| 54 |
Title |
TI |
[DE] FLUGZEUGRAHMENANORDNUNG, FLUGZEUGSTRUKTURRAHMEN UND FLUGZEUG MIT EINEM FLUGZEUGSTRUKTURRAHMEN
[EN] AIRCRAFT FRAMEWORK ASSEMBLY, AIRCRAFT STRUCTURAL FRAMEWORK AND AIRCRAFT WITH AN AIRCRAFT STRUCTURAL FRAMEWORK
[FR] ENSEMBLE DE STRUCTURE D'AÉRONEF, CADRE STRUCTURAL D'AÉRONEF ET AÉRONEF COMPORTANT UN CADRE STRUCTURAL D'AÉRONEF |
| 71/73 |
Applicant/owner |
PA |
AIRBUS OPERATIONS GMBH, DE
|
| 72 |
Inventor |
IN |
BENTHIEN HERMANN, DE
;
KAISER NILS, DE
|
| 22/96 |
Application date |
AD |
Oct 17, 2018 |
| 21 |
Application number |
AN |
18200875 |
|
Country of application |
AC |
EP |
|
Publication date |
PUB |
May 8, 2019 |
33
31
32 |
Priority data |
PRC
PRN
PRD |
DE
102017219334
20171027
|
| 51 |
IPC main class |
ICM |
B64C 1/06
(2006.01)
|
| 51 |
IPC secondary class |
ICS |
F16B 37/08
(2006.01)
F16B 5/02
(2006.01)
|
|
IPC additional class |
ICA |
|
|
IPC index class |
ICI |
|
|
Cooperative patent classification |
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 main class |
MCM |
B64C 1/06
(2006.01)
|
|
MCD secondary class |
MCS |
F16B 37/08
(2006.01)
F16B 5/02
(2006.01)
|
|
MCD additional class |
MCA |
|
| 57 |
Abstract |
AB |
[EN] The invention concerns a pole-shaped aircraft framework assembly (10) comprising 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 the second 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). The first rod (110) is configured to be inserted into the tubular part (120) of the coupling component (12) in a state where a cross-sectional projection of the at least one ridged section of the first rod (110) coincides with a cross-sectional projection of the at least one plain section of the coupling component (12). One of the first rod (110) and the coupling component (12) is configured to be rotated relative to the other one of the first rod (110) and the coupling component (12), thereby engaging respective ridges of the first rod (113) and the coupling component (123). |
| 56 |
Cited documents identified in the search |
CT |
EP000002766533A1
EP000003135833A1
EP000003254951A1
FR000002952146A1
US020090218777A1
US020170159700A1
|
| 56 |
Cited documents indicated by the applicant |
CT |
|
| 56 |
Cited non-patent literature identified in the search |
CTNP |
|
| 56 |
Cited non-patent literature indicated by the applicant |
CTNP |
|
|
Citing documents |
|
Determine documents
|
|
Sequence listings |
|
|
|
Search file IPC |
ICP |
B64C 1/06
F16B 37/08
F16B 5/02
F16B 7/18
F16B 7/20
|
