CN113463247B - Carbon fiber felt pad weaving and extruding integrated forming machine for aircraft engine hoop and using method of carbon fiber felt pad weaving and extruding integrated forming machine - Google Patents
Carbon fiber felt pad weaving and extruding integrated forming machine for aircraft engine hoop and using method of carbon fiber felt pad weaving and extruding integrated forming machine Download PDFInfo
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- CN113463247B CN113463247B CN202110695757.7A CN202110695757A CN113463247B CN 113463247 B CN113463247 B CN 113463247B CN 202110695757 A CN202110695757 A CN 202110695757A CN 113463247 B CN113463247 B CN 113463247B
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- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D15/00—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used
- D03D15/20—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads
- D03D15/242—Woven fabrics characterised by the material, structure or properties of the fibres, filaments, yarns, threads or other warp or weft elements used characterised by the material of the fibres or filaments constituting the yarns or threads inorganic, e.g. basalt
- D03D15/275—Carbon fibres
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
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- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D47/00—Looms in which bulk supply of weft does not pass through shed, e.g. shuttleless looms, gripper shuttle looms, dummy shuttle looms
- D03D47/27—Drive or guide mechanisms for weft inserting
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- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D49/00—Details or constructional features not specially adapted for looms of a particular type
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- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D49/00—Details or constructional features not specially adapted for looms of a particular type
- D03D49/04—Control of the tension in warp or cloth
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- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D49/00—Details or constructional features not specially adapted for looms of a particular type
- D03D49/70—Devices for cutting weft threads
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- D—TEXTILES; PAPER
- D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
- D06H—MARKING, INSPECTING, SEAMING OR SEVERING TEXTILE MATERIALS
- D06H7/00—Apparatus or processes for cutting, or otherwise severing, specially adapted for the cutting, or otherwise severing, of textile materials
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- Chemical & Material Sciences (AREA)
- Inorganic Chemistry (AREA)
- Woven Fabrics (AREA)
Abstract
The invention belongs to the field of fiber weaving and forming, and particularly relates to a carbon fiber felt mat weaving and extruding integrated forming machine for an aircraft engine hoop and a using method of the carbon fiber felt mat weaving and extruding integrated forming machine. The technical scheme of the invention is as follows: a carbon fiber felt pad is woven and extrusion integration make-up machine for aeroengine clamp, including braider module, extrusion tailor module and base, braider module and extrusion tailor module fixed mounting be in on the base, the braider module is used for weaving of carbon fiber felt pad, and the extrusion tailors the module and is used for the extrusion of carbon fiber felt pad and tailors. The carbon fiber felt mat weaving and extruding integrated forming machine for the aircraft engine hoop and the using method thereof can realize the conveying and two-dimensional automatic weaving of carbon fiber yarns and can realize the integrated processing of extruding, forming and cutting of carbon fiber cloth.
Description
Technical Field
The invention belongs to the field of fiber weaving and forming, and particularly relates to a carbon fiber felt pad weaving and extruding integrated forming machine for an aircraft engine hoop and a using method of the carbon fiber felt pad weaving and extruding integrated forming machine.
Background
The felt pad is an important component of the clamp of the aero-engine, is arranged between a hydraulic pipeline and the clamp, plays the roles of vibration reduction, temperature resistance and restriction gap adjustment, and can enable the installed pipeline piece to be stressed more uniformly, so that the service life of the pipeline can be prolonged, and the felt pad is widely applied to the clamp of the aero-engine in China and Russian. At present, the clamp felt pad of the aero-engine is mainly woven by metal wires, but metal materials are heavy in mass and prone to dent and crack during extrusion forming, elasticity is removed easily under the large-amplitude vibration excitation of a pipeline, vibration reduction effect is weakened gradually, and the thrust-weight ratio and fuel economy are improved without using an advanced aero-engine. The carbon fiber has the outstanding advantages of high specific modulus, high specific strength, high temperature resistance, good corrosion resistance and the like, and if the carbon fiber can be woven into a felt pad structure in the hoop, the carbon fiber can replace a metal felt pad to play a better role, and has a wider application prospect in the field of aeroengines.
However, at present, most of the commercial knitting machines use carbon fiber yarn as a knitting object, most of the industrial knitting machines still use silk-woven cotton yarn as a main service object, no perfect prototype machine exists for the carbon fiber felt knitting machine special for the aircraft engine pipeline hoop, some of the existing concepts are still based on the textile industry, although the textile machine can realize the weaving of common silk yarn, the existing concepts cannot be completely met under the normal condition, the carbon fiber felt knitting machine is used for meeting the knitting requirement of carbon fiber yarn with strong rigidity, and the common knitting machines are more difficult to realize the extrusion molding function of the felt cushion knitted by the fiber yarn. In addition, some weaving techniques and devices available on the market have some problems and defects, for example, chinese patent (publication number: CN202010350347) discloses a beating-up device of a loom, which is designed for a weaving machine, and uses the gravity of the fiber and a spring to control the fiber to reciprocate, so that the control mode has low precision, and the weft length of the woven finished product is not easy to be ensured, thereby causing the quality of the processed finished product to be not over-qualified. Chinese patent (publication No. CN201910104863) discloses a loom device, which is complex in textile structure, too large in occupied space size, large in fit size, not suitable for weaving a felt cushion with relatively simple requirements, and the loom can only realize manual yarn-assembling operation, and cannot realize automation, so that the weaving efficiency is low. Chinese patent (publication number: CN201820644847) and Chinese patent (publication number: CN201921832430) respectively disclose a feeding device for fiber spinning and a novel feeding device for fiber spinning, which are both feeding devices for a braiding machine, and a series of mechanical structures are adopted to assist the yarn feeding link before the braiding machine works, but the feeding devices have the defects of complex mechanism, overlarge occupied space and overlarge loss of an applied power source in the work process, have too harsh requirements on feeding, cannot meet the yarn feeding requirement of flat carbon fiber yarns, and are not suitable for braiding flat carbon fiber felt mats. Chinese patent (publication No. CN201710640153) discloses a winding processing structure for textile fibers, which realizes a novel weaving method other than two-dimensional cross weaving, but has high requirements for the thermal properties of processed filaments, and it is difficult to ensure the continuous weaving of carbon filaments with good heat resistance. Chinese patent (publication No. cn202020764593.x) discloses an anti-winding textile machine for processing cloth, which is added with an anti-winding device on the basis of a traditional textile machine, but the structure has complex mechanical transmission, greatly reduces the efficiency of yarn supply work, and the fiber yarn needs to pass through a longer span, so that the winding distance is overlong, the carbon fiber is not beneficial to maintaining the due shape of the weaving, and the anti-winding textile machine is more suitable for the traditional cotton yarn weaving. Chinese patent (publication No. CN201721578469.9) discloses a cloth-breakage-preventing textile machine, which adopts a yarn guide module and a weaving module on the basis of a conventional textile machine, and can prevent the vertical movement of a machine head during the textile process from cutting off the woven cloth, however, the machine still uses the whole movement of the machine head as the comprehensive movement, and is more energy-consuming than a heddle, and the longitudinal movement of the carbon fiber yarn should be reduced as much as possible to avoid the yarn breakage and the cloth breakage. Chinese patent (publication No. CN 202020299964.1) discloses a silk weaving machine with tension adjustment and burr removal functions, which is added with a structure of tension adjustment and burr removal on the basis of a traditional weaving machine, although burr of silk can be removed in the weaving process, it is difficult to remove burr of carbon fiber yarn by using a common cutter in the weaving process, and this method is more time-consuming in the weaving process of carbon fiber yarn and lacks a mechanism for centralized cutting after weaving.
Disclosure of Invention
The invention provides a carbon fiber felt mat weaving and extruding integrated forming machine for an aircraft engine hoop and a using method thereof, which can realize the conveying and two-dimensional automatic weaving of carbon fiber yarns and can realize the integrated processing of extruding, forming and cutting of carbon fiber cloth.
The technical scheme of the invention is as follows:
a carbon fiber felt pad is woven and extrusion integration make-up machine for aeroengine clamp, including braider module, extrusion tailor module and base, braider module and extrusion tailor module fixed mounting be in on the base, the braider module is used for weaving of carbon fiber felt pad, and the extrusion tailors the module and is used for the extrusion of carbon fiber felt pad and tailors.
Further, the carbon fiber felt mat weaving and extruding integrated forming machine for the aircraft engine hoop comprises a warp-wise wire supply structure, a weft-wise wire supply structure, a heald weaving structure and a machine body;
the machine body comprises a bottom plate, two side walls, a plurality of long rods and a discharge plate, wherein the bottom plate is fixedly arranged on the base, the two side walls are symmetrically and vertically fixedly arranged on two sides of the bottom plate, the long rods are fixedly arranged on the bottom plate in rows, and the discharge plate is fixedly arranged in front of the bottom plate; be equipped with the hair-dryer on the lateral wall, the air-out pipeline of hair-dryer is installed go out flitch rear side.
Furthermore, the carbon fiber felt pad weaving and extruding integrated forming machine for the aircraft engine hoop comprises a warp-wise wire supply structure, wherein the warp-wise wire supply structure comprises a plurality of carbon fiber wire cylinders, a driving clamping wheel, a driven clamping wheel and a stepping motor I, the carbon fiber wire cylinders are arranged on a plurality of long rods, and warp-wise carbon fiber wires are wound on the carbon fiber wire cylinders; the driving clamping wheel and the driven clamping wheel are arranged between the two side walls of the machine body, the two sides of the driving clamping wheel and the driven clamping wheel are respectively fixed on the side walls, and the driving clamping wheel and the driven clamping wheel are meshed together through a gear; the first stepping motor is fixedly arranged outside the side wall, and one end of the driving clamping wheel is connected with the first stepping motor; the warp-wise carbon fiber filaments pass through the space between the driving clamping wheel and the driven clamping wheel and are clamped by the driving clamping wheel and the driven clamping wheel.
Further, the carbon fiber felt mat weaving and extruding integrated forming machine for the aircraft engine hoop comprises a weft-wise reciprocating mechanism, a hydraulic clamping jaw and a mini circular saw, wherein the weft-wise yarn supplying structure comprises a weft-wise reciprocating mechanism, a hydraulic clamping jaw and a mini circular saw;
the weft reciprocating mechanism comprises a fixed seat, a swinging disc, a sector gear swinging belt groove guide rod, a rack rod and a weft box; the fixed seat is arranged outside the side wall and fixedly installed on the base, the swing disc is installed above the fixed seat and connected with a second stepping motor, a raised cylindrical rod is arranged on the swing disc, the cylindrical rod is matched and positioned with a guide rod groove of the sector gear swinging groove guide rod, a sector gear below the sector gear swinging groove guide rod is meshed with the rack rod, and the rack rod is installed on the fixed seat through two buckles; the weft box is arranged on the side wall and is provided with a feeding hole and a discharging hole for weft carbon fiber yarns;
the side wall is provided with a hole, one end of the rack rod penetrates through the side wall, the hydraulic clamping jaw is fixedly installed at the end of the rack rod, and the hydraulic clamping jaw and the latitudinal reciprocating mechanism are respectively positioned on two sides of the side wall; the hydraulic clamping jaw is used for clamping and placing weft-wise carbon fiber yarns;
the mini circular saw is mounted on the bottom plate, is positioned below the hydraulic clamping jaw and is extended out from the side of the discharging plate; the mini circular saw is used for cutting off weft-wise carbon fiber yarns.
Further, the carbon fiber felt mat weaving and extrusion integrated forming machine for the aircraft engine hoop comprises a heald weaving structure, wherein the heald weaving structure comprises a ratchet wheel, a ratchet rod, a long plate with holes, two groove rods, a single-tooth bolt and a double-ring heald, the ratchet rod, the long plate with holes and the two groove rods are arranged between two side walls of the machine body, the two groove rods are positioned above the carbon fiber wire barrel and are respectively positioned at two sides of the carbon fiber wire barrel, the long plate with holes is positioned below the side of the carbon fiber wire barrel, the ratchet rod is positioned under the long plate with holes, one end of the ratchet rod is connected with a rotating motor, and the rotating motor is arranged on the side wall; the plurality of ratchet wheels are fixedly arranged on the ratchet wheel rod at equal intervals, and the tooth shapes of two adjacent ratchet wheels are opposite in direction; the through hole on the long plate with the hole corresponds to the position of the ratchet wheel, the single-tooth bolt is arranged at the through hole of the long plate with the hole in a sliding fit manner, the teeth of the single-tooth bolt are meshed with the ratchet wheel, and the teeth of two adjacent single-tooth bolts face opposite directions; the groove rods are provided with a plurality of grooves at equal intervals, one ring of the double-ring heddle is sleeved on the single-tooth bolt, the double-ring heddle bypasses the grooves of the two groove rods, and the other ring of the double-ring heddle is suspended in front of the machine body and is used for being sleeved with warp-wise carbon fiber wires.
Furthermore, the carbon fiber felt mat weaving and extruding integrated forming machine for the aircraft engine hoop comprises an extrusion forming and cutting module and a cutting and shaping module, wherein the extrusion forming and cutting module comprises a portal frame, an extrusion forming mechanism and a cutting and shaping mechanism;
the portal frame is arranged on the base;
the extrusion forming mechanism comprises a tool magazine and a tool taking extrusion forming structure, the tool magazine comprises a tool rest, a forming tool, a hook claw and a stepping motor III, a transverse support plate is arranged on the portal frame, the tool rest and the stepping motor III are respectively arranged on two sides of the transverse support plate, and the stepping motor is used for driving the tool rest to rotate; the tool rest is of a cubic frame structure, and hook claws and a first sliding rail are arranged on four molded surfaces of the tool rest;
the periphery of a cutter head of the forming cutter is provided with cutting blades, the center of the cutter head is provided with a pressure head, the side wall of the forming cutter is provided with three flat holes and four wedge-shaped holes, and the forming cutter is provided with a sliding chute; four forming cutters with different specifications are respectively placed on four molded surfaces of the cutter rest through matching of the sliding grooves and the sliding rails, and the hook claws are inserted into the flat holes to fix the forming cutters;
the cutter taking extrusion forming structure comprises a hydraulic cylinder, a fixed support, a cutter taking clamping jaw and a lifting table, wherein the fixed support is fixedly arranged on the base, the lifting table is connected and arranged with the fixed support in a sliding manner, the hydraulic cylinder is arranged between the fixed support and the lifting table and used for driving the lifting table to move up and down, the cutter taking clamping jaws are respectively arranged on two sides of the lifting table in a sliding manner, the cutter taking clamping jaws are driven to move transversely through an electric push rod, and the front end size of each cutter taking clamping jaw is in interference fit with the wedge-shaped hole; and two sides of the lifting platform are provided with two sliding rails which are used for being matched with the sliding grooves of the forming cutter.
Furthermore, the carbon fiber felt mat weaving and extrusion integrated forming machine for the aircraft engine hoop comprises an X-direction sliding rail, a Y-direction sliding rail, an X-direction sliding block, a Y-direction sliding block, a first gear, a first rack, a second gear, a second rack, a cutter module, a shaping milling cutter and a screw rod, wherein the X-direction sliding rail and the first rack are installed above the portal frame, the X-direction sliding block and the X-direction sliding rail are installed in a matched mode, the first gear is arranged at the bottom of the X-direction sliding block, the first gear is meshed with the first rack, and a stepping motor is arranged on the X-direction sliding block and used for driving the first gear; a Y-direction sliding rail and a second rack are arranged above the two X-direction sliding blocks, the Y-direction sliding blocks are installed in a matched mode with the Y-direction sliding rails, a second gear is arranged at the bottom of each Y-direction sliding block and meshed with the second rack, and a fifth stepping motor is arranged on each Y-direction sliding block and used for driving the second gear; the tool module is connected with the Y-direction sliding block in a sliding mode, the screw rod is connected with the Y-direction sliding block in a rotating mode, a nut is arranged in the tool module and sleeved with the screw rod, a stepping motor six is arranged on the Y-direction sliding block and used for driving the screw rod, the trimming milling cutter is installed on the tool module, and a push-pull motor is arranged on the tool module and used for driving the trimming milling cutter.
The use method of the carbon fiber felt weaving and extruding integrated forming machine for the aircraft engine hoop comprises the following steps:
step 1: the warp-wise carbon fiber wires are inserted into the rings of the double-ring heddle suspended in front of the machine body through the space between the driving clamping wheel and the driven clamping wheel; penetrating the weft carbon fiber into a weft box and conveying the weft carbon fiber to the position of a hydraulic clamping jaw; starting a first stepping motor, a second stepping motor and a rotating motor;
step 2: the driving clamping wheel rolls to drive the driven clamping wheel to be tensioned and rotate, and pulls a plurality of warp-wise carbon fiber wires to be pulled out from the carbon fiber wire barrel, tensioned and finished wire discharging;
and 3, step 3: the ratchet rod rotates forwards and reversely periodically to drive the double-ring heddles on the single-tooth bolt to move up and down, so that two adjacent warp-wise carbon fiber wires are positioned on different horizontal planes when the warp-wise carbon fiber wires are conveyed forwards;
and 4, step 4: the swing disc drives the rack rod to transversely move back and forth, the hydraulic clamping jaw clamps the weft-wise carbon fiber filaments at the starting point of the swing of the rack rod, the rack rod drives the hydraulic clamping jaw to insert the weft-wise carbon fiber filaments among the warp-wise carbon fiber filaments, the hydraulic clamping jaw loosens the weft-wise carbon fiber filaments at the end point of the swing of the rack rod, the rack rod drives the hydraulic clamping jaw to return to the starting point, and the mini circular saw cuts the weft-wise carbon fiber filaments;
and 5: repeating the step 2-4, and carrying out cross weaving on the weft carbon fiber yarns and the warp carbon fiber yarns in a reciprocating and inserting manner, and processing into carbon fiber cloth by circularly and repeatedly weaving;
step 6: the woven carbon fiber cloth is sent to a station below the cutter-taking extrusion forming structure through a discharge hole by a blower;
and 7: rotating the tool magazine to select a suitable forming tool; the tool taking clamp claw moves forwards, the front end of the tool taking clamp claw is inserted into a wedge-shaped hole of the forming tool, the tool taking clamp claw moves backwards, and the forming tool is installed on the lifting table; the hydraulic cylinder continuously operates to drive the lifting table to move up and down, the forming cutter performs multiple extrusion forming on multiple layers of carbon fiber cloth, and when the number of the carbon fiber cloth layers reaches the required number, a semi-finished product of the carbon fiber felt pad is prepared;
and 8: moving the semi-finished carbon fiber felt pad to a station below the cutting and shaping mechanism for positioning; the cutting and shaping mechanism starts to work, the working path of the shaping milling cutter is controlled, and the shape of the semi-finished carbon fiber felt pad is trimmed; and preparing a finished carbon fiber felt pad product.
The invention has the beneficial effects that:
1. the device is provided with the heald wire weaving mechanism, so that the warp and weft carbon fiber wires can be woven in a crossed manner, and the product performance is greatly improved;
2. the number and the spacing of the carbon fiber yarn drums in the device can be adjusted, so that the change of the number and the spacing of the braided strands of the carbon fiber yarn cloth is realized, and the preparation of carbon fiber felt pads with different strength requirements is met;
3. according to the device, the driving clamping wheel and the driven clamping wheel are adopted to tension the fiber yarns, so that insufficient tensioning of the fiber yarns is avoided, and the strength of the fiber yarns is effectively ensured;
4. the device of the invention integrates extrusion molding and cutting, realizes simultaneous weaving and extrusion molding, saves processing time and improves processing efficiency;
5. the cutting and shaping mechanism in the device can realize the random cutting of the carbon fiber cloth extrusion molding finished product and can meet the requirements of processing finished products in different shapes;
6. the forming tools in the device are in a group of four, the shape of the pressure head can be freely selected and replaced, and the carbon fiber felt pad can meet the requirements of different surface shapes.
Drawings
FIG. 1 is a schematic view of a carbon fiber felt weaving and extrusion integrated molding machine for an aircraft engine clamp;
fig. 2 is a schematic diagram of a braiding machine module;
FIG. 3 is a schematic view of a weft reciprocating mechanism;
FIG. 4 is a schematic view of a heddle weaving structure;
FIG. 5 is a schematic view of a tool magazine;
FIG. 6 is a schematic view of a forming tool;
fig. 7 is a schematic view of an extrusion cutting module.
Detailed Description
As shown in fig. 1-7, the carbon fiber felt mat weaving and extruding integrated forming machine for the aircraft engine hoop comprises a weaving machine module, an extrusion forming and cutting module and a base 1, wherein the weaving machine module and the extrusion forming and cutting module are fixedly installed on the base 1, the weaving machine module is used for weaving the carbon fiber felt mat, and the extrusion forming and cutting module is used for extrusion forming and cutting of the carbon fiber felt mat.
The braiding machine module comprises a warp-wise wire supply structure, a weft-wise wire supply structure, a heald braiding structure and a machine body 2;
the machine body 2 comprises a bottom plate, two side walls, a plurality of long rods and a discharge plate, wherein the bottom plate is fixedly arranged on the base 1, the two side walls are symmetrically and vertically fixedly arranged on two sides of the bottom plate, the plurality of long rods are fixedly arranged on the bottom plate in rows, and the discharge plate is fixedly arranged in front of the bottom plate; be equipped with the hair-dryer on the lateral wall, the air-out pipeline of hair-dryer is installed go out flitch rear side.
The warp-wise filament supply structure comprises carbon fiber filament drums 3, a driving clamping wheel 4, a driven clamping wheel 5 and a first stepping motor, wherein a plurality of carbon fiber filament drums 3 are arranged on a plurality of long rods, and warp-wise carbon fiber filaments are wound on the carbon fiber filament drums 3; the driving clamping wheel 4 and the driven clamping wheel 5 are arranged between two side walls of the machine body 2, two sides of the driving clamping wheel 4 and two sides of the driven clamping wheel 5 are respectively fixed on the side walls, and the driving clamping wheel 4 and the driven clamping wheel 5 are meshed together through a gear; the first stepping motor is fixedly arranged outside the side wall, and one end of the driving clamping wheel 4 is connected with the first stepping motor; the warp carbon fiber filaments pass between the driving clamping wheel 4 and the driven clamping wheel 5 and are clamped by the driving clamping wheel 4 and the driven clamping wheel 5.
The weft-wise wire supply structure comprises a weft-wise reciprocating mechanism 6, a hydraulic clamping jaw 7 and a mini circular saw 8;
the weft reciprocating mechanism 6 comprises a fixed seat 9, a swinging disc 10, a sector gear swinging belt groove guide rod 11, a rack rod 12 and a weft box 13; the fixed seat 9 is arranged outside the side wall and is fixedly installed on the base 1, the swing disc 10 is installed above the fixed seat 9, the swing disc 10 is connected with a second stepping motor, a raised cylindrical rod is arranged on the swing disc 10, the cylindrical rod is matched and positioned with a guide rod groove of the sector gear swing groove guide rod 11, a sector gear below the sector gear swing groove guide rod 11 is meshed with the rack rod 12, and the rack rod 12 is installed on the fixed seat 9 through two buckles; the weft box 13 is arranged on the side wall, and the weft box 13 is provided with a feed inlet and a discharge outlet of weft carbon fiber yarns;
the side wall is provided with a hole, one end of the rack rod 12 penetrates through the side wall, the hydraulic clamping jaw 7 is fixedly installed at the end of the rack rod 12, and the hydraulic clamping jaw 7 and the latitudinal reciprocating mechanism 6 are respectively positioned on two sides of the side wall; the hydraulic clamping jaw 7 is used for clamping and placing weft-wise carbon fiber yarns;
the mini circular saw 8 is installed on the bottom plate, is positioned below the hydraulic clamping jaw 7 and is extended out from the side of the discharging plate; the mini circular saw 8 is used for cutting off weft-wise carbon fiber yarns.
The heddle weaving structure comprises a ratchet wheel 14, a ratchet rod 17, a long perforated plate, two groove rods 18, a single-tooth bolt 15 and a double-ring heddle 16, wherein the ratchet rod 17, the long perforated plate and the two groove rods 18 are arranged between two side walls of the machine body 2, the two groove rods 18 are positioned above the carbon fiber wire barrel 3 and are respectively positioned at two sides of the carbon fiber wire barrel 3, the long perforated plate is positioned below the side of the carbon fiber wire barrel 3, the ratchet rod 17 is positioned right below the long perforated plate, one end of the ratchet rod 17 is connected with a rotating motor, and the rotating motor is arranged on the side wall; a plurality of ratchet wheels 14 are fixedly arranged on the ratchet rod 17 at equal intervals, and the tooth shapes of two adjacent ratchet wheels 14 are opposite in direction; the through hole on the long plate with the hole corresponds to the ratchet wheel 14 in position, the single-tooth bolt 15 is installed at the through hole of the long plate with the hole in a sliding fit mode, the gear teeth of the single-tooth bolt 15 are meshed with the ratchet wheel 14, and the gear teeth of two adjacent single-tooth bolts 15 face opposite directions; a plurality of grooves with equal intervals are arranged on the groove rods 18, one ring of the double-ring heddle 16 is sleeved on the single-tooth bolt 15, the double-ring heddle 16 bypasses the grooves of the two groove rods 18, and the other ring of the double-ring heddle 16 is suspended in front of the machine body 2 and is used for sleeving a warp-wise carbon fiber wire.
The extrusion molding cutting module comprises a portal frame 32, an extrusion molding mechanism and a cutting and shaping mechanism;
the gantry 32 is mounted on the base 1;
the extrusion forming mechanism comprises a tool magazine and a tool taking extrusion forming structure, the tool magazine comprises a tool rest 27, a forming tool 19, a hook 20 and a third stepping motor, a transverse support plate is arranged on the portal frame 32, the tool rest 27 and the third stepping motor are respectively arranged on two sides of the transverse support plate, and the third stepping motor is used for driving the tool rest 27 to rotate; the tool rest 27 is of a cubic frame structure, and hook claws 20 and a first sliding rail are arranged on four molded surfaces of the tool rest 27;
the periphery of the cutter head of the forming cutter 19 is provided with cutting blades, the center of the cutter head is provided with a pressure head, the side wall of the forming cutter 19 is provided with three flat holes 26 and four wedge-shaped holes 25, and the forming cutter 19 is provided with a sliding chute; four forming tools 19 with different specifications are respectively placed on four profiles of the tool rest 27 through the matching of a sliding chute and a sliding rail I, and the hook claw 20 is inserted into the flat hole 26 to fix the forming tools 19;
the cutter taking extrusion forming structure comprises a hydraulic cylinder 21, a fixing support 22, a cutter taking clamp claw 23 and a lifting platform 24, wherein the fixing support 22 is fixedly installed on the base 1, the lifting platform 24 is installed with the fixing support 22 in a sliding connection mode, the hydraulic cylinder 21 is arranged between the fixing support 22 and the lifting platform 24 and used for driving the lifting platform 24 to move up and down, the cutter taking clamp claw 23 is respectively installed on two sides of the lifting platform 24 in a sliding mode, the cutter taking clamp claw 23 is driven to move transversely through an electric push rod, and the size of the front end of the cutter taking clamp claw 23 is in interference fit with the wedge-shaped hole 25; two sides of the lifting platform 24 are provided with two sliding rails for matching with the sliding grooves of the forming cutter 19.
The cutting and shaping mechanism comprises an X-direction slide rail 36, a Y-direction slide rail 34, an X-direction slide block 35, a Y-direction slide block 33, a first gear, a first rack, a second gear, a second rack, a cutter module 29, a shaping milling cutter 30 and a screw rod 31, wherein the X-direction slide rail 36 and the first rack are installed above the portal frame 32, the X-direction slide block 35 is installed in a manner of being matched with the X-direction slide rail 36, the bottom of the X-direction slide block 35 is provided with the first gear, the first gear is meshed with the first rack, and the X-direction slide block 35 is provided with a fourth stepping motor for driving the first gear; a Y-direction sliding rail 34 and a second rack are arranged above the two X-direction sliding blocks 35, the Y-direction sliding block 33 is installed in a matched mode with the Y-direction sliding rail 34, a second gear is arranged at the bottom of the Y-direction sliding block 33 and meshed with the second rack, and a fifth stepping motor is arranged on the Y-direction sliding block 33 and used for driving the second gear; the cutter module 29 is connected with a Y-direction sliding block 33 in a sliding mode, the screw rod 31 is connected with the Y-direction sliding block 33 in a rotating mode, a nut is arranged in the cutter module 29 and sleeved with the screw rod 31, a stepping motor is arranged on the Y-direction sliding block 33 and used for driving the screw rod 31, the cutter module 29 is provided with the shaping milling cutter 30, and a push-pull motor is arranged on the cutter module 29 and used for driving the shaping milling cutter 30.
The use method of the carbon fiber felt weaving and extruding integrated forming machine for the aircraft engine hoop comprises the following steps:
step 1: warp-wise carbon fiber wires are inserted into a ring of a double-ring heddle 16 suspended in front of the machine body 2 through a space between a driving clamping wheel 4 and a driven clamping wheel 5; and the weft carbon fiber yarns penetrate into a weft box 13 and are sent to the position of the hydraulic clamping jaw 7; starting the first stepping motor, the second stepping motor and the rotating motor;
step 2: the driving clamping wheel 4 rolls to drive the driven clamping wheel 5 to be tensioned and rotate, and pulls a plurality of warp-wise carbon fiber yarns out of the carbon fiber yarn drum 3 to be tensioned and finish yarn discharging;
and step 3: the ratchet rod 17 rotates forwards and backwards periodically to control the ratchets 14 and the single-tooth bolts 15 at different odd-even positions to be meshed, when the ratchets rotate forwards, all the ratchets 14 rotate clockwise, the ratchets 14 at odd-numbered positions drive the meshed single-tooth bolts 15 to move upwards, then the other side of the ratchets passes through the double-ring heddles 16 of the warp-wise carbon fiber yarns to move downwards to drive the warp-wise carbon fiber yarns at odd-numbered positions to move downwards, and meanwhile, because all the ratchets 14 rotate clockwise, the ratchets 14 at even-numbered positions cannot be meshed with the single-tooth bolts 15, the single-tooth bolts 15 and the double-ring heddles 16 at even-numbered positions do not move, so that two adjacent warp-wise carbon fiber yarns can be positioned on different horizontal planes; when the warp yarns are reversely rotated, the double-ring heddles 16 at odd positions do not move, and the double-ring heddles 16 at even positions move downwards to drive the warp-wise carbon fiber yarns at even positions to move downwards;
the double-ring heddle 16 moves up and down, so that two adjacent warp carbon fiber wires are positioned on different horizontal planes when the warp carbon fiber wires are conveyed forwards;
and 4, step 4: the swinging disc 10 drives the rack rod 12 to transversely move back and forth, the hydraulic clamping jaw 7 clamps the weft-wise carbon fiber yarns at the swinging starting point of the rack rod 12, the rack rod 12 drives the hydraulic clamping jaw 7 to insert the weft-wise carbon fiber yarns among the warp-wise carbon fiber yarns, the hydraulic clamping jaw 7 loosens the weft-wise carbon fiber yarns at the swinging ending point of the rack rod 12, the rack rod 12 drives the hydraulic clamping jaw 7 to return to the swinging starting point of the rack rod 12, and the mini circular saw 8 cuts the weft-wise carbon fiber yarns;
and 5: repeating the step 2-4, and performing alternate weaving on the weft carbon fiber yarns and the warp carbon fiber yarns in a reciprocating manner, and performing cyclic and reciprocating weaving to process the carbon fiber cloth;
step 6: the woven carbon fiber cloth is sent to a station below the cutter-taking extrusion forming structure through a discharge hole by a blower;
and 7: the tool magazine rotates, selecting a suitable forming tool 19; the tool taking clamp claw 23 moves forwards, the front end of the tool taking clamp claw 23 is inserted into a wedge-shaped hole 25 of the forming tool 19, the tool taking clamp claw 23 moves backwards, and the forming tool 19 is installed on the lifting table 24; the hydraulic cylinder 21 continuously operates to drive the lifting platform 24 to move up and down, the forming cutter 19 performs multiple extrusion forming on multiple layers of carbon fiber cloth, and when the number of the carbon fiber cloth layers reaches the required number, a semi-finished product of the carbon fiber felt pad is manufactured;
and 8: moving the semi-finished carbon fiber felt pad to a station below the cutting and shaping mechanism for positioning; the cutting and shaping mechanism starts to work, the working path of the shaping milling cutter 30 is controlled, and the shape of the semi-finished carbon fiber felt pad is trimmed; and obtaining a finished product of the carbon fiber felt pad.
Claims (2)
1. The carbon fiber felt pad weaving and extruding integrated forming machine for the aircraft engine hoop is characterized by comprising a weaving machine module, an extruding and cutting module and a base, wherein the weaving machine module and the extruding and cutting module are fixedly arranged on the base;
the knitting machine module comprises a warp-wise wire supply structure, a weft-wise wire supply structure, a heald knitting structure and a machine body;
the machine body comprises a bottom plate, two side walls, a plurality of long rods and a discharge plate, wherein the bottom plate is fixedly arranged on the base, the two side walls are symmetrically and vertically fixedly arranged on two sides of the bottom plate, the plurality of long rods are fixedly arranged on the bottom plate in rows, and the discharge plate is fixedly arranged in front of the bottom plate; a blower is arranged on the side wall, and an air outlet pipeline of the blower is arranged on the rear side of the discharging plate;
the warp-wise wire supply structure comprises carbon fiber wire drums, a driving clamping wheel, a driven clamping wheel and a first stepping motor, wherein the carbon fiber wire drums are arranged on the long rods, and warp-wise carbon fiber wires are wound on the carbon fiber wire drums; the driving clamping wheel and the driven clamping wheel are arranged between the two side walls of the machine body, the two sides of the driving clamping wheel and the two sides of the driven clamping wheel are respectively fixed on the side walls, and the driving clamping wheel and the driven clamping wheel are meshed together through a gear; the first stepping motor is fixedly arranged outside the side wall, and one end of the driving clamping wheel is connected with the first stepping motor; the warp-wise carbon fiber filaments pass through the space between the driving clamping wheel and the driven clamping wheel and are clamped by the driving clamping wheel and the driven clamping wheel;
the weft-wise wire supply structure comprises a weft-wise reciprocating mechanism, a hydraulic clamping jaw and a mini circular saw;
the weft reciprocating mechanism comprises a fixed seat, a swinging disc, a sector gear swinging belt groove guide rod, a rack rod and a weft box; the fixed seat is arranged outside the side wall and fixedly installed on the base, the swing disc is installed above the fixed seat and connected with a second stepping motor, a raised cylindrical rod is arranged on the swing disc and matched and positioned with a guide rod groove of a sector gear swing groove guide rod, a sector gear below the sector gear swing groove guide rod is meshed with the rack rod, and the rack rod is installed on the fixed seat through two buckles; the weft box is arranged on the side wall and is provided with a feeding hole and a discharging hole for weft carbon fiber yarns;
the hydraulic clamping jaw and the latitudinal reciprocating mechanism are respectively positioned at two sides of the side wall; the hydraulic clamping jaw is used for clamping and placing weft-wise carbon fiber yarns;
the mini circular saw is installed on the bottom plate, is positioned below the hydraulic clamping jaw and is extended out from the side of the discharging plate; the mini circular saw is used for cutting off weft-wise carbon fiber yarns;
the heddle weaving structure comprises a ratchet wheel, a ratchet rod, a long perforated plate, two groove rods, a single-tooth bolt and a double-ring heddle, wherein the ratchet rod, the long perforated plate and the two groove rods are arranged between two side walls of the machine body; the plurality of ratchet wheels are fixedly arranged on the ratchet wheel rod at equal intervals, and the tooth shapes of two adjacent ratchet wheels are opposite in direction; the through hole on the long plate with the hole corresponds to the ratchet wheel in position, the single-tooth bolt is arranged at the through hole of the long plate with the hole in a sliding fit manner, the gear teeth of the single-tooth bolt are meshed with the ratchet wheel, and the gear teeth of two adjacent single-tooth bolts face opposite directions; the groove rods are provided with a plurality of grooves at equal intervals, one ring of the double-ring heddle is sleeved on the single-tooth bolt, the double-ring heddle bypasses the grooves of the two groove rods, and the other ring of the double-ring heddle is suspended in front of the machine body and is used for sleeving a warp-wise carbon fiber wire;
the extrusion molding cutting module comprises a portal frame, an extrusion molding mechanism and a cutting and shaping mechanism;
the portal frame is arranged on the base;
the extrusion forming mechanism comprises a tool magazine and a tool taking extrusion forming structure, the tool magazine comprises a tool rest, a forming tool, a hook claw and a stepping motor III, a transverse support plate is arranged on the portal frame, the tool rest and the stepping motor III are respectively arranged on two sides of the transverse support plate, and the stepping motor is used for driving the tool rest to rotate; the tool rest is of a cubic frame structure, and four molded surfaces of the tool rest are provided with first hook claws and first slide rails;
the periphery of a cutter head of the forming cutter is provided with cutting blades, the center of the cutter head is provided with a pressure head, the side wall of the forming cutter is provided with three flat holes and four wedge-shaped holes, and the forming cutter is provided with a sliding chute; four forming cutters with different specifications are respectively placed on four molded surfaces of the cutter rest through matching of the sliding grooves and the sliding rails, and the hook claws are inserted into the flat holes to fix the forming cutters;
the cutter taking extrusion forming structure comprises a hydraulic cylinder, a fixed support, a cutter taking clamping jaw and a lifting table, wherein the fixed support is fixedly arranged on the base, the lifting table is connected and arranged with the fixed support in a sliding manner, the hydraulic cylinder is arranged between the fixed support and the lifting table and used for driving the lifting table to move up and down, the cutter taking clamping jaws are respectively arranged on two sides of the lifting table in a sliding manner, the cutter taking clamping jaws are driven to move transversely through an electric push rod, and the front end size of each cutter taking clamping jaw is in interference fit with the wedge-shaped hole; two sides of the lifting platform are provided with second sliding rails which are used for being matched with the sliding grooves of the forming cutter;
the cutting and shaping mechanism comprises an X-direction sliding rail, a Y-direction sliding rail, an X-direction sliding block, a Y-direction sliding block, a first gear, a first rack, a second gear, a second rack, a cutter module, a shaping milling cutter and a screw rod, wherein the X-direction sliding rail and the first rack are arranged above the portal frame, the X-direction sliding block and the X-direction sliding rail are installed in a matched mode, the first gear is arranged at the bottom of the X-direction sliding block and meshed with the first rack, and a stepping motor is arranged on the X-direction sliding block and used for driving the first gear; a Y-direction sliding rail and a second rack are arranged above the two X-direction sliding blocks, the Y-direction sliding blocks are installed in a matched mode with the Y-direction sliding rails, a second gear is arranged at the bottom of each Y-direction sliding block and meshed with the second rack, and a fifth stepping motor is arranged on each Y-direction sliding block and used for driving the second gear; the tool module is connected with the Y-direction sliding block in a sliding mode, the screw rod is connected with the Y-direction sliding block in a rotating mode, a nut is arranged in the tool module and sleeved with the screw rod, a stepping motor six used for driving the screw rod is arranged on the Y-direction sliding block, the trimming milling cutter is installed on the tool module, and a push-pull motor used for driving the trimming milling cutter is arranged on the tool module.
2. Use of a machine for weaving and extruding a carbon fibre felt for aircraft engine clips according to claim 1, characterised in that it comprises the following steps:
step 1: the warp-wise carbon fiber wires are inserted into the rings of the double-loop heddles suspended in front of the machine body through the space between the driving clamping wheel and the driven clamping wheel; penetrating the weft carbon fiber into a weft box and conveying the weft carbon fiber to the position of a hydraulic clamping jaw; starting a first stepping motor, a second stepping motor and a rotating motor;
step 2: the driving clamping wheel rolls to drive the driven clamping wheel to tension and rotate, and pulls a plurality of warp-wise carbon fiber yarns to be pulled out from the carbon fiber yarn drum, and the carbon fiber yarns are tensioned and discharged;
and 3, step 3: the ratchet rod rotates forwards and reversely periodically to drive the double-ring heddles on the single-tooth bolt to move up and down, so that two adjacent warp-wise carbon fiber wires are positioned on different horizontal planes when the warp-wise carbon fiber wires are conveyed forwards;
and 4, step 4: the swing disc drives the rack rod to transversely move back and forth, the hydraulic clamping jaw clamps the weft-wise carbon fiber filaments at the starting point of the swing of the rack rod, the rack rod drives the hydraulic clamping jaw to insert the weft-wise carbon fiber filaments among the warp-wise carbon fiber filaments, the hydraulic clamping jaw loosens the weft-wise carbon fiber filaments at the end point of the swing of the rack rod, the rack rod drives the hydraulic clamping jaw to return to the starting point, and the mini circular saw cuts the weft-wise carbon fiber filaments;
and 5: repeating the step 2-4, and carrying out cross weaving on the weft carbon fiber yarns and the warp carbon fiber yarns in a reciprocating and inserting manner, and processing into carbon fiber cloth by circularly and repeatedly weaving;
step 6: the woven carbon fiber cloth is sent to a station below the cutter-taking extrusion forming structure through a discharge hole by a blower;
and 7: rotating the tool magazine to select a suitable forming tool; the tool taking clamp claw moves forwards, the front end of the tool taking clamp claw is inserted into a wedge-shaped hole of the forming tool, the tool taking clamp claw moves backwards, and the forming tool is installed on the lifting table; the hydraulic cylinder continuously operates to drive the lifting table to move up and down, the forming cutter performs multiple extrusion forming on multiple layers of carbon fiber cloth, and when the number of the carbon fiber cloth layers reaches the required number, a semi-finished product of the carbon fiber felt pad is prepared;
and 8: moving the semi-finished carbon fiber felt pad to a station below the cutting and shaping mechanism for positioning; the cutting and shaping mechanism starts to work, the working path of the shaping milling cutter is controlled, and the shape of the semi-finished carbon fiber felt pad is trimmed; and obtaining a finished product of the carbon fiber felt pad.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110695757.7A CN113463247B (en) | 2021-06-23 | 2021-06-23 | Carbon fiber felt pad weaving and extruding integrated forming machine for aircraft engine hoop and using method of carbon fiber felt pad weaving and extruding integrated forming machine |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110695757.7A CN113463247B (en) | 2021-06-23 | 2021-06-23 | Carbon fiber felt pad weaving and extruding integrated forming machine for aircraft engine hoop and using method of carbon fiber felt pad weaving and extruding integrated forming machine |
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| CN113463247A CN113463247A (en) | 2021-10-01 |
| CN113463247B true CN113463247B (en) | 2022-07-19 |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN212193296U (en) * | 2020-05-22 | 2020-12-22 | 深圳市诚达碳纤维科技有限公司 | Carbon fiber plate processing device |
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| CN103628224A (en) * | 2013-12-10 | 2014-03-12 | 天津昂林贸烽高新材料有限公司 | Broad-width carbon-fiber knitting machine and method for producing carbon-fiber gridding cloth by using same |
| DE102019123127A1 (en) * | 2019-08-28 | 2021-03-04 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Semi-finished product, fiber composite component and process for its production |
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