| 54 |
Titel |
TI |
[DE] Fluggerät |
| 71/73 |
Anmelder/Inhaber |
PA |
Wiggerich, Burkhard, 59757 Arnsberg, DE
|
| 72 |
Erfinder |
IN |
Wiggerich, Burkhard, 59757 Arnsberg, DE
|
| 22/96 |
Anmeldedatum |
AD |
31.03.2007 |
| 21 |
Anmeldenummer |
AN |
112007001997 |
|
Anmeldeland |
AC |
DE |
|
Veröffentlichungsdatum |
PUB |
28.05.2009 |
33
31
32 |
Priorität |
PRC
PRN
PRD |
DE
102006029603
26.06.2006
|
33
31
32 |
PRC
PRN
PRD |
DE
2007000592
31.03.2007
|
| 51 |
IPC-Hauptklasse |
ICM |
B64C 27/10
(2006.01)
|
| 51 |
IPC-Nebenklasse |
ICS |
B64C 27/20
(2006.01)
|
|
IPC-Zusatzklasse |
ICA |
|
|
IPC-Indexklasse |
ICI |
|
|
Gemeinsame Patentklassifikation |
CPC |
B64U 10/16
B64U 10/80
B64U 2101/70
B64U 30/24
B64U 30/299
B64U 50/19
|
|
MCD-Hauptklasse |
MCM |
B64C 27/10
(2006.01)
|
|
MCD-Nebenklasse |
MCS |
B64C 27/20
(2006.01)
|
|
MCD-Zusatzklasse |
MCA |
|
| 57 |
Zusammenfassung |
AB |
[EN] An aircraft includes at least three drive units, each of which has a first rotor and a first, rotary speed-controlled electrical motor, suitable for driving the first rotor during operation of the aircraft. Each of the drive units has at least a second rotor and at least one second, rotary speed-controlled electrical motor, suitable for driving the second rotor during operation of the aircraft in a rotational direction that is opposite to the rotational direction of the first rotor of each drive unit. Autonomous means for controlling the location and position of the aircraft are also provided. |
| 56 |
Entgegengehaltene Patentdokumente/Zitate,
in Recherche ermittelt |
CT |
|
| 56 |
Entgegengehaltene Patentdokumente/Zitate,
vom Anmelder genannt |
CT |
|
| 56 |
Entgegengehaltene Nichtpatentliteratur/Zitate,
in Recherche ermittelt |
CTNP |
|
| 56 |
Entgegengehaltene Nichtpatentliteratur/Zitate,
vom Anmelder genannt |
CTNP |
|
|
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|
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Sequenzprotokoll |
|
|
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Prüfstoff-IPC |
ICP |
B64C 39/02
|
