FR2977296B1 - METHOD OF CONNECTION BETWEEN OVERLAPPING PIECES ON SEVERAL PLANS AND APPLICATION TO AN AIRCRAFT FUSELAGE PANEL - Google Patents
METHOD OF CONNECTION BETWEEN OVERLAPPING PIECES ON SEVERAL PLANS AND APPLICATION TO AN AIRCRAFT FUSELAGE PANELInfo
- Publication number
- FR2977296B1 FR2977296B1 FR1155738A FR1155738A FR2977296B1 FR 2977296 B1 FR2977296 B1 FR 2977296B1 FR 1155738 A FR1155738 A FR 1155738A FR 1155738 A FR1155738 A FR 1155738A FR 2977296 B1 FR2977296 B1 FR 2977296B1
- Authority
- FR
- France
- Prior art keywords
- parts
- flanges
- aircraft fuselage
- connection
- application
- 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.)
- Expired - Fee Related
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
- B64C1/12—Construction or attachment of skin panels
-
- 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
-
- 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
Abstract
The method involves attaching flanges (42) of a first set of parts (4) to a positioning plane (3). A second set of parts (2) is formed with perforation zones at intervals. Extensions (5) are formed with central openings (53) at periphery of projections (41) of the first set of parts while positioning flanges (22) of the second set of parts on the positioning plane. The extensions partially attached to the flanges of the second set of parts and positioned to support flanges of the first set of parts are attached with the positioning plane through the flanges of the second set of parts. An independent claim is also included for an aircraft fuselage skin panel.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1155738A FR2977296B1 (en) | 2011-06-28 | 2011-06-28 | METHOD OF CONNECTION BETWEEN OVERLAPPING PIECES ON SEVERAL PLANS AND APPLICATION TO AN AIRCRAFT FUSELAGE PANEL |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1155738A FR2977296B1 (en) | 2011-06-28 | 2011-06-28 | METHOD OF CONNECTION BETWEEN OVERLAPPING PIECES ON SEVERAL PLANS AND APPLICATION TO AN AIRCRAFT FUSELAGE PANEL |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2977296A1 FR2977296A1 (en) | 2013-01-04 |
FR2977296B1 true FR2977296B1 (en) | 2013-08-02 |
Family
ID=44543479
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1155738A Expired - Fee Related FR2977296B1 (en) | 2011-06-28 | 2011-06-28 | METHOD OF CONNECTION BETWEEN OVERLAPPING PIECES ON SEVERAL PLANS AND APPLICATION TO AN AIRCRAFT FUSELAGE PANEL |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2977296B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104339290A (en) * | 2013-08-01 | 2015-02-11 | 空中客车运营简化股份公司 | Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3009352B1 (en) | 2013-08-01 | 2016-01-01 | Airbus Operations Sas | TOOLING FOR THE SIMULTANEOUS MAINTENANCE OF SEVERAL FASTENING CLIPS AGAINST AN AIRCRAFT FUSELAGE FRAME ELEMENT |
FR3009274A1 (en) * | 2013-08-01 | 2015-02-06 | Airbus Operations Sas | AIRCRAFT FUSELAGE FRAME ELEMENT INTEGRATING TABS FOR ATTACHING STIFFENERS |
WO2015094059A1 (en) * | 2013-12-20 | 2015-06-25 | Saab Ab | Stiffening element and reinforced structure |
ES2707864T3 (en) * | 2013-12-31 | 2019-04-05 | Airbus Operations Sl | Structure of an aircraft made of composite material |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2489779A1 (en) * | 1980-09-09 | 1982-03-12 | Aerospatiale | FUSELAGE STRUCTURE FOR AN AIRCRAFT RESISTANT TO THE LONGITUDINAL BREAKAGE OF THE EXTERIOR COATING |
JP4318381B2 (en) * | 2000-04-27 | 2009-08-19 | 本田技研工業株式会社 | Manufacturing method of fuselage structure made of fiber reinforced composite material, and fuselage structure manufactured thereby |
US6648273B2 (en) * | 2001-10-30 | 2003-11-18 | The Boeing Company | Light weight and high strength fuselage |
US7159822B2 (en) * | 2004-04-06 | 2007-01-09 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
DE102007029500B4 (en) * | 2007-06-25 | 2013-02-14 | Airbus Operations Gmbh | Method for coupling stiffening profile elements and structural component |
-
2011
- 2011-06-28 FR FR1155738A patent/FR2977296B1/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104339290A (en) * | 2013-08-01 | 2015-02-11 | 空中客车运营简化股份公司 | Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element |
CN104339290B (en) * | 2013-08-01 | 2017-09-26 | 空中客车运营简化股份公司 | Several installs fixtures are maintained to the instrument on aircraft fuselage frame element simultaneously |
Also Published As
Publication number | Publication date |
---|---|
FR2977296A1 (en) | 2013-01-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 5 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
ST | Notification of lapse |
Effective date: 20200206 |