| 54 |
Title |
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 |
Applicant/owner |
PA |
AIRBUS SAS, FR
|
| 72 |
Inventor |
IN |
GALEK MAREK, DE
;
KAPAUN FLORIAN, DE
|
| 22/96 |
Application date |
AD |
Nov 9, 2023 |
| 21 |
Application number |
AN |
23208812 |
|
Country of application |
AC |
EP |
|
Publication date |
PUB |
May 14, 2025 |
33
31
32 |
Priority data |
PRC
PRN
PRD |
|
| 51 |
IPC main class |
ICM |
H02K 3/26
(2006.01)
|
| 51 |
IPC secondary class |
ICS |
H02K 11/33
(2016.01)
H02K 16/00
(2006.01)
H02K 16/04
(2006.01)
H02K 21/24
(2006.01)
|
|
IPC additional class |
ICA |
|
|
IPC index class |
ICI |
|
|
Cooperative patent classification |
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 main class |
MCM |
H02K 3/26
(2006.01)
|
|
MCD secondary class |
MCS |
H02K 11/33
(2016.01)
H02K 16/00
(2006.01)
H02K 16/04
(2006.01)
H02K 21/24
(2006.01)
|
|
MCD additional class |
MCA |
|
| 57 |
Abstract |
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 |
Cited documents identified in the search |
CT |
EP000003568899B1
EP000004243245A1
KR102023140279A
US000008785784B1
US000011710991B2
US020150318751A1
US020190074744A1
|
| 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 |
|
