CN207197466U - Helicopter Main oar hoop lower plate detecting tool - Google Patents

Helicopter Main oar hoop lower plate detecting tool Download PDF

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Publication number
CN207197466U
CN207197466U CN201720145147.9U CN201720145147U CN207197466U CN 207197466 U CN207197466 U CN 207197466U CN 201720145147 U CN201720145147 U CN 201720145147U CN 207197466 U CN207197466 U CN 207197466U
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CN
China
Prior art keywords
detecting tool
boss
helicopter main
lower plate
main oar
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Expired - Fee Related
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CN201720145147.9U
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Chinese (zh)
Inventor
佟飞
温洲
李野
杨昊
李星伟
杨微微
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Harbin Hafei Aviation Industry Co Ltd
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Harbin Aircraft Industry Group Co Ltd
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Priority to CN201720145147.9U priority Critical patent/CN207197466U/en
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Publication of CN207197466U publication Critical patent/CN207197466U/en
Expired - Fee Related legal-status Critical Current
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Abstract

The utility model belongs to Helicopter Main oar hoop detection technique, and in particular to a kind of Helicopter Main oar hoop lower plate detecting tool.The Helicopter Main oar hoop lower plate detecting tool is structure as a whole, its front-end and back-end is provided with boss, middle part is a bar hole, and spring leaf clamping column is respectively arranged between bar hole both ends and front end boss and rear end boss, and bar hole on both sides of the middle is provided with two Auxiliary support posts.Pass through the actual use to detecting tool, the function and technical indicator of detecting tool comply fully with design requirement, compared with past clamping method, realize accurate positioning, clamping it is quick, it is easy to use, meet the features such as clamped one time completes all detection needs, detection efficiency is more importantly improved, meets that part volume detects needs.

Description

直升机主桨箍下夹板检测工装Helicopter main rotor hoop splint inspection tooling

技术领域technical field

本实用新型属于直升机主桨箍检测技术,具体涉及一种直升机主桨箍下夹板检测工装。The utility model belongs to the detection technology of a helicopter main propeller hoop, in particular to a detection tool for a splint under the helicopter main propeller hoop.

背景技术Background technique

如图1所示,下夹板是直升机主桨箍关键件,为复杂不规则零件,在实际加工制造和装配各环节中,均需要对下夹板进行检测。现有技术检测时没有专用检测工装,造成检测稳定性差。通过一段时间的检测发现,原有的检测方法存在以下几个问题:As shown in Figure 1, the lower splint is a key part of the helicopter main propeller hoop, and is a complex and irregular part. In the actual processing, manufacturing and assembly, the lower splint needs to be inspected. There is no special detection tool during detection in the prior art, resulting in poor detection stability. After a period of detection, it was found that the original detection method had the following problems:

1)由于该零件未锻件外形不规则,这给装夹带来困难,如果每件的检测都用手动检测很难保证每次检测方法的一致性,而且检测时间长,同时给编制CNC 检测程序带来困难,对检测数据需要花费较长的时间进行处理,非常繁琐。1) Due to the irregular shape of the unforged part, it is difficult to clamp. If each piece is inspected manually, it is difficult to ensure the consistency of each inspection method, and the inspection time is long. It is difficult, and it takes a long time to process the detection data, which is very cumbersome.

2)检测结果发现检测数据不稳定,通过复测我们发现两次检测结果有较大差异,经过仔细查找发现造成差异的原因是装夹变形造成上夹板变形而产生误差。过去装夹方法采用2个等高25mm量块配合橡皮泥固定,因此原有的装夹方法无法保证批量零件检测需要及检测稳定性。2) The test results found that the test data was unstable. Through retesting, we found that the two test results were quite different. After careful investigation, it was found that the reason for the difference was that the clamping deformation caused the deformation of the upper splint and caused errors. In the past, the clamping method used two 25mm measuring blocks with equal heights to be fixed with plasticine. Therefore, the original clamping method could not guarantee the testing requirements and testing stability of batch parts.

实用新型内容Utility model content

本实用新型的目的是:提供一种能够实现零件快速装夹及精确定位的直升机主桨箍下夹板检测工装。The purpose of the utility model is to provide a tool for detecting the splint under the main propeller hoop of a helicopter, which can realize fast clamping and precise positioning of parts.

本实用新型的技术方案是:一种直升机主桨箍下夹板检测工装,为一体结构,其前端和后端均设置有凸台,中部为一条形孔,条形孔两端与前端凸台和后端凸台之间分别设置有弹簧片夹持立柱,条形孔中部两侧设置有两个辅助支撑柱。The technical scheme of the utility model is: a detection tool for the splint under the main propeller hoop of a helicopter, which has an integral structure, and its front and rear ends are provided with bosses, the middle part is a strip hole, and the two ends of the strip hole are connected with the front boss and Spring clamping columns are respectively arranged between the bosses at the rear end, and two auxiliary supporting columns are arranged on both sides of the middle part of the strip hole.

前端凸台高度低于后端凸台高度。The height of the boss at the front end is lower than the height of the boss at the rear end.

前端凸台与后端凸台之间的高度差为25mm。The height difference between the front end boss and the rear end boss is 25mm.

本实用新型的技术效果是:通过对检测工装的实际使用,检测工装的功能以及技术指标完全符合设计要求,与过去的装夹方法相比,实现了定位准确、装夹快速、使用方便、满足一次装夹完成所有检测需要等特点,更重要的是提高了检测效率,满足批量零件检测需要,从原来检测一件需要2小时提高到0.5 小时。The technical effect of the utility model is: through the actual use of the detection tool, the function and technical indicators of the detection tool fully meet the design requirements. It has the characteristics of completing all the inspection needs in one clamping, and more importantly, it improves the inspection efficiency and meets the inspection needs of batch parts. It takes 2 hours to inspect one piece from the original to 0.5 hours.

附图说明Description of drawings

图1是下夹板的示意图;Fig. 1 is the schematic diagram of lower splint;

图2是本实用新型直升机主桨箍下夹板检测工装结构示意图;Fig. 2 is a structural schematic diagram of the splint detection tool under the main propeller hoop of the utility model helicopter;

图3是本实用新型直升机主桨箍下夹板检测工装装夹示意图;Fig. 3 is a schematic diagram of the installation and clamping of the splint detection tool under the main propeller hoop of the utility model helicopter;

图4是本实用新型直升机主桨箍下夹板检测工装装夹侧视图;Fig. 4 is a side view of the utility model helicopter main propeller hoop splint detection tool clamping side view;

其中,1-弹簧片夹持立柱、2-前端凸台、3-后端凸台、4-两个辅助支撑柱。Among them, 1-spring clamping column, 2-front end boss, 3-rear end boss, 4-two auxiliary support columns.

具体实施方式Detailed ways

下面结合实施例和附图对本实用新型做详细说明:Below in conjunction with embodiment and accompanying drawing, the utility model is described in detail:

请参阅图2、直升机主桨箍下夹板检测工装为一体结构,其前端和后端均设置有凸台,中部为一条形孔,条形孔两端与前端凸台和后端凸台之间分别设置有弹簧片夹持立柱,条形孔中部两侧设置有两个辅助支撑柱。Please refer to Figure 2. The detection tooling for the splint under the main propeller hoop of the helicopter is an integrated structure. There are bosses at the front and rear ends, and a strip hole in the middle. The two ends of the strip hole are between the front boss and the rear boss. A spring sheet clamping column is arranged respectively, and two auxiliary support columns are arranged on both sides of the middle part of the strip hole.

前端凸台高度低于后端凸台高度,二者之间的高度差为25mm。The height of the boss at the front end is lower than that of the boss at the rear end, and the height difference between the two is 25mm.

在支撑和夹紧方法上采用支撑和压紧的形式,增大支撑面使支撑面加宽到了120×60(mm)接触面积增大使支撑更加稳定,从而可有效提高减小晃动,提高测量精度,而且压板采用了弹簧片压紧的形式,压紧和拆卸比较方便。在设计检测工装满足上夹板零件批量检测需要,所采取的方法是,检测工装利用两个孔定位,用两个孔的下端面做基准,由于这两个平面相差25mm,因此在检测工装上加工出这两个高度差,从而保证下夹板检测时保持平行状态,这样就可以大大减少更换测针的数量,达到了优化测针的目的,在工装的中部设计了两个辅助支撑以防止零件的变形,底板开槽即减轻重量又便于将工装固定在三坐标测量机上。In the support and clamping method, support and compression are adopted, and the support surface is increased to widen the support surface to 120×60 (mm). The contact area is increased to make the support more stable, which can effectively reduce shaking and improve measurement accuracy. , and the pressure plate adopts the form of spring compression, which is more convenient for compression and disassembly. When designing the testing tool to meet the needs of batch testing of upper splint parts, the method adopted is that the testing tool uses two holes for positioning, and uses the lower end faces of the two holes as a reference. Since the difference between the two planes is 25mm, it is processed on the testing tool These two height differences are made to ensure that the lower splint is kept in a parallel state during detection, which can greatly reduce the number of replacement styli and achieve the purpose of optimizing the stylus. Two auxiliary supports are designed in the middle of the tooling to prevent the parts from collapsing. Deformation, the slotting of the bottom plate not only reduces the weight but also facilitates fixing the tooling on the three-coordinate measuring machine.

本实用新型实现了定位准确、装夹方便、满足一次装夹就能完成所有检测需要、缩短了安装调整时间,满足批量零件检测需要,从原来检测一件需要2 小时提高到0.5小时,大大提高了检测效率。The utility model realizes accurate positioning, convenient clamping, meets all testing needs in one clamping, shortens the installation and adjustment time, and meets the testing needs of batch parts. detection efficiency.

Claims (3)

1. a kind of Helicopter Main oar hoop lower plate detecting tool, it is characterised in that be structure as a whole, its front-end and back-end is respectively provided with There is boss, middle part is a bar hole, and spring leaf clamping is respectively arranged between bar hole both ends and front end boss and rear end boss Column, bar hole on both sides of the middle are provided with two Auxiliary support posts.
2. Helicopter Main oar hoop lower plate detecting tool according to claim 1, it is characterised in that front end boss height is low In rear end boss height.
3. Helicopter Main oar hoop lower plate detecting tool according to claim 2, it is characterised in that front end boss and rear end Difference in height between boss is 25mm.
CN201720145147.9U 2017-02-17 2017-02-17 Helicopter Main oar hoop lower plate detecting tool Expired - Fee Related CN207197466U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720145147.9U CN207197466U (en) 2017-02-17 2017-02-17 Helicopter Main oar hoop lower plate detecting tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720145147.9U CN207197466U (en) 2017-02-17 2017-02-17 Helicopter Main oar hoop lower plate detecting tool

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CN207197466U true CN207197466U (en) 2018-04-06

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109202197A (en) * 2018-11-14 2019-01-15 中国航发动力股份有限公司 A kind of thin-walled diaphragm seal multi-process wire cutting positioning fixture and method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109202197A (en) * 2018-11-14 2019-01-15 中国航发动力股份有限公司 A kind of thin-walled diaphragm seal multi-process wire cutting positioning fixture and method

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TR01 Transfer of patent right

Effective date of registration: 20191209

Address after: 150066 Heilongjiang city of Harbin province Harbin Pingfang District Youxie Street No. 15

Patentee after: HARBIN HAFEI AVIATION INDUSTRY Co.,Ltd.

Address before: 150066 Heilongjiang Province, Harbin city Youxie Street Pingfang District No. 15

Patentee before: HARBIN AIRCRAFT INDUSTRY (Group) Co.,Ltd.

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: 20180406