CN105626656A - Anchor nut connection form - Google Patents

Anchor nut connection form Download PDF

Info

Publication number
CN105626656A
CN105626656A CN201410589210.9A CN201410589210A CN105626656A CN 105626656 A CN105626656 A CN 105626656A CN 201410589210 A CN201410589210 A CN 201410589210A CN 105626656 A CN105626656 A CN 105626656A
Authority
CN
China
Prior art keywords
plate nut
composite material
plate
structure part
composite structure
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
CN201410589210.9A
Other languages
Chinese (zh)
Inventor
曾小苗
吴昊
姜华强
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.)
China Aviation Industry General Aircraft Co Ltd
Original Assignee
China Aviation Industry General Aircraft 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 China Aviation Industry General Aircraft Co Ltd filed Critical China Aviation Industry General Aircraft Co Ltd
Priority to CN201410589210.9A priority Critical patent/CN105626656A/en
Publication of CN105626656A publication Critical patent/CN105626656A/en
Pending legal-status Critical Current

Links

Landscapes

  • Connection Of Plates (AREA)

Abstract

The invention relates to an anchor nut connection form, in particular to an installing method of anchor nuts on a composite material structural part. Anchor nut rivets are not directly connected with the composite material structural part, instead, the anchor nuts are fixed to a connecting plate firstly and then the connecting plate is glued to the composite material structural part. The composite material structural part does not need to be provided with rivet connecting holes and only needs to be provided with anchor nut bolt connecting holes. In this way, the rivet holes in the composite material structural part are reduced, the cut-off influence of the rivet holes on composite material fibers is reduced, and the problem that the hole forming distance cannot meet the requirement for the minimum value when the anchor nuts are connected to the composite material structural part is solved.

Description

A kind of plate nut type of attachment
Technical field
Patent of the present invention is a kind of plate nut type of attachment
Background technology
Conventional plate nut connected mode, one plate nut needs to open three holes on composite material parts, two rivet holes and a screw hole, three pitchs of holes are less, it is unsatisfactory for the requirement of the composite pitch-row diameter of bolt more than 4 times, two rivet holes of plate nut are perforate meeting cut staple on composite material parts, and the intensity effect of composite material parts is bigger. Boring also can make composite material parts be layered, and affects part life. This method of attachment is not suitable for composite material parts.
Summary of the invention
Deficiency for plate nut type of attachment, plate nut is first fixed on connecting plate by patent of the present invention by plate nut connection rivet, connecting plate is connected with composite material parts again through the mode gluedd joint, composite material parts only need to output plate nut bolt connecting hole, plate nut rivet interlacement hole need not be opened, solve composite material parts and be connected perforate with plate nut apart from too small, affect composite material parts strength problem.
In order to solve above-mentioned technical problem, patent of the present invention be the technical scheme is that and first fixed by plate nut rivet and connecting plate by plate nut, connecting plate is not belonging to structure-bearing part, again by connecting plate and composite structure part glue joint, composite material parts only need to be outputed the bolt hole that plate nut connects, thoroughly solve composite material parts mounting plate nut connection perforate distance and cross minor issue.
For prior art, patent of the present invention provides the benefit that: need not make the rivet hole that plate nut connects on composite material parts, only need to output plate nut bolt connecting hole, the connection perforate spacing thoroughly solving composite material parts mounting plate nut crosses minor issue, it is greatly improved the composite material parts life-span, it is adaptable to all plate nuts being connected with composite structure part.
Accompanying drawing explanation
Fig. 1 is plate nut connection diagram
In figure, 1 is connecting plate, and 2 be plate nut 3 is adhesive, and 4 is metal welding joints, 5 composite material parts
Detailed description of the invention
The detailed description of the invention of patent of the present invention is further illustrated below in conjunction with accompanying drawing.
Refer to shown in Fig. 1, on 1, only make plate nut rivet interlacement hole, and by 2 and 1 by 2 rivet interlacement, then glued joint connection by 1 and 5 with 3,5 and 4 are made plate nut bolt connecting hole, then is connected 4 with 5 with plate nut connecting bolt.
The above disclosed example being only patent of the present invention, it is impossible to once limit patent of the present invention interest field, the equivalent variations therefore made according to the present patent application the scope of the claims, still belong to the scope that patent of the present invention contains.

Claims (3)

1. a plate nut type of attachment, including connecting plate, plate nut, composite structure part, it is characterized in that plate nut rivet is not directly connected with composite structure part, and is integrally fixed on connecting plate, and composite structure part only need to make plate nut bolt hole.
2. the plate nut type of attachment according to right 1, it is characterized in that: composite structure part need not be opened plate nut connection rivet hole, have only to output plate nut bolt connecting hole, perforate can be reduced composite fiber is cut off, solving composite structure part mounting plate nut perforate many, perforate distance is unsatisfactory for composite perforate required distance.
3. the composite mounting plate nut type of attachment according to right 1 and 2, it is characterised in that: plate nut is first fixed with connecting plate, and composite structure part is only opened plate nut screw connecting hole, connects band plate and composite structure part glue joint.
CN201410589210.9A 2014-10-28 2014-10-28 Anchor nut connection form Pending CN105626656A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410589210.9A CN105626656A (en) 2014-10-28 2014-10-28 Anchor nut connection form

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410589210.9A CN105626656A (en) 2014-10-28 2014-10-28 Anchor nut connection form

Publications (1)

Publication Number Publication Date
CN105626656A true CN105626656A (en) 2016-06-01

Family

ID=56041892

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410589210.9A Pending CN105626656A (en) 2014-10-28 2014-10-28 Anchor nut connection form

Country Status (1)

Country Link
CN (1) CN105626656A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110206798A (en) * 2019-03-14 2019-09-06 苏州同捷汽车工程技术股份有限公司 A kind of fixed structure of nutplate in aluminum profile

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02200943A (en) * 1989-01-27 1990-08-09 Onoda Autoclaved Light Weight Concrete Co Ltd Hole filling structure of counter-sunk hole in lightweight gas concrete panel and form for cap material used in filling structure
CN101595314A (en) * 2006-11-01 2009-12-02 思普斯技术有限责任公司 The nut plate fastener assembly that is used for composite material
JP2010031944A (en) * 2008-07-28 2010-02-12 Sumitomo Forestry Co Ltd Bolt bracket and installation method of bolt bracket
CN103057841A (en) * 2012-12-21 2013-04-24 中航通飞研究院有限公司 Device for conveniently installing and dismantling airplane power supply heat-preserving box
CN104053596A (en) * 2012-01-19 2014-09-17 空中客车营运有限公司 Fastener receptacle strip

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH02200943A (en) * 1989-01-27 1990-08-09 Onoda Autoclaved Light Weight Concrete Co Ltd Hole filling structure of counter-sunk hole in lightweight gas concrete panel and form for cap material used in filling structure
CN101595314A (en) * 2006-11-01 2009-12-02 思普斯技术有限责任公司 The nut plate fastener assembly that is used for composite material
JP2010031944A (en) * 2008-07-28 2010-02-12 Sumitomo Forestry Co Ltd Bolt bracket and installation method of bolt bracket
CN104053596A (en) * 2012-01-19 2014-09-17 空中客车营运有限公司 Fastener receptacle strip
CN103057841A (en) * 2012-12-21 2013-04-24 中航通飞研究院有限公司 Device for conveniently installing and dismantling airplane power supply heat-preserving box

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110206798A (en) * 2019-03-14 2019-09-06 苏州同捷汽车工程技术股份有限公司 A kind of fixed structure of nutplate in aluminum profile

Similar Documents

Publication Publication Date Title
GB2468418A (en) Method for reinforcing composite structures
ATE531617T1 (en) ARRANGEMENT OF TWO FUSION CELL SKINS OF AN AIRCRAFT AND A CONNECTION STRUCTURE FOR CONNECTING THE FULL CELL SKINS
DE602008004513D1 (en) METHOD OF MANUFACTURING A COMPOSITE SKIN IN THE FIELD OF AIR AND SPACE
US20150375795A1 (en) Method of fastening vehicle parts
US20150098755A1 (en) Structural component
CN109532036B (en) Full composite material wing glue joint method and full composite material wing
MX2019010637A (en) Wind turbine blade made of thermoplastic polymer composite, part of said blade and production method.
RU2015151956A (en) GAS TURBINE CONNECTING SHAFT CONSTRUCTION CONTAINING A SHAFT LOCATED BETWEEN THE CONNECTING SHAFT AND ROTOR
US20180193900A1 (en) Blind tack bolt with higher clamp-up strength
CN109025061A (en) A kind of silent Section Column-column connected node of detachable assembling type steel construction
GB0130853D0 (en) Method of forming a bond on or in an aircraft component
CN105626656A (en) Anchor nut connection form
CN103629251A (en) Press mounting method for composite bush
CN204199830U (en) Combined type electric pole
JP2008019566A (en) Column joint structure
CN104477404A (en) Ground validation method of main load-bearing structural member of fuselage under large load
CN204980941U (en) Tower crane that can make up different length attaches wall pole
CN205333429U (en) Combined material draws and cuts experimental frock
CN204061469U (en) Two tack Fast Blind blind rivet
RU2504697C1 (en) Part connection method
CN205244053U (en) Plate fitment or household articles's connection combination piece
CN205527195U (en) Elevator compartment wall
CN204341226U (en) Automobile passage brace panel assembly
CN207458387U (en) A kind of analog machine stringer connection structure
CN103236756B (en) For the motor flange dish fixed jig of tipper

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20160601

WD01 Invention patent application deemed withdrawn after publication