CN204604663U - A kind of paddle molding mould - Google Patents
A kind of paddle molding mould Download PDFInfo
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- CN204604663U CN204604663U CN201520283909.2U CN201520283909U CN204604663U CN 204604663 U CN204604663 U CN 204604663U CN 201520283909 U CN201520283909 U CN 201520283909U CN 204604663 U CN204604663 U CN 204604663U
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Abstract
本实用新型属于机械加工类技术,特别涉及一种桨叶成型模具,解决现有模具出模时桨叶容易变形以及桨叶表面容易碰伤的问题。桨叶成型模具包括匹配的上模和下模,所述上模和下模相接处的面为分模面,在所述上模上沿竖直方向贯穿开设有至少四个螺纹孔,所述至少四个螺纹孔均匀分布在所述上模上相对的两个所述分模面上;每个所述螺纹孔内设有一根相匹配的启模螺栓,所述启模螺栓的长度大于所述上模的厚度。本实用新型的叶成型模具操作方便、工作量少且安全性能高,桨叶不容易变形且桨叶表面不容易碰伤,保证了桨叶的质量,提高了生产合格率。
The utility model belongs to the mechanical processing technology, and in particular relates to a paddle forming die, which solves the problems that the paddle is easily deformed and the surface of the paddle is easily damaged when the existing mold is released. The paddle forming mold includes a matching upper mold and a lower mold, the surface where the upper mold and the lower mold meet is a parting surface, and at least four threaded holes are vertically opened on the upper mold, so The at least four threaded holes are evenly distributed on the two opposite parting surfaces of the upper die; each threaded hole is provided with a matched mold opening bolt, and the length of the mold opening bolt is longer than The thickness of the upper mold. The blade forming mold of the utility model has the advantages of convenient operation, less workload and high safety performance, the blade is not easily deformed and the surface of the blade is not easily damaged, which ensures the quality of the blade and improves the qualified rate of production.
Description
技术领域technical field
本实用新型属于机械加工类技术,特别涉及一种桨叶成型模具。The utility model belongs to the mechanical processing technology, in particular to a paddle forming die.
背景技术Background technique
复合材料桨叶是直升机旋翼系统必不可少的零件产品,模具是制造生产复合材料桨叶的重要工装,模具的结构方式是决定复合材料桨叶是否合格的关键。Composite blade is an essential part of helicopter rotor system. Mold is an important tool for manufacturing composite blade. The structure of the mold is the key to determine whether the composite blade is qualified.
目前在国内直升机复合材料桨叶成型中,模具启模是一个往往被忽略的问题,导致桨叶在成型后启模比较困难,比较常用的方法是用强制的方式使上模和下模分开,这种启模方式操作困难,工作量大,危险系数大,而且在启模过程中容易导致桨叶变形和碰伤桨叶表面,从而降低了产品的合格率。At present, in the domestic helicopter composite material blade molding, the mold opening is a problem that is often ignored, which makes it difficult to open the blade after molding. The more common method is to separate the upper mold and the lower mold by force. This mode of mold opening is difficult to operate, the workload is large, and the risk factor is large, and it is easy to cause deformation of the blade and scratch the surface of the blade during the mold opening process, thereby reducing the qualified rate of the product.
实用新型内容Utility model content
本实用新型要解决的技术问题:提供一种桨叶成型模具,以解决现有模具出模时桨叶容易变形以及桨叶表面容易碰伤的问题。The technical problem to be solved by the utility model is to provide a paddle forming mold to solve the problems that the paddle is easily deformed and the surface of the paddle is easily scratched when the existing mold is released.
本实用新型的技术方案:Technical scheme of the utility model:
一种桨叶成型模具,包括匹配的上模和下模,所述上模和下模相接处的面为分模面,在所述上模上沿竖直方向贯穿开设有至少四个螺纹孔,所述四个螺纹孔均匀分布在所述上模上相对的两个所述分模面上;每个所述螺纹孔内设有一根相匹配的启模螺栓,所述启模螺栓的长度大于所述上模的厚度。A blade forming die, comprising a matching upper die and a lower die, the surface where the upper die and the lower die meet is a parting surface, and at least four screw threads are vertically penetrating on the upper die holes, the four threaded holes are evenly distributed on the two opposite parting surfaces of the upper mold; each threaded hole is provided with a matched mold bolt, and the mold bolt The length is greater than the thickness of the upper die.
可选地,所述下模的所述分模面上与至少四个所述螺纹孔相对应的位置处开设有至少四个柱状凹槽,所述凹槽的直径大于所述启模螺栓直径。Optionally, at least four columnar grooves are provided on the parting surface of the lower mold at positions corresponding to at least four of the threaded holes, and the diameter of the grooves is larger than the diameter of the opening bolts. .
可选地,所述螺纹孔包括四个,均匀分布在所述上模长度方向上的两个所述分模面上。Optionally, the threaded holes include four, which are evenly distributed on the two parting surfaces in the length direction of the upper die.
本实用新型的有益效果:本实用新型的桨叶成型模具,在上模具的两侧上设计四个螺栓孔,启模时上模通过模具上四个螺栓不断的对下模进行挤压,从而能较好地控制启模的速度,使上模和下模缓慢分开,达到启模的目的,本实用新型操作方便、工作量少且安全性能高,桨叶不容易变形且桨叶表面不容易碰伤,保证了桨叶的质量,提高了生产合格率。Beneficial effects of the utility model: the blade forming mold of the utility model has four bolt holes designed on both sides of the upper mold, and when the mold is opened, the upper mold continuously squeezes the lower mold through the four bolts on the mold, thereby The speed of mold opening can be well controlled, so that the upper mold and the lower mold can be slowly separated to achieve the purpose of mold opening. The utility model is easy to operate, has less workload and high safety performance, and the blade is not easily deformed and the surface of the blade is not easy Bruises ensure the quality of the blades and improve the qualified rate of production.
附图说明Description of drawings
图1是本实用新型桨叶成型模具的立体图;Fig. 1 is the perspective view of the utility model paddle forming mold;
图2是本实用新型安装有启模螺栓的上模的立体图;Fig. 2 is the perspective view of the upper mold that the mold opening bolt is installed in the utility model;
图3是本实用新型安装有启模螺栓的下模的立体图;Fig. 3 is the three-dimensional view of the lower mold that the mold opening bolt is installed in the utility model;
图4是本实用新型未安装启模螺栓的上模的立体图;Fig. 4 is the three-dimensional view of the upper die of the utility model that the mold bolt is not installed;
图5是本实用新型启模螺栓主视图的局部示意图;Fig. 5 is a partial schematic diagram of the front view of the mold opening bolt of the present invention;
图6是图5中A-A剖视图。Fig. 6 is a sectional view of A-A in Fig. 5 .
具体实施方式Detailed ways
下面结合附图对本实用新型所涉及的桨叶成型模具做进一步详细说明。The paddle forming die involved in the present invention will be described in further detail below in conjunction with the accompanying drawings.
如图1、2、3、4、5、6所示,本实用新型的桨叶成型模具,包括匹配的上模5和下模4,上模5和下模4两侧相接处的面均为分模面6,上模5与下模4之间通过多个均匀布置的加压螺栓2贯穿以进行固定。As shown in Figures 1, 2, 3, 4, 5, and 6, the blade forming mold of the present invention includes a matching upper mold 5 and a lower mold 4, and the surfaces where the upper mold 5 and the lower mold 4 are connected Both are parting surfaces 6, and a plurality of uniformly arranged pressure bolts 2 pass through between the upper mold 5 and the lower mold 4 for fixing.
在上模5上沿竖直方向贯穿开设有至少四个螺纹孔8,四个螺纹孔8均匀分布在上模5上相对的两个分模面6上。具体地,本实施例中优选螺纹孔8为四个,均匀分布在上模5长度方向上的两个分模面6上,即两两对称布置。At least four threaded holes 8 are provided vertically on the upper mold 5 , and the four threaded holes 8 are evenly distributed on the two opposing mold parting surfaces 6 on the upper mold 5 . Specifically, in this embodiment, the number of threaded holes 8 is preferably four, which are evenly distributed on the two parting surfaces 6 in the length direction of the upper mold 5 , that is, symmetrically arranged in pairs.
在每个螺纹孔8内设有一根相匹配的启模螺栓1,启模螺栓1的长度大于上模5的厚度,本实施例中优选启模螺栓1长度是上模5厚度的两倍。起模时,将加压螺栓全部卸完,再通过旋转上模5上均匀分布的四个启模螺栓1来顶住下模4的分模面6上,让下模4缓慢且平稳地远离上模5,达到初步起模,不会因为启模速度的过快,避免了通过吊环3强制启模过程中碰伤桨叶的情况。完成初步起模以后,可以根据传统的方法采用吊车钩住上模5和下模4上的吊环3将上模5和下模4快速分离。In each threaded hole 8, be provided with a matched mold bolt 1, the length of the mold bolt 1 is greater than the thickness of the upper mold 5, preferred mold bolt 1 length is twice the thickness of the upper mold 5 in the present embodiment. When the mold is ejected, all the pressure bolts are removed, and then the four mold opening bolts 1 evenly distributed on the upper mold 5 are rotated to withstand the parting surface 6 of the lower mold 4, so that the lower mold 4 is slowly and steadily away from the mold. The upper mold 5 reaches the preliminary mold opening, and the situation of damaging the propeller blade during the forced mold opening process through the suspension ring 3 will not be avoided because of the excessive speed of the mold opening. After completing the initial mold removal, a crane can be used to hook the suspension ring 3 on the upper mold 5 and the lower mold 4 according to the traditional method to separate the upper mold 5 and the lower mold 4 quickly.
进一步,在下模4的分模面6上与至少四个螺纹孔8相对应的位置处开设有至少四个柱状凹槽7,凹槽7的直径大于启模螺栓1直径,与上述优选实施例相匹配的,本实施例中优选柱状凹槽7为四个。起模时,启模螺栓1到达下模4的分模面6时可以进入这四个柱状凹槽7,在挤压下模4时只对柱状凹槽7的底面进行挤压,而不会损伤分模面6。最终使上模5和下模4缓慢分开,达到启模的作用,不会因为启模速度的过快,而损伤桨叶。Further, at least four columnar grooves 7 are provided at positions corresponding to at least four threaded holes 8 on the parting surface 6 of the lower mold 4, and the diameter of the grooves 7 is greater than the diameter of the mold opening bolt 1, which is the same as that of the above-mentioned preferred embodiment. Correspondingly, there are preferably four columnar grooves 7 in this embodiment. When the mold is ejected, the opening bolt 1 can enter the four columnar grooves 7 when it reaches the parting surface 6 of the lower mold 4. When the lower mold 4 is squeezed, only the bottom surface of the columnar groove 7 is squeezed without Damage parting surface 6. Finally, the upper mold 5 and the lower mold 4 are slowly separated to achieve the effect of mold opening, and the blades will not be damaged due to the excessive speed of mold opening.
本实用新型的桨叶成型模具能根据不同的形状的产品,合理选择启模螺栓1的数量和布置位置,从而控制或者是避免桨叶固化成型后启模过程中碰伤桨叶的情况,以及操作方便、工作量少和安全等的优点。另外,本实用新型的桨叶成型模具结构简单,操作方便,稳定性好,适合大批量生产和课题预研模型桨叶研制类型,从而缩短了零件的启模时间,提高了操作者的安全性和产品的质量,提高了直升机复合材料桨叶的生产合格率。The paddle forming mold of the present utility model can reasonably select the quantity and arrangement position of the mold-opening bolts 1 according to products of different shapes, thereby controlling or avoiding damage to the paddle during the mold-opening process after the paddle is solidified and formed, and It has the advantages of convenient operation, less workload and safety. In addition, the blade forming mold of the utility model has the advantages of simple structure, convenient operation and good stability, and is suitable for mass production and project pre-research model blade development type, thereby shortening the mold opening time of the parts and improving the safety of the operator And the quality of the product has improved the production pass rate of helicopter composite blades.
以上所述仅是本实用新型的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本实用新型原来的前提下,这些改进和润饰也应视为本实用新型的保护范围。The above descriptions are only preferred implementations of the present utility model. It should be pointed out that for those of ordinary skill in the art, without departing from the original premise of the present utility model, these improvements and modifications should also be regarded as the present utility model. protected range.
Claims (3)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520283909.2U CN204604663U (en) | 2015-05-05 | 2015-05-05 | A kind of paddle molding mould |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520283909.2U CN204604663U (en) | 2015-05-05 | 2015-05-05 | A kind of paddle molding mould |
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| Publication Number | Publication Date |
|---|---|
| CN204604663U true CN204604663U (en) | 2015-09-02 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520283909.2U Expired - Fee Related CN204604663U (en) | 2015-05-05 | 2015-05-05 | A kind of paddle molding mould |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112720952A (en) * | 2020-11-20 | 2021-04-30 | 惠阳航空螺旋桨有限责任公司 | Manufacturing die for long-petiole composite material blade |
| CN116262379A (en) * | 2021-12-14 | 2023-06-16 | 惠阳航空螺旋桨有限责任公司 | Blade root forming die |
-
2015
- 2015-05-05 CN CN201520283909.2U patent/CN204604663U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112720952A (en) * | 2020-11-20 | 2021-04-30 | 惠阳航空螺旋桨有限责任公司 | Manufacturing die for long-petiole composite material blade |
| CN112720952B (en) * | 2020-11-20 | 2023-04-25 | 惠阳航空螺旋桨有限责任公司 | Manufacturing die for long-petiole composite material blade |
| CN116262379A (en) * | 2021-12-14 | 2023-06-16 | 惠阳航空螺旋桨有限责任公司 | Blade root forming die |
| CN116262379B (en) * | 2021-12-14 | 2025-08-12 | 惠阳航空螺旋桨有限责任公司 | Blade root forming die |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150902 |
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| CF01 | Termination of patent right due to non-payment of annual fee |