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CN106739020A - A kind of sample prototype blade bushing - Google Patents

A kind of sample prototype blade bushing Download PDF

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Publication number
CN106739020A
CN106739020A CN201611148869.6A CN201611148869A CN106739020A CN 106739020 A CN106739020 A CN 106739020A CN 201611148869 A CN201611148869 A CN 201611148869A CN 106739020 A CN106739020 A CN 106739020A
Authority
CN
China
Prior art keywords
bushing
blade
model machine
mold
blade bushing
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.)
Pending
Application number
CN201611148869.6A
Other languages
Chinese (zh)
Inventor
孙于涛
骆红云
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.)
AVIC Huiyang Aviation Propeller Co Ltd
Original Assignee
AVIC Huiyang Aviation Propeller 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 AVIC Huiyang Aviation Propeller Co Ltd filed Critical AVIC Huiyang Aviation Propeller Co Ltd
Priority to CN201611148869.6A priority Critical patent/CN106739020A/en
Publication of CN106739020A publication Critical patent/CN106739020A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543Fixing the position or configuration of fibrous reinforcements before or during moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/36Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and impregnating by casting, e.g. vacuum casting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/08Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B29L2031/082Blades, e.g. for helicopters
    • B29L2031/085Wind turbine blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention discloses a kind of sample prototype blade bushing, including metal body;There is a major thread hole at the center of body, the minor thread location hole for having more than three on end face;Four perisporium outer surfaces are taper, and multi-turn groove is distributed with thereon.The blade made using bushing of the present invention, glass fabric is high with bushing fixation reliability, is difficult delamination, and blade can bear larger centrifugal force;Mould and bushing accurate positioning, do not result in blade biasing in a mold.

Description

一种小样模型机叶片衬套A small sample model machine blade bushing

技术领域technical field

本发明涉及一种小样模型机叶片衬套。The invention relates to a small sample model machine blade bushing.

背景技术Background technique

目前,我国生产的风机系列产品,大多是利用研制好的模型样机,然后按几何相似原理放大或缩小尺寸,生产出各种不同机号的风机。因此,每一款新型的产品都需制作小样模型机,通过它来验证风机的性能,由于叶片较小,制作过程中玻璃布铺层厚度比较薄,既要保证质量轻,还要保证强度、刚度。所以,小样模型机叶片的制作十分重要,尤其是叶片桨根处的小样模型机叶片衬套的制作十分重要。At present, most of the fan series products produced in our country use the developed model prototype, and then enlarge or reduce the size according to the principle of geometric similarity to produce fans of various machine numbers. Therefore, each new product needs to make a small sample model machine to verify the performance of the fan. Because the blades are small, the thickness of the glass cloth layer is relatively thin during the production process. It is necessary to ensure light weight, strength, and stiffness. Therefore, it is very important to make a small model machine blade, especially the production of the small model machine blade bushing at the blade root.

现有的衬套如图1所示,其锥形外表面平整,为加大与玻璃纤维布的接触,在加工时要求表面必须粗糙,必要时还需进行吹砂处理;同时,在制作叶片时,对衬套要进行彻底的清洗,如有油污会造成玻璃布与衬套粘接不牢固,易脱层等问题。玻璃纤维布的粘接固定,完全依靠模具的过盈压量来保证,所以在此位置需专门增加玻璃纤维布的布层厚度,不但浪费材料,且费时费力。使用这种衬套的叶片制作时定位只能靠模具加工的尺寸和限位保证,为了安装顺利模具与衬套间会留有间隙,所以在模具与衬套安放的时候会有位置不一致的现象发生;且在模具加压过程中,可能造成叶片向上或向下移动,不在叶片中心轴线上。这种衬套只能使用气袋成型工艺制作叶片,叶片制作方法单一。总之,现有衬套不适合小样模型机叶片的使用。The existing bushing is shown in Figure 1, and its tapered outer surface is flat. In order to increase the contact with the glass fiber cloth, the surface must be rough during processing, and sand blasting is required if necessary; at the same time, the When cleaning, the bushing should be thoroughly cleaned. If there is oil, it will cause problems such as weak bonding between the glass cloth and the bushing, and easy delamination. The bonding and fixing of the glass fiber cloth is completely guaranteed by the interference pressure of the mold, so it is necessary to increase the thickness of the glass fiber cloth at this position, which not only wastes materials, but also takes time and effort. The positioning of the blades using this bushing can only be guaranteed by the size and limit of the mold processing. In order to install smoothly, there will be a gap between the mold and the bushing, so there will be inconsistency when the mold and the bushing are placed. ; and during the pressurization process of the mold, it may cause the blade to move up or down, not on the central axis of the blade. This liner can only use the air bag forming process to make blades, and the blade manufacturing method is single. In conclusion, existing bushings are not suitable for use with small model machine blades.

发明内容Contents of the invention

本发明的目的就是解决现有技术中存在的上述问题,提供一种小样模型机叶片衬套,使用该衬套制作的叶片,玻璃纤维布与衬套固定可靠性高,不易脱层,叶片能够承受较大的离心力;模具与衬套定位准确,不会造成叶片在模具中的偏置。The purpose of the present invention is to solve the above-mentioned problems existing in the prior art, to provide a small model machine blade bushing, the blade made by using the bushing, the glass fiber cloth and the bushing are fixed with high reliability, it is not easy to delaminate, and the blade can Withstand large centrifugal force; the mold and bushing are positioned accurately, which will not cause the blade to be biased in the mold.

为实现上述目的,本发明的技术解决方案是:一种小样模型机叶片衬套,包括金属本体;本体的中心有一个大螺纹孔,端面上有三个以上的小螺纹定位孔;四周壁外表面为锥形,其上分布有多圈凹槽。In order to achieve the above object, the technical solution of the present invention is: a small sample model machine blade bushing, including a metal body; a large threaded hole in the center of the body, and more than three small threaded positioning holes on the end surface; It is conical with multiple circles of grooves distributed on it.

优选地,在所述的本体内有梯形凹槽。减轻了衬套重量。Preferably, there are trapezoidal grooves in the body. Reduced bushing weight.

优选地,所述的四周壁的锥形锥度为5°。Preferably, the taper of the surrounding walls is 5°.

优选地,所述的四周壁分布的多圈凹槽均匀分布,且为半圆形凹槽。不但增加了玻璃纤维布的粘结能力,且粘结能力大,分布均衡,使叶片能够承受更大的离心力,使用寿命长。Preferably, the multi-circle grooves distributed on the surrounding walls are evenly distributed and are semicircular grooves. Not only the bonding ability of the glass fiber cloth is increased, but also the bonding ability is large and the distribution is balanced, so that the blade can withstand greater centrifugal force and has a long service life.

本发明叶片衬套端面有四个螺纹孔,可以通过螺栓与模具上的模套紧密连接,实现准确定位,避免叶片在模具中发生偏置。衬套中间有一个螺纹孔,不仅能够将泡沫顺利灌注到叶片内腔内,且在泡沫固化时能够拧上堵塞,避免泡沫固化时因膨胀而溢出,还可以排出固化时产生的气体。四周壁外表面的多圈凹槽和锥度,使第一层的玻璃纤维布与衬套外壁粘接牢固,再铺第二层和第三层等层玻璃纤维布时,只要在铺好的玻璃纤维布上进行纤维缠绕,又能达到很好的粘接,且可以增加贴实度,使玻璃纤维布能层层牢牢固定;不需刻意增加厚度;总之,四周壁外表面的多圈凹槽和锥度的存在在叶片制作过程中增加了与玻璃钢的粘结能力,使叶片能够承受较大的离心力。叶片衬套内部的梯形槽减轻了衬套重量The end face of the blade bushing of the present invention has four threaded holes, which can be tightly connected with the mold sleeve on the mold through bolts, so as to realize accurate positioning and prevent the blade from being biased in the mold. There is a threaded hole in the middle of the bush, which can not only pour the foam into the inner cavity of the blade smoothly, but also screw on the plug when the foam is solidified, so as to avoid overflow due to expansion when the foam is solidified, and can also discharge the gas generated during solidification. The multi-circle grooves and tapers on the outer surface of the surrounding wall make the first layer of glass fiber cloth and the outer wall of the bushing firmly bonded. When laying the second and third layers of glass fiber cloth, as long as the laid glass Fiber winding on the fiber cloth can achieve good bonding, and can increase the compactness, so that the glass fiber cloth can be firmly fixed layer by layer; there is no need to deliberately increase the thickness; in short, the multi-circle concave on the outer surface of the surrounding wall The existence of grooves and tapers increases the bonding ability with FRP during the blade manufacturing process, so that the blade can withstand greater centrifugal force. Trapezoidal slots inside the vane bushing reduce bushing weight

总之,使用本发明的衬套制作的叶片,玻璃纤维布与衬套固定可靠性高,贴实度好,不易脱层,叶片能够承受较大的离心力;模具与衬套定位准确,不会造成叶片在模具中的偏置;且叶片可以采用灌注、手糊、气袋等多种方法制作;特备适合小样模型机叶片的使用。In a word, the blade made of the bushing of the present invention has high fixing reliability between the glass fiber cloth and the bushing, good adhesion, and is not easy to delaminate, and the blade can withstand relatively large centrifugal force; the mold and the bushing are positioned accurately without causing The offset of the blade in the mold; and the blade can be made by pouring, hand lay-up, air bag and other methods; it is especially suitable for the use of small sample model machine blades.

附图说明Description of drawings

图1为现有的衬套的主视图。Figure 1 is a front view of a conventional bushing.

图2本发明的主视图;The front view of the present invention of Fig. 2;

图3为本发明的左视图;Fig. 3 is the left view of the present invention;

图4为本发明与模具的装配结构示意图。Fig. 4 is a schematic diagram of the assembly structure of the present invention and the mold.

具体实施方式detailed description

下面结合附图和具体实施例对本发明做进一步的描述。The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

如图2和图3所示,本实施例包括金属本体1;本体1的中心有一个大螺纹孔4,端面上有四个(也可根据需要设置三个、六个等)小螺纹定位孔5。四周壁外表面为锥形,优选锥度为5°,其上分布有多圈凹槽2,优选多圈凹槽2均匀分布,且为半圆形凹槽。优选地,在所述的本体1内有梯形凹槽。As shown in Figure 2 and Figure 3, this embodiment includes a metal body 1; there is a large threaded hole 4 in the center of the body 1, and there are four (three, six, etc.) small threaded positioning holes on the end face 5. The outer surface of the surrounding walls is tapered, preferably with a taper of 5°, and there are multiple circles of grooves 2 distributed thereon, preferably the multiple circles of grooves 2 are evenly distributed and are semicircular grooves. Preferably, there are trapezoidal grooves in the body 1 .

图4为本发明衬套与模具的装配结构示意图,6为模具,7为本发明衬套,8为玻璃纤维布层。Fig. 4 is a schematic diagram of the assembly structure of the bushing and the mold of the present invention, 6 is a mold, 7 is a bushing of the present invention, and 8 is a glass fiber cloth layer.

上述实施例仅是优选的和示例性的,本领域技术人员可以根据本专利的精神做等同技术改进,这些都由本专利的保护范围所覆盖。The above-mentioned embodiments are only preferred and exemplary, and those skilled in the art can make equivalent technical improvements according to the spirit of this patent, and these are covered by the protection scope of this patent.

Claims (5)

1.一种小样模型机叶片衬套,其特征在于:包括金属本体;本体的中心有一个大螺纹孔,端面上有三个以上的小螺纹定位孔;四周壁外表面为锥形,其上分布有多圈凹槽。1. A small sample model machine blade bushing is characterized in that: it includes a metal body; there is a large threaded hole in the center of the body, and more than three small threaded positioning holes are arranged on the end face; the outer surface of the surrounding wall is tapered, and the distribution of There are multiple grooves. 2.根据权利要求1所述的小样模型机叶片衬套,其特征在于:在所述的本体内有梯形凹槽。2. The blade bushing of the prototype model machine according to claim 1, characterized in that: there is a trapezoidal groove in the said main body. 3.根据权利要求1或2所述的小样模型机叶片衬套,其特征在于:所述的四周壁的锥形锥度为5°。3. The blade bushing of a prototype model machine according to claim 1 or 2, characterized in that: the taper of the surrounding walls is 5°. 4.根据权利要求3所述的小样模型机叶片衬套,其特征在于:所述的四周壁分布的多圈凹槽均匀分布,且为半圆形凹槽。4. The blade bushing of the prototype model machine according to claim 3, characterized in that: the multi-circle grooves distributed on the surrounding walls are evenly distributed and are semicircular grooves. 5.根据权利要求1或2所述的小样模型机叶片衬套,其特征在于:所述的四周壁分布的多圈凹槽均匀分布,且为半圆形凹槽。5. The blade bushing of the prototype model machine according to claim 1 or 2, characterized in that: the multi-circle grooves distributed on the surrounding walls are evenly distributed and are semicircular grooves.
CN201611148869.6A 2016-12-13 2016-12-13 A kind of sample prototype blade bushing Pending CN106739020A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611148869.6A CN106739020A (en) 2016-12-13 2016-12-13 A kind of sample prototype blade bushing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611148869.6A CN106739020A (en) 2016-12-13 2016-12-13 A kind of sample prototype blade bushing

Publications (1)

Publication Number Publication Date
CN106739020A true CN106739020A (en) 2017-05-31

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0822683D0 (en) * 2008-12-12 2009-01-21 Gen Electric Bushing and clock spring assembly for moveable turbine vane
CN201329636Y (en) * 2008-12-11 2009-10-21 江西昌河航空工业有限公司 Mould unidirectional positioning device
CN203499928U (en) * 2013-09-26 2014-03-26 黑龙江天华风电设备制造有限公司 Novel locating device of blade root bolts
CN105089944A (en) * 2015-08-21 2015-11-25 东方电气风电有限公司 Blade root connecting structure of wind-driven generator and manufacturing method of blade root connecting structure
US20150354542A1 (en) * 2014-06-05 2015-12-10 Siemens Aktiengesellschaft Root bushing for a blade root of a wind turbine rotor blade, a blade root, a wind turbine rotor blade and a wind turbine
CN206733645U (en) * 2016-12-13 2017-12-12 惠阳航空螺旋桨有限责任公司 A kind of sample prototype blade bushing

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201329636Y (en) * 2008-12-11 2009-10-21 江西昌河航空工业有限公司 Mould unidirectional positioning device
GB0822683D0 (en) * 2008-12-12 2009-01-21 Gen Electric Bushing and clock spring assembly for moveable turbine vane
CN203499928U (en) * 2013-09-26 2014-03-26 黑龙江天华风电设备制造有限公司 Novel locating device of blade root bolts
US20150354542A1 (en) * 2014-06-05 2015-12-10 Siemens Aktiengesellschaft Root bushing for a blade root of a wind turbine rotor blade, a blade root, a wind turbine rotor blade and a wind turbine
CN105089944A (en) * 2015-08-21 2015-11-25 东方电气风电有限公司 Blade root connecting structure of wind-driven generator and manufacturing method of blade root connecting structure
CN206733645U (en) * 2016-12-13 2017-12-12 惠阳航空螺旋桨有限责任公司 A kind of sample prototype blade bushing

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Application publication date: 20170531