Inventor · name-matched record
LABRECQUE MICHEL
4 granted patents·7 pending applications·0 citations·filing 2023–2025
51Inventor score
Files withPRATT & WHITNEY CANADA11
This identity is grouped by exact name match (no disambiguated inventor record was available for these filings) — it may combine same-named inventors.
Top patents by PatentIndex Score
11 records- 0176US2026077870A1Hybrid electric propulsion system for aircraftPRATT & WHITNEY CANADA·Filed 2025·Application pending·0 cites
- 0272US12534216B1Clutch assembly for a hybrid-electric aircraft propulsion systemPRATT & WHITNEY CANADA·Filed 2025·Granted Jan 27, 2026·0 cites·20 claims
- 0371US12583608B2Electric motor propulsion system for an aircraftPRATT & WHITNEY CANADA·Filed 2023·Granted Mar 24, 2026·0 cites·18 claims
- 0471US2026078717A1Blended exhaust system for an aircraft propulsion systemPRATT & WHITNEY CANADA·Filed 2025·Application pending·0 cites
- 0558US12540587B1Gas turbine engine nozzle with variable areaPRATT & WHITNEY CANADA·Filed 2024·Granted Feb 3, 2026·0 cites·18 claims
- 0655US12584443B2Accelerating turbine engine rotating structure with compressed airPRATT & WHITNEY CANADA·Filed 2024·Granted Mar 24, 2026·0 cites·15 claims
- 0753US2026055732A1Jet nozzle effective area control system for gas turbine enginePRATT & WHITNEY CANADA·Filed 2024·Application pending·0 cites
- 0853US2026055744A1Jet nozzle effective area control system for gas turbine enginePRATT & WHITNEY CANADA·Filed 2024·Application pending·0 cites
- 0953US2026055743A1Jet nozzle effective area control system for gas turbine enginePRATT & WHITNEY CANADA·Filed 2024·Application pending·0 cites
- 1053US2026055741A1Jet nozzle effective area control system for gas turbine enginePRATT & WHITNEY CANADA·Filed 2024·Application pending·0 cites
- 1152US2026009331A1Partial exit centrifugal compressorPRATT & WHITNEY CANADA·Filed 2024·Application pending·0 cites
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Identity basis: exact name match across USPTO filings. How scoring works →