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Dokument US000011021225B2 (Seiten: 23)

Bibliografische Daten Dokument US000011021225B2 (Seiten: 23)
INID Kriterium Feld Inhalt
54 Titel TI [EN] Aircraft framework assembly, aircraft structural framework and aircraft with an aircraft structural framework
71/73 Anmelder/Inhaber PA AIRBUS OPERATIONS GMBH, DE
72 Erfinder IN BENTHIEN HERMANN, DE ; KAISER NILS, DE
22/96 Anmeldedatum AD 19.10.2018
21 Anmeldenummer AN 201816165245
Anmeldeland AC US
Veröffentlichungsdatum PUB 01.06.2021
33
31
32
Priorität PRC
PRN
PRD
DE
102017219334
20171027
51 IPC-Hauptklasse ICM B64C 1/06 (2006.01)
51 IPC-Nebenklasse ICS F16B 7/18 (2006.01)
F16B 7/20 (2006.01)
IPC-Zusatzklasse ICA B33Y 80/00 (2015.01)
F16B 37/08 (2006.01)
F16B 5/02 (2006.01)
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 F16B 7/18 (2006.01)
F16B 7/20 (2006.01)
MCD-Zusatzklasse MCA B33Y 80/00 (2015.01)
F16B 37/08 (2006.01)
F16B 5/02 (2006.01)
57 Zusammenfassung AB [EN] A pole-shaped aircraft framework assembly including a first plug-and-turn connector forming a first end, a second plug-and-turn connector forming a second end, the second end opposite the first end, a first rod extending from the first plug-and-turn connector towards the second plug-and-turn connector, and a coupling component coupled to the second plug-and-turn connector for detachable coupling with the first rod. The first rod has a circumferential outer surface including alternately on a circumferential path in a cross-sectional plane of the first rod a ridged section and a plain section. The coupling component includes a tubular part having a circumferential inner surface including alternately on a circumferential path in a cross-sectional plane of the tubular part at least one ridged section and at least one plain section. One of the first rod and the coupling component is rotatable relative to the other one, engaging respective ridges of the first rod and the coupling component.
56 Entgegengehaltene Patentdokumente/Zitate,
in Recherche ermittelt
CT US020170058959A1
US020170130766A1
US020170159700A1
US020180323493A1
US020180363689A1
56 Entgegengehaltene Patentdokumente/Zitate,
vom Anmelder genannt
CT DE102015121018A1
EP000002766533B1
EP000003135833A1
EP000003254951A1
FR000002952146A1
US000009091387B2
US000009568040B2
US020090218777A1
US020170235062A1
56 Entgegengehaltene Nichtpatentliteratur/Zitate,
in Recherche ermittelt
CTNP
56 Entgegengehaltene Nichtpatentliteratur/Zitate,
vom Anmelder genannt
CTNP Extended European Search Report for Application No. 18200875.5 dated Apr. 10, 2019. 1;
German Search Report for German Application No. 10 2017 219 334.4 dated Feb. 14, 2018. 1;
Interview Summary for European Application No. 18200875.5 dated Dec. 20, 2019. 1
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Sequenzprotokoll
Prüfstoff-IPC ICP B64C 1/06
F16B 37/08
F16B 5/02
F16B 7/18
F16B 7/20