Francois C. BISSON

Person

Vallee-Jonction, CA

People

Patents Grantslast 30 patents

Information Patent Grant
Gas turbine engine with inertial particle separator
- Patent number 11,536,196
- Issue date Dec 27, 2022
- Pratt & Whitney Canada Corp.
- Roberto Marrano
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Inertial particle separator for engine inlet
- Patent number 10,765,980
- Issue date Sep 8, 2020
- Pratt & Whitney Canada Corp.
- Francois Bisson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine exhaust mixer with lobes cross-over offset
- Patent number 10,436,149
- Issue date Oct 8, 2019
- Pratt & Whitney Canada Corp.
- Francois Bisson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Inertial particle separator for engine inlet
- Patent number 10,245,540
- Issue date Apr 2, 2019
- Pratt & Whitney Canada Corp.
- Francois Bisson
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Grant
Air intake for turboprop engine
- Patent number 10,087,839
- Issue date Oct 2, 2018
- Pratt & Whitney Canada Corp.
- Eugene Gekht
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Air intake with scroll portion and strutted portion for gas turbine...
- Patent number 10,030,581
- Issue date Jul 24, 2018
- Pratt & Whitney Canada Corp.
- Eugene Gekht
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Integrated TEC/mixer strut axial position
- Patent number 10,018,150
- Issue date Jul 10, 2018
- PRATT & WHITNEY CANADA INC.
- Remo Marini
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
GAS TURBINE ENGINE WITH INERTIAL PARTICLE SEPARATOR
- Publication number 20190331025
- Publication date Oct 31, 2019
- Pratt & Whitney Canada Corp.
- Roberto MARRANO
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
INERTIAL PARTICLE SEPARATOR FOR ENGINE INLET
- Publication number 20190217234
- Publication date Jul 18, 2019
- Pratt & Whitney Canada Corp.
- Francois BISSON
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
INERTIAL PARTICLE SEPARATOR FOR ENGINE INLET
- Publication number 20180193782
- Publication date Jul 12, 2018
- Pratt & Whitney Canada Corp.
- Francois BISSON
- B01 - PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
Information Patent Application
AIR INTAKE WITH SCROLL PORTION AND STRUTTED PORTION FOR GAS TURBINE...
- Publication number 20170241341
- Publication date Aug 24, 2017
- Pratt & Whitney Canada Corp.
- Eugene GEKHT
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIR INTAKE FOR TURBOPROP ENGINE
- Publication number 20170241342
- Publication date Aug 24, 2017
- Pratt & Whitney Canada Corp.
- Eugene GEKHT
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE EXHAUST MIXER WITH LOBES CROSS-OVER OFFSET
- Publication number 20170089296
- Publication date Mar 30, 2017
- Pratt & Whitney Canada Corp.
- Francois BISSON
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INTEGRATED TEC/MIXER STRUT AXIAL POSITION
- Publication number 20160326983
- Publication date Nov 10, 2016
- Pratt & Whitney Canada Corp.
- Remo MARINI
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Francois C. BISSON

Person

Patents Grantslast 30 patents

Gas turbine engine with inertial particle separator

Inertial particle separator for engine inlet

Gas turbine engine exhaust mixer with lobes cross-over offset

Inertial particle separator for engine inlet

Air intake for turboprop engine

Air intake with scroll portion and strutted portion for gas turbine...

Integrated TEC/mixer strut axial position

Patents Applicationslast 30 patents

GAS TURBINE ENGINE WITH INERTIAL PARTICLE SEPARATOR

INERTIAL PARTICLE SEPARATOR FOR ENGINE INLET

INERTIAL PARTICLE SEPARATOR FOR ENGINE INLET

AIR INTAKE WITH SCROLL PORTION AND STRUTTED PORTION FOR GAS TURBINE...

AIR INTAKE FOR TURBOPROP ENGINE

GAS TURBINE ENGINE EXHAUST MIXER WITH LOBES CROSS-OVER OFFSET

INTEGRATED TEC/MIXER STRUT AXIAL POSITION