54 |
Titel |
TI |
[DE] STATORSYSTEM FÜR EINE AXIALFLUSSMASCHINE FÜR EIN FLUGZEUG SOWIE ANTRIEBSSTRANG UND FLUGZEUG DAMIT [EN] STATOR SYSTEM FOR AN AXIAL FLUX MACHINE FOR AN AIRCRAFT, AS WELL AS DRIVE TRAIN AND AIRCRAFT EQUIPPED THEREWITH [FR] SYSTÈME DE STATOR POUR UNE MACHINE À FLUX AXIAL POUR UN AÉRONEF, ET CHAÎNE CINÉMATIQUE ET AÉRONEF ÉQUIPÉ DE CELUI-CI |
71/73 |
Anmelder/Inhaber |
PA |
AIRBUS SAS, FR
|
72 |
Erfinder |
IN |
GALEK MAREK, DE
;
KAPAUN FLORIAN, DE
|
22/96 |
Anmeldedatum |
AD |
09.11.2023 |
21 |
Anmeldenummer |
AN |
23208812 |
|
Anmeldeland |
AC |
EP |
|
Veröffentlichungsdatum |
PUB |
14.05.2025 |
33 31 32 |
Priorität |
PRC PRN PRD |
|
51 |
IPC-Hauptklasse |
ICM |
H02K 3/26
(2006.01)
|
51 |
IPC-Nebenklasse |
ICS |
H02K 11/33
(2016.01)
H02K 16/00
(2006.01)
H02K 16/04
(2006.01)
H02K 21/24
(2006.01)
|
|
IPC-Zusatzklasse |
ICA |
|
|
IPC-Indexklasse |
ICI |
|
|
Gemeinsame Patentklassifikation |
CPC |
H02K 1/182
H02K 1/2798
H02K 11/33
H02K 16/02
H02K 16/04
H02K 21/24
H02K 2211/03
H02K 2213/06
H02K 2213/12
H02K 3/26
|
|
MCD-Hauptklasse |
MCM |
H02K 3/26
(2006.01)
|
|
MCD-Nebenklasse |
MCS |
H02K 11/33
(2016.01)
H02K 16/00
(2006.01)
H02K 16/04
(2006.01)
H02K 21/24
(2006.01)
|
|
MCD-Zusatzklasse |
MCA |
|
57 |
Zusammenfassung |
AB |
[EN] In order to improve an axial flux machine (18) for use of on an aircraft, especially for propulsion of an aircraft, and preferably with regard to reliability and redundancy, the invention provides a stator system (24) for an axial flux machine (18) for an aircraft (10), the stator system (24) comprising a plurality of inverters (32.1-32.n) and a stator (34) including a plurality of disks (36.1-36.n) wherein each disk (36.1-36.n) comprises at least one dielectric substrate (38) and at least a one conductive trace (40.1-40.3) included in at least one conductive layer defined by the dielectric substrate (38), the at least one conductive trace (40.1-40.3) forming at least a part of a winding (42.1-42.3) of a at least one phase of the stator (34), wherein each disk (36.1-36.n) is associated and connected to its own inverter (32.1-32.n). |
56 |
Entgegengehaltene Patentdokumente/Zitate, in Recherche ermittelt |
CT |
EP000003568899B1 EP000004243245A1 KR102023140279A US000008785784B1 US000011710991B2 US020150318751A1 US020190074744A1
|
56 |
Entgegengehaltene Patentdokumente/Zitate, vom Anmelder genannt |
CT |
|
56 |
Entgegengehaltene Nichtpatentliteratur/Zitate, in Recherche ermittelt |
CTNP |
|
56 |
Entgegengehaltene Nichtpatentliteratur/Zitate, vom Anmelder genannt |
CTNP |
|
|
Zitierende Dokumente |
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keine Treffer
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Sequenzprotokoll |
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Prüfstoff-IPC |
ICP |
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