WIPO logo
Mobile | Deutsch | Español | Français | 日本語 | 한국어 | Português | Русский | 中文 | العربية |
PATENTSCOPE

Search International and National Patent Collections
World Intellectual Property Organization
Options
Query Language
Stem
Sort by:
List Length
Some content of this application is unavailable at the moment.
If this situation persist, please contact us atFeedback&Contact
1. (WO2010112644) STRUCTURE FOR ASSEMBLY OF THE PRESSURE BULKHEAD OF AN AIRCRAFT
Latest bibliographic data on file with the International Bureau   

Pub. No.: WO/2010/112644 International Application No.: PCT/ES2010/070115
Publication Date: 07.10.2010 International Filing Date: 04.03.2010
IPC:
B64C 1/10 (2006.01) ,B29C 70/30 (2006.01) ,B29C 70/48 (2006.01)
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
10
Bulkheads
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
30
Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
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
46
using matched moulds, e.g. for deforming sheet moulding compounds (SMC), prepregs
48
and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding (RTM)
Applicants: VERA VILLARES, Enrique[ES/ES]; ES (UsOnly)
OUTON HERNÁNDEZ, Ignacio[ES/ES]; ES (UsOnly)
AIRBUS OPERATIONS, S.L.[ES/ES]; Avenida John Lennon, s/n E-28906 GETAFE (Madrid), ES (AllExceptUS)
Inventors: VERA VILLARES, Enrique; ES
OUTON HERNÁNDEZ, Ignacio; ES
Agent: UNGRIA LÓPEZ, Javier; Avenida Ramón y Cajal, 78 E-28043 Madrid, ES
Priority Data:
P20093001831.03.2009ES
Title (EN) STRUCTURE FOR ASSEMBLY OF THE PRESSURE BULKHEAD OF AN AIRCRAFT
(FR) STRUCTURE D'ASSEMBLAGE DE LA CLOISON ÉTANCHE D'UN AÉRONEF
(ES) ESTRUCTURA DE ENSAMBLAJE DEL MAMPARO DE PRESIÓN DE UNA AERONAVE
Abstract:
(EN) The structure comprises: a bulkhead ring (22) including a front portion and a rear portion which is inclined upwards and rearwards and by means of which the pressure bulkhead (1) is connected, a simple frame (18) which is connected to the front portion of the bulkhead ring (22), an extended flange plate (23) which is arranged between the front portion of the bulkhead ring (22) and the skin (6, 7), and tensioning attachments (24, 25) coupled between the extended flange plate (23) and the stringers (8, 9).
(FR) La présente invention concerne une structure comprenant: un anneau de cloison (22) pourvu d'une portion avant et d'une portion arrière inclinée vers le bas et vers l'arrière et permettant le raccordement à la cloison étanche (1); une couple de fuselage simple (18) conçu pour être raccordé à la portion avant de l'anneau de cloison (22); une plate-bande allongée (23) qui est ménagée entre la portion avant de l'anneau de cloison (22) et le revêtement (6, 7); et des ferrures de tension (24, 25) qui sont raccordées entre la plate-bande allongée (23) et les lisses (8, 9).
(ES) La estructura comprende: un anillo de mamparo (22) con una porción anterior y una porción posterior inclinada hacia 5 arriba y hacia atrás, por la que se conecta al mamparo de presión(1); una cuaderna simple (18), que se conecta a la porción anterior del anillo de mamparo (22); una platabanda extendida (23), que se dispone entre la porción anterior del anillo de mamparo (22) y el revestimiento (6, 7); y unos 10 herrajes de tensión (24,25), que se acoplan entre la platabanda extendida (23) y los larguerillos (8,9).
front page image
Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IS, JP, KE, KG, KM, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LT, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PE, PG, PH, PL, PT, RO, RS, RU, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, 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 Office (AM, AZ, BY, KG, KZ, MD, RU, TJ, TM)
European Patent Office (EPO) (AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, ML, MR, NE, SN, TD, TG)
Publication Language: Spanish (ES)
Filing Language: Spanish (ES)