CN204461892U - Honeycomb core sheet material peeling strength test fixture - Google Patents

Honeycomb core sheet material peeling strength test fixture Download PDF

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Publication number
CN204461892U
CN204461892U CN201520156566.3U CN201520156566U CN204461892U CN 204461892 U CN204461892 U CN 204461892U CN 201520156566 U CN201520156566 U CN 201520156566U CN 204461892 U CN204461892 U CN 204461892U
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CN
China
Prior art keywords
honeycomb core
bolt
sheet material
clamping plate
core sheet
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
CN201520156566.3U
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Chinese (zh)
Inventor
董茜娟
刘伟健
阮媛
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.)
Jiangxi Hongdu Aviation Industry Group Co Ltd
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Jiangxi Hongdu Aviation Industry Group Co Ltd
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Application filed by Jiangxi Hongdu Aviation Industry Group Co Ltd filed Critical Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority to CN201520156566.3U priority Critical patent/CN204461892U/en
Application granted granted Critical
Publication of CN204461892U publication Critical patent/CN204461892U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

蜂窝芯板材分离强度测试夹具,包括连接杆、第一夹板及第二夹板;其中,连接杆上设置有用于与电子拉力机加载装置连接的销孔、用于安装第一螺栓的第一螺栓孔及用于安装第二螺栓的第二螺栓孔,且连接杆通过第一螺栓、第二螺栓固定在第一夹板与第二夹板组成的装夹载体上端,待检测蜂窝芯板材装夹在装夹载体中;同时在第一夹板与第二夹板下部分别开设有通槽,并通过通槽在待检测蜂窝芯板材中插入销钉;在电子拉力机加载装置的作用下,对待检测蜂窝芯板材分离强度进行测试,不易损坏待检测蜂窝芯板材,且实现对蜂窝芯板材连片面积测试,有效提高工作效率,节约了测试成本。

The jig for testing the separation strength of the honeycomb core plate includes a connecting rod, a first splint, and a second splint; wherein, the connecting rod is provided with a pin hole for connecting with an electronic tensile machine loading device, and a first bolt hole for installing the first bolt And the second bolt hole for installing the second bolt, and the connecting rod is fixed on the upper end of the clamping carrier composed of the first splint and the second splint through the first bolt and the second bolt, and the honeycomb core plate to be tested is clamped in the clamping In the carrier; at the same time, a through groove is respectively opened in the lower part of the first splint and the second splint, and a pin is inserted into the honeycomb core plate to be tested through the through groove; under the action of the loading device of the electronic tension machine, the separation strength of the honeycomb core plate to be tested The test is not easy to damage the honeycomb core plate to be tested, and the test of the connected area of the honeycomb core plate is realized, which effectively improves the work efficiency and saves the test cost.

Description

Honeycomb core sheet material peeling strength test fixture
Technical field
The utility model relates to honeycomb core plate property proving installation technical field, is specially a kind of honeycomb core sheet material peeling strength test fixture.
Background technology
Domestic existing honeycomb core sheet material peeling strength method of testing, be only unilateral and stick to the test of single node peeling strength, test specification is confined to single node, needs repeatedly repeated clamping to test, and just can draw the test result of honeycomb core sheet material area in flakes; Not only hand labor intensity is large, and inefficiency, also easily causes damage and the loss of honeycomb core sheet material to be detected simultaneously, and then affects test result, add testing cost to a certain extent in clamping process.
Utility model content
The technical matters that the utility model solves is to provide honeycomb core sheet material peeling strength test fixture, to solve the shortcoming in above-mentioned background technology.
The technical matters that the utility model solves realizes by the following technical solutions:
Honeycomb core sheet material peeling strength test fixture, comprises connecting link, the first clamping plate and the second clamping plate; Wherein, connecting link is provided with the pin-and-hole for being connected with electronic tensile machine charger, for installing the first bolt hole of the first bolt and the second bolt hole for installing the second bolt, and connecting link is bolted to by the first bolt, second the clamping carrier upper end that first clamping plate and the second clamping plate form, honeycomb core sheet material clamping to be detected is in clamping carrier; Offer groove respectively at the first clamping plate and the second clamping plate bottom simultaneously,
And in honeycomb core sheet material to be detected, insert pin by groove, under the effect of electronic tensile machine charger, honeycomb core plate material peeling strength to be detected is tested, not fragile honeycomb core sheet material to be detected, and can realize testing honeycomb core sheet material peeling strength.
In the utility model, the first clamping plate are identical with the second clamp region, and are provided with the bolt hole for installing the first bolt and the second bolt on the first clamping plate and the second clamping plate.
In the utility model, clamping upper carrier is trapezium structure, and bottom is rectangle structure, is convenient to observe the to be detected honeycomb core sheet material released state of clamping in clamping carrier.
In the utility model, the groove symmetrically structure that the first clamping plate and the second clamping plate bottom are offered.
In the utility model, groove is rectangle structure, and it is of a size of long 127mm, wide 8 mm.
In the utility model, pin is that 30CrMnSiA material is made, and specification is φ5, long is 50mm.
Beneficial effect: in the utility model, connecting link is provided with the pin-and-hole for being connected with electronic tensile machine charger, and honeycomb core sheet material clamping to be detected is in clamping carrier, offer groove respectively at the first clamping plate and the second clamping plate bottom simultaneously, in honeycomb core sheet material to be detected, pin is inserted by groove, under the effect of electronic tensile machine charger, honeycomb core plate material peeling strength to be detected is tested, not fragile honeycomb core sheet material to be detected, and realize the area test in flakes of honeycomb core sheet material, effectively increase work efficiency, saved testing cost.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model preferred embodiment.
Embodiment
The technological means realized to make the utility model, creation characteristic, reaching object and effect is easy to understand, below in conjunction with concrete diagram, setting forth the utility model further.
See the honeycomb core sheet material peeling strength test fixture of Fig. 1, comprise connecting link 1, first clamping plate 2, second clamping plate 3, pin-and-hole 4, first bolt 5, second bolt 6 and groove 7; Wherein, connecting link 1 is fixed on by the first bolt 5, second bolt 6 the clamping carrier upper end that first clamping plate 2 and the second clamping plate 3 form, and the pin-and-hole 4 had on connecting link 1 for being connected with electronic tensile machine charger, honeycomb core sheet material clamping to be detected is in clamping carrier; Offer groove 7 at the first clamping plate 2 and the second clamping plate 3 bottom symmetry simultaneously, according to the quantity of honeycomb hole on honeycomb core sheet material to be detected, in honeycomb core sheet material to be detected, pin is inserted by groove 7, under the effect of electronic tensile machine charger, honeycomb core plate material peeling strength to be detected is tested, not fragile honeycomb core sheet material to be detected, and can realize testing honeycomb core sheet material peeling strength.
In the present embodiment, groove 7 is rectangle structure, and it is of a size of long 127mm, wide 8 mm.
In the present embodiment, pin is that 30CrMnSiA material is made, and specification is φ5, long is 50mm.
More than show and describe ultimate principle of the present utility model, principal character and advantage of the present utility model.The technician of the industry should understand; the utility model is not restricted to the described embodiments; what describe in above-described embodiment and instructions just illustrates principle of the present utility model; under the prerequisite not departing from the utility model spirit and scope; the utility model also has various changes and modifications, and these changes and improvements all fall within the scope of claimed the utility model.The claimed scope of the utility model is defined by appending claims and equivalent thereof.

Claims (5)

1. honeycomb core sheet material peeling strength test fixture, comprises connecting link, the first clamping plate and the second clamping plate; It is characterized in that, connecting link is provided with the pin-and-hole for being connected with electronic tensile machine charger, for installing the first bolt hole of the first bolt and the second bolt hole for installing the second bolt, and connecting link is bolted to by the first bolt, second the clamping carrier upper end that first clamping plate and the second clamping plate form, honeycomb core sheet material clamping to be detected is in clamping carrier; Offer groove respectively at the first clamping plate and the second clamping plate bottom simultaneously, and in honeycomb core sheet material to be detected, insert pin by groove.
2. honeycomb core sheet material peeling strength test fixture according to claim 1, it is characterized in that, the first clamping plate are identical with the second clamp region, and are provided with the bolt hole for installing the first bolt and the second bolt on the first clamping plate and the second clamping plate.
3. honeycomb core sheet material peeling strength test fixture according to claim 1, it is characterized in that, clamping upper carrier is trapezium structure, and bottom is rectangle structure.
4. honeycomb core sheet material peeling strength test fixture according to claim 1, is characterized in that, the groove symmetrically structure that the first clamping plate and the second clamping plate bottom are offered.
5. honeycomb core sheet material peeling strength test fixture according to claim 4, it is characterized in that, groove is rectangle structure.
CN201520156566.3U 2015-03-19 2015-03-19 Honeycomb core sheet material peeling strength test fixture Expired - Lifetime CN204461892U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520156566.3U CN204461892U (en) 2015-03-19 2015-03-19 Honeycomb core sheet material peeling strength test fixture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520156566.3U CN204461892U (en) 2015-03-19 2015-03-19 Honeycomb core sheet material peeling strength test fixture

Publications (1)

Publication Number Publication Date
CN204461892U true CN204461892U (en) 2015-07-08

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520156566.3U Expired - Lifetime CN204461892U (en) 2015-03-19 2015-03-19 Honeycomb core sheet material peeling strength test fixture

Country Status (1)

Country Link
CN (1) CN204461892U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105043980A (en) * 2015-08-18 2015-11-11 佛山市顺德区惠美庄材料实业有限公司 Test tool for adhesive strength of honeycomb paper core
CN108072604A (en) * 2016-11-18 2018-05-25 成都飞机工业(集团)有限责任公司 A kind of test device of honeycomb core Joint Strength
CN108645787A (en) * 2018-05-16 2018-10-12 常州市新创智能科技有限公司 Honeycomb core plate electronic stripping tester and its application method
CN109100216A (en) * 2018-09-17 2018-12-28 江西洪都航空工业集团有限责任公司 A kind of missile block hanging load tool structure

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105043980A (en) * 2015-08-18 2015-11-11 佛山市顺德区惠美庄材料实业有限公司 Test tool for adhesive strength of honeycomb paper core
CN108072604A (en) * 2016-11-18 2018-05-25 成都飞机工业(集团)有限责任公司 A kind of test device of honeycomb core Joint Strength
CN108645787A (en) * 2018-05-16 2018-10-12 常州市新创智能科技有限公司 Honeycomb core plate electronic stripping tester and its application method
CN109100216A (en) * 2018-09-17 2018-12-28 江西洪都航空工业集团有限责任公司 A kind of missile block hanging load tool structure
CN109100216B (en) * 2018-09-17 2021-05-18 江西洪都航空工业集团有限责任公司 Guided missile slider hanging and loading tool structure

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Granted publication date: 20150708