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1. (WO2007003372) PROCESS FOR PRODUCING A SUBSTANTIALLY SHELL-SHAPED COMPONENT
Latest bibliographic data on file with the International Bureau

Pub. No.: WO/2007/003372 International Application No.: PCT/EP2006/006384
Publication Date: 11.01.2007 International Filing Date: 30.06.2006
IPC:
B29C 70/84 (2006.01) ,B29C 70/44 (2006.01) ,B29D 99/00 (2010.01) ,B64C 1/12 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
29
WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
C
SHAPING OR JOINING OF PLASTICS; SHAPING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL; AFTER- TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
70
Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
68
by incorporating or moulding on preformed parts, e.g. inserts, layers
84
Moulding material on preformed parts to be joined
B PERFORMING OPERATIONS; TRANSPORTING
29
WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
C
SHAPING OR JOINING OF PLASTICS; SHAPING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL; AFTER- TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
70
Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
04
comprising reinforcements only, e.g. self-reinforcing plastics
28
Shaping operations therefor
40
Shaping or impregnating by compression
42
for producing articles of definite length, i.e. discrete articles
44
using isostatic pressure, e.g. pressure difference-, vacuum bag-, autoclave- or expanding rubber-moulding
B PERFORMING OPERATIONS; TRANSPORTING
29
WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
D
PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
99
Subject matter not provided for in other groups of this subclass
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
1
Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
06
Frames; Stringers; Longerons
12
Construction or attachment of skin panels
Applicants:
AIRBUS DEUTSCHLAND GMBH [DE/DE]; Kreetslag 10 21129 Hamburg, DE (AllExceptUS)
LAW, Barnaby [DE/DE]; DE (UsOnly)
SCHUMACHER, Kai [DE/DE]; DE (UsOnly)
KOMADINA, Jonathon [AU/AU]; AU (UsOnly)
MUELLER, Jochen [DE/DE]; DE (UsOnly)
HELTSCH, Norbert [DE/DE]; DE (UsOnly)
Inventors:
LAW, Barnaby; DE
SCHUMACHER, Kai; DE
KOMADINA, Jonathon; AU
MUELLER, Jochen; DE
HELTSCH, Norbert; DE
Agent:
PECKMANN, Ralf; Reinhard, Skuhra, Weise & Partner GbR Postfach 44 01 51 80750 M√ľnchen, DE
Priority Data:
10 2005 030 939.930.06.2005DE
Title (EN) PROCESS FOR PRODUCING A SUBSTANTIALLY SHELL-SHAPED COMPONENT
(FR) PROCÉDÉ PERMETTANT DE PRODUIRE UN COMPOSANT PRÉSENTANT SENSIBLEMENT UNE FORME DE COQUE
Abstract:
(EN) The invention relates to a process for producing a substantially shell-shaped component, from substantially carbon-fiber-reinforced synthetic material having at least one local reinforcing zone 3 and at least one stiffening element, in particular a fuselage shell, a wing shell, a vertical stabilizer shell or horizontal stabilizer shell of an aircraft or the like. The process according to the invention comprises the following steps: arranging at least one doubler 1 which has already been cured, on an at most partially cured shell skin 2 to form the local reinforcing zone 3, applying at least one stiffening element which has already been cured, and placing at least one at most partially cured connecting angle bracket 6 against the at least one stiffening element at least in the region of the at least one doubler 1, and curing the shell skin 2 and the connecting angle bracket 6. The invention also includes a substantially shell-shaped component having at least one local reinforcing zone 3 and having at least one stiffening element produced by the process according to the invention.
(FR) La présente invention concerne un procédé permettant de produire un composant présentant sensiblement une forme de coque, à partir d’une matière synthétique en fibres de carbone sensiblement renforcée comprenant au moins une zone de renforcement local (3) et au moins un élément raidisseur, en particulier une coque de fuselage, une coque d’aile, une coque de stabilisateur vertical ou une coque de stabilisateur horizontal d’un aéronef ou d’un engin analogue. Selon l’invention, le procédé comprend les étapes suivantes : l’agencement d’au moins une tôle de renfort (1) qui a déjà été durcie, sur un revêtement de coque durci au maximum partiellement (2) afin de former une zone de renforcement local (3) ; l’application d’au moins un élément raidisseur qui a déjà été durci, et l’agencement d’au moins une équerre d’angle de raccordement (6), durci au maximum partiellement, contre l’élément raidisseur au moins dans la région de la tôle de renfort (1) ; et le durcissement du revêtement de la coque (2) et du support de l’angle de raccordement (6). Cette invention porte également sur un composant présentant sensiblement une forme de coque qui comprend au moins une zone de renforcement local (3) ainsi qu’au moins un élément raidisseur obtenus grâce au procédé de l’invention.
front page image
Designated States: AE, AG, AL, AM, AT, AU, AZ, BA, BB, BG, BR, BW, BY, BZ, CA, CH, CN, CO, CR, CU, CZ, DE, DK, DM, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, HN, HR, HU, ID, IL, IN, IS, JP, KE, KG, KM, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LT, LU, LV, LY, MA, MD, MG, MK, MN, MW, MX, MZ, NA, NG, NI, NO, NZ, OM, PG, PH, PL, PT, RO, RS, RU, SC, SD, SE, SG, SK, SL, SM, SY, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW
African Regional Intellectual Property Organization (ARIPO) (BW, GH, GM, KE, LS, MW, MZ, NA, SD, SL, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, MD, RU, TJ, TM)
European Patent Office (AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HU, IE, IS, IT, LT, LU, LV, MC, NL, PL, PT, RO, SE, SI, SK, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, ML, MR, NE, SN, TD, TG)
Publication Language: English (EN)
Filing Language: English (EN)
Also published as:
EP1899149BRPI0613477-7JP2009500188RU02404059US20090115088CN101203374
CA2611248