CN115647843A - Strutting arrangement is used in aeroengine blade processing - Google Patents
Strutting arrangement is used in aeroengine blade processing Download PDFInfo
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- CN115647843A CN115647843A CN202210955917.1A CN202210955917A CN115647843A CN 115647843 A CN115647843 A CN 115647843A CN 202210955917 A CN202210955917 A CN 202210955917A CN 115647843 A CN115647843 A CN 115647843A
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Abstract
The invention discloses a supporting device for machining an aircraft engine blade, which specifically comprises: the base is provided with a stable lower plate and an adhesion strip arranged below the base, and a reinforcing and supporting mechanism is arranged above the base; the device comprises a shell, a detection device and a control device, wherein the shell is provided with a smooth lower plate and a circular groove arranged below the shell, the outer part of the shell is provided with the groove, an auxiliary detection mechanism is arranged in the groove, and a protective shell is sleeved outside the auxiliary detection mechanism; the invention relates to the technical field of support, and discloses a top plate which is provided with a smooth upper plate and a fixing groove arranged in the middle of the top plate, wherein a clamping mechanism is arranged in the fixing groove. This strutting arrangement is used in aeroengine blade processing plays the fixed effect of support to the course of working of blade, keeps the stationarity in the equipment use, can decide whether equipment adopts rotatory mode work according to the kind of processing, has reached the purpose that improves work efficiency.
Description
Technical Field
The invention relates to the technical field of support, in particular to a support device for machining an aircraft engine blade.
Background
The aircraft engine is a highly complex and precise thermal machine, is used as the heart of an aircraft, is not only the power of the aircraft flight, but also an important driving force for promoting the development of the aviation industry, each important change in the human aviation history is inseparable from the technical progress of the aircraft engine, the curved surface configuration of the aircraft engine blade is extremely complex, the curved surface configuration transmits considerable torque and extremely high combustion temperature, and therefore, the blade is made of a high-temperature-resistant and high-strength material.
The existing supporting device for machining the aero-engine blade is not stable enough for supporting and fixing the blade, and the position of equipment is easy to change when polishing and milling work is carried out, so that the blade is damaged.
Disclosure of Invention
In order to realize the purpose, the invention is realized by the following technical scheme: the utility model provides a strutting arrangement is used in processing of aeroengine blade, specifically includes:
the base is provided with a stable lower plate and an adhesion strip arranged below the base, and a reinforcing and supporting mechanism is arranged above the base;
the detection device comprises a shell, a detection device and a control device, wherein the shell is provided with a smooth lower plate and a circular groove arranged below the shell, the outer part of the shell is provided with the groove, an auxiliary detection mechanism is arranged inside the groove, the outer part of the auxiliary detection mechanism is sleeved with a protective shell, and the middle part of the shell is provided with a receiving box;
the top plate is provided with a smooth upper plate and a fixing groove arranged in the middle of the top plate, and a clamping mechanism is arranged inside the fixing groove;
the reinforcing and supporting mechanism is fixedly connected with the circular groove, the top plate is arranged above the shell, and the clamping hole is formed in the upper portion inside the protective shell.
Preferably, the reinforcing and supporting mechanism comprises a groove slide way, the groove slide way is provided with a smooth inner plate, and a sliding base is arranged inside the groove slide way, a supporting column is fixedly connected to the upper side of the sliding base, and the supporting column is fixedly connected to the lower side of the circular groove.
Preferably, consolidate supporting mechanism still includes supporting platform, and this supporting platform has steady upper plate to and set up the motor in the supporting platform top, the top fixedly connected with rotary column of motor, the outside cover of rotary column is equipped with a protection section of thick bamboo, the outside cover of rotary column is equipped with the control box, the outside fixedly connected with of control box links up the pole, the middle part fixedly connected with of linking up the pole glues even board. The processing is consolidated to the top shell, and the adhesion board is used for the adhesion top impurity that falls, plays the effect of protection below recess slide, prevents that recess slide from blockking up, and the outside cover of rotary column is equipped with a protection section of thick bamboo, and the inside case of accepting of shell is in the outside of a protection section of thick bamboo, prevents that the impurity adhesion from influencing normal work in the position of rotary column.
Preferably, supplementary detection mechanism includes the bottom plate, the top fixedly connected with supporting component of bottom plate, the supplementary box of supporting component's top fixedly connected with, the top fixedly connected with screens post of supplementary box, screens post and screens hole block and connect.
Preferably, supplementary detection mechanism still includes control mechanism, control mechanism's the place ahead fixedly connected with links up the post, the place ahead fixedly connected with riser of linking the post, the top fixedly connected with of riser connects, the below fixedly connected with first bearing that connects, the below of first bearing is rotated and is connected with the grabhook clamp, the below fixedly connected with fixed slot of riser. The blade is fixed and placed, the equipment is in a stable and airtight state, the detection work cannot be disturbed, the position of the equipment is convenient to adjust, and the blade is convenient to take.
Preferably, screens mechanism includes the fretwork bottom plate, the circulation mouth has been seted up to the inside of fretwork bottom plate, the top fixedly connected with of fretwork bottom plate glues even post, the inside of gluing even post is provided with the adhesion riser.
Preferably, the screens mechanism includes the fixed station, the circulation round hole has been seted up to the top of fixed station, the mounting groove has been seted up at the middle part of fixed station, the inside fixedly connected with gusset plate of mounting groove, both sides fixedly connected with fixed establishment respectively around the gusset plate, fixed establishment's below fixedly connected with adhesion accessory plate, the drain has been seted up to the bottom of mounting groove. Fix the blade, carry out unified collection to the impurity that polishing and mill the production simultaneously, prevent that impurity from piling up, polluting the blade to the blade is in the within range of mounting groove top, produces impurity and is convenient for collect.
Preferably, control mechanism is including linking up the shell, the inside fixedly connected with elasticity post that links up the shell, the place ahead fixedly connected with backup plate of elasticity post, magnetic force screens hole has been seted up at the middle part of backup plate, control mechanism's inside is provided with the fixed plate, the inside fixedly connected with steering column of fixed plate, the place ahead of steering column is rotated and is connected with the fixed band, the place ahead fixedly connected with magnetic force screens ball of fixed band. The length of elasticity post is convenient for adjust, and the fixed blade mode is simple, and equipment is convenient for fix, keeps the stability of blade, and the supplementary detection achievement goes on, links up the shell and plays outside guard action to the elasticity post.
Preferably, the fixed establishment includes the upper plate, the below fixedly connected with screens board of upper plate, the screens groove has been seted up at the middle part of screens board, the inside fixedly connected with elasticity member in screens groove, the right side fixedly connected with arm-tie of elasticity member, the right side fixedly connected with actuation of arm-tie presss from both sides. Through adjusting the position that the actuation pressed from both sides and elastic rod spare, control the blade, easy operation, and be difficult for causing the injury to the blade, but the blade adhesion is in the place ahead of adhesion accessory plate, supplementary polishing work.
The invention provides a supporting device for machining an aircraft engine blade. The method has the following beneficial effects:
1. this strutting arrangement is used in aeroengine blade processing through setting up the reinforcement supporting mechanism, consolidates the top shell and handles, and the adhesion board is used for the impurity that the adhesion top falls, plays the effect of protection below recess slide, prevents that recess slide from blockking up, and the outside cover of rotary column is equipped with a protection section of thick bamboo, and the inside case of accepting of shell is in the outside of a protection section of thick bamboo, prevents that the impurity adhesion from influencing normal work in the position of rotary column. The purposes of reinforcing the upper shell and adhering the impurities falling from the upper shell are achieved.
2. This strutting arrangement is used in aeroengine blade processing through setting up supplementary detection mechanism, fixes and lays the blade, and equipment is in steady inclosed state, can not disturbed when carrying out detection achievement, and the position of equipment is convenient for adjust, and the blade is taken conveniently, has reached and has fixed the blade, supplementary detection achievement's purpose.
3. This strutting arrangement is used in aeroengine blade processing through setting up screens mechanism, fixes the blade, carries out unified collection to the impurity of polishing and milling production simultaneously, prevents that impurity from piling up, pollutes the blade to the blade is in the within range of mounting groove top, produces impurity and is convenient for collect, has reached and has collected the impurity that the during operation produced, and carries out fixed purpose to the blade.
4. This strutting arrangement is used in aero-engine blade processing, through setting up control mechanism, the length of elasticity post is convenient for adjust, and the fixed blade mode is simple, and equipment is convenient for fix, keeps the stability of blade, and the going on of supplementary detection achievement links up the shell and plays outside guard action to the elasticity post, has reached supplementary fixed blade, and the control mechanism position purpose of being convenient for adjust.
5. This strutting arrangement is used in aeroengine blade processing through setting up fixed establishment, through adjusting the position that the actuation pressed from both sides and elasticity member, controls the blade, easy operation, and is difficult for causing the injury to the blade, but the blade adhesion is in the place ahead of adhesion accessory plate, supplementary polishing work has reached supplementary fixed blade, and easy operation's purpose.
Drawings
FIG. 1 is a schematic overall structure diagram of a supporting device for machining an aircraft engine blade according to the invention;
FIG. 2 is a schematic top view of the present invention;
FIG. 3 is a schematic structural view of a reinforcing support mechanism according to the present invention;
FIG. 4 is a schematic view of an auxiliary detection mechanism according to the present invention;
FIG. 5 is a schematic view of the locking mechanism of the present invention;
FIG. 6 is a schematic view of the control mechanism of the present invention;
fig. 7 is a schematic structural diagram of the fixing mechanism of the present invention.
In the figure: 1. a base; 2. adhering the long strips; 3. reinforcing the supporting mechanism; 301. a groove slideway; 302. a sliding base; 303. a support pillar; 304. a support platform; 305. a motor; 306. turning the column; 307. a protective cylinder; 308. a control box; 309. a connecting rod; 310. sticking the connecting plate; 4. a housing; 5. a circular groove; 6. a groove; 7. an auxiliary detection mechanism; 701. a base plate; 702. a support assembly; 703. an auxiliary box; 704. a position clamping column; 705. connecting the column; 706. a vertical plate; 707. a joint; 708. a first bearing; 709. grabbing and clamping; 710. a fixing groove; A. a control mechanism; a01, connecting shells; a02, an elastic column; a03, backing plate; a04, a magnetic clamping hole; a05, fixing a plate; a06, a steering column; a07, fixing a belt; a08, a magnetic clamping ball; 8. a protective shell; 9. a top plate; 10. a clamping mechanism; 1001. hollowing out the bottom plate; 1002. a flow port; 1003. adhering the column; 1004. adhering a vertical plate; 1005. a fixed table; 1006. a circulation circular hole; 1007. a placing groove; 1008. a reinforcing plate; 1009. adhering the auxiliary plate; B. a fixing mechanism; b01, an upper plate; b02, a clamping plate; b03, a clamping groove; b04, an elastic rod piece; b05, pulling a plate; and B06, attracting and clamping.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and specific embodiments. The embodiments of the present invention have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to practitioners skilled in this art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
In the first embodiment, as shown in fig. 1-2, the present invention provides a technical solution: the method specifically comprises the following steps:
the base 1 is provided with a stable lower plate and an adhesion strip 2 arranged below the base 1, and a reinforcing and supporting mechanism 3 is arranged above the base 1;
the device comprises a shell 4, a detection device and a control device, wherein the shell 4 is provided with a smooth lower plate and a circular groove 5 arranged below the shell 4, the outer part of the shell 4 is provided with a groove 6, an auxiliary detection mechanism 7 is arranged inside the groove 6, the outer part of the auxiliary detection mechanism 7 is sleeved with a protective shell 8, and the middle part of the shell 4 is provided with a receiving box;
the top plate 9 is provided with a smooth upper plate, and a fixing groove is arranged in the middle of the top plate 9, and a clamping mechanism 10 is arranged inside the fixing groove;
the reinforcing and supporting mechanism 3 is fixedly connected with the circular groove 5, the top plate 9 is arranged above the shell 4, and the clamping hole is formed in the upper part inside the protective shell 8. The device has the advantages of reinforcing equipment and fixedly supporting the engine blade. Fix the adhesion rectangular of base bottom and ground adhesion, start the reinforcement supporting mechanism, the shell of reinforcement supporting mechanism can support the top prevents that the position from taking place to change when rotatory. The protective housing is pulled upwards manually, so that the clamping hole in the protective housing is separated from the auxiliary detection mechanism, the auxiliary detection mechanism is operated, the blade can be detected, when the blade needs to be milled and polished, the blade can be placed in the clamping mechanism, the auxiliary fixing work is carried out, and meanwhile, produced impurities and polishing liquid can enter the carrying box below through the clamping mechanism, and the carrying box can be detached and processed in the later period.
In the second embodiment, as shown in fig. 3, the reinforcing support mechanism 3 includes a groove sliding way 301, the groove sliding way 301 has a smooth inner plate, and a sliding base 302 disposed inside the groove sliding way 301, a support column 303 is fixedly connected above the sliding base 302, and the support column 303 is fixedly connected below the circular groove 5.
The reinforcing and supporting mechanism 3 further comprises a supporting platform 304, the supporting platform 304 is provided with a stable upper plate, a motor 305 is arranged above the supporting platform 304, a rotating column 306 is fixedly connected above the motor 305, a protective cylinder 307 is sleeved outside the rotating column 306, a control box 308 is sleeved outside the rotating column 306, an engaging rod 309 is fixedly connected to the outside of the control box 308, and an adhesion plate 310 is fixedly connected to the middle of the engaging rod 309. The method has the advantages of reinforcing the upper shell and simultaneously adhering the impurities falling from the upper part. And the motor is manually started, and the motor starts to drive the rotary column above the rotary column to rotate, so that the control box, the shell and the connecting rod outside the rotary column are driven to rotate. The below of shell is provided with the ring groove, and when the shell rotated, the ring groove of below rotated together, can drive the support column of below and rotate together, and the support column bottom is provided with sliding base, and sliding base can follow the rotation in the recess slide, plays the supporting role to the equipment of top. When the connecting rod rotates, the connecting plate is driven to move and is used for connecting the impurities falling from the upper part.
In the third embodiment, as shown in fig. 4, the auxiliary detection mechanism 7 includes a bottom plate 701, a support component 702 is fixedly connected above the bottom plate 701, an auxiliary box 703 is fixedly connected above the support component 702, a position-locking column 704 is fixedly connected above the auxiliary box 703, and the position-locking column 704 is connected with a position-locking hole in a locking manner.
The auxiliary detection mechanism 7 further comprises a control mechanism A, a connection column 705 is fixedly connected to the front of the control mechanism A, a vertical plate 706 is fixedly connected to the front of the connection column 705, a joint 707 is fixedly connected to the upper side of the vertical plate 706, a first bearing 708 is fixedly connected to the lower side of the joint 707, a gripping clamp 709 is rotatably connected to the lower side of the first bearing 708, and a fixing groove 710 is fixedly connected to the lower side of the vertical plate 706. The blade fixing device has the advantages of fixing the blade and assisting in detection. When the blade detection device is used, the protective shell is pulled upwards manually, the clamping hole in the protective shell is separated from the clamping column, the control mechanism is operated manually, after the distance is adjusted, the position of the clamping clamp below the first bearing is adjusted manually, the blade is fixed by opening the clamping clamp manually, the bottom of the blade can naturally fall into a fixing groove below the blade, and the blade can be detected.
In a fourth embodiment, as shown in fig. 5, the clamping mechanism 10 includes a hollow bottom plate 1001, a circulation port 1002 is formed in the hollow bottom plate 1001, an adhesion column 1003 is fixedly connected to the upper side of the hollow bottom plate 1001, and an adhesion riser 1004 is disposed in the adhesion column 1003.
In a fifth embodiment, as shown in fig. 6, the control mechanism a includes a joining shell a01, an elastic column a02 is fixedly connected inside the joining shell a01, a backup plate a03 is fixedly connected in front of the elastic column a02, a magnetic clamping hole a04 is formed in the middle of the backup plate a03, a fixing plate a05 is arranged inside the control mechanism a, a steering column a06 is fixedly connected inside the fixing plate a05, a fixing band a07 is rotatably connected in front of the steering column a06, and a magnetic clamping ball a08 is fixedly connected in front of the fixing band a 07. The auxiliary fixing device has the advantages that the auxiliary fixing device can be used for assisting in fixing the blades, and the position of the control mechanism is convenient to adjust. When the blade needs to be fixed, the elastic column is pulled forwards, the backup plate is located at the foremost end, after the fixing is finished, the fixing band is pulled manually, the direction of the fixing band in front of the steering column is adjusted, the elastic column is pushed inwards, the magnetic clamping ball and the magnetic clamping hole are attracted and fixed, and therefore the position of the blade is fixed.
In a sixth embodiment, as shown in fig. 7, the fixing mechanism B includes an upper plate B01, a clamping plate B02 is fixedly connected below the upper plate B01, a clamping groove B03 is formed in the middle of the clamping plate B02, an elastic rod B04 is fixedly connected inside the clamping groove B03, a pulling plate B05 is fixedly connected to the right side of the elastic rod B04, and a suction clamp B06 is fixedly connected to the right side of the pulling plate B05. Has the advantages of auxiliary fixed blades and simple operation. The suction clamp is pulled to the left side and the right side manually, the suction clamp can extrude the pull plate to the left side and the right side at the moment, so that the elastic rod piece is extruded, the blade is arranged in the middle of the suction clamp, the suction clamp is released, and the elastic rod piece rebounds to the middle to fix the blade at the moment.
The working principle is as follows: the adhesion strip of base bottom is fixed with the ground adhesion, starts to consolidate supporting mechanism, and the motor is opened to the manual, and the motor begins to drive the rotary column rotation of top this moment to drive the outside control box of rotary column, shell and joint pole and rotate. The below of shell is provided with the ring recess, and when the shell rotated, the ring recess of below together rotated, can drive the support column of below and together rotate, and the support column bottom is provided with sliding bottom, and sliding bottom can follow the rotation in the recess slide, plays the supporting role to the equipment of top. When the joint rod rotates, the joint rod can drive the adhesion plate to move, the adhesion plate is used for adhering impurities falling from the upper side, the reinforcing and supporting mechanism can support the shell above, and the position is prevented from changing during rotation. The protective housing is pulled upwards manually during use, the screens hole and the screens post separation in the protective housing this moment, manual control mechanism, pull the elasticity post forward, make the backup plate be in foremost, after fixed, the manual fixed band that pulls, adjust the direction of fixed band in steering column the place ahead, and promote the elasticity post to inside, it is fixed with magnetic force screens ball and the actuation of magnetic force screens hole, thereby with the blade rigidity, after the adjustment distance, the position of manual regulation tongs below the primary shaft holds, it is fixed with the blade to open the tongs manually, the blade bottom can fall in the fixed slot of below naturally, can begin to detect work to the blade. When the blade needs to be milled and polished, the fixing mechanism is manually operated, the suction clamp is manually pulled to the left side and the right side, the suction clamp can extrude the pulling plate to the left side and the right side, the elastic rod piece is extruded, the blade is arranged in the middle of the suction clamp, the suction clamp is released, and the elastic rod piece rebounds to the middle to fix the blade. The below of blade can glue the place ahead at the adhesion accessory plate, can open the motor, carry out polishing treatment to the blade at rotatory in-process, can close the motor when milling and carry out work, the impurity of production can be followed drain and the circulation round hole downstream of settling tank bottom, outside impurity can fall into the top of fretwork bottom plate, adhesion post and adhesion riser can hang some impurity of adhesion, impurity can follow circulation mouth downstream afterwards and get into the case of accepting of bottom, but later stage disassembly holds the case and handles.
It is to be understood that the described embodiments are merely a few embodiments of the invention, and not all embodiments. All other embodiments, which can be derived by one of ordinary skill in the art and related arts based on the embodiments of the present invention without any creative effort, shall fall within the protection scope of the present invention. Structures, devices, and methods of operation not specifically described or illustrated herein are not specifically illustrated or described, but are instead contemplated to be practiced in the art by those skilled in the art.
Claims (9)
1. The utility model provides a strutting arrangement is used in processing of aeroengine blade, specifically includes:
base (1), its characterized in that: the base (1) is provided with a stable lower plate and an adhesion strip (2) arranged below the base (1), and a reinforcing and supporting mechanism (3) is arranged above the base (1);
the detection device comprises a shell (4), wherein the shell (4) is provided with a smooth lower plate and a circular groove (5) arranged below the shell (4), a groove (6) is formed in the outer part of the shell (4), an auxiliary detection mechanism (7) is arranged in the groove (6), a protective shell (8) is sleeved on the outer part of the auxiliary detection mechanism (7), and a receiving box is arranged in the middle of the shell (4);
the top plate (9), the top plate (9) has smooth upper plates, and set up the fixed groove in the middle part of the top plate (9), there are clamping mechanisms (10) inside the said fixed groove;
the reinforcing and supporting mechanism (3) is fixedly connected with the circular groove (5), the top plate (9) is arranged above the shell (4), and the clamping hole is formed in the upper portion inside the protective shell (8).
2. The support device for machining the blade of the aircraft engine as claimed in claim 1, wherein: consolidate supporting mechanism (3) including recess slide (301), this recess slide (301) have smooth inner panel to and set up sliding base (302) inside recess slide (301), sliding base's (302) top fixedly connected with support column (303), support column (303) fixed connection is in the below of ring groove (5).
3. The support device for machining the blade of the aircraft engine as claimed in claim 2, wherein: consolidate supporting mechanism (3) and still include supporting platform (304), and this supporting platform (304) have steady upper plate to and set up motor (305) in supporting platform (304) top, the top fixedly connected with of motor (305) changes post (306), the outside cover of changeing post (306) is equipped with a protection section of thick bamboo (307), the outside cover of changeing post (306) is equipped with control box (308), the outside fixedly connected with of control box (308) links pole (309), the middle part fixedly connected with adhesion plate (310) of linking pole (309).
4. The support device for machining the blade of the aircraft engine as claimed in claim 1, wherein: the auxiliary detection mechanism (7) comprises a bottom plate (701), a supporting component (702) is fixedly connected to the upper portion of the bottom plate (701), an auxiliary box (703) is fixedly connected to the upper portion of the supporting component (702), a clamping column (704) is fixedly connected to the upper portion of the auxiliary box (703), and the clamping column (704) is connected with a clamping hole in a clamping mode.
5. The support device for machining the blade of the aircraft engine as claimed in claim 4, wherein: the auxiliary detection mechanism (7) further comprises a control mechanism (A), the front fixedly connected with of the control mechanism (A) is connected with a connecting column (705), the front fixedly connected with vertical plate (706) of the connecting column (705), the upper fixedly connected with of the vertical plate (706) is connected with a joint (707), the lower fixedly connected with of the joint (707) is connected with a first bearing (708), the lower portion of the first bearing (708) is rotatably connected with a grabbing clamp (709), and the lower portion of the vertical plate (706) is fixedly connected with a fixing groove (710).
6. The support device for machining the blade of the aircraft engine as claimed in claim 1, wherein: clamping mechanism (10) include fretwork bottom plate (1001), circulation mouth (1002) have been seted up to the inside of fretwork bottom plate (1001), the top fixedly connected with of fretwork bottom plate (1001) glues even post (1003), the inside of gluing even post (1003) is provided with adhesion riser (1004).
7. The support device for machining the blade of the aircraft engine as claimed in claim 6, wherein: screens mechanism (10) are including fixed station (1005), circulation round hole (1006) have been seted up to the top of fixed station (1005), mounting groove (1007) have been seted up at the middle part of fixed station (1005), inside fixedly connected with gusset plate (1008) of mounting groove (1007), both sides fixedly connected with fixed establishment (B) respectively around gusset plate (1008), below fixedly connected with adhesion accessory plate (1009) of fixed establishment (B), the drain has been seted up to the bottom of mounting groove (1007).
8. The support device for machining the blade of the aircraft engine as claimed in claim 5, wherein: control mechanism (A) is including linking up shell (A01), link up inside fixedly connected with elasticity post (A02) of shell (A01), place ahead fixedly connected with backup plate (A03) of elasticity post (A02), magnetic force screens hole (A04) has been seted up at the middle part of backup plate (A03), the inside of control mechanism (A) is provided with fixed plate (A05), inside fixedly connected with steering column (A06) of fixed plate (A05), the place ahead rotation of steering column (A06) is connected with fixed band (A07), the place ahead fixedly connected with magnetic force screens ball (A08) of fixed band (A07).
9. The support device for machining the blade of the aircraft engine as claimed in claim 7, wherein: fixed establishment (B) includes upper plate (B01), below fixedly connected with screens board (B02) of upper plate (B01), screens groove (B03) has been seted up at the middle part of screens board (B02), the inside fixedly connected with elasticity member (B04) in screens groove (B03), the right side fixedly connected with arm-tie (B05) of elasticity member (B04), the right side fixedly connected with actuation clamp (B06) of arm-tie (B05).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210955917.1A CN115647843B (en) | 2022-08-10 | 2022-08-10 | Supporting device for machining aero-engine blades |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210955917.1A CN115647843B (en) | 2022-08-10 | 2022-08-10 | Supporting device for machining aero-engine blades |
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| CN115647843A true CN115647843A (en) | 2023-01-31 |
| CN115647843B CN115647843B (en) | 2023-09-15 |
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| SU1484552A1 (en) * | 1987-05-14 | 1989-06-07 | Научно-производственное объединение "Атомкотломаш" | Apparatus for securing parts |
| CN109333099A (en) * | 2018-10-11 | 2019-02-15 | 西北工业大学 | Blade of aviation engine processes multiple spot slewing supporting device |
| KR102053667B1 (en) * | 2019-06-07 | 2019-12-09 | 진광복 | Jig device for machining spindle head for machine tool |
| CN111054955A (en) * | 2019-12-30 | 2020-04-24 | 贵州乾鼎物资贸易有限公司 | Multi-point rotary supporting device for machining of aero-engine blade |
| CN111922743A (en) * | 2020-09-01 | 2020-11-13 | 郭翠丽 | Clamping device is used in processing of new energy automobile spare part |
| CN112589528A (en) * | 2020-12-18 | 2021-04-02 | 龚爽 | Motor housing trompil auxiliary assembly with adjustable |
| CN214322580U (en) * | 2020-12-24 | 2021-10-01 | 石家庄峥嵘泵业有限公司 | Clamping device is used in production of sediment stuff pump impeller |
| CN214603597U (en) * | 2021-02-03 | 2021-11-05 | 江苏江航智飞机发动机部件研究院有限公司 | High-precision blade polishing device for aero-engine |
| CN215432572U (en) * | 2021-02-03 | 2022-01-07 | 江苏江航智飞机发动机部件研究院有限公司 | Aeroengine high-precision blade machining and milling device |
| CN214490493U (en) * | 2021-03-18 | 2021-10-26 | 泰成半导体精密(苏州)有限公司 | Angle-adjustable tool clamp for machining aero-engine blade |
| CN215145048U (en) * | 2021-06-02 | 2021-12-14 | 山东透平新能源科技有限公司 | Turbine blade parallel milling rotary tool |
| CN114042951A (en) * | 2021-12-06 | 2022-02-15 | 成都市鸿侠科技有限责任公司 | General machining process and device for central hole of engine blade |
| CN114700784A (en) * | 2022-04-26 | 2022-07-05 | 朱张奎 | Telescopic supporting auxiliary device for machining pitch-variable bearing |
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