and top panel or lower panel and door are installed together by fuselage connector in the same side, install easily; Top panel inserts in slot, and easy installation and removal, is convenient to maintenance, debugging and the use of process equipment.Lower panel, fuselage connector, installing plate top easily form fluid collection chamber, meet the needs such as oil, cooling fluid of collecting from machining apparatus.Because top panel and slot are flexibly connected, top panel can be used plastic plate, very convenient like this on plastic plate one-body molded side shield, lower baffle plate etc.
Brief description of the drawings
Fig. 1 is the perspective exploded view of the embodiment of the present invention 1.
Fig. 2 is the cross-sectional schematic of the A-A of Fig. 1.
Fig. 3 is the perspective exploded view of the embodiment of the present invention 2.
Fig. 4 is the schematic perspective view of the embodiment of the present invention 3.
Fig. 5 is the cross-sectional schematic of the B-B of Fig. 4.
Fig. 6 is the enlarged diagram of the I portion of Fig. 5.
Fig. 7 is the schematic top plan view of the fuselage connector of the embodiment of the present invention 3.
Fig. 8 is the schematic perspective view of the embodiment of the present invention 4.
Fig. 9 is the schematic perspective view of the door open mode of the embodiment of the present invention 4.
Figure 10 is the schematic perspective view of the embodiment of the present invention 5.
Figure 11 is the perspective exploded view of the embodiment of the present invention 6.
Figure 12 is the another perspective exploded view of the embodiment of the present invention 6.
Schematic perspective view when Figure 13 is the embodiment of the present invention 6 apparatus lid opening.
Schematic perspective view when Figure 14 is the embodiment of the present invention 7 apparatus lid opening.
Schematic perspective view when Figure 15 is the embodiment of the present invention 8 apparatus lid opening.
Schematic perspective view when Figure 16 is the embodiment of the present invention 9 apparatus lid opening.
Detailed description of the invention
Embodiment 1
As shown in Figure 1 and Figure 2, a kind of machining apparatus casing, comprises and is arranged on four integrated section bar fuselage connector 1, fuselage connector 2, fuselage connector 3, fuselage connectors 4 that angle position structure is identical.Fuselage connector 4 comprises arc corner segments 5 and is arranged on arc corner segments 5 two ends, orthogonal straightway 6, straightway 7, on straightway 6, be provided with side direction slot 8, on straightway 7, be provided with the side direction slot 9 vertical with side direction slot 8, be provided with and make the uniform through hole 10 of fuselage connector wall thickness in arc corner segments 5.
Machining apparatus casing also comprises between the slot that insertion fuselage connector 1 is relative with fuselage connector 2 and fixing front lower panel 11, and activity is inserted between the slot that fuselage connector 1 is relative with fuselage connector 2, dismountable front top panel 12; Insert between the slot that fuselage connector 2 is relative with fuselage connector 3 and fixing lower-left panel 13, activity is inserted between the slot that fuselage connector 2 is relative with fuselage connector 3, dismountable upper left panel 14; Insert between the slot that fuselage connector 3 is relative with fuselage connector 4 and fixing rear lower panel 15, activity is inserted between the slot that fuselage connector 3 is relative with fuselage connector 4, dismountable rear top panel 16; Insert between the slot that fuselage connector 4 is relative with fuselage connector 1 and fixing bottom right panel 17, activity is inserted between the slot that fuselage connector 4 is relative with fuselage connector 1, dismountable upper right panel 18.End face and the bottom surface of the front lower panel 11 of panel beating, lower-left panel 13, rear lower panel 15, bottom right panel 17 flush, the end face of the front top panel 12 of panel beating, upper left panel 14, rear top panel 16, upper right panel 18 and bottom surface flushes and be supported on respectively on corresponding front lower panel 11, lower-left panel 13, rear lower panel 15, bottom right panel 17.Be fixed with near the bottom of front lower panel 11, lower-left panel 13, rear lower panel 15, bottom right panel 17 base plate 19 that four sides are connected with front lower panel 11, lower-left panel 13, rear lower panel 15, bottom right panel 17 respectively, above base plate 19, be also fixed with side successively with front lower panel 11, fuselage connector 2, lower-left panel 13, fuselage connector 3, rear lower panel 15, fuselage connector 4, bottom right panel 17 installing plate 20 that be connected, fitting machine process equipment main body.The end face of installing plate 20 is lower than the end face of front lower panel 11.Between base plate 19 and installing plate 20, form accommodation space 21.Be provided with in the corner of corresponding fuselage connector 2 both sides respectively with the sealing plate (not shown) of front lower panel 11 and lower-left panel 13 solder joints, bottom surface and installing plate 20 solder joints; Be provided with in the corner of corresponding fuselage connector 3 both sides respectively with the sealing plate (not shown) of lower-left panel 13 and rear lower panel 15 solder joints, bottom surface and installing plate 20 solder joints; Be provided with in the corner of corresponding fuselage connector 4 both sides respectively with the sealing plate 22 of rear lower panel 15 and bottom right panel 17 solder joints, bottom surface and installing plate 20 solder joints; Be provided with in the corner of corresponding fuselage connector 1 both sides respectively with the sealing plate (not shown) of bottom right panel 17 and front lower panel 11 solder joints, bottom surface and installing plate 20 solder joints.The sealing plate of installing plate 20 and front lower panel 11, lower-left panel 13, rear lower panel 15, bottom right panel 17, four corners be formed on seam crossing by weld seam (not shown) liquid sealing, be positioned at the fluid collection chamber 23 of installing plate 20 tops; On installing plate 20, be provided with liquid-leaking nozzle 24; In accommodation space 21, be provided with hydrops pond 25; Liquid-leaking nozzle 24 is just to hydrops pond 25.
On the end face of fuselage connector 1, fuselage connector 2, fuselage connector 3, fuselage connector 4, be all fixed with seal cover 26, seal cover 27, seal cover 28, the seal cover 29 of the identical sealing through hole of structure.The neighboring of seal cover 29 cross sections is identical with the neighboring of fuselage connector 4 cross sections.
The top panel of four sides all can be opened, and need to, from which side operation, only need, from the corresponding top panel of upper extraction, after having operated, more corresponding top panel be inserted in corresponding slot.
Embodiment 2
As shown in Figure 3, as different from Example 1, rear top panel 40 inserts in the slot of fuselage connector 41, fuselage connector 42 and fixes by securing member (not shown) with fuselage connector 41, fuselage connector 42, upper right panel 43 is inserted in the slot of fuselage connector 42, fuselage connector 44 and is fixed by securing member (not shown) with fuselage connector 42, fuselage connector 44, in the movable slot that inserts fuselage connectors 44, fuselage connector 46 of front top panel 45.In the movable slot that inserts fuselage connector 46, fuselage connector 41 of upper left panel 47.Installing plate 48 and front lower panel 49, fuselage connector 46, lower-left panel 50, fuselage connector 41, rear lower panel 51, fuselage connector 42, bottom right panel 52, fuselage connector 44 be formed on seam crossing by glass cement (not shown) liquid sealing, be positioned at the fluid collection chamber of installing plate 48 tops.
Embodiment 3
As shown in Figures 4 to 6, as different from Example 1, in two relative slots of fuselage connector 60, fuselage connector 61, be fixed with lower panel 62 and top panel 63 is installed removably, the plastic plate that top panel 63 is formed in one, plate 63 is provided with the slanting baffle 64 blocking with the seam of fuselage connector 60 near fuselage connector 60 positions in the above, plate 63 is provided with the slanting baffle 65 blocking with the seam of fuselage connector 61 near fuselage connector 61 positions in the above, is being provided with the lower baffle plate 66 blocking with the seam of lower panel 62 near top panel 63 bottom positions.On the top panel of its excess-three side, be equipped with slanting baffle and lower baffle plate.
As shown in Figure 7, the structure of four fuselage connectors is identical.Fuselage connector 61 is section bar, comprise circular arc-shaped corner V-shape portion 67, circular arc-shaped corner V-shape portion 68 and the connecting portion 69, connecting portion 70, the connecting portion 71 that are connected V-shape portion 67, V-shape portion 68; V-shape portion 67, V-shape portion 68 form two vertical side direction slots 72 with connecting portion 71, and V-shape portion 67, V-shape portion 68 form two vertical side direction slots 73 with connecting portion 69.
Embodiment 4
As shown in Figure 8, Figure 9, as different from Example 1, rear top panel 90 inserts in the slot of fuselage connector 91, fuselage connector 92 and fixes by securing member (not shown) with fuselage connector 91, fuselage connector 92, and upper right panel 93 is inserted in the slot of fuselage connector 92, fuselage connector 94 and fixed by securing member (not shown) with fuselage connector 92, fuselage connector 94.
Fuselage connector 94 is different from fuselage connector 92, is also provided with columniform protuberance 97 on the medial surface of the corresponding slot 96 of fuselage connector 94, is provided with axial installation through hole 98 in protuberance 97.
Fuselage connector 91 is different from fuselage connector 92, is also provided with the L shaped protuberance 101 that forms locating slot 100 on the medial surface of the corresponding slot 99 of fuselage connector 91.
Fuselage connector 95 is different from fuselage connector 92, is also provided with columniform protuberance 103 on the medial surface of the corresponding side slot 102 of fuselage connector 95, is provided with axial installation through hole 104 in protuberance 103; On the medial surface of the corresponding opposite side slot 106 of fuselage connector 95, be also provided with the L shaped protuberance 108 that forms locating slot 107.
Axially installing in through hole 98 rotating shaft 109 is installed, hinge 110, lower jaw (not shown) are installed in rotating shaft 109, also comprise the door 111 being installed together by upper hinge 110, lower jaw and fuselage connector 94.Axially installing in through hole 104 rotating shaft 112 is installed, hinge 113, lower jaw 114 are installed in rotating shaft 112, also comprise the door 125 being installed together by upper hinge 113, lower jaw 114 and fuselage connector 95.
The upper hinge 115, the lower jaw 116 that on fuselage connector 95, are provided with, also comprise the door 117 being installed together by upper hinge 115, lower jaw 116 and fuselage connector 95, be arranged on upper hinge 118, lower jaw 119 on door 117, by upper hinge 118, lower jaw 119 and 117 door 120 that are installed together, be arranged on upper hinge 121, lower jaw 122 on door 120, by upper hinge 121, lower jaw 122 and 120 door 123 that are installed together.In locating slot 100, locating slot 107, positioning strip 124 is installed.On the medial surface of front lower panel 96, be provided with the end face of lower panel 96 before protruding, with 111,125 keeper that coordinate 126.
Embodiment 5
As shown in figure 10, as different from Example 3, upper left panel 140, rear top panel 141, the upper right panel 142 fuselage connector corresponding with it are fixed.The end face of upper left panel 140, upper right panel 142 is flexuose cascaded surface, and the minimum end face of upper left panel 140, upper right panel 142 flushes with the end face of front top panel 143, and the highest end face flushes with the end face of rear top panel 141.Also be provided with the cover 145 that the end face the highest with end face, upper left panel 140 and the upper right panel 142 of the end face of two fuselage connectors 144 of rear side, rear top panel 141 coordinates; Cover 145 is installed together by hinge 146, hinge 147 opening or closing with rear top panel 141.
Embodiment 6
As shown in Figure 11, Figure 12, as different from Example 4, between the relative draw-in groove of fuselage connector 161, the fuselage connector 162 of front side, can move back and forth be up and down provided with before top panel 164.Also comprise the driving mechanism that before driving, top panel 164 moves up and down.
Be provided with protuberance 165, protuberance 166 in the both sides of front top panel 164, in protuberance 165, be provided with vertical through holes 167, in protuberance 166, be provided with vertical through holes 168.
Fuselage connector 161 is different from fuselage connector 160, is provided with the screw rod installing hole 170 being communicated with a side slot 169 on fuselage connector 161.
Fuselage connector 162 is different from fuselage connector 160, is provided with the screw rod installing hole 172 being communicated with a side slot 171 on fuselage connector 162; On the medial surface of the corresponding opposite side slot 173 of fuselage connector 162, be also provided with the L shaped protuberance 175 that forms locating slot 174.
Driving mechanism comprises the drive motors 176 being arranged on fuselage connector 161, coaxially install with drive motors 176, with motor coaxle install synchromesh gear 177, fix, be arranged on the screw rod 178 in screw rod installing hole 170 with motor shaft, the nut (not shown) that be arranged in vertical through holes 167, coordinates with screw rod 178; Be arranged on the screw rod 179 in screw rod installing hole 172, be arranged in vertical through holes 168, with the nut that screw rod 179 coordinates, be fixed on the synchromesh gear 180 on screw rod 179; What coordinate with synchromesh gear 177, synchromesh gear 180 synchronizes tooth bar 181.
Embodiment 7
As shown in figure 13, as different from Example 1, also comprise flat cover 190, cover 190 is arranged on rear top panel 192 by hinge 191.
On the fuselage connector 193 of front side, be also provided with fuselage locating hole 194; On cover 190, be also provided with the cover locating dowel 195 coordinating with fuselage locating hole 194.
Embodiment 7
As shown in figure 14, as different from Example 1, on the fuselage connector 219 of front side, be also provided with fuselage locating hole 211, on the fuselage connector 216 of front side, be also provided with fuselage locating hole 210.In fuselage locating hole 210, be fixed with locating dowel 212, in fuselage locating hole 211, be fixed with locating dowel 213.
Also comprise cover.Cover comprises and is arranged on four angle positions, with corresponding fuselage connector 216, fuselage connector 217, fuselage connector 218, the cover connector 198 that fuselage connector 219 coordinates, cover connector 199, cover connector 200, cover connector 201, be fixed on the cover connector 198 of the same side, cover panel 202 in the relative cover slot of cover connector 199, be fixed on the cover connector 199 of the same side, cover panel 203 in the relative cover slot of cover connector 200, be fixed on the cover connector 200 of the same side, cover panel 204 in the relative cover slot of cover connector 201, be fixed on the cover connector 201 of the same side, cover panel 205 in the relative cover slot of cover connector 198, cover also comprises the top board 206 of the end face that is fixed on all cover connectors and cover panel, the top board 206 of cover and corresponding rear top panel 207 by gas support 208, gas support 209 links together opening or closing.Cover connector 198, cover connector 199, cover connector 200, cover the connector 201 respectively cross section of the fuselage connector 216 corresponding with it, fuselage connector 217, fuselage connector 218, fuselage connector 219 are identical.
On cover connector 198 cover locating hole 214 coordinate with locating dowel 212; On cover connector 201 cover locating hole 215 coordinate with locating dowel 213.
Embodiment 8
As shown in figure 15, as different from Example 7, the rear board 230 of cover is installed together with rear top panel 233 by hinge 231, hinge 232.
Embodiment 9
As shown in figure 16, as different from Example 7, all cover connectors that are installed together and the end face of cover panel are cascaded surface 240.The rear board 241 of cover is installed together by hinge (not shown) and rear top panel 242.
Protection scope of the present invention is not limited to embodiment scope of disclosure, and if the number of the connecting plate of corner is five, the number of fuselage connector is five, and two slots of fuselage connector become 108 ° to form pentagonal casing; The number of connecting plate is 6, and the number of fuselage connector is 6, and two slots of fuselage connector become 120 ° to form hexagonal casing; Or the angle of two slots on the fuselage connector on same casing is different, form irregular polygonal casing; Fuselage connector only need comprise two slots, and its structure can be ever-changing, and technique scheme all can realize according to embodiment disclosed by the invention, thus in the present invention, no longer draw and illustrate, but all in protection scope of the present invention.
Claims (10)
1. a machining apparatus casing, comprises fuselage panel, it is characterized in that: also comprise the integrated section bar fuselage connector that is arranged on four angle positions, is provided with arc corner; Described fuselage panel comprises lower panel or lower panel and top panel; On fuselage connector, form two side direction slots of setting angle; In the relative slot of two fuselage connectors of the same side, be all fixed with described lower panel and top panel is installed removably or two slots relative at the same side fuselage connector in be fixed with described lower panel and be arranged on the fuselage connector of this side; Be fixed with in the bottom near lower panel the base plate that side is connected with lower panel, above base plate, be also fixed with installing plate that side is connected with lower panel, fitting machine process equipment main body, between base plate and installing plate, form accommodation space; Installing plate top forms the fluid collection chamber of liquid sealing; On installing plate, be provided with liquid-leaking nozzle; In accommodation space, be provided with hydrops pond; Liquid-leaking nozzle is just to hydrops pond.
2. a kind of machining apparatus casing as claimed in claim 1, is characterized in that: in the relative slot of two fuselage connectors of every side, be all fixed with described lower panel and top panel is installed removably; Also comprise cover, cover comprises the cover connector that is arranged on four angle positions, coordinates with corresponding fuselage connector; Cover connector comprises the cover connector body of arc corner, sets the cover slot of angle for two; In two relative cover slots of cover connector, be all fixed with cover panel; Cover also comprises the top board of the end face that is fixed on cover connector and cover panel; Cover links together opening or closing with a corresponding top panel.
3. a kind of machining apparatus casing as claimed in claim 2, is characterized in that: on fuselage connector, be also provided with fuselage locating hole; On cover connector, be also provided with the cover locating hole coordinating with fuselage locating hole; In relative fuselage locating hole or cover locating hole, be fixed with locating dowel.
4. a kind of machining apparatus casing as claimed in claim 2, is characterized in that: the cover connector being installed together and the end face of cover panel are cascaded surface.
5. a kind of machining apparatus casing as claimed in claim 1, it is characterized in that: in relative two slots of fuselage connector described in two more than a side, be fixed with described lower panel and be arranged on described the door more than fan on a fuselage connector of this side or be arranged on respectively described the door more than fan on two fuselage connectors of this side, described door is arranged on the fuselage connector of this side by hinge.
6. a kind of machining apparatus casing as claimed in claim 5, is characterized in that: be more than two fans at the door described in a side, corresponding described fuselage connector also comprises locating slot, and positioning strip is installed in locating slot.
7. a kind of machining apparatus casing as claimed in claim 1, is characterized in that: in the relative slot of two fuselage connectors of each side, be all fixed with described lower panel and top panel is installed removably; The fuselage connector being installed together and the end face of top panel are cascaded surface; Also be provided with the cover that the top planes the highest with cascaded surface coordinates; Cover links together opening or closing with a corresponding top panel.
8. a kind of machining apparatus casing as claimed in claim 1, is characterized in that: described fuselage panel comprises lower panel and top panel; On fuselage connector more than a side, extrusion modling has installing hole, also comprises with installing hole and is installed together the driving mechanism that drives described top panel automatically to move up and down.
9. a kind of machining apparatus casing as described in claim 1 to 8 any one, is characterized in that: in two relative slots of each side fuselage connector, be all fixed with described lower panel and top panel is installed removably; Be provided with to block near the position of corresponding fuselage connector at described top panel and be provided with the lower baffle plate blocking with the seam of corresponding lower panel with the slanting baffle of the seam of this fuselage connector, near bottom position.
As described in claim 1 to 8 any one a kind of machining apparatus casing, it is characterized in that: be equipped with both sides and adjacent lower panel engages, bottom surface engages with installing plate sealing plate four corners; Lower panel, installing plate, sealing plate form the described fluid collection chamber that is positioned at installing plate top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210359706.8A CN102941474B (en) | 2012-09-25 | 2012-09-25 | Casing of machining device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210359706.8A CN102941474B (en) | 2012-09-25 | 2012-09-25 | Casing of machining device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102941474A CN102941474A (en) | 2013-02-27 |
| CN102941474B true CN102941474B (en) | 2014-11-12 |
Family
ID=47724514
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210359706.8A Expired - Fee Related CN102941474B (en) | 2012-09-25 | 2012-09-25 | Casing of machining device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102941474B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2538056Y (en) * | 2002-03-26 | 2003-02-26 | 时贞训 | Dry transformer protective casing |
| CN2904806Y (en) * | 2006-06-09 | 2007-05-30 | 马银亮 | Combined arc-shape drawer face plate |
| CN201926092U (en) * | 2010-12-22 | 2011-08-10 | 上海诺地乐通用设备制造有限公司 | Corner connecting structure with heat-insulating sleeve for heat-insulating panel of air handling unit |
| CN202143315U (en) * | 2011-07-07 | 2012-02-08 | 深圳日海通讯技术股份有限公司 | Cabinet |
| CN202804659U (en) * | 2012-09-25 | 2013-03-20 | 杨东佐 | Machine shell of machining equipment |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8500428B2 (en) * | 2010-11-17 | 2013-08-06 | I-Chiang Yang | Scraping unit of a machine for making cotton candy |
-
2012
- 2012-09-25 CN CN201210359706.8A patent/CN102941474B/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2538056Y (en) * | 2002-03-26 | 2003-02-26 | 时贞训 | Dry transformer protective casing |
| CN2904806Y (en) * | 2006-06-09 | 2007-05-30 | 马银亮 | Combined arc-shape drawer face plate |
| CN201926092U (en) * | 2010-12-22 | 2011-08-10 | 上海诺地乐通用设备制造有限公司 | Corner connecting structure with heat-insulating sleeve for heat-insulating panel of air handling unit |
| CN202143315U (en) * | 2011-07-07 | 2012-02-08 | 深圳日海通讯技术股份有限公司 | Cabinet |
| CN202804659U (en) * | 2012-09-25 | 2013-03-20 | 杨东佐 | Machine shell of machining equipment |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102941474A (en) | 2013-02-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202804659U (en) | Machine shell of machining equipment | |
| CN203982720U (en) | Led display device | |
| CN206245526U (en) | Toilet's modular wall panel | |
| CN215588591U (en) | Totally enclosed CNC frame dustcoat | |
| CN102941474B (en) | Casing of machining device | |
| CN204087313U (en) | Combined type wing lock | |
| CN212613207U (en) | Box-shaped yin-yang staggered special-shaped glass curtain wall | |
| CN112627400A (en) | Frame assembling structure of inclined ventilation type triangular glass curtain wall | |
| CN111042425A (en) | Integrated decorative suspended ceiling | |
| CN104499605A (en) | Steel partition and partition door thereof | |
| CN211817326U (en) | Integrated decorative suspended ceiling | |
| CN206289821U (en) | A kind of frame-supported glass curtain wall | |
| CN201943226U (en) | Insertion and hang type pottery tube curtain wall | |
| CN203858397U (en) | Assembled-type optical-cable cross-connecting box | |
| CN211288232U (en) | Bird wing type blade | |
| CN202470351U (en) | Wind cabinet casing | |
| CN203829826U (en) | Indoor air purifier | |
| CN110565855A (en) | Point-supported torsional double-curved-surface colored drawing metal plate curtain wall | |
| CN203364534U (en) | Locating structure of refrigerator air pipe | |
| CN203188412U (en) | Baffle opening-closing structure of metal plate curtain wall | |
| CN218632971U (en) | Assembled block terminal | |
| CN216672224U (en) | Power distribution cabinet convenient to disassemble and assemble | |
| CN211128562U (en) | Stainless steel box with isolating mechanism | |
| CN203475735U (en) | Seal shell of sunshade decoration plate | |
| CN215863992U (en) | Convenient central air conditioning pipeline vent of dismantling |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20171013 Address after: 523860 Guangdong city of Dongguan province Changan Zhen Wu Sha Li Wu Cun Xing FA Lu Patentee after: Dongguan State Machinery Co.,Ltd. Address before: Li Wu Xingfa Economic Development Zone sixth Changan Nan Lu Zhen Wu Sha Cun 523860 Guangdong city of Dongguan province No. 41 West Stone Arts crafts emporium Patentee before: Yang Dongzuo |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20181012 Address after: 510000 Fenghuang three road, Kowloon Town, Luogang District, Guangzhou, Guangdong, 16 Patentee after: GUANGZHOU CCM ELECTRICAL APPLIANCE Co.,Ltd. Address before: 523860 Xingfa Road, Wu Sha Lee Village, Changan Town, Dongguan, Guangdong Patentee before: Dongguan State Machinery Co.,Ltd. |
|
| 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: 20141112 |