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Inventor profile of:

Ghislain PLANTE

City:

Verdun

Country:

Canada

Published Applications:

30

Last publication date:

2023-08-03

Top Assignees for applications by Ghislain PLANTE

The entities that hold a legal rights for patent applications filed by inventor PLANTE Ghislain:

Recent patent applications by PLANTE Ghislain

Ghislain PLANTE from Verdun, CA has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2023-08-03
US20230243310A1
Mechanical engineering

GAS TURBINE ENGINE WITH CLUTCH SYSTEM BETWEEN LOW-PRESSURE COMPRESSOR AND LOW-PRESSURE TURBINE

 #2 | 2023-05-18
US20230151772A1
Mechanical engineering

Reverse-flow gas turbine engine

 #3 | 2022-03-10
US20220074349A1
Mechanical engineering

SPLIT COMPRESSOR GAS TURBINE ENGINE

 #4 | 2021-12-30
US20210404388A1
Mechanical engineering

Reverse-flow gas turbine engine

 #5 | 2021-12-14
US15871323
Mechanical engineering

Turbomachine blade

 #6 | 2021-12-09
US20210381517A1
Mechanical engineering

Reverse flow engine architecture

 #7 | 2021-09-02
US20210270183A1
Mechanical engineering

Reverse-flow gas turbine engine

 #8 | 2021-08-05
US20210239053A1
Mechanical engineering

Corrected parameters control logic for variable geometry mechanisms

 #9 | 2021-07-29
US20210231058A1
Mechanical engineering

Gas turbine engine with clutch system between low-pressure compressor and low-pressure turbine

 #10 | 2020-05-07
US20200141416A1
Mechanical engineering

Reverse flow engine architecture

 #11 | 2020-05-07
US20200141328A1
Mechanical engineering

Engine family platform design

 #12 | 2020-04-16
US20200116041A1
Mechanical engineering

Gas turbine engine with low pressure compressor stages

 #13 | 2020-03-12
US20200080516A1
Mechanical engineering

Gas turbine engine and method of creating classes of same

 #14 | 2020-03-12
US20200080476A1
Mechanical engineering

SPILT COMPRESSOR SYSTEM ON MULTI-SPOOL ENGINE

 #15 | 2019-03-07
US20190071975A1
Mechanical engineering

Power turbine blade airfoil profile

 #16 | 2019-02-28
US20190063331A1
Mechanical engineering

Corrected parameters control logic for variable geometry mechanisms

 #17 | 2018-08-09
US20180223739A1
Mechanical engineering

Turbine rotor with low over-speed requirements

 #18 | 2018-08-02
US20180216525A1
Mechanical engineering

GAS TURBINE ENGINE ARCHITECTURE WITH SPLIT COMPRESSOR SYSTEM

 #19 | 2018-06-21
US20180172012A1
Mechanical engineering

Reverse flow engine architecture

 #20 | 2018-05-17
US20180135525A1
Mechanical engineering

GAS TURBINE ENGINE TANGENTIAL ORIFICE BLEED CONFIGURATION

 #21 | 2018-04-26
US20180112603A1
Mechanical engineering

Power plant thrust management system for turboprop engines

 #22 | 2018-03-15
US20180073428A1
Mechanical engineering

Reverse-flow gas turbine engine

 #23 | 2017-04-06
US20170096901A1
Mechanical engineering

Shrouded blade for a gas turbine engine

 #24 | 2016-09-22
US20160273366A1
Mechanical engineering

Internally cooled gas turbine engine airfoil

 #25 | 2016-02-04
US20160032733A1
Mechanical engineering

Outer shroud with gusset

 #26 | 2015-12-17
US20150361800A1
Mechanical engineering

Airfoil with variable land width at trailing edge

 #27 | 2015-08-13
US20150226070A1
Mechanical engineering

Shrouded blade for a gas turbine engine

 #28 | 2014-08-07
US20140219816A1
Mechanical engineering

High pressure turbine blade cooling hole distribution

 #29 | 2014-03-27
US20140086756A1
Mechanical engineering

Internally cooled gas turbine engine airfoil

 #30 | 2009-10-29
US20090269193A1
Performing operations; transporting

Multi-cast turbine airfoils and method for making same
InventorID:

702890 ⎘