CN102950774A - Integral manufacturing process for enhancement layer at root end of fan blade and mold - Google Patents

Integral manufacturing process for enhancement layer at root end of fan blade and mold Download PDF

Info

Publication number
CN102950774A
CN102950774A CN2012104760955A CN201210476095A CN102950774A CN 102950774 A CN102950774 A CN 102950774A CN 2012104760955 A CN2012104760955 A CN 2012104760955A CN 201210476095 A CN201210476095 A CN 201210476095A CN 102950774 A CN102950774 A CN 102950774A
Authority
CN
China
Prior art keywords
enhancement layer
support frame
inner support
layer
butt
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
Application number
CN2012104760955A
Other languages
Chinese (zh)
Other versions
CN102950774B (en
Inventor
怀涛
顾从进
葛小飞
李秀凯
成海娃
卢洋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Air Damper Power Technology Co Ltd Kunshan China
Original Assignee
Air Damper Power Technology Co Ltd Kunshan China
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Air Damper Power Technology Co Ltd Kunshan China filed Critical Air Damper Power Technology Co Ltd Kunshan China
Priority to CN201210476095.5A priority Critical patent/CN102950774B/en
Publication of CN102950774A publication Critical patent/CN102950774A/en
Application granted granted Critical
Publication of CN102950774B publication Critical patent/CN102950774B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention relates to the field of wind power generation blades, in particular to an integral manufacturing process for an enhancement layer at the root end of a fan blade, and a mold. The integral manufacturing process comprises the following steps of: (1) paving and pre-curing an upper shell of a blade which is free from an enhancement layer; (2) paving other cloth layers of a lower shell except the enhancement layer; (3) paving a vacuum bag film and a diversion material on an inner support frame provided with a gap, paving enhancement layers of upper and lower molds, and leaving abutment joints of the cloth layers in the gap of the inner support frame; (4) hoisting an inner support frame which is finally obtained in the step (3) at the root end of the lower mold; (5) performing butted joint on the cloth layers of the enhancement layers in sequence in the gap of the inner support frame; and (6) matching the molds, and performing vacuum infusion. The enhancement layers at the root ends of the upper and lower half molds of the blade are infused together, so that mold matching seams are avoided, and the root end strength is high.

Description

Fan blade butt enhancement layer integral production technique and mould
?
Technical field
The present invention relates to the wind power generation blade field, be specifically related to a kind of fan blade butt enhancement layer integral production technique and mould.
 
Background technology
The bolt that blade pass is crossed butt links to each other with wheel hub, and the operating stressed strong point of blade is at butt, so the stressed maximum of butt is the highest to requirement of strength.Divide female die respectively after the moulding but traditional blade production technology pattern is blade, by matched moulds behind the coating bonded adhesives upper female die is integrated again.Because adopted the secondary bonding forming, often there are the problems such as bonding plane too highly needs polishing, adhesive surface to cross low to be inconvenient to bond, the extra reinforcement of bonding plane needs.The present invention makes upper and lower radical of semimodules end enhancement layer realize common perfusion by changing traditional work pattern, and it is as a whole that butt becomes, thereby avoided the matched moulds seam, just do not had traditional defective.
 
Summary of the invention
Technical purpose of the present invention is to overcome the problems of the prior art, provides a kind of upper and lower half module butt enhancement layer of blade that makes to realize jointly pouring into, avoiding fan blade butt enhancement layer integral production technique and the mould that matched moulds stitches, butt intensity is high.
For realizing purpose of the present invention, the technical solution used in the present invention is: fan blade butt enhancement layer integral production technique comprises the steps: 1) finish laying, precuring without enhancement layer blade upper shell; 2) lower house is finished the laying of all the other layer of cloths except enhancement layer; 3) after containing inner support frame laying vacuum bag film jaggy and water conservancy diversion material, successively lay the enhancement layer of upper and lower mould and the enhancement layer of patrix, the carvel joint of layer of cloth stays the indentation, there in inner support frame; 4) inner support frame that step (3) is finally obtained is lifted on the counterdie butt; 5) in the indentation, there of inner support frame, the layer of cloth of enhancement layer is pressed a layer butt up; 6) matched moulds is implemented priming by vacuum.
For realizing purpose of the present invention, another technical solution used in the present invention is: fan blade butt enhancement layer integral production mould, comprise mould for blade forming, precuring and without the blade upper shell of enhancement layer, it is characterized in that: also comprise containing inner support frame jaggy, also comprise the vacuum bag film, the enhancement layer that are layed in successively on the inner support frame, the carvel joint of layer of cloth stays the indentation, there in inner support frame; Inner support frame is lifted on the counterdie butt.
Aforesaid fan blade butt enhancement layer integral production mould, the blade upper shell is without enhancement layer.
Prerequisite of the present invention is an existing patrix housing (containing enhancement layer) of finishing without the precuring of enhancement layer, counterdie is except the layer of cloth of butt enhancement layer, all the other layer of cloth normal layings, be layed on the inner support frame by technological requirement according to the difference of the internal-and external diameter layer of cloth with enhancement layer, then inner support frame and cloth are lifted to the counterdie butt, lay vacuum material, realize common perfusion with counterdie behind the matched moulds, make the upper and lower half module butt enhancement layer of blade realize common perfusion, avoid the matched moulds seam, butt intensity is high.
 
Description of drawings
Fig. 1 is the schematic diagram of fan blade butt enhancement layer integral production technique of the present invention;
Wherein, 1 mould, 2 housings without enhancement layer, 3 enhancement layers, 4 vacuum bag films, 5 inner support frames.
 
The specific embodiment
Below in conjunction with accompanying drawing the embodiment of the invention is described in detail: present embodiment is to implement under the prerequisite in technical solution of the present invention, provided detailed embodiment and concrete operating process, but protection scope of the present invention is not limited to following embodiment.
Referring to Fig. 1, the step of manufacture craft of the present invention is: 1) finish laying, precuring without the upper shell of enhancement layer, without the housing 2 of enhancement layer; 2) counterdie is finished the laying of all the other layer of cloths except enhancement layer 3; 3) after inner support frame 5 lays vacuum bag film 4 and water conservancy diversion material, the layer of cloth of the enhancement layer 3 of upper and lower mould 1 to be spread, the carvel joint of layer of cloth stays in the indentation, there of inner support frame 5; 4) will lift and the counterdie butt by technological requirement with the inner support frame 5 of layer of cloth; 5) in the indentation, there of inner support frame 5, the layer of cloth of enhancement layer 3 is pressed a layer butt up; 6) matched moulds is finished all the other vacuum operations; 7) after vacuum condition meets the requirements, perfusion.
Fan blade butt enhancement layer integral production mould, comprise mould 1 for blade forming, precuring and without the blade upper shell of enhancement layer, it is characterized in that: also comprise containing inner support frame 5 jaggy, also comprise the vacuum bag film 4, the enhancement layer 3 that are layed in successively on the inner support frame 5, the carvel joint of layer of cloth stays in the indentation, there of inner support frame 5; Inner support frame 5 is lifted on the counterdie butt.
Prerequisite of the present invention is an existing patrix housing of finishing without the precuring of enhancement layer, counterdie is except the layer of cloth of butt enhancement layer, all the other layer of cloth normal layings, be layed on the inner support frame by technological requirement according to the difference of the internal-and external diameter layer of cloth with enhancement layer, then inner support frame and cloth lifted to the counterdie butt, lay vacuum material, realize common perfusion with counterdie behind the matched moulds, make the upper and lower half module butt enhancement layer of blade realize common perfusion, avoid the matched moulds seam, butt intensity is high.
More than show and described basic principle of the present invention, principal character and advantage of the present invention.The technical staff of the industry should understand; the present invention is not restricted to the described embodiments; that describes in above-described embodiment and the specification just illustrates principle of the present invention; without departing from the spirit and scope of the present invention; the present invention also has various changes and modifications, and these changes and improvements all fall in the claimed scope of the invention.The claimed scope of the present invention is defined by appending claims and equivalent thereof.

Claims (3)

1. fan blade butt enhancement layer integral production technique comprises the steps: 1) finish laying, precuring without enhancement layer blade upper shell; 2) lower house is finished the laying of all the other layer of cloths except enhancement layer; 3) after containing inner support frame laying vacuum bag film jaggy and water conservancy diversion material, lay the enhancement layer of upper and lower mould, the carvel joint of layer of cloth stays the indentation, there in inner support frame; 4) inner support frame that step (3) is finally obtained is lifted on the counterdie butt; 5) in the indentation, there of inner support frame, the layer of cloth of enhancement layer is pressed a layer butt up; 6) matched moulds is implemented priming by vacuum.
2. fan blade butt enhancement layer integral production mould, comprise mould for blade forming, precuring and without the blade upper shell of enhancement layer, it is characterized in that: also comprise containing inner support frame jaggy, also comprise the vacuum bag film, the enhancement layer that are layed in successively on the inner support frame, the carvel joint of layer of cloth stays the indentation, there in inner support frame; Inner support frame is lifted on the counterdie butt.
3. fan blade butt enhancement layer integral production mould according to claim 2, it is characterized in that: the blade upper shell is without enhancement layer.
CN201210476095.5A 2012-11-22 2012-11-22 Integral manufacturing process for enhancement layer at root end of fan blade and mold Expired - Fee Related CN102950774B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210476095.5A CN102950774B (en) 2012-11-22 2012-11-22 Integral manufacturing process for enhancement layer at root end of fan blade and mold

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210476095.5A CN102950774B (en) 2012-11-22 2012-11-22 Integral manufacturing process for enhancement layer at root end of fan blade and mold

Publications (2)

Publication Number Publication Date
CN102950774A true CN102950774A (en) 2013-03-06
CN102950774B CN102950774B (en) 2015-04-15

Family

ID=47760430

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210476095.5A Expired - Fee Related CN102950774B (en) 2012-11-22 2012-11-22 Integral manufacturing process for enhancement layer at root end of fan blade and mold

Country Status (1)

Country Link
CN (1) CN102950774B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104002486A (en) * 2014-04-30 2014-08-27 广东明阳风电产业集团有限公司 Method for hanging wind power generation blade trailing edge UD prefabricated member into main mold shell body laying layer

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101439559A (en) * 2008-12-22 2009-05-27 中材科技风电叶片股份有限公司 Heating layer and heating method of megawatt level wind-powered blade mold
CN202965220U (en) * 2012-11-22 2013-06-05 昆山华风风电科技有限公司 Integral manufacturing mould for root-end reinforcing layer of wind turbine blade

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101439559A (en) * 2008-12-22 2009-05-27 中材科技风电叶片股份有限公司 Heating layer and heating method of megawatt level wind-powered blade mold
CN202965220U (en) * 2012-11-22 2013-06-05 昆山华风风电科技有限公司 Integral manufacturing mould for root-end reinforcing layer of wind turbine blade

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104002486A (en) * 2014-04-30 2014-08-27 广东明阳风电产业集团有限公司 Method for hanging wind power generation blade trailing edge UD prefabricated member into main mold shell body laying layer
CN104002486B (en) * 2014-04-30 2016-04-13 广东明阳风电产业集团有限公司 Wind power generation blade trailing edge UD prefabricated component hangs in the method for main die housing laying

Also Published As

Publication number Publication date
CN102950774B (en) 2015-04-15

Similar Documents

Publication Publication Date Title
CN101905538B (en) Process for integrally manufacturing megawatt wind turbine blade
CN105128358A (en) Manufacturing method for wind power blade
CN103507277B (en) Improved method for layering of root of blade of wind driven generator
CN102756481B (en) Manufacturing method of carbon fiber girder for fan blade
CN103921457A (en) Method for manufacturing main beam or auxiliary beam of fan blade by unidirectional sheets manufactured by use of pultrusion process
CN102226446B (en) Method for preparing megawatt fan blade shear web and auxiliary bonding angle thereof
CN105346105B (en) The making mould and preparation method of a kind of wind electricity blade
CN105346100A (en) Method for manufacturing wind power blade crossbeam mold
CN102350801A (en) Method for bonding front edges of megawatt wind power generator blade in mold closing
CN106584886A (en) Process for controlling thickness of glued rubber layer by using self-made rubber cover plate
CN104325577A (en) Flanging mould, assembling mould, and paving method and moulding method of moulding material
CN106965456A (en) A kind of leafy composite propeller forming method
CN205185306U (en) Integral blade bonding angle mould utensil
CN104002402B (en) A kind of general web mold structure of wind electricity blade
CN102241140B (en) Reinforcing technology of blower fan blade inner edging die
CN202965220U (en) Integral manufacturing mould for root-end reinforcing layer of wind turbine blade
CN209141488U (en) A kind of rear edge of wind turbine blade bonding angle molding machine
CN106881879A (en) A kind of method that use second bonding technique manufactures adhesive bonding of composites structure
CN102950774A (en) Integral manufacturing process for enhancement layer at root end of fan blade and mold
CN102672978B (en) Technique for manufacturing blade of wind-driven generator
CN105128353B (en) Forming die of integrally solidified composite material stator blade, and tail rim coating method thereof
CN109203516A (en) A kind of manufacturing method of wind electricity blade
CN105150555A (en) Vacuum infusion processing method
CN210422886U (en) Fan blade trailing edge bonding structure
CN207172789U (en) A kind of wind electricity blade forming defect controls frock

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
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150415

Termination date: 20201122