METHOD OF FABRICATING A PRE-LITHIATED ELECTRODE AND LITHIUM-ION BATTERY CELLThe present invention provides a method of fabricating a pre-lithiated electrode, comprising: disposing a Li-PET sheet comprising a layer of lithium metal adjacent to a prefabricated electrode compris…DRIVE·Oct 30·1 min readFollowH01M10/0525LILIUM EAIRCRAFT GMBH [DE]
ELECTRIC AIRCRAFT ENGINEThe present invention provides an electric aircraft engine. It also provides an aircraft, comprising such an electric aircraft engine. According to a first aspect of the present invention, the electri…DRIVE·Aug 21·2 min readFollowB64D15/12LILIUM EAIRCRAFT GMBH [DE]
TIME VARIABLE ELECTRICAL LOAD SHARING IN A POWER DISTRIBUTION NETWORK OF AN AIRCRAFTAn electrical power distribution network (306) of an electric power system (300) of an aircraft is operated such that it sequentially adopts a plurality of different partial load sharing modes in a ti…DRIVE·Jun 5·1 min readFollowB60L50/60LILIUM EAIRCRAFT GMBH [DE]
BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIR VEHICLEThe present invention relates to a battery management system and method for performing a battery health parameter observation, in particular cell impedance observation, with two redundant, independent…DRIVE·May 29·1 min readFollowB60L50/60LILIUM EAIRCRAFT GMBH [DE]
ELECTRICAL FAULT ISOLATION IN A POWER DISTRIBUTION NETWORK OF AN AIRCRAFTAn electrical power distribution network (306) of an electric power system (300) of an aircraft is operated in at least one normal operation mode such that it provides for load sharing across electric…DRIVE·May 15·1 min readFollowB60L3/04LILIUM EAIRCRAFT GMBH [DE]
BATTERY AIRCRAFT INTEGRATIONThe present invention relates to an aircraft (10), comprising a fuselage (12), at least one pair of wings (14, 16) and a battery system, wherein the battery system comprises at least one battery pack …DRIVE·Mar 13·2 min readFollowB60L50/64LILIUM EAIRCRAFT GMBH [DE]
AIRCRAFT, COMPRISING A BATTERY ASSEMBLYThe present invention relates to an aircraft (10), comprising a fuselage (12), at least one pair of wings (14) and a battery assembly for providing power to electrical systems of the aircraft (10), wh…DRIVE·Mar 6·2 min readFollowB64C17/02LILIUM EAIRCRAFT GMBH [DE]
AIRCRAFT ENGINE COMPRISING A VARIABLE AREA EXHAUST NOZZLEThe present invention provides an engine 310 of a vertical take-off and landing aircraft 300, wherein the engine is configured to be movable with respect to an aircraft component 342 of the aircraft 3…DRIVE·May 24·1 min readFollowB64C11/001LILIUM EAIRCRAFT GMBH [DE]
BATTERY MANAGEMENT SYSTEM FOR AN ELECTRIC AIR VEHICLEThe present invention relates to a battery management system and method for performing a battery state and optionally health parameter observation, in particular cell state-of-charge (SOC) observation…DRIVE·May 10·1 min readFollowB60L3/0038LILIUM EAIRCRAFT GMBH [DE]
SELF-SUPPORTING VAPOR CYCLE REFRIGERATION SYSTEM FOR AN AIRCRAFTA vapor cycle refrigeration system (100) for an aircraft comprises a compressor (10), a condenser unit (20) with a condenser radiator (22), a condenser fan (24) and a condenser air duct (26) configure…DRIVE·Apr 5·2 min readFollowB60H1/3229LILIUM EAIRCRAFT GMBH [DE]
