CN107020759A - A kind of localization method for composite material interlayer part honeycomb hole - Google Patents
A kind of localization method for composite material interlayer part honeycomb hole Download PDFInfo
- Publication number
- CN107020759A CN107020759A CN201710078148.0A CN201710078148A CN107020759A CN 107020759 A CN107020759 A CN 107020759A CN 201710078148 A CN201710078148 A CN 201710078148A CN 107020759 A CN107020759 A CN 107020759A
- Authority
- CN
- China
- Prior art keywords
- honeycomb hole
- aperture
- composite material
- localization method
- material interlayer
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping 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
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
- B29L2031/608—Honeycomb structures
Landscapes
- Engineering & Computer Science (AREA)
- Robotics (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
The present invention relates to a kind of localization method for composite material interlayer part honeycomb hole, the composite material interlayer part includes keriotheca and skinning layer；Described skinning layer has aperture, and described keriotheca is provided with honeycomb hole, and described honeycomb hole aperture is more than small aperture；The localization method of described honeycomb hole is the method by described honeycomb hole and aperture concentric locating.This method is simple and practical, efficiency high of mating formation, it is ensured that technical requirement.
Description
Technical field
Mat formation field the present invention relates to composite, honeycomb hole and covering aperture more particularly in composite material interlayer part
Concentric locating method, is also a kind of localization method for composite material interlayer part honeycomb hole.
Background technology
It is that larger on-right angle is lateral opening to be inserted on described aperture, honeycomb, and the inside, which is carried in laminated area, laminated area, one
Individual concentric aperture.The hole position line of laminated area aperture is carried on the forming frock of such part, still, during forming parts,
When covering under the complete honeycomb of paving, laminated area hole position line is capped, it is impossible to recognize its accurate location, when placing honeycomb, not fixed
Position benchmark, it is difficult to ensure that the hole in hole and laminated area on honeycomb is concentric, it is easy to produce error, cause part unqualified.
The content of the invention
The purpose of the present invention is：A kind of localization method for composite material interlayer part honeycomb hole is provided, honeycomb hole is realized
Positioning.
The technical scheme is that：The present invention provides a kind of localization method for composite material interlayer part honeycomb hole,
The composite material interlayer part includes keriotheca and skinning layer；Described skinning layer has aperture, and described keriotheca is provided with honeycomb
Hole, described honeycomb hole aperture is more than small aperture；The localization method of described honeycomb hole is by described honeycomb hole and aperture
The method of concentric locating, comprises the following steps：
Step 1: driving locating slot in frock or mould, and alignment pin is inserted into fixation in locating slot；Described determines
Position pin bottom is fixing end, and top is taper；
Step 2:
Described covering is mated formation onto frock or mould so that passed at the top of alignment pin from aperture；
Step 3: keriotheca is mated formation onto covering, using the circle at the top of the alignment pin passed from aperture as honeycomb hole
The heart, is positioned to described honeycomb hole site.
Beneficial effects of the present invention：
This method is simple and practical, efficiency high of mating formation, it is ensured that technical requirement.
Embodiment
The embodiment to the present invention is described in further details below：
A kind of localization method for composite material interlayer part honeycomb hole is specifically provided, the composite material interlayer part includes honeybee
Nest layer and skinning layer；Described skinning layer has aperture, and described keriotheca is provided with honeycomb hole, and described honeycomb hole aperture is more than
Small aperture；The localization method of described honeycomb hole be by the method for described honeycomb hole and aperture concentric locating, it is including as follows
Step：
Step 1: driving locating slot in frock or mould, and alignment pin is inserted into fixation in locating slot；Described determines
Position pin bottom is fixing end, and top is taper；
Step 2:
Described covering is mated formation onto frock or mould so that passed at the top of alignment pin from aperture；
Step 3: keriotheca is mated formation onto covering, using the circle at the top of the alignment pin passed from aperture as honeycomb hole
The heart, is positioned to described honeycomb hole site.
Claims (1)
1. a kind of localization method for composite material interlayer part honeycomb hole, the composite material interlayer part includes keriotheca and covering
Layer；Described skinning layer has aperture, and described keriotheca is provided with honeycomb hole, and described honeycomb hole aperture is more than small aperture；
The localization method of described honeycomb hole is the method by described honeycomb hole and aperture concentric locating, is comprised the following steps：
Step 1: driving locating slot in frock or mould, and alignment pin is inserted into fixation in locating slot；Described alignment pin
Bottom is fixing end, and top is taper；
Step 2:
Described covering is mated formation onto frock or mould so that passed at the top of alignment pin from aperture；
Step 3: keriotheca is mated formation onto covering, it is right using the alignment pin passed from aperture top as the center of circle of honeycomb hole
Described honeycomb hole site is positioned.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710078148.0A CN107020759A (en) | 2017-02-14 | 2017-02-14 | A kind of localization method for composite material interlayer part honeycomb hole |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710078148.0A CN107020759A (en) | 2017-02-14 | 2017-02-14 | A kind of localization method for composite material interlayer part honeycomb hole |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107020759A true CN107020759A (en) | 2017-08-08 |
Family
ID=59525603
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710078148.0A Pending CN107020759A (en) | 2017-02-14 | 2017-02-14 | A kind of localization method for composite material interlayer part honeycomb hole |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107020759A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109591334A (en) * | 2018-10-12 | 2019-04-09 | 江西昌河航空工业有限公司 | A kind of localization method of pair of honeycomb parts punching |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102555240A (en) * | 2011-12-27 | 2012-07-11 | 成都飞机工业（集团）有限责任公司 | Method for refining skin assembly positioning hole on composite material member |
| CN204357867U (en) * | 2014-09-19 | 2015-05-27 | 上海航天设备制造总厂 | A kind of polylith composite sheet glueds joint proper alignment positioning apparatus |
| CN105035354A (en) * | 2015-08-04 | 2015-11-11 | 航天材料及工艺研究所 | Composite material skin net edge coordination tools and assembling method for skins |
| CN205044193U (en) * | 2015-09-21 | 2016-02-24 | 哈尔滨飞机工业集团有限责任公司 | Close matter honeycomb piece location frock in honeycomb moulding |
-
2017
- 2017-02-14 CN CN201710078148.0A patent/CN107020759A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102555240A (en) * | 2011-12-27 | 2012-07-11 | 成都飞机工业（集团）有限责任公司 | Method for refining skin assembly positioning hole on composite material member |
| CN204357867U (en) * | 2014-09-19 | 2015-05-27 | 上海航天设备制造总厂 | A kind of polylith composite sheet glueds joint proper alignment positioning apparatus |
| CN105035354A (en) * | 2015-08-04 | 2015-11-11 | 航天材料及工艺研究所 | Composite material skin net edge coordination tools and assembling method for skins |
| CN205044193U (en) * | 2015-09-21 | 2016-02-24 | 哈尔滨飞机工业集团有限责任公司 | Close matter honeycomb piece location frock in honeycomb moulding |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109591334A (en) * | 2018-10-12 | 2019-04-09 | 江西昌河航空工业有限公司 | A kind of localization method of pair of honeycomb parts punching |
| CN109591334B (en) * | 2018-10-12 | 2021-04-30 | 江西昌河航空工业有限公司 | Positioning method for punching honeycomb part |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2017160536A3 (en) | Assembly process for automated footwear platform | |
| WO2012048319A8 (en) | Transverse transcranial magnetic stimulation coil placement for improved analgesia | |
| WO2012005524A3 (en) | The printed circuit board and the method for manufacturing the same | |
| GB2488333B (en) | A method of repairing a component | |
| WO2007014106A3 (en) | System and method of delivering radiation therapy to a moving region of interest | |
| WO2009092115A3 (en) | Method and apparatus for enabling machine to machine communication | |
| WO2009148692A3 (en) | Systems and methods for treating autism spectrum disorders (asd) and related dysfunctions | |
| WO2011050344A3 (en) | Cancer immunotherapy and method of treatment | |
| CN107020759A (en) | A kind of localization method for composite material interlayer part honeycomb hole | |
| WO2017040335A3 (en) | Transfection complexes and methods of using the same | |
| EP2727849A3 (en) | Device and method for providing containers with adhesive labels | |
| WO2019103831A3 (en) | Methods for manufacturing an outer skin of a rotor blade | |
| CN203892328U (en) | Board connection nail | |
| WO2013167750A3 (en) | Method for diagnosis and treatment of prolactin associated disorders | |
| CN107755948A (en) | A kind of electric machine stand auxiliary welding equipment and its application | |
| CN204354400U (en) | With the injection mold of inserts guiding mechanism | |
| CN205044193U (en) | Close matter honeycomb piece location frock in honeycomb moulding | |
| CN204446087U (en) | Interlocked intramedullary-nail fitting instrument | |
| CN205502237U (en) | Building is along watering connecting elements of board with post | |
| WO2011107044A3 (en) | Waterproof structure for bonding pad, waterproof bonding pad and method for forming waterproof structure | |
| CN207124128U (en) | A kind of return coil structures of combined switch for automobile | |
| CN207074320U (en) | A kind of localization tool of the anti-assembling off normal of bottom backlight | |
| WO2017221033A3 (en) | An apparatus and method for void forming within a casting | |
| CN204177721U (en) | A kind of FERRITE CORE coating adhesion testing tool | |
| WO2009073426A3 (en) | Fluorinated alkanesulfonic acid anhydrides and processes for making the same |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170808 |