Spring-back of Thick Uni-Directional Carbon Fibre Reinforced Composite Laminate for Aircraft Structure Application

The springback phenomena of CFRP after curing process through autoclave manufacturing method results on the out of tolerance for its utilisation in aerospace industry. This paper relates to the measurements of springback for Uni-directional flat laminate as a first steps to the springback study for...

Full description

Saved in:
Bibliographic Details
Published inJournal of physics. Conference series Vol. 1005; no. 1; pp. 12003 - 12009
Main Authors Zakaria, M, Aminanda, Y, Rashidi, S A, Sah, M A Mat
Format Journal Article
LanguageEnglish
Published Bristol IOP Publishing 01.04.2018
Subjects
Aerospace industry
Aircraft
Aircraft structures
Carbon fibers
Fiber composites
Lay-up
Micrometers
Optical scanners
Physics
Production methods
Springback
Online AccessGet full text

Cover

Abstract The springback phenomena of CFRP after curing process through autoclave manufacturing method results on the out of tolerance for its utilisation in aerospace industry. This paper relates to the measurements of springback for Uni-directional flat laminate as a first steps to the springback study for the real aircraft composite laminate structures. A flat laminate with dimension of 300 mm x 300 mm, 400 mm x 400 mm and 500mm x 500 mm with different number of ply; 20, 24 and 28 are manufactured. The choice of dimension and number of lay-up corresponds to the dimension and lay-up of rib structure. After process, the springbacks are measured using 3D scanner (optical-based three-dimensional) with an accuracy of 42 micrometers to obtain an accurate measurement. The analysis of the effect of dimension and number of ply to the magnitude of springback are presented within the range of specimen studied in this work.
AbstractList The springback phenomena of CFRP after curing process through autoclave manufacturing method results on the out of tolerance for its utilisation in aerospace industry. This paper relates to the measurements of springback for Uni-directional flat laminate as a first steps to the springback study for the real aircraft composite laminate structures. A flat laminate with dimension of 300 mm x 300 mm, 400 mm x 400 mm and 500mm x 500 mm with different number of ply; 20, 24 and 28 are manufactured. The choice of dimension and number of lay-up corresponds to the dimension and lay-up of rib structure. After process, the springbacks are measured using 3D scanner (optical-based three-dimensional) with an accuracy of 42 micrometers to obtain an accurate measurement. The analysis of the effect of dimension and number of ply to the magnitude of springback are presented within the range of specimen studied in this work.
Author Aminanda, Y
Zakaria, M
Rashidi, S A
Sah, M A Mat
Author_xml – sequence: 1
  givenname: M
  surname: Zakaria
  fullname: Zakaria, M
  organization: CTRM AC , Malaysia
– sequence: 2
  givenname: Y
  surname: Aminanda
  fullname: Aminanda, Y
  email: yulfian@iium.edu.my
  organization: International Islamic University Malaysia , Malaysia
– sequence: 3
  givenname: S A
  surname: Rashidi
  fullname: Rashidi, S A
  organization: Aerospace Malaysia Innovation Centre , Malaysia
– sequence: 4
  givenname: M A Mat
  surname: Sah
  fullname: Sah, M A Mat
  organization: CTRM Test Laboratory , Malaysia
BookMark eNqFkN1LwzAUxYNMcJv-DQZ8E2qTph_J46jODwaK255DmiaauTU1aR_8702pKILgfbkH7jkH7m8GJo1tFADnGF1hRGmMizSJ8ozlMUYoi3GMcIIQOQLT78vkW1N6Ambe74IhTDEFbt0607xElZBv0Gq4eTVBbBsTXRunZGdsI_awFK6yDVyayin4rEyjrZOqhqU9tNabTsGVOJhGBBEucGGcdEJ3cN25XnZ9CC3adm-kGPpOwbEWe6_OvvYcbJc3m_IuWj3e3peLVSRTTLpIaMZwTlmqaUaKGlPCpFAiJynLa5XRVLIcVVhjIXHFNGGMIpFUdZUyWtMckzm4GHtbZ9975Tu-s70L73ieZEWCGS1YGlzF6JLOeu-U5gHIQbgPjhEfAPMBHR8w8gEwx3wEHJJkTBrb_lT_n7r8I_XwVK5_G3lba_IJSVuMvQ
CitedBy_id crossref_primary_10_1016_j_measurement_2020_108867
crossref_primary_10_3390_app12105288
crossref_primary_10_3390_ma16134844
Cites_doi 10.1177/0021998302036021784
10.1016/S0266-3538(03)00172-6
10.1016/j.compositesa.2005.05.019
10.1016/S1359-835X(03)00131-3
10.1016/j.compositesa.2005.05.006
10.1016/S0266-3538(01)00148-8
10.1016/j.compstruct.2013.07.020
10.1016/j.compstruct.2014.09.069
10.1016/j.compstruct.2015.01.005
10.1016/S1359-835X(03)00132-5
10.1177/0021998313501532
10.1016/S0263-8223(03)00117-X
10.4028/www.scientific.net/AMM.606.113
ContentType Journal Article
Copyright Published under licence by IOP Publishing Ltd
2018. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
Copyright_xml – notice: Published under licence by IOP Publishing Ltd
– notice: 2018. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
DBID O3W
TSCCA
AAYXX
CITATION
8FD
8FE
8FG
ABUWG
AFKRA
ARAPS
AZQEC
BENPR
BGLVJ
CCPQU
DWQXO
H8D
HCIFZ
L7M
P5Z
P62
PIMPY
PQEST
PQQKQ
PQUKI
PRINS
DOI 10.1088/1742-6596/1005/1/012003
DatabaseName IOP Publishing Free Content
IOPscience (Open Access)
CrossRef
Technology Research Database
ProQuest SciTech Collection
ProQuest Technology Collection
ProQuest Central (Alumni)
ProQuest Central
Advanced Technologies & Aerospace Collection
ProQuest Central Essentials
ProQuest Central
Technology Collection
ProQuest One Community College
ProQuest Central Korea
Aerospace Database
SciTech Premium Collection (Proquest) (PQ_SDU_P3)
Advanced Technologies Database with Aerospace
Advanced Technologies & Aerospace Database
ProQuest Advanced Technologies & Aerospace Collection
Publicly Available Content Database
ProQuest One Academic Eastern Edition (DO NOT USE)
ProQuest One Academic
ProQuest One Academic UKI Edition
ProQuest Central China
DatabaseTitle CrossRef
Publicly Available Content Database
Advanced Technologies & Aerospace Collection
Technology Collection
Technology Research Database
ProQuest Advanced Technologies & Aerospace Collection
ProQuest Central Essentials
ProQuest One Academic Eastern Edition
ProQuest Central (Alumni Edition)
SciTech Premium Collection
ProQuest One Community College
ProQuest Technology Collection
ProQuest SciTech Collection
ProQuest Central China
ProQuest Central
Advanced Technologies & Aerospace Database
Aerospace Database
ProQuest One Academic UKI Edition
ProQuest Central Korea
ProQuest One Academic
Advanced Technologies Database with Aerospace
DatabaseTitleList
Publicly Available Content Database
Database_xml – sequence: 1
  dbid: O3W
  name: IOP Publishing Free Content
  url: http://iopscience.iop.org/
  sourceTypes:
    Enrichment Source
    Publisher
– sequence: 2
  dbid: 8FG
  name: ProQuest Technology Collection
  url: https://search.proquest.com/technologycollection1
  sourceTypes: Aggregation Database
DeliveryMethod fulltext_linktorsrc
Discipline Physics
DocumentTitleAlternate Spring-back of Thick Uni-Directional Carbon Fibre Reinforced Composite Laminate for Aircraft Structure Application
EISSN 1742-6596
ExternalDocumentID 10_1088_1742_6596_1005_1_012003
JPCS_1005_1_012003
GroupedDBID 1JI
29L
2WC
4.4
5B3
5GY
5PX
5VS
7.Q
AAJIO
AAJKP
AALHV
ABHWH
ACAFW
ACHIP
AEFHF
AEJGL
AFKRA
AFYNE
AIYBF
AKPSB
ALMA_UNASSIGNED_HOLDINGS
ARAPS
ASPBG
ATQHT
AVWKF
AZFZN
BENPR
BGLVJ
CCPQU
CEBXE
CJUJL
CRLBU
CS3
DU5
E3Z
EBS
EDWGO
EJD
EQZZN
F5P
FRP
GROUPED_DOAJ
GX1
HCIFZ
HH5
IJHAN
IOP
IZVLO
J9A
KNG
KQ8
LAP
N5L
N9A
O3W
OK1
P2P
PIMPY
PJBAE
RIN
RNS
RO9
ROL
SY9
T37
TR2
TSCCA
UCJ
W28
XSB
~02
02O
1WK
AAYXX
AERVB
AHSEE
BBWZM
C1A
CITATION
FEDTE
H13
HVGLF
JCGBZ
M48
Q02
S3P
8FD
8FE
8FG
ABUWG
AZQEC
DWQXO
H8D
L7M
P62
PQEST
PQQKQ
PQUKI
PRINS
ID FETCH-LOGICAL-c413t-af9916894f8537d1839caea63496de584c960b1f1ac1b9f39980a2bdb498d8613
IEDL.DBID IOP
ISSN 1742-6588
IngestDate Thu Oct 10 17:31:24 EDT 2024
Thu Sep 26 18:49:35 EDT 2024
Wed Aug 21 03:40:18 EDT 2024
Thu Jan 07 13:49:18 EST 2021
IsDoiOpenAccess true
IsOpenAccess true
IsPeerReviewed true
IsScholarly true
Issue 1
Language English
License Content from this work may be used under the terms of the Creative Commons Attribution 3.0 licence. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.
LinkModel DirectLink
MergedId FETCHMERGED-LOGICAL-c413t-af9916894f8537d1839caea63496de584c960b1f1ac1b9f39980a2bdb498d8613
OpenAccessLink https://proxy.k.utb.cz/login?url=https://iopscience.iop.org/article/10.1088/1742-6596/1005/1/012003
PQID 2572198794
PQPubID 4998668
PageCount 7
ParticipantIDs iop_journals_10_1088_1742_6596_1005_1_012003
proquest_journals_2572198794
crossref_primary_10_1088_1742_6596_1005_1_012003
PublicationCentury 2000
PublicationDate 20180401
PublicationDateYYYYMMDD 2018-04-01
PublicationDate_xml – month: 04
  year: 2018
  text: 20180401
  day: 01
PublicationDecade 2010
PublicationPlace Bristol
PublicationPlace_xml – name: Bristol
PublicationTitle Journal of physics. Conference series
PublicationTitleAlternate J. Phys.: Conf. Ser
PublicationYear 2018
Publisher IOP Publishing
Publisher_xml – name: IOP Publishing
References 11
12
13
14
Airbus Operation GmbH. RIB-MAIN 05 (15) 2011
Zaharia V D (17) 2014; 55
1
2
3
4
5
6
Hahn HT. (8) 1984; 32
Hexagon Metrology. HP-L-8.9 LASER SCANNER (16)
7
9
Hexagon Metrology. Romer Absolute Arm (18)
10
References_xml – ident: 5
  doi: 10.1177/0021998302036021784
– ident: 3
  doi: 10.1016/S0266-3538(03)00172-6
– ident: 18
  publication-title: Factsheet No. 797356, Wetzlar 2015
  contributor:
    fullname: Hexagon Metrology. Romer Absolute Arm
– ident: 2
  doi: 10.1016/j.compositesa.2005.05.019
– ident: 4
  doi: 10.1016/S1359-835X(03)00131-3
– volume: 32
  start-page: 253
  year: 1984
  ident: 8
  publication-title: J Astro Sci.
  contributor:
    fullname: Hahn HT.
– ident: 1
  doi: 10.1016/j.compositesa.2005.05.006
– ident: 6
  doi: 10.1016/S0266-3538(01)00148-8
– ident: 9
  doi: 10.1016/j.compstruct.2013.07.020
– year: 2011
  ident: 15
  publication-title: Drawing Number V57591144-02
  contributor:
    fullname: Airbus Operation GmbH. RIB-MAIN 05
– ident: 12
  doi: 10.1016/j.compstruct.2014.09.069
– ident: 14
  doi: 10.1016/j.compstruct.2015.01.005
– ident: 10
  doi: 10.1016/S1359-835X(03)00132-5
– ident: 16
  publication-title: Product Brochure, No. 839991, Wetzlar 2015
  contributor:
    fullname: Hexagon Metrology. HP-L-8.9 LASER SCANNER
– volume: 55
  year: 2014
  ident: 17
  publication-title: Mediamira Science Publisher
  contributor:
    fullname: Zaharia V D
– ident: 7
  doi: 10.1177/0021998313501532
– ident: 11
  doi: 10.1016/S0263-8223(03)00117-X
– ident: 13
  doi: 10.4028/www.scientific.net/AMM.606.113
SSID ssj0033337
Score 2.227757
Snippet The springback phenomena of CFRP after curing process through autoclave manufacturing method results on the out of tolerance for its utilisation in aerospace...
SourceID proquest
crossref
iop
SourceType Aggregation Database
Enrichment Source
Publisher
StartPage 12003
SubjectTerms Aerospace industry
Aircraft
Aircraft structures
Carbon fibers
Fiber composites
Lay-up
Micrometers
Optical scanners
Physics
Production methods
Springback
SummonAdditionalLinks – databaseName: ProQuest Central
  dbid: BENPR
  link: http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwhV3dS8MwEA9uIvgifuJ0SkAfDWvTdkmeZI6NISqyD9hbSdIEh7DWbf7_XtqUMQTtU2muL5fkfr-7XO4Qug9tbHjCIqJYIEnMIkGkYYzEEQewCACgtYt3vL51R7P4eZ7MfcBt7dMqa5tYGuos1y5G3oGlRZ2DLOLH4ou4rlHudNW30GigfQqeAm2i_afB2_u4tsURPKy6EkkJYC2vM7zA7fPfRBcMR5B0wo67Rlr3zvL41FjkxS8jXSLP8BgdecqIe9Ucn6A9szxFB2Xqpl6foVUVmyNK6k-cWzz9WMALcEnizZnj2rgvVypf4iF4xwaPTVkvVZsMO3vg8rYMfpEuKwZeYAT3Fiu9knaDJ2V92W_4qbc96j5Hs-Fg2h8R30mBaACpDZHW0UAuYgvozDLHirQ0suuqxWcGOIgGR0aFNpQ6VMICaeGBpCpTseAZB8S_QM1lvjSXCCeUCaGEZpFRsPmpotZQocDtk-DdGNVCQa2_tKgKZqTlQTfnqVN56lTuKiUnaZhWKm-hB9Bz6jfP-n_xux3x5_f-ZFciLTLbQu162rai20V09ffwNToEZsSrFJ02aoKuzQ2wj4269UvsB1OD0RE
  priority: 102
  providerName: ProQuest
Title Spring-back of Thick Uni-Directional Carbon Fibre Reinforced Composite Laminate for Aircraft Structure Application
URI https://iopscience.iop.org/article/10.1088/1742-6596/1005/1/012003
https://www.proquest.com/docview/2572198794
Volume 1005
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwpV3dT9swED8N0CReYGMgCqyyNB7nNp-1_VgqOoYGVHwI3iLbsUWF1FalvPDXcxcngjJN07Q8RFZyTpyLc_c7-_wLwGHsMydzkXIjIs0zkSqunRA8SyU6iwgdtKXxjrPz3slNdnqX371dCzOd1aa_g8VAFBxUWCfEyS5i6IT3ctXDI1Hejbu0_pMIP9dS_GKoZ_-8GDXWOMVNhEWRVEnKJsfrzxda8lAr2IrfzHTle4abYJtWh5STh87TwnTs8ztCx_97rE-wUUNT1g81PsMHN9mCj1WKqH38AvMwBsiNtg9s6tn1_RgLiFl5bTYJ07OBnpvphA0xCnfs0lW8rNaVjOwO5Yc59ktT9g0W8Azrj-d2rv2CXVU8tk9Yqf86pb4NN8Pj68EJr__YwC06wwXXnuCmVJlHFCBKQl9WO90jVvrSIdaxGDCZ2MfaxkZ5BEcy0okpTaZkKRFZ7MDqZDpxu8DyRChllBWpM2hkEpN4lyiD4aXGKMqZFkTNWypmgZijqCbUpSxIlQWpkhiZ8yIugipb8B2VX9Qf6ePfxb8tiZ-OBlfLEsWs9C04aDrHqyjawYRGc1S292_33Id1RGQypAYdwCrq3n1F1LMwbViRwx9tWDs6Ph9dtskD5e2qq-P-Ir19ATeu9CE
link.rule.ids 315,783,787,12779,21402,27938,27939,33387,33758,38879,38904,43614,43819,53856,53882
linkProvider IOP Publishing
linkToHtml http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwhV1Li9swEBZNSulelj5pumkraI8V8TOSTksI6023SShNArkJSZZoWIhTJ_3_nbFlwlLo-mSs8WUkzffNaDRDyJfYZ07kPGWGR5plPJVMO85ZlgoAiwgA2mK8Y7EczzbZ3TbfhoDbMaRVdjaxMdRlZTFGPoKllaCDLLPrw2-GXaPwdDW00OiRp1kKQIM3xYvbzhKn8PD2QmTCAGlFl98FTl_4JsdgNqJ8FI_wEmnXOSugU29XHf4x0Q3uFC_IZSCMdNLO8EvyxO1fkWdN4qY9viZ1G5ljRtt7Wnm6_rWDF2CSLBgzZNp0qmtT7WkBvrGjP11TLdW6kqI1wKwtR-cac2LgBUboZFfbWvsTXTXVZf_AT5PzQfcbsilu1tMZC30UmAWIOjHtkQQKmXnAZl4iJ7La6THWii8dMBALboyJfaxtbKQHyiIinZjSZFKUAvD-Lenvq717R2iecCmNtDx1BrZ-YhLvEmnA6dPg2zgzIFGnP3Voy2Wo5phbCIUqV6hyrJOcq1i1Kh-Qr6BnFbbO8XHxzw_E735MVw8l1KH0AzLspu0sel5C7_8__Ik8n60XczX_tvx-RS6AI4k2WWdI-qB39wF4yMl8bBbbX7Cs0pw
linkToPdf http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwpV3dT9swED9BERMvjLFNlHVgCR7nNp-1_Vh1i4DxUfEh8WbZjj0QUluV8sJfv3OcDBWEJkSerOQcO3f23e_s8wVgP3aZ5TlLqWaRohlLBVWWMZqlHI1FhAba-PWOk9P-wVV2dJ1fL0Hx7yzMZFqr_i4WQ6LgwMI6II73EEMntJ-LPt6J8l7c8-c_o7Q3Ld0yrOAEzv1IPzwbNRo5xYuFg5G-IudNnNfrL1uwUsvYkxequrI_xUf40_Q8hJ3cdR_mumsenyV1fP-nbcB6DVHJINT6BEt2vAmrVaiouf8Ms7AWSLUyd2TiyOXNLRYQu9JafXpsT4ZqpidjUqA3bsm5rfKzGlsSr398nJglx8pH4WABn5DB7czMlJuTiyqf7QNWGjxtrX-Bq-LX5fCA1n9uoAaN4pwq52EnF5lDNMBKj8KMsqrvs9OXFjGPQcdJxy5WJtbCIUjikUp0qTPBS44I4yu0xpOx3QKSJ0wILQxLrUZlk-jE2URodDMVelNWtyFqJCWnIUGHrDbWOZeendKz02dmzmUsAzvb8AMFIOvJev9_8r0F8qPR8GKRQqJ82tBpBsgTKerDxK_qiGz7bW3uwofRz0IeH57-_gZrCNJ4iBbqQAvFYL8jEJrrnWqU_wUBf_Uh
openUrl ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=Spring-back+of+Thick+Uni-Directional+Carbon+Fibre+Reinforced+Composite+Laminate+for+Aircraft+Structure+Application&rft.jtitle=Journal+of+physics.+Conference+series&rft.au=Zakaria%2C+M&rft.au=Aminanda%2C+Y&rft.au=Rashidi%2C+S+A&rft.au=Sah%2C+M+A+Mat&rft.date=2018-04-01&rft.pub=IOP+Publishing&rft.issn=1742-6588&rft.eissn=1742-6596&rft.volume=1005&rft.issue=1&rft_id=info:doi/10.1088%2F1742-6596%2F1005%2F1%2F012003&rft.externalDocID=JPCS_1005_1_012003
thumbnail_l http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1742-6588&client=summon
thumbnail_m http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1742-6588&client=summon
thumbnail_s http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1742-6588&client=summon