GB201906794D0 - Aircraft panel assembly - Google Patents

Aircraft panel assembly

Info

Publication number
GB201906794D0
GB201906794D0 GBGB1906794.1A GB201906794A GB201906794D0 GB 201906794 D0 GB201906794 D0 GB 201906794D0 GB 201906794 A GB201906794 A GB 201906794A GB 201906794 D0 GB201906794 D0 GB 201906794D0
Authority
GB
United Kingdom
Prior art keywords
panel assembly
aircraft panel
aircraft
assembly
panel
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.)
Withdrawn
Application number
GBGB1906794.1A
Other versions
GB2583940A (en
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.)
Airbus Operations GmbH
Airbus Operations Ltd
Original Assignee
Airbus Operations GmbH
Airbus Operations 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 Airbus Operations GmbH, Airbus Operations Ltd filed Critical Airbus Operations GmbH
Priority to GB1906794.1A priority Critical patent/GB2583940A/en
Publication of GB201906794D0 publication Critical patent/GB201906794D0/en
Priority to EP23196669.8A priority patent/EP4269059A3/en
Priority to US17/298,501 priority patent/US20220024556A1/en
Priority to CN202080006459.6A priority patent/CN113165222A/en
Priority to EP20726742.8A priority patent/EP3894168B1/en
Priority to PCT/EP2020/063249 priority patent/WO2020229501A1/en
Publication of GB2583940A publication Critical patent/GB2583940A/en
Withdrawn legal-status Critical Current

Links

GB1906794.1A 2019-05-14 2019-05-14 Aircraft panel assembly Withdrawn GB2583940A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB1906794.1A GB2583940A (en) 2019-05-14 2019-05-14 Aircraft panel assembly
EP23196669.8A EP4269059A3 (en) 2019-05-14 2020-05-13 Aircraft wing assembly
US17/298,501 US20220024556A1 (en) 2019-05-14 2020-05-13 Aircraft panel assembly
CN202080006459.6A CN113165222A (en) 2019-05-14 2020-05-13 Aircraft panel assembly
EP20726742.8A EP3894168B1 (en) 2019-05-14 2020-05-13 Aircraft wing assembly
PCT/EP2020/063249 WO2020229501A1 (en) 2019-05-14 2020-05-13 Aircraft panel assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1906794.1A GB2583940A (en) 2019-05-14 2019-05-14 Aircraft panel assembly

Publications (2)

Publication Number Publication Date
GB201906794D0 true GB201906794D0 (en) 2019-06-26
GB2583940A GB2583940A (en) 2020-11-18

Family

ID=67384513

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1906794.1A Withdrawn GB2583940A (en) 2019-05-14 2019-05-14 Aircraft panel assembly

Country Status (1)

Country Link
GB (1) GB2583940A (en)

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3739753A1 (en) * 1987-11-24 1989-06-08 Dornier Gmbh Process for producing components from fibre-reinforced plastics
DE19845863B4 (en) * 1998-10-05 2005-05-19 Deutsches Zentrum für Luft- und Raumfahrt e.V. Structural element with large unidirectional stiffness
US20050161861A1 (en) * 2003-09-26 2005-07-28 Brunswick Corporation Apparatus and method for making preforms in mold
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7198739B2 (en) * 2004-05-25 2007-04-03 Honeywell International Inc. Manufacture of thick preform composites via multiple pre-shaped fabric mat layers
US8042767B2 (en) * 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
IL223443A (en) * 2012-12-04 2014-06-30 Elbit Systems Cyclone Ltd Composite material structures with integral composite fittings and methods of manufacture
WO2014175795A1 (en) * 2013-04-25 2014-10-30 Saab Ab A method and a production line for the manufacture of a torsion-box type skin composite structure
GB2516830A (en) * 2013-07-31 2015-02-11 Airbus Operations Ltd Aircraft Structure
US20160101543A1 (en) * 2013-12-03 2016-04-14 The Boeing Company Hybrid Laminate and Molded Composite Structures
WO2017112012A2 (en) * 2015-09-17 2017-06-29 Jerez Roberto Velozzi Load-bearing composite panels, materials, products, and processes to make and use same
GB201522327D0 (en) * 2015-12-17 2016-02-03 Airbus Operations Ltd Wing structure

Also Published As

Publication number Publication date
GB2583940A (en) 2020-11-18

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)