CN205780092U - A kind of anti-out-of-plane bending connector - Google Patents
A kind of anti-out-of-plane bending connector Download PDFInfo
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- CN205780092U CN205780092U CN201620514633.9U CN201620514633U CN205780092U CN 205780092 U CN205780092 U CN 205780092U CN 201620514633 U CN201620514633 U CN 201620514633U CN 205780092 U CN205780092 U CN 205780092U
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Abstract
Description
技术领域technical field
本实用新型属于飞机强度设计领域,尤其涉及一种防面外弯曲连接件。The utility model belongs to the field of aircraft strength design, in particular to an anti-out-of-plane bending connector.
背景技术Background technique
目前飞机广泛采用耳片连接形式传递集中载荷,耳片结构连接形式简单,一般承受面内载荷。如某型飞机结构采用耳片螺栓连接传递集中力矩,见图1。连接件1'与结构件4'相连,连接件1'力偶M通过螺栓3'、耳片2'接触形式传递,连接件1'传至耳片2'的力矩有两种方式平衡:方式一通过螺栓3'对耳孔挤压作用反力F1-F1形成的力偶平衡,方式二通过连接件1'与上下耳片挤压力F2-F2形成的力偶平衡,力矩平衡示意图见图2,耳片受力F1为面内拉压载荷,力F2对耳片结构来说为面外载荷。在F2作用下耳片根部弯曲应力很高。但某些型号出于空间限制及特殊研制需求,耳片需承受面内拉伸载荷及面外载荷,面外载荷引起的弯矩使耳片局部应力显著提高,为防止耳片由于强度不足而破坏,耳片2'及结构件4'被迫设计的较重,连接件1'也较大,付出较大的重量代价。At present, the aircraft widely adopts the lug connection form to transfer the concentrated load. The lug structure connection form is simple, and generally bears the in-plane load. For example, a certain type of aircraft structure adopts lug bolt connection to transfer concentrated moment, see Figure 1. The connecting piece 1' is connected with the structural piece 4', and the force couple M of the connecting piece 1' is transmitted through the contact form of the bolt 3' and the lug 2'. There are two ways to balance the torque transmitted from the connecting piece 1' to the lug 2': Method 1 The force couple balance is formed by the reaction force F1-F1 of the bolt 3' on the ear hole. The second method is the force couple balance formed by the connecting piece 1' and the upper and lower ear piece extrusion force F2-F2. The schematic diagram of the moment balance is shown in Figure 2, the ear piece The force F1 is an in-plane tension and compression load, and the force F2 is an out-of-plane load for the lug structure. Under the action of F2, the bending stress at the root of the lug is very high. However, for some models due to space constraints and special development requirements, the lugs need to bear in-plane tensile loads and out-of-plane loads. The bending moment caused by out-of-plane loads significantly increases the local stress of the lugs. If it is damaged, the lug 2' and the structural part 4' are forced to be designed to be heavier, and the connecting part 1' is also larger, and a larger weight price is paid.
实用新型内容Utility model content
本实用新型的目的是提供一种防面外弯曲连接件,解决上述问题。The purpose of this utility model is to provide an anti-out-of-plane bending connector to solve the above problems.
为达到上述目的,本实用新型采用的技术方案是:一种防面外弯曲连接件,用于使耳片连接结构中上下耳片仅承受面内载荷,其包括耳片、连接件、连接螺栓及锁紧螺母,所述连接螺栓中部设有凹陷的台阶,且所述台阶表面光滑,连接件置于所述台阶内,所述连接螺栓穿过对称的两个耳片及连接件并用锁紧螺母锁紧,连接件与上下耳片具有间隙。In order to achieve the above purpose, the technical solution adopted by the utility model is: an anti-out-of-plane bending connecting piece, which is used to make the upper and lower lugs in the lug connection structure only bear the in-plane load, which includes lugs, connecting pieces, connecting bolts and a lock nut, the middle part of the connecting bolt is provided with a concave step, and the surface of the step is smooth, the connecting piece is placed in the step, and the connecting bolt passes through the two symmetrical lugs and the connecting piece and is locked The nut is locked tightly, and there is a gap between the connecting piece and the upper and lower lugs.
进一步地,所述连接件包括本体和拼接件,本体和拼接件均有半圆槽,且本体及拼接件拼接后两个半圆槽形成圆孔,所述圆孔的直径与连接螺栓中部台阶处的直径大小相同,且圆孔与台阶配合,本体与拼接件通过螺栓固定连接。Further, the connecting piece includes a body and a splicing piece, both of which have semicircular grooves, and after splicing the body and the splicing pieces, the two semicircular grooves form a circular hole, the diameter of the circular hole is the same as the diameter of the middle step of the connecting bolt. The diameters are the same, and the round hole matches the step, and the body and the splicing piece are fixedly connected by bolts.
进一步地,所述连接螺栓台阶处还有过渡段。Further, there is a transition section at the step of the connecting bolt.
进一步地,所述过渡段为倒角。Further, the transition section is chamfered.
进一步地,所述倒角为倒圆角。Further, the chamfer is a rounded corner.
本实用新型的一种防面外弯曲连接件通过连接件置于连接螺栓内,且使连接件与耳片之间设有间隙,使得耳片面外弯曲载荷转化为面内拉压载荷,进而载荷只能以面内拉压的形式传递,降低结构应力水平,减轻了结构重量。An anti-out-of-plane bending connector of the utility model is placed in the connecting bolt through the connector, and a gap is provided between the connector and the ear piece, so that the out-of-plane bending load of the ear piece is converted into an in-plane tension and compression load, and then the load It can only be transmitted in the form of in-plane tension and compression, which reduces the structural stress level and reduces the structural weight.
附图说明Description of drawings
此处的附图被并入说明书中并构成本说明书的一部分,示出了符合本实用新型的实施例,并与说明书一起用于解释本实用新型的原理。The accompanying drawings, which are incorporated in the specification and constitute a part of the specification, illustrate embodiments consistent with the present utility model, and are used together with the specification to explain the principle of the utility model.
图1为现有技术的耳片连接结构示意图;Fig. 1 is a schematic diagram of the connection structure of the tabs in the prior art;
图2为现有技术的耳片受力示意图;Fig. 2 is a schematic diagram of the stress of the ear piece in the prior art;
图3为本实用新型的耳片与连接件连接结构示意图;Fig. 3 is a schematic diagram of the connecting structure of the ear piece and the connector of the present invention;
图4为本实用新型的连接件结构示意图。Fig. 4 is a structural schematic diagram of the connector of the present invention.
其中,1-连接螺栓,2-锁紧螺母,3-耳片,4-连接件,11-台阶,12-过渡段,41-本体,42-拼接件,43-半圆槽,44-圆孔,1'-连接件,2'-耳片,3'-螺栓,4'-结构件。Among them, 1-connecting bolt, 2-lock nut, 3-lug, 4-connecting piece, 11-step, 12-transition section, 41-body, 42-splice, 43-semi-circular groove, 44-round hole , 1'-connector, 2'-ear, 3'-bolt, 4'-structure.
具体实施方式detailed description
为使本实用新型实施的目的、技术方案和优点更加清楚,下面将结合本实用新型实施例中的附图,对本实用新型实施例中的技术方案进行更加详细的描述。在附图中,自始至终相同或类似的标号表示相同或类似的元件或具有相同或类似功能的元件。所描述的实施例是本实用新型一部分实施例,而不是全部的实施例。下面通过参考附图描述的实施例是示例型的,旨在用于解释本实用新型,而不能理解为对本实用新型的限制。基于本实用新型中的实施例,本领域普通技术人员在没有作出创造型劳动前提下所获得的所有其他实施例,都属于本实用新型保护的范围。下面结合附图对本实用新型的实施例进行详细说明。In order to make the purpose, technical solutions and advantages of the utility model more clear, the technical solution in the utility model embodiment will be described in more detail below in conjunction with the accompanying drawings in the utility model embodiment. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some embodiments of the present utility model, but not all embodiments. The embodiments described below with reference to the figures are exemplary and are intended to explain the present invention, but should not be construed as limitations of the present invention. Based on the embodiments of the present utility model, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the scope of protection of the present utility model. Embodiments of the utility model are described in detail below in conjunction with the accompanying drawings.
在本实用新型的描述中,需要理解的是,术语“中心”、“纵向”、“横向”、“前”、“后”、“左”、“右”、“竖直”、“水平”、“顶”、“底”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本实用新型和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本实用新型保护范围的限制。In describing the present invention, it should be understood that the terms "central", "longitudinal", "transverse", "front", "rear", "left", "right", "vertical", "horizontal" , "top", "bottom", "inner", "outer" and other indicated orientations or positional relationships are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the utility model and simplifying the description, rather than indicating Or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as limiting the protection scope of the present utility model.
如图3所示,本实用新型的防面外弯曲连接件包括耳片3、连接件4、连接螺栓1及锁紧螺母2,耳片3数量为两个,对称的设置在飞机的结构部位,通过连接螺栓1将耳片3和连接件4进行连接,之后用锁紧螺母2锁紧即可,即实现飞机的两个结构部件之间的连接。本实用新型中的连接螺栓1是中间部分具有凹陷台阶11的螺栓,凹陷的部位表面光滑可减少应力,在台阶端部还有过渡段12,过渡段12部分是以倒圆角的形式存在,这样可以减少连接螺栓1上的应力集中,提高承载能力。此外,连接件4包括本体41及拼接件42,本体41及拼接件42均有半圆槽43,将本体41及拼接件42的半圆槽对准后拼接在一起,使两个半圆槽43形成一个圆孔44,连接螺栓的台阶11穿过圆孔44,所以圆孔44的直径与台阶11的直径相同,之后用螺栓将本体41及拼接件42连接,如图4所示。在本实用新型中,连接件4与耳片3之间有足够大的间隙,耳片面外弯曲载荷转化为面内拉压载荷,进而载荷只能以面内拉压的形式传递,降低结构应力水平,减轻结构重量。As shown in Figure 3, the out-of-plane bending connector of the present invention includes lugs 3, connectors 4, connecting bolts 1 and lock nuts 2, and the number of lugs 3 is two, which are symmetrically arranged on the structural parts of the aircraft. The lug 3 and the connecting piece 4 are connected through the connecting bolt 1, and then locked with the lock nut 2, that is, the connection between the two structural parts of the aircraft is realized. The connecting bolt 1 in the utility model is a bolt with a recessed step 11 in the middle part, and the surface of the recessed part is smooth to reduce stress, and there is a transition section 12 at the end of the step, and the transition section 12 part exists in the form of rounded corners. This can reduce the stress concentration on the connecting bolt 1 and improve the bearing capacity. In addition, the connecting piece 4 includes a body 41 and a splicing piece 42. Both the body 41 and the splicing piece 42 have semicircular grooves 43. After aligning the semicircular grooves of the body 41 and the splicing piece 42, they are spliced together so that the two semicircular grooves 43 form a Circular hole 44, the step 11 of the connecting bolt passes through the circular hole 44, so the diameter of the circular hole 44 is the same as the diameter of the step 11, and then the body 41 and the splice 42 are connected with bolts, as shown in Figure 4 . In the utility model, there is a large enough gap between the connector 4 and the lug 3, and the out-of-plane bending load of the lug is converted into an in-plane tension and compression load, and then the load can only be transmitted in the form of in-plane tension and compression, reducing structural stress level, reducing structural weight.
本实用新型的一种防面外弯曲连接件具有以下优点和积极效果:An anti-out-of-plane bending connector of the present utility model has the following advantages and positive effects:
1)采用阶梯型螺栓连接形式,保证了耳片受载形式为面内拉压;1) The stepped bolt connection form is adopted to ensure that the lug is loaded in the form of in-plane tension and compression;
2)阶梯型螺栓连接形式有效降低了结构局部应力水平,减轻了结构重量,降低了生产成本;2) The stepped bolt connection form effectively reduces the local stress level of the structure, reduces the structural weight, and reduces the production cost;
3)连接形式设计,装配形式简单,工艺实施方便,具有良好的互换性。3) The connection form is designed, the assembly form is simple, the process is convenient to implement, and it has good interchangeability.
以上所述,仅为本实用新型的最优具体实施方式,但本实用新型的保护范围并不局限于此,任何熟悉本技术领域的技术人员在本实用新型揭露的技术范围内,可轻易想到的变化或替换,都应涵盖在本实用新型的保护范围之内。因此,本实用新型的保护范围应以所述权利要求的保护范围为准。The above is only the best specific implementation of the utility model, but the scope of protection of the utility model is not limited thereto, any skilled person familiar with the technical field can easily think of All changes or replacements should fall within the protection scope of the present utility model. Therefore, the protection scope of the present utility model should be based on the protection scope of the claims.
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| CN201620514633.9U CN205780092U (en) | 2016-05-31 | 2016-05-31 | A kind of anti-out-of-plane bending connector |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112412940A (en) * | 2020-10-30 | 2021-02-26 | 江西昌河航空工业有限公司 | Lug connection structure |
| CN113167213A (en) * | 2018-12-13 | 2021-07-23 | 通用电气公司 | Joint-type rotor blade with chordwise extending pins supported via one or more structural members |
-
2016
- 2016-05-31 CN CN201620514633.9U patent/CN205780092U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113167213A (en) * | 2018-12-13 | 2021-07-23 | 通用电气公司 | Joint-type rotor blade with chordwise extending pins supported via one or more structural members |
| CN112412940A (en) * | 2020-10-30 | 2021-02-26 | 江西昌河航空工业有限公司 | Lug connection structure |
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