FR2952906B1 - AIRCRAFT FLOOR STRUCTURE AND METHOD FOR MANUFACTURING THE SAME - Google Patents
AIRCRAFT FLOOR STRUCTURE AND METHOD FOR MANUFACTURING THE SAMEInfo
- Publication number
- FR2952906B1 FR2952906B1 FR0958277A FR0958277A FR2952906B1 FR 2952906 B1 FR2952906 B1 FR 2952906B1 FR 0958277 A FR0958277 A FR 0958277A FR 0958277 A FR0958277 A FR 0958277A FR 2952906 B1 FR2952906 B1 FR 2952906B1
- Authority
- FR
- France
- Prior art keywords
- manufacturing
- same
- aircraft floor
- floor structure
- floor 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.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D24/00—Producing articles with hollow walls
- B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
- B29D24/005—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
-
- 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
- B64C1/18—Floors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
- B29L2031/3082—Fuselages
-
- 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)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
L'invention concerne une structure support de panneau de plancher d'aéronef, qui est constituée d'un treillis tridimensionnel (1 ) formé d'une seule pièce en matériau composite à base d'une pluralité de plis de fibres longues disposés sensiblement perpendiculairement à une face (7) de réception du panneau de plancher que présente la structure, et de sorte à assurer une continuité des fibres entre des mailles (2) du treillis voisines.The invention relates to an aircraft floor panel support structure, which consists of a three-dimensional mesh (1) formed in one piece of composite material based on a plurality of long fiber plies arranged substantially perpendicular to a face (7) for receiving the floor panel that the structure presents, and so as to ensure continuity of the fibers between the meshes (2) of the neighboring mesh.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0958277A FR2952906B1 (en) | 2009-11-23 | 2009-11-23 | AIRCRAFT FLOOR STRUCTURE AND METHOD FOR MANUFACTURING THE SAME |
| PCT/EP2010/067702 WO2011061234A1 (en) | 2009-11-23 | 2010-11-17 | Aircraft floor structure and method for manufacturing same |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0958277A FR2952906B1 (en) | 2009-11-23 | 2009-11-23 | AIRCRAFT FLOOR STRUCTURE AND METHOD FOR MANUFACTURING THE SAME |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2952906A1 FR2952906A1 (en) | 2011-05-27 |
| FR2952906B1 true FR2952906B1 (en) | 2011-12-16 |
Family
ID=42244553
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR0958277A Expired - Fee Related FR2952906B1 (en) | 2009-11-23 | 2009-11-23 | AIRCRAFT FLOOR STRUCTURE AND METHOD FOR MANUFACTURING THE SAME |
Country Status (2)
| Country | Link |
|---|---|
| FR (1) | FR2952906B1 (en) |
| WO (1) | WO2011061234A1 (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10982439B2 (en) * | 2018-07-13 | 2021-04-20 | The Boeing Company | Dry floor liquid disposal system |
| CN111055513B (en) * | 2018-10-17 | 2021-09-14 | 哈尔滨工业大学 | Preparation method of foldable fiber reinforced resin matrix composite truss and truss |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2872782B1 (en) * | 2004-07-08 | 2007-10-05 | Airbus France Sas | FLOOR FOR AIRCRAFT |
| US7938362B2 (en) * | 2006-02-21 | 2011-05-10 | The Boeing Company | Airplane floor assembly |
| US7967251B2 (en) * | 2008-03-18 | 2011-06-28 | The Boeing Company | Truss network for aircraft floor attachment |
-
2009
- 2009-11-23 FR FR0958277A patent/FR2952906B1/en not_active Expired - Fee Related
-
2010
- 2010-11-17 WO PCT/EP2010/067702 patent/WO2011061234A1/en active Application Filing
Also Published As
| Publication number | Publication date |
|---|---|
| WO2011061234A1 (en) | 2011-05-26 |
| FR2952906A1 (en) | 2011-05-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Kaule et al. | Modeling and testing the mechanical strength of solar cells | |
| EP2100725A4 (en) | TRANSPARENT LAMINATE AND METHOD FOR MANUFACTURING THE SAME | |
| ATE462812T1 (en) | 3D COMPOSITE | |
| EP2280094A4 (en) | METALLIC MATERIAL AND METHOD FOR PRODUCING THE SAME | |
| EP1804562A4 (en) | COMPOSITE MULTILAYER SUBSTRATE AND METHOD FOR MANUFACTURING THE SAME | |
| TW200702835A (en) | Diffusion plate used in direct-type backlight module and method for making the same | |
| DE602005014612D1 (en) | CABLE CONTAINING METAL-CAPSULATED METAL MATRIX COMPOSITE WIRE | |
| EP2159182A4 (en) | METHOD FOR INSPECTING THREADED YARN LINES AND METHOD FOR MANUFACTURING CARBON FIBERS USING THE SAME | |
| FR2886290B1 (en) | METHOD FOR MANUFACTURING A PIECE WITH AN INSERT IN METALLIC MATRIX COMPOSITE MATERIAL AND CERAMIC FIBERS | |
| EP1974791A4 (en) | ALVEOLAR STRUCTURE AND METHOD FOR MANUFACTURING THE SAME | |
| EP2267825A4 (en) | FUEL CELL AND METHOD FOR MANUFACTURING THE SAME | |
| FR2952906B1 (en) | AIRCRAFT FLOOR STRUCTURE AND METHOD FOR MANUFACTURING THE SAME | |
| PE20130789A1 (en) | MEDIUM DENSITY FIBER PANELS | |
| IL191871A0 (en) | Composite material structure with embedded optical fibre and method for repairing same | |
| TW201623748A (en) | Improved acoustic performance of timber frame partitions | |
| JP5156080B2 (en) | Method for scribing bonded substrates | |
| EP1962123A4 (en) | Composite material structure having an embedded optical fibre in one of the surface layers thereof and method for connecting and repairing same | |
| JP2013214643A (en) | Solar cell module | |
| EP2154702A4 (en) | PLASMA DISPLAY PANEL AND METHOD FOR MANUFACTURING THE SAME | |
| ES2401517R1 (en) | AIRCRAFT NOTEBOOK IN COMPOSITE MATERIAL. | |
| CN208428780U (en) | A kind of cellular board | |
| CN209891605U (en) | Crystal glass railing mounting structure of light convenient to overhaul | |
| WO2013114386A8 (en) | 3d fiber composite | |
| JP2012219512A (en) | Frame unit | |
| WO2009156684A3 (en) | Luminous panel and its manufacturing process |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PLFP | Fee payment |
Year of fee payment: 7 |
|
| PLFP | Fee payment |
Year of fee payment: 8 |
|
| PLFP | Fee payment |
Year of fee payment: 9 |
|
| PLFP | Fee payment |
Year of fee payment: 11 |
|
| PLFP | Fee payment |
Year of fee payment: 12 |
|
| PLFP | Fee payment |
Year of fee payment: 13 |
|
| PLFP | Fee payment |
Year of fee payment: 14 |
|
| PLFP | Fee payment |
Year of fee payment: 15 |
|
| ST | Notification of lapse |
Effective date: 20250705 |