| 54 |
Titel |
TI |
[EN] AIRCRAFT FRAMEWORK ASSEMBLY, AIRCRAFT STRUCTURAL FRAMEWORK AND AIRCRAFT |
| 71/73 |
Anmelder/Inhaber |
PA |
AIRBUS OPERATIONS GMBH
|
| 72 |
Erfinder |
IN |
BENTHIEN HERMANN
;
KAISER NILS
|
| 22/96 |
Anmeldedatum |
AD |
23.10.2018 |
| 21 |
Anmeldenummer |
AN |
201811235745 |
|
Anmeldeland |
AC |
CN |
|
Veröffentlichungsdatum |
PUB |
07.05.2019 |
33
31
32 |
Priorität |
PRC
PRN
PRD |
DE
102017219334
20171027
|
| 51 |
IPC-Hauptklasse |
ICM |
B64C 1/06
(2006.01)
|
| 51 |
IPC-Nebenklasse |
ICS |
|
|
IPC-Zusatzklasse |
ICA |
|
|
IPC-Indexklasse |
ICI |
|
|
Gemeinsame Patentklassifikation |
CPC |
B33Y 80/00
B64C 1/061
B64C 1/064
B64C 1/065
B64C 1/069
F16B 37/085
F16B 5/0233
F16B 7/182
F16B 7/20
F16C 2326/43
F16C 7/02
|
|
MCD-Hauptklasse |
MCM |
B64C 1/06
(2006.01)
|
|
MCD-Nebenklasse |
MCS |
|
|
MCD-Zusatzklasse |
MCA |
|
| 57 |
Zusammenfassung |
AB |
[EN] The invention concerns an aircraft framework assembly, an aircraft structural framework and an aircraft. The pole-shaped aircraft framework assembly (10) comprises a first plug-and-turn connector (101) forming a first end of the pole-shaped aircraft framework assembly (10), a second plug-and-turn connector (102) forming a second end of the pole-shaped aircraft framework assembly (10), the second end being opposite the first end, a first rod (110) extending from the first plug-and-turn connector (101) towards the second plug-and-turn connector (102), and a coupling component (12) coupled to thesecond plug-and-turn connector (102) and configured for detachable coupling with the first rod (110). The first rod (110) has a circumferential outer surface including alternately on a circumferential path in a cross-sectional plane of the first rod (110) at least one ridged section (111) and at least one plain section (112), wherein each ridged section (111) includes at least one ridge (113). The coupling component (12) comprises a tubular part (120) having a circumferential inner surface, wherein the circumferential inner surface includes alternately on a circumferential path in a cross-sectional plane of the tubular part (120) at least one ridged section (121) and at least one plain section (122), wherein each ridged section (121) includes at least one ridge (123). |
| 56 |
Entgegengehaltene Patentdokumente/Zitate,
in Recherche ermittelt |
CT |
CN000103523198A
CN000105263804A
US020170159700A1
WO002007031851A1
|
| 56 |
Entgegengehaltene Patentdokumente/Zitate,
vom Anmelder genannt |
CT |
|
| 56 |
Entgegengehaltene Nichtpatentliteratur/Zitate,
in Recherche ermittelt |
CTNP |
??;??;??;: "???????????????????????????????", ?????????, no. 07, 15 February 2016 (2016-02-15), pages 1614 - 1622 0;
???;???;???;???;???;: "????????????????????", ????????(?????), no. 05, 30 September 2016 (2016-09-30), pages 68 - 74 0
|
| 56 |
Entgegengehaltene Nichtpatentliteratur/Zitate,
vom Anmelder genannt |
CTNP |
|
|
Zitierende Dokumente |
|
Dokumente ermitteln
|
|
Sequenzprotokoll |
|
|
|
Prüfstoff-IPC |
ICP |
F16B 37/08
F16B 7/18
F16B 7/20
|
