GB201718846D0 - Stiffened panel assembly - Google Patents
Stiffened panel assemblyInfo
- Publication number
- GB201718846D0 GB201718846D0 GBGB1718846.7A GB201718846A GB201718846D0 GB 201718846 D0 GB201718846 D0 GB 201718846D0 GB 201718846 A GB201718846 A GB 201718846A GB 201718846 D0 GB201718846 D0 GB 201718846D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- panel assembly
- stiffened panel
- stiffened
- 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- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/064—Stringers; Longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/182—Stringers, longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/187—Ribs
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1718846.7A GB2568469A (en) | 2017-11-15 | 2017-11-15 | Stiffened panel assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1718846.7A GB2568469A (en) | 2017-11-15 | 2017-11-15 | Stiffened panel assembly |
Publications (2)
Publication Number | Publication Date |
---|---|
GB201718846D0 true GB201718846D0 (en) | 2017-12-27 |
GB2568469A GB2568469A (en) | 2019-05-22 |
Family
ID=60788448
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1718846.7A Withdrawn GB2568469A (en) | 2017-11-15 | 2017-11-15 | Stiffened panel assembly |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2568469A (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7134629B2 (en) * | 2004-04-06 | 2006-11-14 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
GB2528078B (en) * | 2014-07-08 | 2020-07-29 | Airbus Operations Ltd | Structure |
GB2528080A (en) * | 2014-07-08 | 2016-01-13 | Airbus Operations Ltd | Structure |
US9809297B2 (en) * | 2015-08-26 | 2017-11-07 | The Boeing Company | Structures containing stiffeners having transition portions |
-
2017
- 2017-11-15 GB GB1718846.7A patent/GB2568469A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2568469A (en) | 2019-05-22 |
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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) |