CN203110205U - Mold for manufacturing propeller made of carbon fiber composite material - Google Patents

Mold for manufacturing propeller made of carbon fiber composite material Download PDF

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Publication number
CN203110205U
CN203110205U CN 201320047354 CN201320047354U CN203110205U CN 203110205 U CN203110205 U CN 203110205U CN 201320047354 CN201320047354 CN 201320047354 CN 201320047354 U CN201320047354 U CN 201320047354U CN 203110205 U CN203110205 U CN 203110205U
Authority
CN
China
Prior art keywords
mold
counterdie
patrix
upper mold
lower mold
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.)
Expired - Lifetime
Application number
CN 201320047354
Other languages
Chinese (zh)
Inventor
周利峰
吴基祥
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.)
Jiangsu Yueke New Material Co ltd
Original Assignee
SHANGHAI YUEKE COMPOSITE CO Ltd
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 SHANGHAI YUEKE COMPOSITE CO Ltd filed Critical SHANGHAI YUEKE COMPOSITE CO Ltd
Priority to CN 201320047354 priority Critical patent/CN203110205U/en
Application granted granted Critical
Publication of CN203110205U publication Critical patent/CN203110205U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

The utility model relates to a mold for manufacturing a propeller made of a carbon fiber composite material. The mold comprises an upper mold, a lower mold, a slide block, an overflow trough and a center shaft, wherein the upper mold and the lower mold are mutually fitted; the upper mold comprises a mold closing bolt, a vacuum pumping hole and a mold opening bolt which penetrate through the upper mold respectively; the slide block is arranged in the upper mold; the lower mold comprises a thread hole which penetrates through the lower mold, and the thread hole corresponds to the mold closing bolt in position; the overflow trough is formed in the fitting surface of the upper mold and the lower mold; the center shaft is arranged in the upper mold and the lower mold in a penetrating way, and an injection hole is further formed in the outer side of the center shaft; and O-shaped sealing rings are arranged between the upper mold and the lower mold and between the center shaft and the lower mold. The mold for manufacturing the propeller made of the carbon fiber composite material has the characteristics of good mechanical performance, small specific gravity, good toughness, impact resistance, small noises and corrosion resistance.

Description

Mould for the manufacture of the carbon fibre composite screw
Technical field
The utility model relates to a kind of mould for the manufacture of the carbon fibre composite screw.
Background technology
The screw of existing hull adopts metal casting or metal solder to make usually.Its weight is big, noise is big, be subjected to seriously corroded, the life-span is short.Along with the fast development of domestic carbon fibre composite is popularized.With the screw that carbon fibre composite is made, have in light weight, intensity is high, Rotation Noise is low, good toughness, shock-resistant, and stronger corrosion resistance ability is arranged.The spirality blade of novel carbon fiber composite adopts the steel die compacting, the dimensional accuracy height, and dynamic balancing is effective, production efficiency is high, is convenient to mass production.
The utility model content
The purpose of this utility model be to provide a kind of in light weight, intensity is high, good toughness, shock-resistant, the mould for the manufacture of the carbon fibre composite screw that noise is little.
For solving the problems of the technologies described above, the utility model comprises for the manufacture of the mould of carbon fibre composite screw: mutual patrix and counterdie of fitting; Wherein said patrix comprises the matched moulds bolt that is arranged in described patrix respectively, vacuumizes the hole and open the mould bolt; Slide block, described slide block are arranged in the described patrix; Described counterdie comprises the screwed hole that is arranged in described counterdie, and described screwed hole is corresponding with the position of described matched moulds bolt; Overflow launder, described overflow launder are arranged on the binding face of described patrix and described counterdie; And central shaft, described central shaft runs through and is arranged in described patrix and the described counterdie, also is provided with hand-hole in the outside of described central shaft.Between described patrix and the described counterdie, be provided with the O RunddichtringO between described central shaft and the described counterdie.
The utility model for the manufacture of the mould of carbon fibre composite screw have favorable mechanical performance, light specific gravity, good toughness, shock-resistant, noise is little, etch-proof characteristics.
Description of drawings
Fig. 1 is that the utility model is for the manufacture of the die cut view of carbon fibre composite screw.
The utility model is for the manufacture of description of reference numerals in the mould accompanying drawing of carbon fibre composite screw:
1-patrix 2-matched moulds bolt 3-slide block
4-central shaft 5-hand-hole 6-O RunddichtringO
7-opens mould bolt 8-screwed hole 9-and vacuumizes the hole
10-overflow launder 11-counterdie
The specific embodiment
Below in conjunction with accompanying drawing the mould of the utility model for the manufacture of the carbon fibre composite screw is described in further detail.
As shown in Figure 1, the utility model comprises for the manufacture of the mould of carbon fibre composite screw: mutual patrix 1 and counterdie 11 of fitting; Wherein patrix 1 comprises the matched moulds bolt 2 that is arranged in patrix 1 respectively, vacuumizes hole 9 and open mould bolt 7; Slide block 3, slide block 3 are arranged in the patrix 1; Counterdie 11 comprises the screwed hole 8 that is arranged in counterdie 11, and screwed hole 8 is corresponding with the position of matched moulds bolt 2; Overflow launder 10, overflow launder 10 are arranged on the binding face of patrix 1 and counterdie 11; And central shaft 4, central shaft 4 runs through and is arranged in patrix 1 and the counterdie 11, also is provided with hand-hole 5 in the outside of central shaft 4.Between patrix 1 and the counterdie 11, be provided with O RunddichtringO 6 between central shaft 4 and the counterdie 11.
Patrix 1, counterdie 11, slide block 3 link into an integrated entity by matched moulds bolt 2.Central shaft 4 is connected with upper and lower mould 11 interstitial holes.
At counterdie 11 O RunddichtringO 6 is arranged, be used for the sealing of upper and lower mould 11 matched moulds and use.Be provided with O RunddichtringO 6 at central shaft 4 two ends, be used for the sealing between central shaft 4 and the upper and lower mould 11.
The making of product is laid the carbon fibre material that has cut at counterdie 11, and twines at central shaft 4.
Patrix 1 and slide block 3 and counterdie 11 beginning matched moulds.Fastening bolt begins to vacuumize from vacuumizing hole 9.Reach certain vacuum, begin to inject resin from hand-hole 5.Unnecessary resin can overflow in the overflow launder 10 of counterdie 11, and is saturated to guarantee the resin in the product.Outer surface at product forms frp layer.
The demoulding: behind the products solidifying, unclamp the bolt of patrix 1, open and being connected of slide block 3.By opening mould bolt 7, patrix 1 is opened.Owing to due to the shape back-off of product, slide block 3 must be set, so that prevent can't the demoulding.Open slide block 3 separately, can take out product.
The utility model carbon fibre composite screw is made.Be characterized in: in light weight, intensity is high, anti-fire-retardant, good toughness, shock-resistant, Rotation Noise is low.Has stronger resistance to corrosion.The spirality blade of novel carbon fiber composite adopts the steel die compacting, the dimensional accuracy height, and dynamic balancing is effective, production efficiency is high, is convenient to mass production.
Below the preferred embodiment of the utility model having been created specifies, but the utility model is created and is not limited to embodiment, those of ordinary skill in the art also can make all modification that is equal to or replacement under the prerequisite of the invention spirit, the modification that these are equal to or replacement all are included in the application's claim institute restricted portion.

Claims (2)

1. for the manufacture of the mould of carbon fibre composite screw, it is characterized in that, comprise patrix and the counterdie of mutual applying; Wherein
Described patrix comprises the matched moulds bolt that is arranged in described patrix respectively, vacuumizes the hole and open the mould bolt;
Slide block, described slide block are arranged in the described patrix;
Described counterdie comprises the screwed hole that is arranged in described counterdie, and described screwed hole is corresponding with the position of described matched moulds bolt;
Overflow launder, described overflow launder are arranged on the binding face of described patrix and described counterdie; And
Central shaft, described central shaft run through and are arranged in described patrix and the described counterdie, also are provided with hand-hole in the outside of described central shaft.
2. the mould for the manufacture of the carbon fibre composite screw according to claim 1 is characterized in that, between described patrix and the described counterdie, be provided with the O RunddichtringO between described central shaft and the described counterdie.
CN 201320047354 2013-01-29 2013-01-29 Mold for manufacturing propeller made of carbon fiber composite material Expired - Lifetime CN203110205U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201320047354 CN203110205U (en) 2013-01-29 2013-01-29 Mold for manufacturing propeller made of carbon fiber composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201320047354 CN203110205U (en) 2013-01-29 2013-01-29 Mold for manufacturing propeller made of carbon fiber composite material

Publications (1)

Publication Number Publication Date
CN203110205U true CN203110205U (en) 2013-08-07

Family

ID=48890582

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201320047354 Expired - Lifetime CN203110205U (en) 2013-01-29 2013-01-29 Mold for manufacturing propeller made of carbon fiber composite material

Country Status (1)

Country Link
CN (1) CN203110205U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104149361A (en) * 2014-07-08 2014-11-19 常州神鹰碳塑复合材料有限公司 Two-time forming method for manufacturing carbon fiber composite material propeller
CN108501405A (en) * 2018-05-30 2018-09-07 安徽卓尔航空科技有限公司 A kind of annular excessive glue groove composite propeller compression molding die
CN112405954A (en) * 2020-11-06 2021-02-26 惠阳航空螺旋桨有限责任公司 Carbon fiber blade forming die and die opening method
CN114245769A (en) * 2019-08-22 2022-03-25 辛北尔康普机器及成套设备有限责任公司 Method for producing a structural element

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104149361A (en) * 2014-07-08 2014-11-19 常州神鹰碳塑复合材料有限公司 Two-time forming method for manufacturing carbon fiber composite material propeller
CN108501405A (en) * 2018-05-30 2018-09-07 安徽卓尔航空科技有限公司 A kind of annular excessive glue groove composite propeller compression molding die
CN108501405B (en) * 2018-05-30 2024-05-03 安徽劲旋风航空科技有限公司 Annular glue overflow groove composite material screw compression molding die
CN114245769A (en) * 2019-08-22 2022-03-25 辛北尔康普机器及成套设备有限责任公司 Method for producing a structural element
US12097974B2 (en) 2019-08-22 2024-09-24 Siempelkan Maschinen- und Anlagenbau GmbH Method for producing a structural component
CN112405954A (en) * 2020-11-06 2021-02-26 惠阳航空螺旋桨有限责任公司 Carbon fiber blade forming die and die opening method

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 201199 room E9, building 3302, No. 89, Xinbang Road, Minhang District, Shanghai

Patentee after: SHANGHAI YUEKE NEW MATERIALS Co.,Ltd.

Address before: 201199 room E9, building 3302, No. 89, Xinbang Road, Minhang District, Shanghai

Patentee before: SHANGHAI YUEKE COMPOSITE Co.,Ltd.

TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20211130

Address after: 224237 No. 75, Yingbin Road, Dongtai Coastal Economic Development Zone, Yancheng City, Jiangsu Province

Patentee after: JIANGSU YUEKE NEW MATERIAL Co.,Ltd.

Address before: 201199 room E9, building 3302, No. 89, Xinbang Road, Minhang District, Shanghai

Patentee before: SHANGHAI YUEKE NEW MATERIALS CO.,LTD.

CX01 Expiry of patent term
CX01 Expiry of patent term

Granted publication date: 20130807