EP 3844019 A1 20210707 - AIRCRAFT MONITORING SYSTEM AND METHOD FOR ELECTRIC OR HYBRID AIRCRAFTS
Title (en)
AIRCRAFT MONITORING SYSTEM AND METHOD FOR ELECTRIC OR HYBRID AIRCRAFTS
Title (de)
FLUGZEUGÜBERWACHUNGSSYSTEM UND VERFAHREN FÜR ELEKTRISCHE ODER HYBRIDFLUGZEUGE
Title (fr)
SYSTÈME ET PROCÉDÉ DE SURVEILLANCE D'AÉRONEF POUR AÉRONEFS ÉLECTRIQUES OU HYBRIDES
Publication
Application
Priority
- US 201862724503 P 20180829
- US 201862758299 P 20181109
- US 201816211079 A 20181205
- IB 2018060696 W 20181228
- IB 2019053644 W 20190503
- IB 2019055110 W 20190618
Abstract (en)
[origin: WO2020044134A1] This disclosure describes at least embodiments of an aircraft monitoring system for an electric or hybrid airplane. The aircraft monitoring system can be constructed to enable the electric or hybrid aircraft to pass certification requirements relating to a safety risk analysis. The aircraft monitoring system can have different subsystems for monitoring and alerting of failures of a component, such as a battery pack, a motor controller, and/ or a motors. The failures that pose a greater safety risk may be monitored and indicated by one or more subsystems without use of programmable components.
IPC 8 full level
B60L 58/10 (2019.01); B60L 58/12 (2019.01); G01R 31/00 (2006.01); G01R 31/382 (2019.01); G01R 31/396 (2019.01); H02J 1/10 (2006.01); H02J 7/00 (2006.01); H02J 7/14 (2006.01); H02J 7/34 (2006.01)
CPC (source: CN EP)
B60L 3/003 (2013.01 - EP); B60L 3/0046 (2013.01 - EP); B60L 3/0061 (2013.01 - EP); B60L 3/0084 (2013.01 - EP); B60L 3/0092 (2013.01 - EP); B60L 3/12 (2013.01 - EP); B60L 15/007 (2013.01 - EP); B60L 50/60 (2019.02 - EP); B60L 50/61 (2019.02 - EP); B60L 58/14 (2019.02 - EP); B60L 58/15 (2019.02 - EP); B60L 58/21 (2019.02 - EP); B64D 27/026 (2024.01 - EP); B64F 5/60 (2017.01 - CN); G01R 31/008 (2013.01 - EP); G01R 31/3647 (2019.01 - EP); G01R 31/396 (2019.01 - EP); H02J 1/10 (2013.01 - EP); H02J 7/0013 (2013.01 - EP); H02J 7/0048 (2020.01 - EP); H02J 7/005 (2020.01 - EP); H02J 7/0063 (2013.01 - EP); H02J 7/00712 (2020.01 - EP); H02J 7/342 (2020.01 - EP); B60L 2200/10 (2013.01 - EP); B60L 2220/50 (2013.01 - EP); B60L 2240/36 (2013.01 - EP); B60L 2240/421 (2013.01 - EP); B60L 2240/425 (2013.01 - EP); B60L 2240/526 (2013.01 - EP); B60L 2240/527 (2013.01 - EP); B60L 2240/529 (2013.01 - EP); B60L 2240/545 (2013.01 - EP); B60L 2240/547 (2013.01 - EP); B60L 2240/549 (2013.01 - EP); B60L 2250/10 (2013.01 - EP); B60L 2250/16 (2013.01 - EP); B64D 27/24 (2013.01 - EP); B64D 45/00 (2013.01 - EP); B64D 2221/00 (2013.01 - EP); G01R 31/343 (2013.01 - EP); G01R 31/3646 (2019.01 - EP); G01R 31/374 (2019.01 - EP); G01R 31/3842 (2019.01 - EP); H02J 2310/44 (2020.01 - EP); Y02T 10/62 (2013.01 - EP); Y02T 10/64 (2013.01 - EP); Y02T 10/70 (2013.01 - EP); 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
DOCDB simple family (publication)
WO 2020044134 A1 20200305; CN 112203892 A 20210108; CN 112203892 B 20231201; CN 112623266 A 20210409; CN 112623266 B 20240705; EP 3844019 A1 20210707; SI 3790762 T1 20240531
DOCDB simple family (application)
IB 2019055110 W 20190618; CN 201980030274 A 20190618; CN 202011344254 A 20190618; EP 19735410 A 20190618; SI 201831053 T 20181228