Inventor · Longueuil, QC, CA

Daniel Coutu

18Patents
1h-index
14Co-inventors
43Inventor score

Filing activity: Sep 28, 2016 → Apr 18, 2023

Most-cited inventions

PatentTitleAreaCited byStatus
US10502061B2 Damper groove with strain derivative amplifying pockets Mechanical Engineering; Lighting; Heating 3 Active
US11913342B1 Variable guide vane assembly and control system thereof Mechanical Engineering; Lighting; Heating 1 Active
US10844741B2 Brush seal assembly and method Mechanical Engineering; Lighting; Heating 1 Active
US10801441B2 Flow mixer stiffener ring segmented springs Mechanical Engineering; Lighting; Heating 1 Active
US11486265B1 Sealing variable guide vanes Emerging Cross-Sectional Technologies 0 Active
US11274556B2 Damper groove with strain derivative amplifying pockets Mechanical Engineering; Lighting; Heating 0 Active
US11859554B2 Fast engine re-start for multi-engine system and method Mechanical Engineering; Lighting; Heating 0 Active
US11725595B2 Control logic for gas turbine engine fuel economy Emerging Cross-Sectional Technologies 0 Active
US10927958B2 Non-axisymmetric brush seal assembly Mechanical Engineering; Lighting; Heating 0 Active
US11274611B2 Control logic for gas turbine engine fuel economy Emerging Cross-Sectional Technologies 0 Active
US11674456B1 System and method of operating multi-engine system Emerging Cross-Sectional Technologies 0 Active
US12410757B2 System and method of operating multi-engine system Mechanical Engineering; Lighting; Heating 0 Active
US11814969B2 Gas turbine engine with low-pressure compressor bypass Mechanical Engineering; Lighting; Heating 0 Active
US11939914B2 System and method of operating multi-engine system Mechanical Engineering; Lighting; Heating 0 Active
US11905888B2 Multi-engine system and power transfer between engines thereof Mechanical Engineering; Lighting; Heating 0 Active
US11073103B2 Encapsulated flow mixer stiffener ring Mechanical Engineering; Lighting; Heating 0 Active
US11668253B2 System and method for providing in-flight reverse thrust for an aircraft Mechanical Engineering; Lighting; Heating 0 Active
US12313010B2 Systems and methods for adjusting a modulation characteristic of a bleed-off valve of a gas turbine engine Mechanical Engineering; Lighting; Heating 0 Active

Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.