Longueuil
Canada
2,032
2026-06-23
2,028
2026-06-23
These are the the leading inventors for applications assigned to PRATT & WHITNEY CANADA CORP.:
PRATT & WHITNEY CANADA CORP. based in Longueuil, CA has been assigned the rights to these inventions. The list includes both Pending Applications and Patent Grants:
Bi-metal impeller rotor
#2 | 2026-06-23 β Patent 12,662,944 granted on 2026-06-23Combustor scroll de-swirler
#3 | 2026-06-23 β Patent 12,662,948 granted on 2026-06-23Turbine exhaust duct with probe interface
#4 | 2026-06-16 β Patent 12,655,776 granted on 2026-06-16Method and apparatus for impeller retention during assembly of a turbine engine
#5 | 2026-06-16 β Patent 12,655,796 granted on 2026-06-16Impeller backface cooled P3 passage through diffuser/reducing high temp exposure of cooled air
#6 | 2026-06-02 β Patent 12,644,387 granted on 2026-06-02Turbine vane assembly for controlling tip clearance
#7 | 2026-05-26 β Patent 12,638,180 granted on 2026-05-26Combustor inlet plenum and baffle
#8 | 2026-05-26 β Patent 12,637,225 granted on 2026-05-26System and method for managing electric motor propulsion command limits on a hybrid rotorcraft
#9 | 2026-05-26 β Patent 12,637,226 granted on 2026-05-26Bifurcated exhaust duct for hybrid aircraft powerplant
#10 | 2026-05-21 β Patent 12,637,986 granted on 2026-05-26GAS TURBINE ACCELERATION LIMIT BIASING FOR PREMATURE ASYMMETRIC OPERATING REGIME EXITS
#11 | 2026-05-21 β Patent 12,644,407 granted on 2026-06-02TRACTOR AIRCRAFT POWER PLANT WITH SWIRL RECOVERY VANES
#12 | 2026-05-19 β Patent 12,631,141 granted on 2026-05-19Shaft centering systems for air bearings
#13 | 2026-05-19 β Patent 12,631,125 granted on 2026-05-19Compressor cooling system for a turbofan engine
#14 | 2026-05-12 β Patent 12,624,660 granted on 2026-05-12Hybrid aircraft power plant with ventilated exhaust duct cavity
#15 | 2026-05-12 β Patent 12,624,664 granted on 2026-05-12Overspeed protection for a turbocompressor of an aircraft powerplant assembly
#16 | 2026-05-05 β Patent 12,618,342 granted on 2026-05-05Turbine exhaust case with stiffening brace
#17 | 2026-05-05 β Patent 12,617,541 granted on 2026-05-05Exhaust case for aircraft engine
#18 | 2026-04-30 β Patent 12,631,148 granted on 2026-05-19SYSTEMS AND METHODS FOR OPERATING AN AIRCRAFT ENGINE USING MULTIPLE FUEL TYPES
#19 | 2026-04-30 β Patent 12,631,129 granted on 2026-05-19AIRCRAFT ENGINE HAVING SCROLL CASE WITH FLANGE CONNECTION
#20 | 2026-04-21 β Patent 12,607,133 granted on 2026-04-21Propulsive engine having a lubricant system driven by compressed air
#21 | 2026-04-14 β Patent 12,601,278 granted on 2026-04-14Through-casing guide vane mechanism for gas turbine engines
#22 | 2026-04-14 β Patent 12,601,263 granted on 2026-04-14Radially captured in situ balancing masses for aircraft powerplant
#23 | 2026-04-09ROTOR BEARING LOADING MECHANISM
#24 | 2026-04-07 β Patent 12,595,749 granted on 2026-04-07Oil system for aircraft engine having features to prevent drainage of component
#25 | 2026-04-07 β Patent 12,595,750 granted on 2026-04-07Turbine support case with axial spokes and brackets
#26 | 2026-04-02 β Patent 12,638,184 granted on 2026-05-26ENGINE FUEL INJECTORS WITH COMMON FUEL TARGET LOCATION
#27 | 2026-04-02 β Patent 12,654,264 granted on 2026-06-16Gas Turbine Engine Gearbox Alignment Tool and Method
#28 | 2026-03-31 β Patent 12,590,543 granted on 2026-03-31Gas turbine engine with shaft retention system
#29 | 2026-03-26 β Patent 12,655,935 granted on 2026-06-16OIL TANK ACCESS PORT COVER FOR AN AIRCRAFT ENGINE OIL SYSTEM
#30 | 2026-03-26 β Patent 12,590,551 granted on 2026-03-31OIL TANK RETURN FOR AN AIRCRAFT ENGINE OIL SYSTEM
#31 | 2026-03-24 β Patent 12,584,482 granted on 2026-03-24Gear pump parallel load path
#32 | 2026-03-24 β Patent 12,584,422 granted on 2026-03-24System and method for assembling a rotational equipment assembly of an aircraft propulsion system
#33 | 2026-03-17 β Patent 12,577,912 granted on 2026-03-17Active de-aerator for aircraft power plant
#34 | 2026-03-12 β Patent 12,624,663 granted on 2026-05-12AIRCRAFT ENGINE WITH RECUPERATOR AND BYPASS
#35 | 2026-03-05 β Patent 12,601,280 granted on 2026-04-14BOSS WITH INTEGRAL FIRE PROTECTION
#36 | 2026-03-05 β Patent 12,601,273 granted on 2026-04-14Stator Vane Braze Joints
#37 | 2026-03-03 β Patent 12,565,325 granted on 2026-03-03Propulsor reverse rotation protection for hybrid-electric aircraft propulsion systems
#38 | 2026-03-03 β Patent 12,565,846 granted on 2026-03-03Turbine case structure for an aircraft propulsion system engine
#39 | 2026-03-03 β Patent 12,565,847 granted on 2026-03-03Aircraft engine having a scroll case and a turbine support case secured together
#40 | 2026-03-03 β Patent 12,565,845 granted on 2026-03-03Dual air source bearing assembly housing for an aircraft propulsion system
#41 | 2026-02-26 β Patent 12,584,443 granted on 2026-03-24ACCELERATING TURBINE ENGINE ROTATING STRUCTURE WITH COMPRESSED AIR
#42 | 2026-02-26 β Patent 12,577,909 granted on 2026-03-17RADIAL INLET COMPRESSOR
#43 | 2026-02-24 β Patent 12,560,100 granted on 2026-02-24Double directionally pre-loaded damped ball bearing
#44 | 2026-02-17 β Patent 12,553,346 granted on 2026-02-17Gas turbine engine with rotational spool balancing system
#45 | 2026-02-17 β Patent 12,553,608 granted on 2026-02-17Additively manufactured combustor liner v-band cooling ring
#46 | 2026-02-12 β Patent 12,624,659 granted on 2026-05-12AIR PURGING ARRANGEMENT
#47 | 2026-02-10 β Patent 12,546,232 granted on 2026-02-10Inducing windmilling to allow oil flow during fire-induced emergency state
#48 | 2026-02-10 β Patent 12,546,229 granted on 2026-02-10Gas turbine engine rotor stage with seal members
#49 | 2026-02-10 β Patent 12,545,419 granted on 2026-02-10Emergency energy protection assembly for hybrid-electric aircraft propulsion systems
#50 | 2026-02-05 β Patent 12,571,403 granted on 2026-03-10NON-LINEAR IMPELLER BACKSWEEP
#51 | 2026-02-05 β Patent 12,644,426 granted on 2026-06-02TURBOPROP WITH A VARIABLE AREA NOZZLE EJECTOR
#52 | 2026-02-03 β Patent 12,540,628 granted on 2026-02-03Impeller blade turning distribution
#53 | 2026-02-03 β Patent 12,540,580 granted on 2026-02-03Automatic bleed valve
#54 | 2026-01-27 β Patent 12,534,216 granted on 2026-01-27Clutch assembly for a hybrid-electric aircraft propulsion system
#55 | 2026-01-27 β Patent 12,534,214 granted on 2026-01-27Aircraft engine auxiliary oil system
#56 | 2026-01-27 β Patent 12,535,034 granted on 2026-01-27Joint between aircraft engine components with spring beams
#57 | 2026-01-20 β Patent 12,529,325 granted on 2026-01-20Turbine exhaust duct with stiffeners for aircraft engines
#58 | 2026-01-20 β Patent 12,529,322 granted on 2026-01-20Gas turbine engine stator vane stage
#59 | 2026-01-15 β Patent 12,540,550 granted on 2026-02-03TIE SHAFT FOR ENGINE ROTATING ASSEMBLY
#60 | 2026-01-13 β Patent 12,523,174 granted on 2026-01-13Mounting seal runner onto aircraft powerplant rotor
#61 | 2026-01-08 β Patent 12,545,418 granted on 2026-02-10CONTROL ASSEMBLY FOR AIRCRAFT PROPULSION SYSTEMS
#62 | 2026-01-06 β Patent 12,516,636 granted on 2026-01-06Accommodation for mismatch in guide vane feedback via undesired engine behavior
#63 | 2026-01-06 β Patent 12,516,605 granted on 2026-01-06In situ balancing mass(es) for aircraft powerplant
#64 | 2026-01-01 β Patent 12,644,408 granted on 2026-06-02POWERPLANT FUEL SYSTEM UTILIZING AMMONIA
#65 | 2026-01-01 β Patent 12,595,746 granted on 2026-04-07AIRCRAFT PROPULSION SYSTEM WITH CLOCKED ELECTRIC MACHINE AND ACCESSORY GEARBOX
#66 | 2025-12-25 β Patent 12,618,340 granted on 2026-05-05CONTROLLED CONTACT INDUCED BUCKLING OF SPOKED BEARING SUPPORT
#67 | 2025-12-25 β Patent 12,618,339 granted on 2026-05-05DESTABILIZER INDUCED BUCKLING IN SPOKED BEARING SUPPORT
#68 | 2025-12-25SPRAY NOZZLE FOR CLEANING APU
#69 | 2025-12-23 β Patent 12,503,975 granted on 2025-12-23Housing assembly for rotary engine and method of manufacturing thereof
#70 | 2025-12-23 β Patent 12,503,961 granted on 2025-12-23Slip based radial bearing support
#71 | 2025-12-18 β Patent 12,516,609 granted on 2026-01-06SERVICEABLE PROPELLER SHAFT ZERO AIR GAP SEAL
#72 | 2025-12-18 β Patent 12,571,323 granted on 2026-03-10TURBINE ENGINE AIRFOIL
#73 | 2025-12-18 β Patent 12,509,988 granted on 2025-12-30TURBINE ENGINE AIRFOIL
#74 | 2025-12-18 β Patent 12,618,330 granted on 2026-05-05TURBINE ENGINE AIRFOIL
#75 | 2025-12-11 β Patent 12,553,356 granted on 2026-02-17AIRCRAFT ENGINE STATIONARY LABYRINTH SEAL FOR USE IN A GEARBOX OF AN AIRCRAFT ENGINE OIL SYSTEM
#76 | 2025-12-09 β Patent 12,492,643 granted on 2025-12-09Extended banana foot stator
#77 | 2025-12-04 β Patent 12,553,547 granted on 2026-02-17DUAL SEALING FOR HIGH PRESSURE GASEOUS FUELS
#78 | 2025-12-04 β Patent 12,540,667 granted on 2026-02-03COMBINED ROTATING COMPONENT AND FLUID PORT BAFFLE
#79 | 2025-12-04 β Patent 12,612,863 granted on 2026-04-28TEST BLADE FOR GAS TURBINE ENGINE AND METHOD OF MAKING
#80 | 2025-12-02 β Patent 12,486,788 granted on 2025-12-02Turbine support case supported by stopping ribs
#81 | 2025-11-27 β Patent 12,560,280 granted on 2026-02-24ENGINE OIL SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM AND METHOD FOR CONTROLLING SAME
#82 | 2025-11-27 β Patent 12,553,450 granted on 2026-02-17PLENUM CLOSURE PANEL WITH INTEGRATED AIRFLOW DIRECTION DEVICE
#83 | 2025-11-25 β Patent 12,480,424 granted on 2025-11-25Active de-aerator for aircraft power plant
#84 | 2025-11-13 β Patent 12,486,984 granted on 2025-12-02CONTROLLED GAP FUEL NOZZLE HEAT SHIELD
#85 | 2025-11-13 β Patent 12,473,840 granted on 2025-11-18Containment Ring for Gas Turbine Engine
#86 | 2025-11-11 β Patent 12,467,365 granted on 2025-11-11In situ balancing mass(es) for aircraft powerplant
#87 | 2025-11-11 β Patent 12,467,473 granted on 2025-11-11Aircraft engine including diffuser secured to a bearing housing
#88 | 2025-11-11 β Patent 12,467,387 granted on 2025-11-11Turbine exhaust case structural flange
#89 | 2025-11-11 β Patent 12,467,403 granted on 2025-11-11Powerplant fuel system utilizing ammonia
#90 | 2025-11-06 β Patent 12,656,102 granted on 2026-06-16SYSTEM AND METHOD FOR PERFORMING DIMENSIONAL INSPECTION
#91 | 2025-11-06 β Patent 12,497,909 granted on 2025-12-16FLANGE WITH STRESS ATTENTUATION FEATURE
#92 | 2025-11-06 β Patent 12,637,959 granted on 2026-05-26CONTAINMENT RING FOR GAS TURBINE ENGINE
#93 | 2025-11-04 β Patent 12,460,580 granted on 2025-11-04Heat management system and method for hydrogen-fueled engine
#94 | 2025-10-30 β Patent 12,460,558 granted on 2025-11-04HEAT EXCHANGER HAVING A MIXING CHAMBER AND PROTRUSIONS
#95 | 2025-10-28 β Patent 12,454,926 granted on 2025-10-28Exhaust nozzle assembly for an aircraft propulsion system
#96 | 2025-10-21 β Patent 12,448,904 granted on 2025-10-21Seal assembly mating plate for aircraft powerplant
#97 | 2025-10-21 β Patent 12,448,893 granted on 2025-10-21Electromagnetic inducer for gas turbine rotating turbomachinery
#98 | 2025-10-21 β Patent 12,451,824 granted on 2025-10-21Hybrid electric propulsion system with regeneration and method for operating the same
#99 | 2025-10-16 β Patent 12,577,878 granted on 2026-03-17LEADING EDGE PLATING ON LOW PRESSURE COMPRESSOR VANE FOR WEIGHT AND STRENGTH OPTIMIZATION
#100 | 2025-10-16 β Patent 12,503,243 granted on 2025-12-23METHOD AND SYSTEM FOR OPERATING A HYBRID AIRCRAFT ENGINE
Also check out PRATT & WHITNEY CANADA CORP.'s (Longueuil, Canada) applicant profile with 2,458 patent applications submitted.
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