CN112296855A - Smoothness processing device for manufacturing aerospace shell - Google Patents
Smoothness processing device for manufacturing aerospace shell Download PDFInfo
- Publication number
- CN112296855A CN112296855A CN202011165304.5A CN202011165304A CN112296855A CN 112296855 A CN112296855 A CN 112296855A CN 202011165304 A CN202011165304 A CN 202011165304A CN 112296855 A CN112296855 A CN 112296855A
- Authority
- CN
- China
- Prior art keywords
- frame
- polishing
- adjusting
- rotating
- motor
- 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.)
- Withdrawn
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B29/00—Machines or devices for polishing surfaces on work by means of tools made of soft or flexible material with or without the application of solid or liquid polishing agents
- B24B29/02—Machines or devices for polishing surfaces on work by means of tools made of soft or flexible material with or without the application of solid or liquid polishing agents designed for particular workpieces
- B24B29/04—Machines or devices for polishing surfaces on work by means of tools made of soft or flexible material with or without the application of solid or liquid polishing agents designed for particular workpieces for rotationally symmetrical workpieces, e.g. ball-, cylinder- or cone-shaped workpieces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B41/00—Component parts such as frames, beds, carriages, headstocks
- B24B41/02—Frames; Beds; Carriages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B41/00—Component parts such as frames, beds, carriages, headstocks
- B24B41/04—Headstocks; Working-spindles; Features relating thereto
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B47/00—Drives or gearings; Equipment therefor
- B24B47/22—Equipment for exact control of the position of the grinding tool or work at the start of the grinding operation
Abstract
The invention discloses a smoothness processing device for manufacturing an aerospace shell, which comprises a rotating mechanism, a moving mechanism, a jacking cylinder, a rack and a jacking seat, wherein the rotating mechanism is used for driving the aerospace shell with a conical curved surface to rotate during smoothness processing, the rotating mechanism is arranged on one side of the rack, the jacking cylinder is arranged on the other side of the rack, the jacking seat is arranged at the telescopic part of the jacking cylinder, the moving mechanism is arranged on the front side and the rear side of the rack, and the smoothness processing device further comprises an adjusting mechanism and a polishing mechanism. The polishing frame is used for driving the five polishing seats and the polishing wheel to rotate, and meanwhile, the polishing seats are used for moving relatively on the polishing frame, so that the polishing wheel can be attached to the curved surface shell, the rotating frame is used for driving the polishing mechanism to rotate around the aerospace shell, and the aerospace shell with the conical curved surface can be polished.
Description
Technical Field
The invention relates to the field of aerospace shell manufacturing, in particular to a smoothness processing device for aerospace shell manufacturing.
Background
Aviation and aerospace are the most active and influential scientific and technical fields in the understanding and modification of natural processes of human beings in the 20 th century, and are also important marks for the high development of human civilization. Aviation refers to the navigation activity of an aircraft in the earth's atmosphere, and aerospace refers to the navigation activity of an aircraft in the space outside the atmosphere. In a very long year of the year, people conquer nature and have a desire to soar the sky and roam the universe; smooth degree during aerospace casing has decided whole spacecraft and has flown the intensity of in-process and air friction, traditional smoothness processing apparatus generally utilizes the burnishing machine to come to carry out burnishing and polishing to aerospace casing and handle, but general aerospace casing is the toper structure of curved surface, consequently traditional polishing processing apparatus is when carrying out polishing processing, the laminating that the buffing wheel can not be complete is in the aerospace casing outside, and then can influence polishing effect, most polishing processing process at present simultaneously, generally all adopt the manual work to carry out polishing processing, this will make whole polishing efficiency reduce.
Disclosure of Invention
The object of the present invention is to solve the above problems by providing a smoothness management device for aerospace shell manufacturing.
The invention realizes the purpose through the following technical scheme:
a smoothness processing device for manufacturing aerospace shells comprises a rotating mechanism, a moving mechanism, a jacking cylinder, a frame and a jacking seat, wherein the rotating mechanism is used for driving the aerospace shell with a conical curved surface to rotate during smoothness processing, the rotating mechanism is arranged on one side of the frame, the jacking cylinder is arranged on the other side of the frame, the jacking seat is arranged at the telescopic part of the jacking cylinder, the moving mechanisms are arranged at the front side and the rear side of the frame, the jacking seat further comprises an adjusting mechanism and a polishing mechanism, the adjusting mechanism comprises an adjusting cylinder, a rotating frame, an adjusting motor, an adjusting gear and a gear ring, the rotating frame is connected with the moving mechanism, the gear ring is arranged in the middle position of the outer side of the rotating frame, the adjusting cylinder fixing parts are arranged on two sides of the rotating frame, the adjusting motor is connected with the moving mechanism, and the adjusting gear is arranged on a rotating part of the adjusting motor; polishing mechanism includes polishing motor, alignment jig, polishing frame, polishing seat, throwing aureola, the alignment jig is installed adjust the cylinder pars contractilis, the polishing motor is installed just be located two on the alignment jig between the adjust the cylinder, the polishing frame is installed just be located on the alignment jig the swivel mount is inboard, it is located to throw the aureola adjust the cylinder inboard, polishing seat one end is located the polishing frame is inboard, the polishing seat other end is installed throw the aureola and be close to adjust one side of cylinder.
Preferably: slewing mechanism is including rotating the motor, rotating seat, band pulley, belt, it passes through bolted connection to rotate the motor the one end in the frame outside, it connects through the bearing to rotate the seat the inboard one end of frame, the band pulley passes through the key-type connection and is in rotate motor rotation portion with rotate seat one side, the belt sets up the band pulley outside.
According to the arrangement, the rotating motor rotating part is utilized to drive the belt wheel to rotate, and the rotating seat is driven to rotate through the transmission of the belt wheel and the belt.
Preferably: slewing mechanism is including rotating the motor, rotating seat, driving gear, driven gear, it passes through bolted connection to rotate the motor the one end in the frame outside, it connects through the bearing to rotate the seat the inboard one end of frame, the driving gear passes through the key-type connection and is in rotate motor rotation portion, driven gear passes through the key-type connection and is in rotate seat one side.
According to the arrangement, the rotating motor rotating part is utilized to drive the driving gear to rotate, and the rotating seat is driven to rotate through the transmission of the driving gear and the driven gear.
Preferably: the moving mechanism comprises a moving motor, a lead screw, a sliding rail, a sliding block and a supporting frame, wherein the moving motor is connected with the front side and the rear side of one end of the rack through bolts, the two ends of the lead screw are connected with the front side and the rear side of the rack through bearings, the sliding rail is connected with the inner side of the rack through bolts, the sliding rail is located below the lead screw, the supporting frame is located in the middle of the rack, and the sliding block is connected with the lower end of the supporting frame through bolts.
According to the arrangement, the moving motor rotating part is used for driving the screw rod to rotate, the support frame is driven to move on two sides through the rotation of the screw rod, and meanwhile the slide rail and the slide block are used for supporting the support frame.
Preferably: the top pressing cylinder fixing part is connected to the other side of the rack through a bolt, and the top pressing seat is connected to the top pressing cylinder telescopic part through a bearing.
According to the arrangement, the jacking cylinder telescopic part is used for pushing the jacking seat to move to one side, and the conical curved aerospace shell is supported by the jacking seat.
Preferably: the ring gear with the swivel mount passes through welded connection, the adjusting cylinder fixed part with the swivel mount passes through bolted connection, adjusting gear with the adjusting motor rotation portion passes through the key-type connection.
According to the arrangement, the adjusting gear is driven to rotate by the rotating part of the adjusting motor, and the rotating frame is driven to rotate through the transmission of the adjusting gear and the gear ring.
Preferably: the adjusting frame is connected with the telescopic part of the adjusting cylinder through threads, the polishing motor is connected with the adjusting frame through bolts, and the polishing frame is connected with the adjusting frame through bearings.
According to the arrangement, the polishing frame is driven to rotate by the rotating part of the polishing motor, the polishing wheel is driven to rotate at a high speed by the rotation of the sliding rail, and accordingly the aerospace shell is polished.
Preferably: the middle of the upper end of the support frame is provided with a circular limiting groove, the gear ring is positioned in the limiting groove on the upper side of the support frame, and the front side and the rear side of the lower end of the support frame are provided with threaded holes.
According to the arrangement, the adjusting mechanism rotates in the inner side of the adjusting mechanism by utilizing the round limiting groove of the supporting frame.
Preferably: the inner parts of two sides of the rotating frame are respectively welded with three concave fixing frames, a rectangular opening is formed in the middle of each fixing frame of the rotating frame, and two round holes are formed in two rectangular sides of each fixing frame of the rotating frame.
According to the arrangement, the adjusting cylinder is supported and fixed by the fixing frame in the rotating frame.
Preferably: and one end of the polishing frame, which is close to the center of the rotating frame, is provided with a limiting groove, and the polishing seat is positioned in the limiting groove of the polishing frame.
According to the arrangement, the polishing seat is used for reciprocating in the limiting groove of the polishing frame.
Compared with the prior art, the invention has the following beneficial effects:
1. the polishing frame is utilized to drive the five polishing seats and the polishing wheel to rotate, and meanwhile, the polishing seats move relative to each other on the polishing frame, so that the polishing wheel can be more attached to the curved surface shell;
2. the rotating frame is used for driving the polishing mechanism to rotate around the aerospace shell, so that the aerospace shell with the conical curved surface can be polished.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
FIG. 1 is a schematic structural view of an embodiment 1 of a smoothness processing apparatus for aerospace housing manufacture in accordance with the present invention;
FIG. 2 is a schematic structural view of example 2 of a smoothness processing apparatus for aerospace housing manufacture in accordance with the present invention;
FIG. 3 is a partial detail view of embodiment 1 of a rotating mechanism of a smoothness processing apparatus for aerospace housing manufacture in accordance with the present invention;
FIG. 4 is a partial detail view of embodiment 2 of a rotating mechanism of a smoothness management apparatus for aerospace housing manufacture in accordance with the present invention;
FIG. 5 is a partial component view of a polishing mechanism for a smoothness processing apparatus for aerospace housing manufacture in accordance with the present invention;
FIG. 6 is a partial part view of an adjustment mechanism for a smoothness management apparatus for aerospace housing manufacture in accordance with the present invention;
FIG. 7 is a partial cross-sectional view of an adjustment mechanism for a smoothness management apparatus for aerospace housing manufacture in accordance with the present invention;
FIG. 8 is a partial part view of a conditioning motor for a smoothness management apparatus for aerospace housing manufacture in accordance with the present invention.
The reference numerals are explained below:
1. a rotating mechanism; 2. a moving mechanism; 3. an adjustment mechanism; 4. a polishing mechanism; 5. the jacking cylinder; 6. a frame; 7. a jacking seat; 11. rotating the motor; 12. a rotating seat; 13. a pulley; 14. a belt; 113. a driving gear; 114. a driven gear; 21. a moving motor; 22. a lead screw; 23. a slide rail; 24. a slider; 25. a support frame; 31. an adjusting cylinder; 32. a rotating frame; 33. adjusting the motor; 34. an adjusting gear; 35. a ring gear; 41. polishing the motor; 42. an adjusting bracket; 43. a polishing stand; 44. polishing the base; 45. and (7) a polishing wheel.
Detailed Description
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used only for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
The invention will be further described with reference to the accompanying drawings in which:
a smoothness processing device for aerospace shell manufacturing comprises a rotating mechanism 1, a moving mechanism 2, a jacking cylinder 5, a rack 6 and a jacking seat 7, wherein the rotating mechanism 1 is used for driving an aerospace shell with a conical curved surface to rotate during smoothness processing, the jacking cylinder 5 is arranged on one side of the rack 6, the jacking cylinder 5 is arranged on the other side of the rack 6, the jacking seat 7 is arranged on a telescopic part of the jacking cylinder 5, the moving mechanism 2 is arranged on the front side and the rear side of the rack 6, the smoothness processing device also comprises an adjusting mechanism 3 and a polishing mechanism 4, the adjusting mechanism 3 comprises an adjusting cylinder 31, a rotating frame 32, an adjusting motor 33, an adjusting gear 34 and a gear ring 35, the rotating frame 32 is arranged on the inner side of the upper end of a supporting frame 25, the gear ring 35 is arranged at the middle position of the outer side of the rotating frame 32, fixing parts of the adjusting cylinder 31 are arranged on two, the adjusting gear 34 is arranged on the rotating part of the adjusting motor 33; the polishing mechanism 4 comprises a polishing motor 41, an adjusting frame 42, a polishing frame 43, a polishing seat 44 and a polishing wheel 45, wherein the adjusting frame 42 is installed at the telescopic part of the adjusting cylinder 31, the polishing motor 41 is installed on the adjusting frame 42 and is located between the two adjusting cylinders 31, the polishing frame 43 is installed on the adjusting frame 42 and is located on the inner side of the rotating frame 32, the polishing wheel 45 is located on the inner side of the adjusting cylinder 31, one end of the polishing seat 44 is located on the inner side of the polishing frame 43, and the other end of the polishing seat 44 is installed on one side, close to the adjusting cylinder 31, of the.
Example 1
As shown in fig. 1, 3, 5, 6, 7 and 8, the rotating mechanism 1 includes a rotating motor 11, a rotating base 12, a belt wheel 13 and a belt 14, the rotating motor 11 is connected to one end of the outer side of the frame 6 through a bolt, the rotating base 12 is connected to one end of the inner side of the frame 6 through a bearing, the belt wheel 13 is connected to one side of the rotating portion of the rotating motor 11 and the rotating base 12 through a key, the belt 14 is arranged on the outer side of the belt wheel 13, the rotating portion of the rotating motor 11 is used for driving the belt wheel 13 to rotate, and the rotating base 12 is driven to rotate through the transmission of the belt wheel 13 and the belt 14; the moving mechanism 2 comprises a moving motor 21, a lead screw 22, a slide rail 23, a slide block 24 and a support frame 25, wherein the moving motor 21 is connected to the front side and the rear side of one end of the rack 6 through bolts, the two ends of the lead screw 22 are connected to the front side and the rear side of the rack 6 through bearings, the slide rail 23 is connected to the inner side of the rack 6 through bolts, the slide rail 23 is positioned below the lead screw 22, the support frame 25 is positioned in the middle of the rack 6, the slide block 24 is connected to the lower end of the support frame 25 through bolts, the rotating part of the moving motor 21 is used for driving the lead screw 22 to rotate, the support frame 25 is driven to move on; the fixed part of the jacking cylinder 5 is connected to the other side of the frame 6 through a bolt, the jacking seat 7 is connected to the telescopic part of the jacking cylinder 5 through a bearing, the telescopic part of the jacking cylinder 5 is used for pushing the jacking seat 7 to move to one side, and the conical curved aerospace shell is supported through the jacking seat 7; the gear ring 35 is connected with the rotating frame 32 through welding, the fixed part of the adjusting cylinder 31 is connected with the rotating frame 32 through bolts, the adjusting gear 34 is connected with the rotating part of the adjusting motor 33 through keys, the rotating part of the adjusting motor 33 is used for driving the adjusting gear 34 to rotate, and the rotating frame 32 is driven to rotate through the transmission of the adjusting gear 34 and the gear ring 35; the adjusting frame 42 is connected with the telescopic part of the adjusting cylinder 31 through threads, the polishing motor 41 is connected with the adjusting frame 42 through bolts, the polishing frame 43 is connected with the adjusting frame 42 through bearings, the rotating part of the polishing motor 41 is used for driving the polishing frame 43 to rotate, and the polishing wheel 45 is driven to rotate at a high speed through the rotation of the sliding rail 23, so that the aerospace shell is polished; a circular limiting groove is formed in the middle of the upper end of the support frame 25, the gear ring 35 is located in the limiting groove on the upper side of the support frame 25, threaded holes are formed in the front side and the rear side of the lower end of the support frame 25, and the adjusting mechanism 3 is enabled to rotate on the inner side of the circular limiting groove of the support frame 25; three concave fixing frames are welded inside the two sides of the rotating frame 32 respectively, a rectangular opening is formed in the middle of each fixing frame of the rotating frame 32, round holes are formed in the two rectangular sides of each fixing frame of the rotating frame 32 respectively, and the air adjusting cylinder 31 is supported and fixed by the fixing frames in the rotating frame 32; a limit groove is arranged at one end of the polishing frame 43 close to the center of the rotating frame 32, and the polishing seat 44 is positioned in the limit groove of the polishing frame 43.
The working principle is as follows: when the support frame is used, the rotating part 22 is driven to rotate by the moving motor 21, the support frame 25 moves to one side under the support of the sliding rail 23 and the sliding block 24 and the rotation of the screw rod 22, and then when the support frame 25 moves to one end of the inner side of the rack 6, the aerospace shell needing to be subjected to smooth processing is placed between the rotating seat 12 and the jacking seat 7, at the moment, the telescoping part of the jacking cylinder 5 is utilized to push the jacking seat 7 to move to one side, and then the aerospace shell is jacked on the rotating seat 12 through the jacking seat 7, so that the aerospace shell is supported and fixed; then, the rotating part of the motor 11 is rotated to drive the belt wheel 13 to rotate, the rotating seat 12 is driven to rotate through the rotation of the belt wheel 13 and the belt 14, and the fixed aerospace shell is driven to rotate through the rotation of the rotating seat 12; meanwhile, the rotating part of the adjusting motor 33 is used for driving the adjusting gear 34 to rotate, the adjusting gear 34 is meshed with the gear ring 35 on the outer side of the rotating frame 32, so that the rotating frame 32 is driven to rotate, the polishing mechanism 4 is driven to rotate on the outer side of the aerospace shell, meanwhile, the adjusting mechanism 3 is driven to rotate, the adjusting frame 42 is pushed by the telescopic part of the adjusting cylinder 31 to extend, so that the polishing wheel 45 is attached to the outer side of the aerospace shell, when the polishing wheel 45 is attached to the curved surface on the outer side of the aerospace shell, the springs of the polishing seats 44 positioned on the inner side of the polishing frame 43 are compressed oppositely, so that different extending lengths of the five polishing seats 44 are adjusted, the polishing wheel 45 is further attached to the curved surface on the outer side of the aerospace shell, when the polishing wheel 45 is completely attached to the curved surface on the aerospace shell, the polishing frame 43 is driven to rotate by the rotating part of the polishing, the polishing wheel 45 is driven to rotate by the high-speed rotation of the polishing frame 43, so that the curved surface of the aerospace shell is polished; when polishing, the rotating part of the moving motor 21 is used for driving the screw rod 22 to rotate reversely, so that the support frame 25 moves slowly to the other side, and the aerospace shell is polished.
Example 2
As shown in fig. 2 and 4, the difference between the embodiment 2 and the embodiment 1 is that the rotating mechanism 1 includes a rotating motor 11, a rotating base 12, a driving gear 113 and a driven gear 114, the rotating motor 11 is connected to one end of the outer side of the frame 6 through a bolt, the rotating base 12 is connected to one end of the inner side of the frame 6 through a bearing, the driving gear 113 is connected to a rotating portion of the rotating motor 11 through a key, the driven gear 114 is connected to one side of the rotating base 12 through a key, the rotating portion of the rotating motor 11 is used for driving the driving gear 113 to rotate, and the rotating base 12 is driven to rotate through the transmission of the driving gear 113 and the driven.
The foregoing illustrates and describes the principles, general features, and advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed.
Claims (10)
1. The utility model provides a smoothness processing apparatus for aerospace casing makes, is including being used for driving aerospace casing pivoted slewing mechanism (1), moving mechanism (2), roof pressure cylinder (5), frame (6), roof pressure seat (7) of circular cone type curved surface when the smoothness is handled, slewing mechanism (1) sets up frame (6) one side, roof pressure cylinder (5) set up frame (6) opposite side, roof pressure seat (7) are installed roof pressure cylinder (5) pars contractilis, moving mechanism (2) set up frame (6) front and back both sides, its characterized in that: the polishing machine is characterized by further comprising an adjusting mechanism (3) and a polishing mechanism (4), wherein the adjusting mechanism (3) comprises an adjusting cylinder (31), a rotating frame (32), an adjusting motor (33), an adjusting gear (34) and a gear ring (35), the rotating frame (32) is connected with the moving mechanism (2), the gear ring (35) is installed at the middle position of the outer side of the rotating frame (32), fixing parts of the adjusting cylinder (31) are installed on two sides of the rotating frame (32), the adjusting motor (33) is connected with the moving mechanism (2), and the adjusting gear (34) is installed at the rotating part of the adjusting motor (33); polishing mechanism (4) are including polishing motor (41), alignment jig (42), polishing frame (43), polishing seat (44), throwing aureola (45), alignment jig (42) are installed adjust cylinder (31) pars contractilis, polishing motor (41) are installed on alignment jig (42) and be located two between adjust cylinder (31), polishing frame (43) are installed on alignment jig (42) and be located swivel mount (32) are inboard, throwing aureola (45) are located adjust cylinder (31) are inboard, polishing seat (44) one end is located polishing frame (43) are inboard, install polishing seat (44) other end throw aureola (45) are close to one side of adjusting cylinder (31).
2. A smoothness processing apparatus for aerospace housing manufacturing according to claim 1 wherein: slewing mechanism (1) is including rotating motor (11), rotating seat (12), band pulley (13), belt (14), it is in to rotate motor (11) through bolted connection the one end in frame (6) outside, it connects through the bearing to rotate seat (12) the inboard one end of frame (6), band pulley (13) is in through the key-type connection rotate motor (11) rotation portion with rotate seat (12) one side, belt (14) set up the band pulley (13) outside.
3. A smoothness processing apparatus for aerospace housing manufacturing according to claim 1 wherein: slewing mechanism (1) is including rotating motor (11), rotating seat (12), driving gear (113), driven gear (114), it is in to rotate motor (11) through bolted connection the one end in frame (6) outside, it connects through the bearing to rotate seat (12) the inboard one end of frame (6), driving gear (113) are in through the key-type connection rotate motor (11) rotation portion, driven gear (114) are in through the key-type connection rotate seat (12) one side.
4. A smoothness processing apparatus for aerospace housing manufacturing according to claim 1 wherein: moving mechanism (2) are including moving motor (21), lead screw (22), slide rail (23), slider (24), support frame (25), moving motor (21) pass through bolted connection both sides around frame (6) one end, lead screw (22) both ends are passed through the bearing and are connected both sides around frame (6), slide rail (23) pass through bolted connection frame (6) are inboard, slide rail (23) are located lead screw (22) below, support frame (25) are located frame (6) intermediate position, slider (24) pass through bolted connection support frame (25) lower extreme.
5. A smoothness processing apparatus for aerospace housing manufacturing according to claim 1 wherein: the fixed part of the jacking cylinder (5) is connected to the other side of the rack (6) through a bolt, and the jacking seat (7) is connected to the telescopic part of the jacking cylinder (5) through a bearing.
6. A smoothness processing apparatus for aerospace housing manufacturing according to claim 1 wherein: ring gear (35) with swivel mount (32) are through welded connection, adjusting cylinder (31) fixed part with swivel mount (32) pass through bolted connection, adjusting gear (34) with adjusting motor (33) rotation portion passes through the key-type connection.
7. A smoothness processing apparatus for aerospace housing manufacturing according to claim 1 wherein: the adjusting frame (42) is connected with the telescopic part of the adjusting cylinder (31) through threads, the polishing motor (41) is connected with the adjusting frame (42) through bolts, and the polishing frame (43) is connected with the adjusting frame (42) through a bearing.
8. A smoothness processing apparatus for aerospace housing manufacturing according to claim 4, wherein: a circular limiting groove is formed in the middle of the upper end of the support frame (25), the gear ring (35) is located in the limiting groove in the upper side of the support frame (25), and threaded holes are formed in the front side and the rear side of the lower end of the support frame (25).
9. A smoothness processing apparatus for aerospace housing manufacturing according to claim 1 wherein: three concave fixing frames are welded inside the two sides of the rotating frame (32), a rectangular opening is formed in the middle of the fixing frame of the rotating frame (32), and round holes are formed in the two rectangular sides of the fixing frame of the rotating frame (32).
10. A smoothness processing apparatus for aerospace housing manufacturing according to claim 1 wherein: one end of the polishing frame (43), which is close to the center of the rotating frame (32), is provided with a limiting groove, and the polishing seat (44) is positioned in the limiting groove of the polishing frame (43).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011165304.5A CN112296855A (en) | 2020-10-27 | 2020-10-27 | Smoothness processing device for manufacturing aerospace shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011165304.5A CN112296855A (en) | 2020-10-27 | 2020-10-27 | Smoothness processing device for manufacturing aerospace shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112296855A true CN112296855A (en) | 2021-02-02 |
Family
ID=74331107
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011165304.5A Withdrawn CN112296855A (en) | 2020-10-27 | 2020-10-27 | Smoothness processing device for manufacturing aerospace shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112296855A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113510595A (en) * | 2021-05-11 | 2021-10-19 | 彭新 | Automatic machining machine and machining process for stainless steel connecting flange |
| CN114800228A (en) * | 2022-06-24 | 2022-07-29 | 南通市博南润滑液压设备有限公司 | Surface reciprocating type polishing device for hydraulic fitting production |
| CN115673987A (en) * | 2022-12-30 | 2023-02-03 | 江苏宏发气阀有限公司 | Burnishing device of rod iron processing usefulness |
-
2020
- 2020-10-27 CN CN202011165304.5A patent/CN112296855A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113510595A (en) * | 2021-05-11 | 2021-10-19 | 彭新 | Automatic machining machine and machining process for stainless steel connecting flange |
| CN114800228A (en) * | 2022-06-24 | 2022-07-29 | 南通市博南润滑液压设备有限公司 | Surface reciprocating type polishing device for hydraulic fitting production |
| CN115673987A (en) * | 2022-12-30 | 2023-02-03 | 江苏宏发气阀有限公司 | Burnishing device of rod iron processing usefulness |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN112296855A (en) | Smoothness processing device for manufacturing aerospace shell | |
| CN212683370U (en) | Pneumatic piston type round tube inner wall polishing tool | |
| CN106064342A (en) | One carries high efficiency multistation letter out machine | |
| CN109292411B (en) | Turnover mechanism based on hub processing equipment | |
| CN113370009B (en) | Grinding device for hub machining | |
| CN111451933B (en) | Bearing machining numerical control machine tool | |
| CN103121188B (en) | Wheel hub polishing machine | |
| CN208992246U (en) | A kind of positioning mechanism that the bearing inner race of different model can be positioned | |
| CN111774955B (en) | A grinding device for automobile parts | |
| CN219504342U (en) | Large-scale spring end face grinding device | |
| CN216327042U (en) | Grinding device is used in processing of deep groove ball bearing outer loop | |
| CN108555619B (en) | A kind of wheel rim double-station positioner device | |
| CN112975683A (en) | Polishing equipment for display screen glass | |
| CN214559582U (en) | Brake disc grinding device of automobile brake | |
| CN216483944U (en) | Thrust ball bearing frame check out test set | |
| CN112894655B (en) | Positioning tool for assembling and machining hub bearing and using method thereof | |
| CN210550398U (en) | Spare tire cover plate polishing tool | |
| CN108907729B (en) | Steel plate machining device | |
| US5327687A (en) | Apparatus for continuously grinding a curved plate | |
| CN214519829U (en) | Supporting assembly with adjusting function for plate heat exchanger | |
| CN110854049A (en) | Rotary crystal expanding device | |
| CN207564956U (en) | A kind of internal supporting body for tyre wind | |
| CN213438326U (en) | Ejector rod device for circumferential positioning of differential shell | |
| CN213532043U (en) | Burnishing device of holographic advertisement casing production | |
| CN220561173U (en) | Bearing inner race raceway grinding device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20210202 |