BE428581A - - Google Patents
Info
- Publication number
- BE428581A BE428581A BE428581DA BE428581A BE 428581 A BE428581 A BE 428581A BE 428581D A BE428581D A BE 428581DA BE 428581 A BE428581 A BE 428581A
- Authority
- BE
- Belgium
- Prior art keywords
- wing
- parts
- cells
- vertical
- wing according
- Prior art date
Links
- 239000000463 material Substances 0.000 claims description 26
- 238000010276 construction Methods 0.000 claims description 15
- 239000004033 plastic Substances 0.000 claims description 12
- 229920003023 plastic Polymers 0.000 claims description 12
- 210000000614 Ribs Anatomy 0.000 claims description 5
- 230000003014 reinforcing Effects 0.000 claims description 4
- 229920003002 synthetic resin Polymers 0.000 claims description 4
- 239000000057 synthetic resin Substances 0.000 claims description 4
- 239000001913 cellulose Substances 0.000 claims description 3
- 229920002678 cellulose Polymers 0.000 claims description 3
- 239000000945 filler Substances 0.000 claims description 3
- 239000005011 phenolic resin Substances 0.000 claims description 2
- 229920001568 phenolic resin Polymers 0.000 claims description 2
- 230000003247 decreasing Effects 0.000 claims 1
- 230000018109 developmental process Effects 0.000 claims 1
- 239000002184 metal Substances 0.000 description 12
- 229910052751 metal Inorganic materials 0.000 description 12
- 239000002023 wood Substances 0.000 description 8
- 239000011248 coating agent Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000002787 reinforcement Effects 0.000 description 3
- 210000001503 Joints Anatomy 0.000 description 2
- 239000002253 acid Substances 0.000 description 2
- 150000007513 acids Chemical class 0.000 description 2
- 239000000789 fastener Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000004566 building material Substances 0.000 description 1
- 238000005253 cladding Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000000875 corresponding Effects 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 210000000056 organs Anatomy 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 230000001681 protective Effects 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE428581A true BE428581A (zh) |
Family
ID=88921
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE428581D BE428581A (zh) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE428581A (zh) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2008007135A2 (en) * | 2006-07-13 | 2008-01-17 | Airbus Uk Limited | A wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof |
-
0
- BE BE428581D patent/BE428581A/fr unknown
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2008007135A2 (en) * | 2006-07-13 | 2008-01-17 | Airbus Uk Limited | A wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof |
| WO2008007135A3 (en) * | 2006-07-13 | 2008-05-22 | Airbus Uk Ltd | A wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof |
| US8398024B2 (en) | 2006-07-13 | 2013-03-19 | Airbus Operations Limited | Wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA1311735C (fr) | Pale pour rotor d'helicoptere en materiau composite multilongeron a caissons de torsion et son procede de fabrication | |
| EP0346210B1 (fr) | Cadre en matériau composite notamment pour fuselage d'aéronef, et son procédé de fabrication | |
| EP0256916B1 (fr) | Pale en matériaux composites, à structure bilongeron et bicaisson, et à revêtements stratifiés à sandwich de nid d'abeilles, et son procédé de fabrication | |
| EP2121295B1 (fr) | Procede de realisation de raidisseurs en materiau composite | |
| EP2665597B1 (fr) | Ferrure multi-branche en materiau composite et procede de fabrication d'une telle ferrure multi-branche | |
| EP2242683B1 (fr) | Panneau composite monolithique auto-raidi et pivotant, notamment pour une partie mobile d'aeronef | |
| CA2726499C (fr) | Procede d'assemblage orbital de troncons d'aeronef en materiau composite | |
| FR2732664A1 (fr) | Poutre pour un aeronef | |
| EP0296964A1 (fr) | Pale en matériaux composites, à noyau structural et revêtement d'habillage profilé, et son procédé de fabrication | |
| FR3060650A1 (fr) | Structure d'entree d'air pour une nacelle d'aeronef | |
| FR3069185A1 (fr) | Profil aerodynamique a noyau creux oblong arrondi en materiau composite renforce par un textile a fibres unidirectionnelles | |
| EP2435301B1 (fr) | Procédé pour la fabrication d'un panneau structurant composite de bord de fuite pour un élément d'un aéronef | |
| BE428581A (zh) | ||
| EP1928648B1 (fr) | Procede de reparation d'une peau externe de structure composite | |
| FR3000019A1 (fr) | Raidisseur de fuselage d'aeronef forme a l'aide d'une tole repliee sur elle-meme | |
| EP2512915A2 (fr) | Procédé de fabrication d'un panneau de composite de bord de fuite pour un élément d'aéronef | |
| CA2775726C (fr) | Panneau en materiau composite | |
| FR2764840A1 (fr) | Systeme d'assemblage pour des structures sandwichs composites renforcees par des fibres en construction modulaire | |
| FR2946009A1 (fr) | Panneau structurant composite de bord de fuite pour un element d'aeronef | |
| FR2599331A1 (fr) | Pelle creuse pour rame de bateau et son procede de fabrication | |
| BE434808A (zh) | ||
| WO2014199066A1 (fr) | Procédé de fabrication d'une pièce composite | |
| FR2712939A1 (fr) | Elément d'assemblage composite, procédé de fabrication et article composite utilisant cet élément d'assemblage. | |
| WO2021165268A1 (fr) | Procede de fabrication d'une structure aerodynamique d'aeronef et structure aerodynamique d'aeronef ainsi obtenue | |
| FR3101064A1 (fr) | Procédé d’assemblage d’une structure primaire d’un mât d’aéronef, structure primaire d’un mât d’aéronef ainsi obtenue et aéronef comprenant ladite structure primaire |