CN101418840A - C/C composite material brake disc seam spreading method - Google Patents
C/C composite material brake disc seam spreading method Download PDFInfo
- Publication number
- CN101418840A CN101418840A CNA200810236194XA CN200810236194A CN101418840A CN 101418840 A CN101418840 A CN 101418840A CN A200810236194X A CNA200810236194X A CN A200810236194XA CN 200810236194 A CN200810236194 A CN 200810236194A CN 101418840 A CN101418840 A CN 101418840A
- Authority
- CN
- China
- Prior art keywords
- seam
- shop
- brake disc
- laying
- slit
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 17
- 238000000034 method Methods 0.000 title claims abstract description 12
- 238000003892 spreading Methods 0.000 title claims description 6
- 239000000835 fiber Substances 0.000 claims abstract description 27
- 239000004744 fabric Substances 0.000 claims abstract description 25
- 238000012360 testing method Methods 0.000 claims abstract description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 26
- 229910052799 carbon Inorganic materials 0.000 claims description 26
- 238000013461 design Methods 0.000 claims description 7
- 238000012545 processing Methods 0.000 claims description 7
- 238000005457 optimization Methods 0.000 claims description 3
- 229910052768 actinide Inorganic materials 0.000 claims description 2
- 150000001255 actinides Chemical class 0.000 claims description 2
- 238000011156 evaluation Methods 0.000 claims description 2
- 230000008676 import Effects 0.000 claims description 2
- 238000002360 preparation method Methods 0.000 claims description 2
- 230000003678 scratch resistant effect Effects 0.000 claims 1
- 238000005520 cutting process Methods 0.000 abstract description 5
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 238000004458 analytical method Methods 0.000 abstract description 2
- 229920000049 Carbon (fiber) Polymers 0.000 abstract 2
- 239000004917 carbon fiber Substances 0.000 abstract 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 abstract 2
- 238000003754 machining Methods 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 6
- 238000000465 moulding Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000003763 carbonization Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000002783 friction material Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
Images
Landscapes
- Braking Arrangements (AREA)
Abstract
Disclosed is a method for laying slit of C/C composite material brake disk, belonging to the technical field of composite material forming. Firstly, preparing the single direction C/C composite material and analyzing the wear resistance performance to obtain the optimal slit laying direction for laying fiber under working environment, thereby making the fiber slit laying track and compiling slit laying motion control codes; the analyzing the prefabricated slit laying brake disk, cutting carbon fiber cloth sheets into fan-shaped sheets according to the radial arc on the designed brake disk, arranging these carbon fiber cloth sheets in ring shape on an automatic slit laying equipment, then machining the laying slit; and performing stand test and performance analysis for the test piece to perform optimized improvement. The method reduces the manufacturing cost, and promotes the market competition of the brake disk and related technical products.
Description
Technical field
Technical field of composite material molding.
Technical background
States such as external English, U.S., method almost are used for the C/C composite material aeroplane brake discs simultaneously at late 1960s, the beginning of the seventies, progressively substituted metal and common friction material become state-of-the-art brake material at present.Mainly contain five big manufacturer production C/C composite material brake discs in the world today, they are respectively American AB S (Aircraft Braking System) company, ALS (Aircraft Landing Systems) company, B.F.Goodrich company, French Mes sier-Bugatti company, Britain Dunlop company, and three states, five major companies have monopolized the international market of C/C composite material brake disc; C/C composite preform technology and carbonization also are the proprietary technology of each company oneself, and core technology rarely has open report.Domesticly develop the C/C composite material brake disc since the end of the seventies in last century, enter the nineties, China adopts the brake disc of pin felt method development to come into operation, and the performance performance is good; But the brake disc expense that adopts pin felt manufactured is compared external brake disc cost competitiveness deficiency than higher.
Summary of the invention
C/C composite material brake disc seam spreading method of the present invention is intended to seek a kind of new brake disc precast body manufacture method and reduces manufacture cost, promotes the market competitiveness of brake disc and relative technological products.
By Fig. 1 the present invention program is described, at first carries out the preparation of unidirectional C/C composite material, these goods are carried out off-axis friction-wear test and finite element analysis; Draw its shop seam direction, performance and the shop seam mechanism of environment lower berth seam fiber under arms, thereby formulate the fiber Topology Optimization Method.
Then shop seam brake disc precast body is analyzed,, the carbon fibre cloth sheet is cut into fanning strip, make all fanning strips can be combined into a ring that meets the brake disc profile according to actinoid arc on the design brake disc; These carbon fibre cloth sheets are arranged in ring on the seam equipment of shop automatically, are adjusting shop seam initial position, spreading seam processing then.
Test specimen is carried out stand test and performance evaluation, fan plate shape optimization on the brake disc is improved, analyze the brake disc design method under the different operating modes, and provide the shop tailor codes and standards of planting.Fan the stitching track of chip architecture and shop seam fiber according to brake disc and work out automatic shop seam control software, the automatic shop of importing seam equipment is spread seam processing then.
The present invention is as the next-generation technology of pin felt manufactured brake disc technology, simple to operate, easy control can produce high-performance C/C composite material brake disc, and added value can improve more than 10%, the easier international high-end C/C composite material brake disc market of squeezing into has extraordinary industrialization prospect.
Description of drawings
Fig. 1, shop seam technology implementation block diagram.
Fig. 2, fan-shaped carbon cloth annulus and shop seam trajectory diagram.
Fig. 3, fan-shaped carbon cloth sheet schematic representation.
Fig. 4, fan-shaped carbon cloth sheet fiber direction schematic representation.
Fig. 5, shop seam apparatus sketch.
Number in the figure title: 1, fan-shaped carbon cloth sheet, 2, the carbon cloth seam, 3, shop seam track, 4, fiber direction one, 5, fiber direction two, 6, precast body, 7, turning axle, 8, the Y linear motion axis, 9, the X linear motion axis, 10, frame.
Embodiment
Embodiment one: present embodiment is described in conjunction with Fig. 1, Fig. 2, Fig. 3 and Fig. 5, present embodiment is by fan-shaped carbon cloth sheet 1, carbon cloth seam 2, shop seam track 3, fiber direction 1, fiber direction 25, precast body 6, turning axle 7, Y linear motion axis 8, X linear motion axis 9 and frame 10 are formed, and wherein all travel axiss and precast body 6 all assemble or be clamped on the frame 10.At the carbon cloth of same shape, be combined into circularly, design different shop seam track, test respectively under the environment under arms after the moulding, determine optimum shop seam track; Fan sheet shape 1 by designing requirement at different carbon cloths, see Fig. 3, fanning strip is arranged in ring shown in Figure 2, seam 2 circumferentially evenly arranges between the assurance fanning strip, and programming design lathe shop seam track 3, ring precast body 6 is clamped on the seam machine of automatic shop, sees Fig. 5, import shop seam machine control routine, find shop seam initial position accurately, spread seam processing, carry out stand test after the moulding, determine that optimum carbon cloth is fan-shaped; According to the optimum shop of optimum carbon cloth shaped design seam track, spread the seam fabricated product at last.
Embodiment two: present embodiment is described in conjunction with Fig. 1, Fig. 2, Fig. 3, Fig. 4 and Fig. 5, present embodiment is by fan-shaped carbon cloth sheet 1, carbon cloth seam 2, shop seam track 3, fiber direction 1, fiber direction 25, precast body 6, turning axle 7, Y linear motion axis 8, X linear motion axis 9 and frame 10 are formed, and wherein all travel axiss and precast body 6 all assemble or be clamped on the frame 10.When becoming fan sheet shape 1 at different fiber direction cutting carbon cloths by designing requirement, the fiber direction difference of carbon cloth, its stressed ability difference that is rubbed is carried out the cutting carbon cloth according to fiber direction 4, spreads seam processing then.All the other steps are identical with mode of execution one with operation.
Embodiment three: present embodiment is described in conjunction with Fig. 1, Fig. 2, Fig. 3, Fig. 4 and Fig. 5, present embodiment is by fan-shaped carbon cloth sheet 1, carbon cloth seam 2, shop seam track 3, fiber direction 1, fiber direction 25, precast body 6, turning axle 7, Y linear motion axis 8, X linear motion axis 9 and frame 10 are formed, and wherein all travel axiss and precast body 6 all assemble or be clamped on the frame 10.When becoming fan sheet shape 1 at different fiber direction cutting carbon cloths by designing requirement, the fiber direction difference of carbon cloth, its stressed ability difference that is rubbed is carried out the cutting carbon cloth according to fiber direction 5, spreads seam processing then.All the other steps are identical with mode of execution one with operation.
Claims (1)
1. C/C composite material brake disc seam spreading method is characterized in that may further comprise the steps:
At first carry out the preparation of unidirectional C/C composite material, these goods are carried out the off-axis friction-wear test, and analyze its scratch-resistant performance by finite element analysis software; Draw its optimum shop seam direction of environment lower berth seam fiber under arms, thereby formulate fiber lay down seam track, and establishment shop seam motion control code;
Then shop seam brake disc precast body is analyzed,, the carbon fibre cloth sheet is cut into fanning strip, make all fanning strips can be combined into a ring that meets the brake disc profile according to actinoid arc on the design brake disc; These carbon fibre cloth sheets are arranged in ring on the seam equipment of shop automatically, are adjusting shop seam initial position, spreading seam processing then;
Test specimen is carried out stand test and performance evaluation, fan plate shape optimization on the brake disc is improved, analyze the fan-shaped design method of brake disc carbon cloth under the different operating modes; Stitching track according to brake disc fan chip architecture and shop seam fiber is worked out shop seam control program automatically, imports automatic shop seam equipment then and spreads seam processing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200810236194XA CN101418840B (en) | 2008-11-26 | 2008-11-26 | C/C composite material brake disc seam spreading method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200810236194XA CN101418840B (en) | 2008-11-26 | 2008-11-26 | C/C composite material brake disc seam spreading method |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101418840A true CN101418840A (en) | 2009-04-29 |
CN101418840B CN101418840B (en) | 2010-06-09 |
Family
ID=40629784
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN200810236194XA Active CN101418840B (en) | 2008-11-26 | 2008-11-26 | C/C composite material brake disc seam spreading method |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101418840B (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102152555A (en) * | 2010-11-01 | 2011-08-17 | 陕西蓝太航空设备有限责任公司 | Annular preform for manufacturing carbon/carbon composite material brake disc and knitting process method thereof |
CN110483086A (en) * | 2019-08-28 | 2019-11-22 | 山东道普安制动材料有限公司 | A kind of preparation method of carbon pottery brake disc |
CN111216266A (en) * | 2019-12-04 | 2020-06-02 | 中航复合材料有限责任公司 | Preparation method of three-dimensional fiber preform based on fiber seam laying process |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3605968A (en) * | 1969-09-18 | 1971-09-20 | Goodrich Co B F | Segmented friction member for brake or clutch |
CN100373071C (en) * | 2004-11-18 | 2008-03-05 | 陕西蓝太航空设备有限责任公司 | Carbon/carbon composite material brake disc bonding process |
-
2008
- 2008-11-26 CN CN200810236194XA patent/CN101418840B/en active Active
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102152555A (en) * | 2010-11-01 | 2011-08-17 | 陕西蓝太航空设备有限责任公司 | Annular preform for manufacturing carbon/carbon composite material brake disc and knitting process method thereof |
CN102152555B (en) * | 2010-11-01 | 2014-06-04 | 陕西蓝太航空设备有限责任公司 | Annular preform for manufacturing carbon/carbon composite material brake disc and knitting process method thereof |
CN110483086A (en) * | 2019-08-28 | 2019-11-22 | 山东道普安制动材料有限公司 | A kind of preparation method of carbon pottery brake disc |
CN110483086B (en) * | 2019-08-28 | 2022-07-05 | 山东道普安制动材料有限公司 | Preparation method of carbon-ceramic brake disc |
CN111216266A (en) * | 2019-12-04 | 2020-06-02 | 中航复合材料有限责任公司 | Preparation method of three-dimensional fiber preform based on fiber seam laying process |
Also Published As
Publication number | Publication date |
---|---|
CN101418840B (en) | 2010-06-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN101418840B (en) | C/C composite material brake disc seam spreading method | |
CN106001570B (en) | A kind of integrated 3D laser printing multicompartment preparation method | |
CN106624727A (en) | Semi-automatic rotary riveting fixture and riveting method thereof | |
CN106715045A (en) | Apparatus and method for machining a workpiece | |
CN1962145A (en) | Method for processing blade form work piece and fittings dedicated therefor | |
CN107014609A (en) | A kind of main spindle box fatigue tester and main spindle box method for testing reliability | |
CN111168195B (en) | IPv 6-based electric welding machine cluster monitoring control method | |
CN105867308B (en) | A kind of sheet metal component rapid development system based on precision controlling | |
CN103389704B (en) | Based on the establishment gypsum block forming production line method of Petri network control flow modeling | |
CN107918359A (en) | The digital control processing macroprogram and automatic generating software of a exposed semiellipsoid | |
CN214137415U (en) | Double-station automatic wire laying forming machine tool | |
CN107414428B (en) | The manufacturing process of ultra-large type fission ring | |
CN105468849A (en) | Aircraft weight control method | |
CN202952118U (en) | Tool setting system of Z direction main shafts of multi-Z-shaft numerical control machine tool | |
CN103913653A (en) | Automatic line-drawing testing system of optical mouse | |
CN204235207U (en) | A kind of operation clamp for machining | |
CN206393165U (en) | A kind of semi-automatic rotary riveting tool | |
CN113844078A (en) | Preparation method of ultra-light multi-feature skin-free framework type composite shell | |
CN210309137U (en) | One-time method mechanical drum for small spare tire | |
CN107378561A (en) | One kind is used for undercarriage toggle part by numerical control clamp for machining structure and its application method | |
CN210703896U (en) | Gear shaper tool setting appearance | |
CN109252299B (en) | Car seat is with backing carpet sewing preparation frock | |
CN202943791U (en) | Mould structure convenient for replacing mould core | |
CN208247003U (en) | A kind of precise positioning structure of die-cutting mould | |
CN106444641A (en) | Combined woodworking processing equipment with independent A/D (analog/digital) conversion module |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant |