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EP 3 088 301 A8 |
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CORRECTED EUROPEAN PATENT APPLICATION |
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published in accordance with Art. 153(4) EPC |
(15) |
Correction information: |
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Corrected version no 1 (W1 A1) |
(48) |
Corrigendum issued on: |
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17.05.2017 Bulletin 2017/20 |
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Date of publication: |
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02.11.2016 Bulletin 2016/44 |
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Date of filing: 24.12.2014 |
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(51) |
International Patent Classification (IPC):
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(86) |
International application number: |
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PCT/JP2014/084185 |
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International publication number: |
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WO 2015/098983 (02.07.2015 Gazette 2015/26) |
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Designated Contracting States: |
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AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL
NO PL PT RO RS SE SI SK SM TR |
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Priority: |
27.12.2013 JP 2013270938
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Applicant: The Nippon Synthetic Chemical Industry Co., Ltd. |
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Osaka-shi, Osaka 530-0018 (JP) |
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Inventors: |
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- IKEBATA, Akira
Osaka-shi
Osaka 530-0018 (JP)
- SAKAI, Junichiro
Osaka-shi
Osaka 530-0018 (JP)
- KAWAZOE, Yuta
Osaka-shi
Osaka 530-0018 (JP)
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(74) |
Representative: Kuhnen & Wacker |
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Patent- und Rechtsanwaltsbüro
Prinz-Ludwig-Straße 40A 85354 Freising 85354 Freising (DE) |
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(54) |
DOUBLE-SIDED ADHESIVE TAPE FOR FASTENING AIRCRAFT COMPONENTS |
(57) To provide a double-sided pressure-sensitive adhesive tape for fixing aircraft parts
which is excellent in terms of hand tearability, flame retardance, and removability
in a well-balanced manner.
A double-sided pressure-sensitive adhesive tape for fixing aircraft parts which is
a double-sided pressure-sensitive adhesive tape having pressure-sensitive adhesive
layers on both sides of a substrate having hand tearability, characterized in that
when S represents an pressure-sensitive adhesive strength of one pressure-sensitive
adhesive layer (I) and W represents an pressure-sensitive adhesive strength of the
other pressure-sensitive adhesive layer (II), the W is 2-20 N/25 mm and S/W is 1.5
or larger, and the double-sided pressure-sensitive adhesive tape passes the flammability
test as provided for in the United States Federal Aviation Administration fire resistance
standards 14CFR Part 25 Appendix F Part I Section (a) (1) (ii).