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1. (WO2018177600) AIRCRAFT DEVICE AND METHOD FOR PRODUCING AN AIRCRAFT DEVICE
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Pub. No.: WO/2018/177600 International Application No.: PCT/EP2018/000139
Publication Date: 04.10.2018 International Filing Date: 29.03.2018
IPC:
B64D 11/06 (2006.01) ,B60N 2/68 (2006.01) ,B60N 2/75 (2018.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
11
Passenger or crew accommodation; Flight-deck installations not otherwise provided for
06
Arrangements or adaptations of seats
B PERFORMING OPERATIONS; TRANSPORTING
60
VEHICLES IN GENERAL
N
VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
2
Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
44
Details or parts not otherwise provided for
68
Seat frames, e.g. for the back-rest
[IPC code unknown for B60N 2/75]
Applicants: E.I.S. AIRCRAFT GMBH[DE/DE]; Kolumbusstrassse 31 53881 Euskirchen, DE
Inventors: ACHILLES, Sven, Ulrich; DE
HUPPERICH, Gerold, Karl; DE
Priority Data:
10 2017 003 121.530.03.2017DE
Title (EN) AIRCRAFT DEVICE AND METHOD FOR PRODUCING AN AIRCRAFT DEVICE
(FR) DISPOSITIF D'AÉRONEF ET PROCÉDÉ DE RÉALISATION D'UN DISPOSITIF D'AÉRONEF
(DE) LUFTFAHRZEUGVORRICHTUNG UND VERFAHREN ZUR HERSTELLUNG EINER LUFTFAHRZEUGVORRICHTUNG
Abstract:
(EN) The invention relates to an aircraft device, in particular an aircraft seating device, comprising at least one load-bearing structural unit (10a-d), which in at least one outer region (12a) of the structural unit (10a-d) consists of a plastic reinforced with reinforcement fibres (14a). It is proposed that the reinforcement fibres (14a) are distributed at least substantially homogeneously over the entire outer region (12a) and/or that the outer region (12a) has substantial load-bearing properties.
(FR) La présente invention concerne un dispositif d'aéronef, notamment un dispositif d'assise d'aéronef, comprenant au moins une unité structurale (10a-d) porteuse de charge, au moins une partie extérieure (12a) de l'unité structurale (10a-d) se composant d'une matière plastique renforcée par fibres de renfort (14a). Selon l'invention, les fibres de renfort (14a) sont réparties de manière au moins sensiblement homogène sur la totalité de la partie extérieure (12a) et/ou la partie extérieure (12a) présente des propriétés de support de charge essentielles.
(DE) Die Erfindung geht aus von einer Luftfahrzeugvorrichtung, insbesondere einer Luftfahrzeugsitzvorrichtung, mit zumindest einer lasttragenden Baueinheit (10a-d), welche in zumindest einem Außenteilbereich (12a) der Baueinheit (10a-d) aus einem mit Verstärkungsfasern (14a) verstärkten Kunststoff besteht. Es wird vorgeschlagen, dass die Verstärkungsfasern (14a) zumindest im Wesentlichen homogen über den gesamten Außenteilbereich (12a) verteilt sind und/oder der Außenteilbereich (12a) wesentliche lasttragende Eigenschaften aufweist.
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Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JO, JP, KE, KG, KH, KN, KP, KR, KW, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, 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, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Office (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (EPO) (AL, 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, RS, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG)
Publication Language: German (DE)
Filing Language: German (DE)