CN112238376A - A unhairing limit processing apparatus for manufacturing of aviation aircraft fin - Google Patents
A unhairing limit processing apparatus for manufacturing of aviation aircraft fin Download PDFInfo
- Publication number
- CN112238376A CN112238376A CN202011091225.4A CN202011091225A CN112238376A CN 112238376 A CN112238376 A CN 112238376A CN 202011091225 A CN202011091225 A CN 202011091225A CN 112238376 A CN112238376 A CN 112238376A
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- CN
- China
- Prior art keywords
- motor
- manufacture
- deflash
- mounting bracket
- support
- Prior art date
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Classifications
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- 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
- B24B9/00—Machines or devices designed for grinding edges or bevels on work or for removing burrs; Accessories therefor
- B24B9/02—Machines or devices designed for grinding edges or bevels on work or for removing burrs; Accessories therefor characterised by a special design with respect to properties of materials specific to articles to be ground
- B24B9/04—Machines or devices designed for grinding edges or bevels on work or for removing burrs; Accessories therefor characterised by a special design with respect to properties of materials specific to articles to be ground of metal, e.g. skate blades
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- 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
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- 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
- B24B41/06—Work supports, e.g. adjustable steadies
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- 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
- B24B47/10—Drives or gearings; Equipment therefor for rotating or reciprocating working-spindles carrying grinding wheels or workpieces
- B24B47/12—Drives or gearings; Equipment therefor for rotating or reciprocating working-spindles carrying grinding wheels or workpieces by mechanical gearing or electric power
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- 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
- B24B47/20—Drives or gearings; Equipment therefor relating to feed movement
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- 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
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Grinding And Polishing Of Tertiary Curved Surfaces And Surfaces With Complex Shapes (AREA)
Abstract
The invention discloses a deburring device for manufacturing an empennage of an aerocraft, which comprises a clamping mechanism and a deburring mechanism, wherein the deburring mechanism is used for processing burrs generated in the manufacturing of the empennage of the aerocraft; clamping mechanism includes support, cushion, and the cushion is installed to the upper end of support, and the slide rail is installed just in the upper end of support in the both sides of cushion, and the slide rail respectively is provided with 3 in the both sides of cushion, all installs clamping component at the other end of every slide rail. The tail wing trimming device clamps and fixes the tail wing through the clamping mechanism, and then the polishing assembly moves from one end of the tail wing to the other end of the tail wing, so that the trimming processing of the tail wing is completed.
Description
Technical Field
The invention relates to the technical field of processing of an aviation aircraft empennage, in particular to a deburring device for manufacturing the aviation aircraft empennage.
Background
An aircraft, in short, is an apparatus that flies in the earth's atmosphere, which is very thick and which can be divided into several layers, two at the bottom: troposphere, stratosphere, air is relatively dense, and in particular troposphere, air is highly mobile, and almost all aviation aircraft fly in these two layers at an altitude of approximately 80 km.
The empennage is an important control operation surface of the aircraft, can participate in the control of various motions of the aircraft, ensures the stability and maneuverability of the aircraft, and has the application of the empennage in most aircraft.
The Chinese patent with the application number of CN201910457278.4 discloses an aviation aircraft empennage processing technology, which comprises the following steps: heating the bar stock to 440-460 ℃, preserving heat for 90-110 min, putting the bar stock into a simple moulding bed, and hammering the bar stock by using an air hammer to enable the bar stock to reach the shape of a blank; step two, blanking: putting the blank in the step one into a band sawing machine, and longitudinally cutting the blank into a blank plate with the thickness of 16-18 cm; step three, forging: heating the blank plate to 440-460 ℃, preserving heat for 25-50 min, putting the blank plate into a preheated die cavity for forging and forming to obtain a primary product, taking out the primary product for water cooling and burr removing treatment, heating the primary product to 440-460 ℃, preserving heat for 10-30 min, putting the primary product into the die cavity for forging and forming again to obtain a semi-finished product, taking out the semi-finished product for water cooling and burr removing treatment; step four, heat treatment: heating the semi-finished product obtained after the third step to 490-500 ℃, preserving heat for 60min, taking out the semi-finished product, cooling with water, putting into a correction die, carrying out static pressure on a hydraulic press for 5-10 s to obtain a finished product, wherein a deburring device is required to be used in the processing process of the empennage, and deburring is carried out on a product formed by forging, but the existing deburring device has poor operation usability, low efficiency, more labor participation, time and labor consumption.
Disclosure of Invention
The invention aims to solve the problems and provide a deburring device for manufacturing an empennage of an aviation aircraft.
The invention realizes the purpose through the following technical scheme:
a deburring device for manufacturing an aviation aircraft empennage comprises a clamping mechanism and a deburring mechanism, wherein the deburring mechanism is used for processing burrs generated in the manufacturing of the aviation aircraft empennage;
the clamping mechanism comprises a bracket and cushion blocks, the upper end of the bracket is provided with the cushion blocks, the two sides of the cushion blocks and the upper end of the bracket are provided with slide rails, the two sides of the cushion blocks are respectively provided with 3 slide rails, the device comprises a sliding rail, a clamping assembly, a first guide rod, a second guide rod, a fixing plate, a first baffle column, a second baffle column, a trimming mechanism and a trimming mechanism, wherein the clamping assembly is arranged at the other end of each sliding rail, the clamping assembly comprises a first telescopic rod and a fixing plate, the fixing plate is arranged at one end of the sliding rail, the first telescopic rod is arranged at the outer side of each fixing plate, a profiling clamping block is arranged on a telescopic shaft of the first telescopic rod, a first guide rod is arranged at the outer side of each profiling clamping block, the first guide rod is connected with the fixing plate in a sliding mode, the first guide rod is connected to the profiling clamping block through screws, the first baffle column is arranged at the upper end of the front portion of the cushion block, the second baffle column;
the deburring mechanism comprises upright posts and a first motor, the upright posts are arranged at four corners of the upper end of the bracket, the first motor is arranged at the front ends of 2 upright posts in front, the first motor is connected with the upright posts through bolts, a slide bar is arranged between the two upright posts at the same side, the slide bar is connected with the upright posts through screws, a screw rod is arranged at the inner side of the slide bar, this screw rod passes through coupling joint in first motor, on this screw rod and sliding connection installs first mounting bracket in the slide bar, 2 second telescopic links are installed to the upper end symmetry of first mounting bracket, the second mounting bracket is installed to the below of first mounting bracket, the telescopic shaft of second telescopic link is connected in the second mounting bracket, the outside of the telescopic shaft of 2 second telescopic links and install the second guide arm in the upper end of second mounting bracket, the second guide arm passes through the screw connection with the second mounting bracket, second guide arm sliding connection is in first mounting bracket, install the subassembly of polishing on the second mounting bracket.
Preferably: the polishing assembly comprises a second motor and a polishing roller, the second motor is installed on one side of the second installation frame, the polishing roller is installed on an output shaft of the second motor, and the polishing roller is connected with the second installation frame through a bearing seat.
Preferably: the polishing assembly comprises a second motor, a polishing roller, the second motor is installed on one side of the front portion of the second mounting frame, the second motor is connected with the second mounting frame through screws, the polishing roller is installed on an output shaft of the second motor and is connected with the second motor through a coupling, the polishing roller is connected to the second mounting frame through a bearing seat, a first chain wheel is installed in the front of the polishing roller in the rotating shaft and on one side of the second mounting frame, a second chain wheel is installed in the rear of the polishing roller in the rotating shaft and on one side of the second mounting frame, and the second chain wheel is connected with the first chain wheel through a transmission chain.
Preferably: the cushion block is connected with the support through a bolt, and the slide rail is connected with the support through a bolt.
Preferably: the clamping assembly is connected with the support through a bolt, and the fixing plate is connected with the support through a bolt.
Preferably: the first telescopic rod is connected with the fixed plate through a bolt, and the profiling clamping block is connected with the sliding rail in a sliding mode.
Preferably: the first bumping post is in threaded connection with the cushion block, and the second bumping post is in threaded connection with the cushion block.
Preferably: the second telescopic rod is connected with the first mounting frame through screws, and the stand column is connected with the support through welding.
Preferably: the second motor passes through the coupling joint with the roller of polishing, and the second motor is provided with 2.
Preferably: the first chain wheel, the second chain wheel and the grinding roller are connected through keys.
Compared with the prior art, the invention has the following beneficial effects:
the empennage is clamped and fixed through the clamping mechanism, then the polishing assembly moves to the other end from one end of the empennage, so that the deburring processing of the empennage is completed, the whole device is simple in structure, convenient to operate and use, time-saving and labor-saving, high in efficiency, and high in popularization and use value.
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 view of a first embodiment of a deflash treatment apparatus for the manufacture of an aircraft tail according to the invention;
FIG. 2 is a second schematic structural view of a first embodiment of a deflash treatment apparatus for use in the manufacture of an aircraft tail according to the present invention;
FIG. 3 is a schematic view of a first configuration of a second embodiment of a deflash treatment apparatus for use in the manufacture of an aircraft tail according to the present invention;
FIG. 4 is a second schematic structural view of a second embodiment of a deflash treatment apparatus for use in the manufacture of an aircraft tail according to the present invention;
FIG. 5 is a schematic view of a first embodiment of a clamping mechanism of a deflash device for use in the manufacture of an aircraft tail according to the invention;
FIG. 6 is a schematic view of a second embodiment of a clamping mechanism of a deflashing device for use in connection with the manufacture of an aircraft empennage according to the invention;
FIG. 7 is a schematic structural diagram of a deflashing mechanism of a deflashing treatment device for manufacturing an empennage of an aircraft according to a first embodiment of the invention;
fig. 8 is a schematic structural diagram of a second embodiment of the deflashing mechanism of the deflashing treatment device for manufacturing the empennage of the aviation aircraft.
The reference numerals are explained below:
1. a clamping mechanism; 11. a support; 12. cushion blocks; 13. a slide rail; 14. a clamping assembly; 141. a first telescopic rod; 142. a fixing plate; 143. profiling clamping blocks; 144. a first guide bar; 15. a first bumping post; 16. a second bumping post; 2. a flash removing mechanism; 21. a column; 22. a first motor; 23. a slide bar; 24. a first mounting bracket; 25. a second mounting bracket; 26. a second guide bar; 27. a second telescopic rod; 28. polishing the assembly; 281. a second motor; 282. grinding a roller; 283. a first sprocket; 284. a drive chain; 285. a second sprocket.
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:
example 1
As shown in fig. 1, 2, 5, 6 and 7, a deflashing treatment device for manufacturing an aircraft tail wing comprises a clamping mechanism 1 and a deflashing mechanism 2 for treating the deflashing generated in the manufacturing of the aircraft tail wing;
the clamping mechanism 1 comprises a support 11 and a cushion block 12, the cushion block 12 is mounted at the upper end of the support 11, slide rails 13 are mounted at two sides of the cushion block 12 and at the upper end of the support 11, the slide rails 13 are respectively provided with 3 parts at two sides of the cushion block 12, a clamping component 14 is mounted at the other end of each slide rail 13, the clamping component 14 comprises a first telescopic rod 141 and a fixed plate 142, the fixed plate 142 is mounted at one end of the slide rail 13, a first telescopic rod 141 is mounted at the outer side of each fixed plate 142, a profiling clamping block 143 is mounted on a telescopic shaft of the first telescopic rod 141, a first guide rod 144 is mounted at the outer side of each profiling clamping block 143, the first guide rod 144 is in sliding connection with the fixed plate 142, the first guide rod 144 is connected to the profiling clamping block 143 through screws, a first retaining column 15 is mounted at the upper end of the front part of the cushion block 12, a second retaining column 16 is mounted at the upper end of the rear part of the cushion block 12, the horizontal, a flash removing mechanism 2 is arranged above the cushion block 12;
the deburring mechanism 2 comprises upright posts 21 and a first motor 22, the upright posts 21 are installed at four corners of the upper end of a support 11, the first motor 22 is installed at the front ends of the 2 upright posts 21 in front, the first motor 22 is connected with the upright posts 21 through bolts, a slide rod 23 is installed between the two upright posts 21 on the same side, the slide rod 23 is connected with the upright posts 21 through screws, a screw rod is installed on the inner side of the slide rod 23 and is connected with the first motor 22 through a coupler, a first mounting frame 24 is installed on the screw rod and is connected with the slide rod 23 in a sliding mode, 2 second telescopic rods 27 are symmetrically installed at the upper end of the first mounting frame 24, a second mounting frame 25 is installed below the first mounting frame 24, a telescopic shaft of each second telescopic rod 27 is connected with the second mounting frame 25, second guide rods 26 are installed on the outer sides of the telescopic shafts of the 2 second telescopic rods 27 and at the upper end of the second mounting frame 25, the second guide bar 26 is slidably connected to the first mounting bracket 24, and the second mounting bracket 25 is provided with a grinding assembly 28.
Preferably: the grinding assembly 28 comprises a second motor 281 and a grinding roller 282, the second motor 281 is arranged at one side of the second mounting frame 25, the grinding roller 282 is arranged on an output shaft of the second motor 281, and the grinding roller 282 is connected with the second mounting frame 25 through a bearing seat; the cushion block 12 is connected with the bracket 11 through a bolt, and the slide rail 13 is connected with the bracket 11 through a bolt; the clamping assembly 14 is connected with the bracket 11 through bolts, and the fixing plate 142 is connected with the bracket 11 through bolts; the first telescopic rod 141 is connected with the fixed plate 142 through a bolt, and the profiling clamping block 143 is connected with the slide rail 13 in a sliding manner; the first catch column 15 is in threaded connection with the cushion block 12, and the second catch column 16 is in threaded connection with the cushion block 12; the second telescopic rod 27 is connected with the first mounting frame 24 through screws, and the upright post 21 is connected with the bracket 11 through welding; the second motor 281 is coupled to the grinding roller 282, and the number of the second motor 281 is 2.
Example 2
As shown in fig. 3, 4, 5, 6 and 8, a deflashing treatment device for manufacturing an aircraft tail wing comprises a clamping mechanism 1 and a deflashing mechanism 2 for treating the deflashing generated in the manufacturing of the aircraft tail wing;
the clamping mechanism 1 comprises a support 11 and a cushion block 12, the cushion block 12 is mounted at the upper end of the support 11, slide rails 13 are mounted at two sides of the cushion block 12 and at the upper end of the support 11, the slide rails 13 are respectively provided with 3 parts at two sides of the cushion block 12, a clamping component 14 is mounted at the other end of each slide rail 13, the clamping component 14 comprises a first telescopic rod 141 and a fixed plate 142, the fixed plate 142 is mounted at one end of the slide rail 13, a first telescopic rod 141 is mounted at the outer side of each fixed plate 142, a profiling clamping block 143 is mounted on a telescopic shaft of the first telescopic rod 141, a first guide rod 144 is mounted at the outer side of each profiling clamping block 143, the first guide rod 144 is in sliding connection with the fixed plate 142, the first guide rod 144 is connected to the profiling clamping block 143 through screws, a first retaining column 15 is mounted at the upper end of the front part of the cushion block 12, a second retaining column 16 is mounted at the upper end of the rear part of the cushion block 12, the horizontal, a flash removing mechanism 2 is arranged above the cushion block 12;
the deburring mechanism 2 comprises upright posts 21 and a first motor 22, the upright posts 21 are installed at four corners of the upper end of a support 11, the first motor 22 is installed at the front ends of the 2 upright posts 21 in front, the first motor 22 is connected with the upright posts 21 through bolts, a slide rod 23 is installed between the two upright posts 21 on the same side, the slide rod 23 is connected with the upright posts 21 through screws, a screw rod is installed on the inner side of the slide rod 23 and is connected with the first motor 22 through a coupler, a first mounting frame 24 is installed on the screw rod and is connected with the slide rod 23 in a sliding mode, 2 second telescopic rods 27 are symmetrically installed at the upper end of the first mounting frame 24, a second mounting frame 25 is installed below the first mounting frame 24, a telescopic shaft of each second telescopic rod 27 is connected with the second mounting frame 25, second guide rods 26 are installed on the outer sides of the telescopic shafts of the 2 second telescopic rods 27 and at the upper end of the second mounting frame 25, the second guide bar 26 is slidably connected to the first mounting bracket 24, and the second mounting bracket 25 is provided with a grinding assembly 28.
Preferably: the grinding assembly 28 comprises a second motor 281 and a grinding roller 282, the second motor 281 is installed on one side of the front portion of the second mounting frame 25, the second motor 281 is connected with the second mounting frame 25 through screws, a grinding roller 282 is installed on an output shaft of the second motor 281, the grinding roller 282 is connected with the second motor 281 through a coupler, the grinding roller 282 is connected with the second mounting frame 25 through a bearing seat, a first chain wheel 283 is installed on a rotating shaft of the front grinding roller 282 and on one side of the second mounting frame 25, a second chain wheel 285 is installed on a rotating shaft of the rear grinding roller 282 and on one side of the second mounting frame 25, and the second chain wheel 285 is connected with the first chain wheel 283 through a transmission chain 284; the cushion block 12 is connected with the bracket 11 through a bolt, and the slide rail 13 is connected with the bracket 11 through a bolt; the clamping assembly 14 is connected with the bracket 11 through bolts, and the fixing plate 142 is connected with the bracket 11 through bolts; the first telescopic rod 141 is connected with the fixed plate 142 through a bolt, and the profiling clamping block 143 is connected with the slide rail 13 in a sliding manner; the first catch column 15 is in threaded connection with the cushion block 12, and the second catch column 16 is in threaded connection with the cushion block 12; the second telescopic rod 27 is connected with the first mounting frame 24 through screws, and the upright post 21 is connected with the bracket 11 through welding; the first chain wheel 283, the second chain wheel 285 and the grinding roller 282 are connected through keys.
The working principle and the using method of the invention are as follows: when the aircraft tail fin polishing device is used, firstly, an aircraft tail fin to be deburred is placed on the cushion block 12, then the aircraft tail fin is limited on the cushion block 12 by the first retaining column 15 and the second retaining column 16, so that the aircraft tail fin is prevented from sliding off, the first telescopic rod 141 is extended to drive the profiling clamping block 143 to move along the slide rail 13 until the aircraft tail fin is clamped, the first motor 22 is operated to drive the screw rod inside the slide rod 23 to rotate, the first mounting frame 24 is further driven to move along the length direction of the slide rod 23, the second telescopic rod 27 is extended and retracted to adjust the height position of the polishing assembly 28, the second motor 281 is started at the same time, the second motor 281 is rotated to drive the polishing roller 282 to rotate, or the polishing roller 282 in front drives the first chain wheel 283 to rotate, the first chain wheel 283 rotates to drive the second chain wheel 285 to rotate by the transmission of the transmission chain 284, and, the grinding roller 282 moves along the length of the slide bar 23 while rotating, and when moving from one end of the tail to the other end, the deburring process is completed.
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. A unhairing limit processing apparatus for aviation aircraft fin is made which characterized in that: comprises a clamping mechanism and a flash removing mechanism used for processing flash generated in the manufacture of an aviation aircraft empennage;
the clamping mechanism comprises a support and cushion blocks, wherein the cushion blocks are installed at the upper ends of the support, slide rails are installed on two sides of each cushion block and at the upper end of each support, the number of the slide rails is 3, a clamping assembly is installed at the other end of each slide rail, a first baffle column is installed at the upper end of the front portion of each cushion block, a second baffle column is installed at the upper end of the rear portion of each cushion block, the horizontal distance between each second baffle column and each first baffle column is the same as the length of the edge of the empennage of the aircraft to be deflashed, and a deflasher mechanism is installed above each cushion block;
the deburring mechanism comprises upright posts and a first motor, the upright posts are arranged at four corners of the upper end of the bracket, the first motor is arranged at the front ends of 2 upright posts in front, the first motor is connected with the upright posts through bolts, a slide bar is arranged between the two upright posts at the same side, the slide bar is connected with the upright posts through screws, a screw rod is arranged at the inner side of the slide bar, this screw rod passes through coupling joint in first motor, on this screw rod and sliding connection installs first mounting bracket in the slide bar, 2 second telescopic links are installed to the upper end symmetry of first mounting bracket, the second mounting bracket is installed to the below of first mounting bracket, the telescopic shaft of second telescopic link is connected in the second mounting bracket, the outside of the telescopic shaft of 2 second telescopic links and install the second guide arm in the upper end of second mounting bracket, the second guide arm passes through the screw connection with the second mounting bracket, second guide arm sliding connection is in first mounting bracket, install the subassembly of polishing on the second mounting bracket.
2. A deflash treatment device for the manufacture of an aircraft tail according to claim 1, characterized in that: the polishing assembly comprises a second motor and a polishing roller, the second motor is installed on one side of the second installation frame, the polishing roller is installed on an output shaft of the second motor, and the polishing roller is connected with the second installation frame through a bearing seat.
3. A deflash treatment device for the manufacture of an aircraft tail according to claim 1, characterized in that: the polishing assembly comprises a second motor, a polishing roller, the second motor is installed on one side of the front portion of the second mounting frame, the second motor is connected with the second mounting frame through screws, the polishing roller is installed on an output shaft of the second motor and is connected with the second motor through a coupling, the polishing roller is connected to the second mounting frame through a bearing seat, a first chain wheel is installed in the front of the polishing roller in the rotating shaft and on one side of the second mounting frame, a second chain wheel is installed in the rear of the polishing roller in the rotating shaft and on one side of the second mounting frame, and the second chain wheel is connected with the first chain wheel through a transmission chain.
4. A deflash treatment device for the manufacture of an aircraft tail according to claim 1, characterized in that: the cushion block is connected with the support through a bolt, and the slide rail is connected with the support through a bolt.
5. A deflash treatment device for the manufacture of an aircraft tail according to claim 1, characterized in that: clamping unit includes first telescopic link, the fixed plate, the one end at the slide rail is installed to the fixed plate, first telescopic link is all installed in the outside of every fixed plate, install the profile modeling clamp splice on the telescopic shaft of first telescopic link, first guide arm is all installed in the outside of every profile modeling clamp splice, first guide arm and fixed plate sliding connection, first guide arm passes through screw connection in the profile modeling clamp splice, clamping unit passes through bolted connection with the support, the fixed plate passes through bolted connection with the support.
6. A deflash treatment device for the manufacture of an aircraft tail according to claim 5, characterized in that: the first telescopic rod is connected with the fixed plate through a bolt, and the profiling clamping block is connected with the sliding rail in a sliding mode.
7. A deflash treatment device for the manufacture of an aircraft tail according to claim 1, characterized in that: the first bumping post is in threaded connection with the cushion block, and the second bumping post is in threaded connection with the cushion block.
8. A deflash treatment device for the manufacture of an aircraft tail according to claim 1, characterized in that: the second telescopic rod is connected with the first mounting frame through screws, and the stand column is connected with the support through welding.
9. A deflash treatment device for the manufacture of an aircraft tail according to claim 2, characterized in that: the second motor passes through the coupling joint with the roller of polishing, and the second motor is provided with 2.
10. A deflash treatment device for the manufacture of an aircraft tail according to claim 3, characterized in that: the first chain wheel, the second chain wheel and the grinding roller are connected through keys.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011091225.4A CN112238376A (en) | 2020-10-13 | 2020-10-13 | A unhairing limit processing apparatus for manufacturing of aviation aircraft fin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011091225.4A CN112238376A (en) | 2020-10-13 | 2020-10-13 | A unhairing limit processing apparatus for manufacturing of aviation aircraft fin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN112238376A true CN112238376A (en) | 2021-01-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011091225.4A Withdrawn CN112238376A (en) | 2020-10-13 | 2020-10-13 | A unhairing limit processing apparatus for manufacturing of aviation aircraft fin |
Country Status (1)
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|---|---|
| CN (1) | CN112238376A (en) |
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| CN111360587A (en) * | 2020-04-16 | 2020-07-03 | 航天海鹰(镇江)特种材料有限公司 | Profiling device for I-shaped composite material stringer workpiece and application method thereof |
| CN211029527U (en) * | 2019-11-14 | 2020-07-17 | 佛山市唯庭家具有限公司 | Novel furniture polishing machine |
| CN211072986U (en) * | 2019-10-15 | 2020-07-24 | 崇阳秦江木业有限责任公司 | Grinding device is used in production of high density fiberboard |
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2020
- 2020-10-13 CN CN202011091225.4A patent/CN112238376A/en not_active Withdrawn
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20160139690A (en) * | 2015-05-28 | 2016-12-07 | 강명조 | A chamfering machine |
| CN108161629A (en) * | 2017-12-26 | 2018-06-15 | 佛山智达思佳机电科技有限公司 | A kind of automatic-lifting type auto parts and components flange sleeve inner ring workpiece polishing mechanism |
| CN211072986U (en) * | 2019-10-15 | 2020-07-24 | 崇阳秦江木业有限责任公司 | Grinding device is used in production of high density fiberboard |
| CN211029527U (en) * | 2019-11-14 | 2020-07-17 | 佛山市唯庭家具有限公司 | Novel furniture polishing machine |
| CN111360587A (en) * | 2020-04-16 | 2020-07-03 | 航天海鹰(镇江)特种材料有限公司 | Profiling device for I-shaped composite material stringer workpiece and application method thereof |
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Application publication date: 20210119 |
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