Laval
Canada
25
2026-05-21
The entities that hold a legal rights for patent applications filed by inventor LISIO Carmine:
Carmine LISIO from Laval, CA has applied for patents for these inventions. The list has both pending applications and granted patents:
SWITCHABLE AERO ENGINE DUAL FUEL CONTROL SYSTEM WITH DHFC
#2 | 2026-01-22MULTICORE HYBRID-ELECTRIC POWERTRAIN CONTROLLER
#3 | 2025-10-21Hybrid electric propulsion system with regeneration and method for operating the same
#4 | 2022-10-20Engine and propeller control system
#5 | 2021-11-04Printed circuit board assembly for aircraft engine, and method monitoring same
#6 | 2020-11-19System and method for detecting an uncommanded or uncontrollable high thrust event in an aircraft
#7 | 2020-10-15METHOD AND SYSTEM FOR FEATHERING A PROPELLER
#8 | 2020-10-01Method and system for operating an aircraft powerplant
#9 | 2020-09-10Method and system for operating an engine in a multi-engine aircraft
#10 | 2020-08-27Methods and systems for controlling operation of aircraft engines
#11 | 2020-08-13Method and system for starting an engine
#12 | 2020-08-06SYSTEM AND METHOD FOR CONTROLLING PROPELLER-DRIVEN AIRCRAFT
#13 | 2020-07-23METHOD AND SYSTEM FOR OPERATING A GAS TURBINE ENGINE COUPLED TO AN AIRCRAFT PROPELLER
#14 | 2020-05-28Integrated propeller and engine controller
#15 | 2020-05-28Engine and propeller control system
#16 | 2020-05-28Autothrottle control for turboprop engines
#17 | 2020-04-30Autothrottle control system on turbopropeller-powered aircraft
#18 | 2020-04-16Reverse thrust in multi-engine propeller aircraft
#19 | 2020-01-16System and method for feathering an aircraft propeller
#20 | 2020-01-16System and method for feathering an aircraft propeller
#21 | 2018-11-15Single lever powerplant control on twin turbopropeller aircraft
#22 | 2018-08-23Autothrottle control for turboprop engines
#23 | 2018-08-23Single lever control in twin turbopropeller aircraft
#24 | 2018-08-09Methods and systems for controlling operation of aircraft engines
#25 | 2015-09-10System and method for operating a multi-engine aircraft in an auxiliary power unit mode
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