EP 4263353 A1 20231025 - COOLING SYSTEM FOR AN AIRCRAFT, AIRCRAFT HAVING A COOLING SYSTEM, AND METHOD FOR COOLING AN ELECTRICAL DRIVE SYSTEM OF AN AIRCRAFT
Title (en)
COOLING SYSTEM FOR AN AIRCRAFT, AIRCRAFT HAVING A COOLING SYSTEM, AND METHOD FOR COOLING AN ELECTRICAL DRIVE SYSTEM OF AN AIRCRAFT
Title (de)
KÜHLSYSTEM FÜR EIN FLUGGERÄT, FLUGGERÄT MIT EINEM KÜHLSYSTEM UND VERFAHREN ZUM KÜHLEN EINES ELEKTRISCHEN ANTRIEBSSYSTEMS EINES FLUGGERÄTS
Title (fr)
SYSTÈME DE REFROIDISSEMENT POUR AÉRONEF, AÉRONEF DOTÉ D'UN SYSTÈME DE REFROIDISSEMENT, ET PROCÉDÉ DE REFROIDISSEMENT D'UN SYSTÈME D'ENTRAÎNEMENT ÉLECTRIQUE D'UN AÉRONEF
Publication
Application
Priority
- DE 102020216090 A 20201216
- DE 2021100939 W 20211126
Abstract (en)
[origin: WO2022127977A1] The invention relates to a cooling system (10) for an aircraft, in particular for cooling at least one element of an electrical drive system (24) of the aircraft, wherein the cooling system (10) is arranged at least in part inside a wing (12) of the aircraft and comprises at least two heat exchangers (16, 42) which are connected via at least one cooling circuit (11), wherein the first heat exchanger (16) is operatively connected to the at least one element to be cooled of the electrical drive system (24), and the second heat exchanger (42) is arranged inside at least one wing (12) and is operatively connected to an upper and/or lower wing shell (46, 48) of the wing (12). The invention also relates to a method for cooling at least one element of an electrical drive system (24) of an aircraft.
IPC 8 full level
B64D 33/10 (2006.01); B64D 27/24 (2006.01)
CPC (source: EP US)
B60L 58/33 (2019.02 - US); B64D 27/24 (2013.01 - EP); B64D 33/08 (2013.01 - US); B64D 33/10 (2013.01 - EP); H01M 8/04029 (2013.01 - US); B60L 2200/10 (2013.01 - US); B64D 27/24 (2013.01 - US); H01M 2250/20 (2013.01 - US); Y02T 50/60 (2013.01 - EP)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated extension state (EPC)
BA ME
Designated validation state (EPC)
KH MA MD TN
DOCDB simple family (publication)
WO 2022127977 A1 20220623; DE 102020216090 A1 20220623; EP 4263353 A1 20231025; US 2024043132 A1 20240208
DOCDB simple family (application)
DE 2021100939 W 20211126; DE 102020216090 A 20201216; EP 21819341 A 20211126; US 202118266073 A 20211126