| 54 |
Title |
TI |
[DE] SYSTEM ZUR BEREITSTELLUNG VON TEMPERATURGEREGELTEM WASSER IN EINEM FLUGZEUG
[EN] SYSTEM FOR PROVIDING TEMPERATURE-CONTROLLED WATER IN AN AIRCRAFT
[FR] SYSTÈME DE FOURNITURE D'EAU À TEMPÉRATURE CONTRÔLÉE DANS UN AÉRONEF |
| 71/73 |
Applicant/owner |
PA |
AIRBUS OPERATIONS GMBH, DE
|
| 72 |
Inventor |
IN |
DELAPLANCHE OLIVIER, DE
;
KEISER DENNIS, DE
;
KIEHNE OLIVER, DE
;
MORTENSEN ERNITS RAFAEL, DE
;
REISS MATTHIAS, DE
;
TIEMANN MARKUS, DE
|
| 22/96 |
Application date |
AD |
Sep 24, 2021 |
| 21 |
Application number |
AN |
21198720 |
|
Country of application |
AC |
EP |
|
Publication date |
PUB |
Mar 30, 2022 |
33
31
32 |
Priority data |
PRC
PRN
PRD |
DE
102020124879
20200924
|
| 51 |
IPC main class |
ICM |
B64D 11/04
(2006.01)
|
| 51 |
IPC secondary class |
ICS |
|
|
IPC additional class |
ICA |
|
|
IPC index class |
ICI |
|
|
Cooperative patent classification |
CPC |
B64D 11/0007
B64D 11/02
B64D 11/04
F24H 1/009
F24H 15/223
F24H 9/2021
|
|
MCD main class |
MCM |
B64D 11/04
(2006.01)
|
|
MCD secondary class |
MCS |
|
|
MCD additional class |
MCA |
|
| 57 |
Abstract |
AB |
[EN] A system for providing temperature-controlled water in an aircraft has at least one tank, at least one water temperature-controlling unit, a control unit, and a power supply terminal, wherein the at least one water temperature-controlling unit can be coupled to the at least one tank in order to heat or to cool water situated therein, wherein the control unit is connected to the at least one water temperature-controlling unit in order to activate the at least one water temperature-controlling unit for controlling the temperature of water in the at least one tank to a predefined temperature, wherein the power supply terminal can be connected to an on-board voltage source in order for the at least one water temperature-controlling unit and the control unit to be supplied with electrical voltage, wherein the system is in the form of a coherent and self-contained unit which can be integrated into a standard parking place of a galley of the aircraft, and wherein the at least one tank is mounted so as to be exchangeable or the system has a water discharge connection which is coupled to the at least one tank. |
| 56 |
Cited documents identified in the search |
CT |
DE102010014392A1
DE102010018273A1
EP000002868243A1
US020150266580A1
|
| 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 |
|
No results
|
|
Sequence listings |
|
|
|
Search file IPC |
ICP |
F24H 1/00
|
