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Inventor profile of:

Bruce L. Morin

City:

Springfield, Massachusetts

Country:

United States

Published Applications:

Last publication date:

2022-07-14

Top Assignees for applications by Bruce L. Morin

The entities that hold a legal rights for patent applications filed by inventor Morin Bruce L.:

UNITED TECHNOLOGIES CORPORATION 13 Hartford, CT United States
UNITED TECHNOLOGIES CORPORATION 7 Farmington, CT United States
Raytheon Technologies Corporation 5 Farmington, CT United States
MTU Aero Engines GmbH 5 Munich, Germany
MTU AERO ENGINES AG 3 Munich, Germany
MTU Aero Engines AG 1 Muenchen, Germany
United Technoloiies Corporation 1 Hartford, CT United States

Recent patent applications by Morin Bruce L.

Bruce L. Morin from Springfield, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2022-07-14

US20220220899A1

Mechanical engineering

Low noise turbine for geared gas turbine engine

#2 | 2022-01-13

US20220010732A1

Mechanical engineering

Low noise turbine for geared gas turbine engine

#3 | 2020-12-24

US20200400075A1

Mechanical engineering

Low noise turbine for geared gas turbine engine

#4 | 2020-09-17

US20200291859A1

Mechanical engineering

Low noise turbine for geared gas turbine engine

#5 | 2020-06-04

US20200173370A1

Mechanical engineering

LOW NOISE COMPRESSOR ROTOR FOR GEARED TURBOFAN ENGINE

#6 | 2019-05-23

US20190153891A1

Mechanical engineering

THREE SPOOL TURBOFAN ENGINE WITH LOW NOISE INTERMEDIATE TURBINE ROTOR

#7 | 2018-10-18

US20180298828A1

Mechanical engineering

LOW NOISE COMPRESSOR ROTOR FOR GEARED TURBOFAN ENGINE

#8 | 2017-11-09

US20170321611A1

Mechanical engineering

LOW NOISE COMPRESSOR ROTOR FOR GEARED TURBOFAN ENGINE

#9 | 2016-06-23

US20160177774A1

Mechanical engineering

Low noise turbine for geared gas turbine engine

#10 | 2016-06-02

US20160153361A1

Mechanical engineering

Bleed valve resonance augmentations

#11 | 2016-06-02

US20160153310A1

Mechanical engineering

Three spool turbofan engine with low noise intermediate turbine rotor

#12 | 2016-02-11

US20160040598A1

Mechanical engineering

Low noise compressor for geared gas turbine engine

#13 | 2016-02-04

US20160032756A1

Mechanical engineering

LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE

#14 | 2016-01-28

US20160025004A1

Mechanical engineering

LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE

#15 | 2015-12-17

US20150361824A1

Mechanical engineering

Gas turbine engine with low fan noise

#16 | 2015-11-26

US20150337684A1

Mechanical engineering

Acoustic treatment to mitigate fan noise

#17 | 2015-07-23

US20150204238A1

Mechanical engineering

LOW NOISE TURBINE FOR GEARED TURBOFAN ENGINE

#18 | 2015-06-04

US20150152787A1

Mechanical engineering

Low noise compressor rotor for geared turbofan engine

#19 | 2014-10-30

US20140318147A1

Mechanical engineering

LOW NOISE COMPRESSOR ROTOR FOR GEARED TURBOFAN ENGINE

#20 | 2014-09-18

US20140271112A1

Mechanical engineering

Low noise turbine for geared gas turbine engine

#21 | 2014-09-16

US14159760

Low noise compressor rotor for geared turbofan engine

#22 | 2014-01-02

US20140003915A1

Mechanical engineering

Low noise compressor rotor for geared turbofan engine

#23 | 2013-08-29

US20130219922A1

Mechanical engineering

GEARED GAS TURBINE ENGINE WITH REDUCED FAN NOISE

#24 | 2013-08-08

US20130202403A1

Mechanical engineering

Low noise turbine for geared turbofan engine

#25 | 2012-08-21

US13403005

Low noise turbine for geared turbofan engine

#26 | 2008-12-04

US20080295518A1

Mechanical engineering

Airfoil acoustic impedance control

#27 | 2007-11-29

US20070272483A1

Physics

Micro-perforated acoustic liner

#28 | 2005-06-23

US20050135924A1

Mechanical engineering

Airfoil surface impedance modification for noise reduction in turbofan engines

InventorID:

375928 ⎘