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Inventor profile of:

Eugene Gekht

City:

Brossard

Country:

Canada

Published Applications:

Last publication date:

2023-05-18

Top Assignees for applications by Eugene Gekht

The entities that hold a legal rights for patent applications filed by inventor Gekht Eugene:

PRATT & WHITNEY CANADA CORP. 16 Longueuil, Canada
Pratt & Whitney Canada Corp. 11 Longueuil, Quebec, -
Pratt & Whitney Canada Corp. 6 Longueuil, Québec, Canada
Pratt & Whitney Canada Corp. 4 Longueuil, QC, Canada
PRATT & WHITNEY CANADA CORP. 4 Longueuil, Canada
Pratt & Whitney Canada Ccorp. 1 Quebec, Canada
Pratt & Whitney Canada Corp. 1 Québec, Canada

Recent patent applications by Gekht Eugene

Eugene Gekht from Brossard, CA has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2023-05-18

US20230151772A1

Mechanical engineering

Reverse-flow gas turbine engine

#2 | 2021-12-30

US20210404388A1

Mechanical engineering

Reverse-flow gas turbine engine

#3 | 2021-09-02

US20210270183A1

Mechanical engineering

Reverse-flow gas turbine engine

#4 | 2019-02-21

US20190055882A1

Mechanical engineering

Rotary internal combustion engine with pilot subchamber

#5 | 2018-07-05

US20180187593A1

Mechanical engineering

Rotary internal combustion engine with pilot subchamber

#6 | 2018-03-22

US20180080371A1

Mechanical engineering

Rotary internal combustion engine with pilot subchamber

#7 | 2018-03-15

US20180073428A1

Mechanical engineering

Reverse-flow gas turbine engine

#8 | 2017-08-24

US20170241342A1

Mechanical engineering

Air intake for turboprop engine

#9 | 2017-08-24

US20170241341A1

Mechanical engineering

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

#10 | 2017-03-09

US20170067395A1

Mechanical engineering

Rotary internal combustion engine with pilot subchamber

#11 | 2016-12-27

US13750523

Mechanical engineering

Rotary internal combustion engine with pilot subchamber

#12 | 2016-09-29

US20160281602A1

Mechanical engineering

Fluid delivery system for a gas turbine engine

#13 | 2016-04-21

US20160107276A1

Performing operations; transporting

Engine structure assembly procedure

#14 | 2015-11-26

US20150337726A1

Mechanical engineering

Rotary internal combustion engine with cooled insert

#15 | 2015-08-27

US20150240710A1

Mechanical engineering

Rotary internal combustion engine with pilot subchamber

#16 | 2015-07-09

US20150192069A1

Mechanical engineering

Recuperator for gas turbine engine

#17 | 2015-06-18

US20150167465A1

Mechanical engineering

Apex and face seals with rotary internal combustion engine

#18 | 2015-04-23

US20150110628A1

Mechanical engineering

Fastening system for rotor hubs

#19 | 2014-08-28

US20140241854A1

Mechanical engineering

Active turbine or compressor tip clearance control

#20 | 2013-09-26

US20130247866A1

Mechanical engineering

Port for rotary internal combustion engine

#21 | 2013-08-08

US20130199491A1

Mechanical engineering

Rotary internal combustion engine with cooled insert

#22 | 2013-01-31

US20130028777A1

Mechanical engineering

Gas seal arrangement for rotary internal combustion engine

#23 | 2013-01-31

US20130028776A1

Mechanical engineering

Apex and face seals with rotary internal combustion engine

#24 | 2013-01-31

US20130028775A1

Mechanical engineering

Apex seal arrangement for rotary internal combustion engine

#25 | 2013-01-31

US20130028774A1

Mechanical engineering

Rotary internal combustion engine with phasing gear

#26 | 2013-01-31

US20130028773A1

Mechanical engineering

APEX SEAL FOR ROTARY INTERNAL COMBUSTION ENGINE

#27 | 2013-01-31

US20130028771A1

Mechanical engineering

Oil seal arrangement for rotary internal combustion engine

#28 | 2013-01-31

US20130028769A1

Mechanical engineering

Apex seal for rotary internal combustion engine

#29 | 2013-01-31

US20130025567A1

Mechanical engineering

Rotary internal combustion engine with pilot subchamber

#30 | 2010-11-04

US20100278643A1

Mechanical engineering

Centrifugal compressor vane diffuser wall contouring

#31 | 2010-09-16

US20100229618A1

Performing operations; transporting

Method and apparatus for forming a turbofan mixer

#32 | 2010-04-29

US20100104422A1

Mechanical engineering

Particle separator and separating method for gas turbine engine

#33 | 2008-11-25

US11520593

Rotating shaft scavenging scoop

#34 | 2008-10-16

US20080253895A1

Mechanical engineering

Blade retention system for use in a gas turbine engine

#35 | 2008-02-21

US20080041033A1

Mechanical engineering

Gas turbine engine exhaust duct ventilation

#36 | 2006-11-23

US20060260127A1

Mechanical engineering

Turbine exhaust case and method of making

#37 | 2006-10-26

US20060239816A1

Mechanical engineering

Integrated labyrinth and carbon seal

#38 | 2006-09-28

US20060213726A1

Mechanical engineering

Rotating shaft scavenging scoop

#39 | 2006-01-19

US20060010852A1

Mechanical engineering

Turbine exhaust case and method of making

#40 | 2005-02-24

US20050042077A1

Mechanical engineering

Sheet metal turbine or compressor static shroud

#41 | 2005-01-04

US10255666

Blade retention scheme using a retention tab

InventorID:

59119 ⎘