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Inventor profile of:

ERIC DUROCHER

City:

Vercheres

Country:

Canada

Published Applications:

87

Last publication date:

2020-03-26

Top Assignees for applications by ERIC DUROCHER

The entities that hold a legal rights for patent applications filed by inventor DUROCHER ERIC:

Recent patent applications by DUROCHER ERIC

ERIC DUROCHER from Vercheres, CA has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2020-03-26
US20200095942A1
Mechanical engineering

Multi-spool gas turbine engine architecture

 #2 | 2020-03-12
US20200080435A1
Mechanical engineering

TURBINE EXHAUST STRUCTURE FOR A GAS TURBINE ENGINE

 #3 | 2020-02-13
US20200049025A1
Mechanical engineering

Multi-engine system and method

 #4 | 2020-02-13
US20200047876A1
Performing operations; transporting

Turboshaft gas turbine engine

 #5 | 2019-04-25
US20190120170A1
Mechanical engineering

TEC mixer with variable thicknesses

 #6 | 2018-06-21
US20180172078A1
Mechanical engineering

Spline alignment

 #7 | 2018-05-17
US20180135522A1
Mechanical engineering

Gas turbine engine accessories arrangement

 #8 | 2018-03-15
US20180073438A1
Mechanical engineering

Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool

 #9 | 2018-03-15
US20180073428A1
Mechanical engineering

Reverse-flow gas turbine engine

 #10 | 2017-11-16
US20170327241A1
Performing operations; transporting

Power plant management system for dual engine helicopter in single engine operation mode

 #11 | 2017-02-23
US20170051632A1
Mechanical engineering

Oil scupper system for bearing housing of gas turbine engine

 #12 | 2017-01-26
US20170022831A9
Mechanical engineering

MANUFACTURING OF TURBINE SHROUD SEGMENT WITH INTERNAL COOLING PASSAGES

 #13 | 2016-10-20
US20160305262A1
Mechanical engineering

MANUFACTURING OF TURBINE SHROUD SEGMENT WITH INTERNAL COOLING PASSAGES

 #14 | 2016-06-02
US20160153398A1
Mechanical engineering

Gas turbine engine exhaust mixer

 #15 | 2015-10-01
US20150273585A1
Performing operations; transporting

Turbine shroud segment with inter-segment overlap

 #16 | 2014-08-21
US20140230404A1
Mechanical engineering

Gas turbine engine exhaust mixer

 #17 | 2014-05-15
US20140133962A1
Mechanical engineering

Interturbine vane with multiple air chambers

 #18 | 2014-03-20
US20140075919A1
Mechanical engineering

Turbine exhaust case mixer of gas turbine with variable thickness

 #19 | 2013-09-26
US20130251508A1
Mechanical engineering

Dual-use of cooling air for turbine vane and method

 #20 | 2013-08-29
US20130224012A1
Mechanical engineering

Gas turbine engine case bosses

 #21 | 2013-08-29
US20130223982A1
Mechanical engineering

Thermal expansion joint connection for sheet metal assembly

 #22 | 2013-07-25
US20130189071A1
Mechanical engineering

Oil purge system for a mid turbine frame

 #23 | 2013-05-09
US20130111906A1
Mechanical engineering

Gas turbine exhaust case

 #24 | 2013-03-28
US20130078080A1
Mechanical engineering

Air system architecture for a mid-turbine frame module

 #25 | 2013-03-14
US20130061473A1
Mechanical engineering

Method for centering engine structures

 #26 | 2013-02-28
US20130052074A1
Performing operations; transporting

Manufacturing of turbine shroud segment with internal cooling passages

 #27 | 2013-02-28
US20130052029A1
Mechanical engineering

Hollow core airfoil stiffener rib

 #28 | 2013-02-28
US20130052007A1
Performing operations; transporting

Turbine shroud segment

 #29 | 2013-02-28
US20130051989A1
Mechanical engineering

Turbine shroud segment with integrated seal

 #30 | 2013-02-28
US20130051987A1
Performing operations; transporting

Turbine shroud segment with inter-segment overlap

 #31 | 2013-02-28
US20130051979A1
Performing operations; transporting

Turbine shroud segment with integrated impingement plate

 #32 | 2012-08-23
US20120211949A1
Mechanical engineering

Split ring seal with spring element

 #33 | 2012-05-10
US20120110849A1
Mechanical engineering

Method for assembling radially loaded vane assembly of gas turbine engine

 #34 | 2011-04-14
US20110085895A1
Mechanical engineering

Oil tube with integrated heat shield

 #35 | 2011-04-07
US20110081240A1
Mechanical engineering

Fabricated gas turbine vane ring

 #36 | 2011-04-07
US20110081239A1
Mechanical engineering

Fabricated static vane ring

 #37 | 2011-04-07
US20110081238A1
Mechanical engineering

GAS TURBINE ENGINE SHEET METAL VANE

 #38 | 2011-04-07
US20110081237A1
Mechanical engineering

Sealing for vane segments

 #39 | 2011-04-07
US20110081234A1
Mechanical engineering

Gas turbine engine thermal expansion joint

 #40 | 2011-04-07
US20110081228A1
Mechanical engineering

Interturbine vane with multiple air chambers

 #41 | 2011-04-07
US20110079020A1
Mechanical engineering

Air metering device for gas turbine engine

 #42 | 2011-04-07
US20110079019A1
Mechanical engineering

Cooling air system for mid turbine frame

 #43 | 2011-04-07
US20110078902A1
Mechanical engineering

Method for centering engine structures

 #44 | 2011-02-17
US20110038706A1
Mechanical engineering

Turbine section architecture for gas turbine engine

 #45 | 2011-02-17
US20110036068A1
Mechanical engineering

Gas turbine engine exhaust mixer

 #46 | 2011-02-03
US20110023499A1
Mechanical engineering

Gas turbine combustor exit duct and hp vane interface

 #47 | 2010-11-04
US20100275572A1
Mechanical engineering

OIL LINE INSULATION SYSTEM FOR MID TURBINE FRAME

 #48 | 2010-10-28
US20100272566A1
Mechanical engineering

Deflector for a gas turbine strut and vane assembly

 #49 | 2010-09-23
US20100237571A1
Mechanical engineering

Split ring seal with spring element

 #50 | 2010-09-23
US20100236257A1
Mechanical engineering

Gas turbine combustor exit duct and HP vane interface

 #51 | 2010-06-03
US20100135770A1
Mechanical engineering

Mid turbine frame system for gas turbine engine

 #52 | 2010-06-03
US20100132377A1
Mechanical engineering

FABRICATED ITD-STRUT AND VANE RING FOR GAS TURBINE ENGINE

 #53 | 2010-06-03
US20100132376A1
Mechanical engineering

Mid turbine frame for gas turbine engine

 #54 | 2010-06-03
US20100132373A1
Mechanical engineering

Method of assembly and disassembly of a gas turbine mid turbine frame

 #55 | 2010-06-03
US20100132372A1
Mechanical engineering

Mid turbine frame system and radial locator for radially centering a bearing for gas turbine engine

 #56 | 2010-06-03
US20100132371A1
Mechanical engineering

MID TURBINE FRAME SYSTEM FOR GAS TURBINE ENGINE

 #57 | 2010-06-03
US20100132370A1
Mechanical engineering

Locking apparatus for a radial locator for gas turbine engine mid turbine frame

 #58 | 2010-06-03
US20100132369A1
Mechanical engineering

Mid turbine frame system for gas turbine engine

 #59 | 2010-04-01
US20100080699A1
Mechanical engineering

Turbine shroud gas path duct interface

 #60 | 2010-03-25
US20100071208A1
Mechanical engineering

Guide tool and method for assembling radially loaded vane assembly of gas turbine engine

 #61 | 2009-08-20
US20090208326A1
Mechanical engineering

Rim seal for a gas turbine engine

 #62 | 2009-06-18
US20090155069A1
Mechanical engineering

Axial loading element for turbine vane

 #63 | 2009-06-18
US20090155068A1
Mechanical engineering

Radial loading element for turbine vane

 #64 | 2009-04-30
US20090110548A1
Mechanical engineering

ABRADABLE RIM SEAL FOR LOW PRESSURE TURBINE STAGE

 #65 | 2008-09-25
US20080232963A1
Mechanical engineering

TURBINE SHROUD SEGMENT TRANSPIRATION COOLING WITH INDIVIDUAL CAST INLET AND OUTLET CAVITIES

 #66 | 2008-04-10
US20080085183A1
Mechanical engineering

Air seal arrangement for a gas turbine engine

 #67 | 2008-04-03
US20080078162A1
Mechanical engineering

TURBINE EXHAUST CASE COWLING FOR A GAS TURBINE ENGINE

 #68 | 2008-03-13
US20080063514A1
Mechanical engineering

Seal system for an interturbine duct within a gas turbine engine

 #69 | 2008-03-13
US20080061515A1
Mechanical engineering

RIM SEAL FOR A GAS TURBINE ENGINE

 #70 | 2008-03-13
US20080060344A1
Mechanical engineering

Exhaust duct and tail cone attachment of aircraft engines

 #71 | 2008-02-28
US20080050238A1
Mechanical engineering

Disc firtree slot with truncation for blade attachment

 #72 | 2008-02-28
US20080050229A1
Mechanical engineering

Interturbine duct with integrated baffle and seal

 #73 | 2008-02-28
US20080050061A1
Mechanical engineering

Oil bearing and tube assembly concept

 #74 | 2008-02-28
US20080047888A1
Performing operations; transporting

Oil strainer for a gas turbine engine

 #75 | 2008-02-28
US20080047242A1
Performing operations; transporting

Strainer for a gas turbine engine

 #76 | 2008-02-21
US20080041033A1
Mechanical engineering

Gas turbine engine exhaust duct ventilation

 #77 | 2007-01-25
US20070020088A1
Mechanical engineering

Turbine shroud segment impingement cooling on vane outer shroud

 #78 | 2007-01-25
US20070020087A1
Mechanical engineering

Turbine shroud segment feather seal located in radial shroud legs

 #79 | 2007-01-25
US20070020086A1
Mechanical engineering

Turbine shroud segment transpiration cooling with individual cast inlet and outlet cavities

 #80 | 2007-01-18
US20070015395A1
Mechanical engineering

Cable connection for a gas turbine engine safety fuel shut-off mechanism

 #81 | 2006-12-14
US20060277922A1
Mechanical engineering

Turbine support case and method of manufacturing

 #82 | 2006-08-10
US20060177309A1
Mechanical engineering

Airfoil locator rib and method of positioning an insert in an airfoil

 #83 | 2006-07-20
US20060159549A1
Mechanical engineering

Gas turbine engine shroud sealing arrangement

 #84 | 2006-06-15
US20060127215A1
Mechanical engineering

Integrated turbine vane support

 #85 | 2006-06-15
US20060127212A1
Mechanical engineering

Airfoil platform impingement cooling

 #86 | 2006-03-02
US20060045732A1
Mechanical engineering

Duct with integrated baffle

 #87 | 2006-03-02
US20060045730A1
Mechanical engineering

Lightweight annular interturbine duct
InventorID:

113095 ⎘