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Inventor profile of:

Brian D. Merry

City:

Andover, Connecticut

Country:

United States

Published Applications:

211

Last publication date:

2026-01-01

Top Assignees for applications by Brian D. Merry

The entities that hold a legal rights for patent applications filed by inventor Merry Brian D.:

UNITED TECHNOLOGIES CORPORATION 98 Hartford, CT United States
UNITED TECHNOLOGIES CORPORATION 53 Farmington, CT United States
Raytheon Technologies Corporation 20 Farmington, CT United States
RTX Corporation 9 Farmington, CT United States
UNITED TECHNOLOGIES CORP. 3 Hartford, CT United States
United Technologies Corporation 2 East Hartford, CT United States
United Technologies Corporation 1 Windsor, CT United States
Pratt & Whitney 1 East Hartford, CT United States
United Technologies Corporaiton 1 Hartford, CT United States
Raytheon Technologies Corporation 1 Waltham, MA United States

Recent patent applications by Merry Brian D.

Brian D. Merry from Andover, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-01-01

US20260002493A1

Mechanical engineering

ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

#2 | 2025-09-18

US20250290454A1

Mechanical engineering

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

#3 | 2025-06-12

US20250188871A1

Mechanical engineering

GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES

#4 | 2025-02-20

US20250058887A1

Performing operations; transporting

ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE

#5 | 2024-12-12

US20240410320A1

Mechanical engineering

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

#6 | 2024-03-07

US20240076050A1

Performing operations; transporting

Engine mount system for a gas turbine engine

#7 | 2024-02-29

US20240068411A1

Mechanical engineering

Gas turbine engine compressor arrangement

#8 | 2023-06-22

US20230193830A1

Mechanical engineering

GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES

#9 | 2021-12-02

US20210372349A1

Mechanical engineering

Engine mount system for a gas turbine engine

#10 | 2021-08-05

US20210239074A1

Mechanical engineering

Gas turbine engine shaft bearing configuration

#11 | 2021-05-20

US20210148289A1

Mechanical engineering

Intercooled cooling air with auxiliary compressor control

#12 | 2021-03-04

US20210062725A1

Mechanical engineering

Gas turbine engine compressor arrangement

#13 | 2020-09-10

US20200284222A1

Mechanical engineering

Gas turbine engine with low stage count low pressure turbine and engine mounting arrangement

#14 | 2020-05-07

US20200141417A1

Mechanical engineering

BOOSTER COMPRESSOR WITH SPEED CHANGE SYSTEM

#15 | 2020-03-26

US20200095929A1

Mechanical engineering

HIGH THRUST GEARED GAS TURBINE ENGINE

#16 | 2020-02-13

US20200049077A1

Mechanical engineering

Gas turbine engine with high speed low pressure turbine section and bearing support features

#17 | 2020-01-23

US20200025105A1

Mechanical engineering

Intercooled cooling air with auxiliary compressor control

#18 | 2020-01-23

US20200025030A1

Mechanical engineering

Gas turbine engine shaft bearing configuration

#19 | 2019-12-19

US20190383167A1

Mechanical engineering

Intercooled cooling air with low temperature bearing compartment air

#20 | 2019-10-24

US20190323789A1

Mechanical engineering

INTERCOOLED COOLING AIR

#21 | 2019-05-23

US20190154059A1

Mechanical engineering

Intercooled cooling air tapped from plural locations

#22 | 2019-04-11

US20190107055A1

Mechanical engineering

Multi-source turbine cooling air

#23 | 2019-04-11

US20190107051A1

Mechanical engineering

Gas turbine engine shaft bearing configuration

#24 | 2019-02-28

US20190063325A1

Mechanical engineering

Intercooled cooling air using cooling compressor as starter

#25 | 2018-12-06

US20180347815A1

Mechanical engineering

Turbine stage cooling

#26 | 2018-10-04

US20180283277A1

Mechanical engineering

Geared turbofan bearing arrangement

#27 | 2018-09-13

US20180258860A1

Mechanical engineering

Intercooled cooling air with heat exchanger packaging

#28 | 2018-09-13

US20180258859A1

Mechanical engineering

Intercooled cooling air with dual pass heat exchanger

#29 | 2018-09-06

US20180252162A1

Mechanical engineering

Gas turbine engine thermal management system

#30 | 2018-08-16

US20180230912A1

Mechanical engineering

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

#31 | 2018-08-16

US20180230909A1

Mechanical engineering

Ceramic matrix composite turbine exhaust case for a gas turbine engine

#32 | 2018-08-09

US20180223668A1

Mechanical engineering

Spoked rotor for a gas turbine engine

#33 | 2018-07-05

US20180187605A1

Mechanical engineering

SYSTEMS AND METHODS INVOLVING MULTIPLE TORQUE PATHS FOR GAS TURBINE ENGINES

#34 | 2018-03-08

US20180066587A1

Mechanical engineering

Intercooled cooling air with dual pass heat exchanger

#35 | 2018-01-25

US20180023576A1

Mechanical engineering

Twin centrifugal single spool engine

#36 | 2018-01-25

US20180023509A1

Mechanical engineering

THRUST REVERSER STRUCTURE MOUNTED TO FAN CASE

#37 | 2017-12-21

US20170363099A1

Mechanical engineering

Engine bleed air system with waste gate valve for compressor surge management

#38 | 2017-12-21

US20170363098A1

Mechanical engineering

BOOSTER COMPRESSOR WITH SPEED CHANGE SYSTEM

#39 | 2017-12-21

US20170363014A1

Mechanical engineering

Engine bleed air with compressor surge management

#40 | 2017-10-26

US20170306847A1

Mechanical engineering

Combined Drive for Cooling Air Using Cooing Compressor and Aircraft Air Supply Pump

#41 | 2017-09-07

US20170254219A1

Mechanical engineering

Firewall mount hub

#42 | 2017-06-15

US20170167388A1

Mechanical engineering

Intercooled cooling air with auxiliary compressor control

#43 | 2017-06-15

US20170167386A1

Mechanical engineering

Multi-source turbine cooling air

#44 | 2017-06-15

US20170167384A1

Mechanical engineering

Compressor core inner diameter cooling

#45 | 2017-05-04

US20170122220A1

Mechanical engineering

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

#46 | 2017-05-04

US20170122219A1

Mechanical engineering

GAS TURBINE ENGINE COMPRESSOR ARRANGEMENT

#47 | 2017-04-27

US20170114724A1

Mechanical engineering

GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES

#48 | 2017-03-02

US20170058830A1

Mechanical engineering

Gas turbine engine with low stage count low pressure turbine

#49 | 2016-12-15

US20160363047A1

Mechanical engineering

HIGH THRUST GEARED GAS TURBINE ENGINE

#50 | 2016-11-10

US20160326957A1

Mechanical engineering

Combined stability and customer bleed with dirt, water and ice rejection

#51 | 2016-10-27

US20160312797A1

Mechanical engineering

Intercooled cooling air tapped from plural locations

#52 | 2016-10-27

US20160312711A1

Mechanical engineering

Intercooled cooling air with plural heat exchangers

#53 | 2016-10-27

US20160312704A1

Mechanical engineering

Intercooled cooling air with dual pass heat exchanger

#54 | 2016-10-06

US20160290241A1

Mechanical engineering

Gas turbine engine compressor arrangement

#55 | 2016-10-06

US20160290149A1

Mechanical engineering

Segmented seal for gas turbine engine

#56 | 2016-09-29

US20160280387A1

Performing operations; transporting

Aircraft thermal management system

#57 | 2016-08-18

US20160237909A1

Mechanical engineering

Intercooled cooling air using cooling compressor as starter

#58 | 2016-08-18

US20160237908A1

Mechanical engineering

INTERCOOLED COOLING AIR USING EXISTING HEAT EXCHANGER

#59 | 2016-08-18

US20160237907A1

Mechanical engineering

INTERCOOLED COOLING AIR WITH AUXILIARY COMPRESSOR CONTROL

#60 | 2016-08-18

US20160237906A1

Mechanical engineering

Intercooled cooling air with heat exchanger packaging

#61 | 2016-08-18

US20160237905A1

Mechanical engineering

INTERCOOLED COOLING AIR

#62 | 2016-08-18

US20160237901A1

Mechanical engineering

Intercooled cooling air with improved air flow

#63 | 2016-08-11

US20160230661A1

Mechanical engineering

Gas turbine engine having section with thermally isolated area

#64 | 2016-08-11

US20160230597A1

Mechanical engineering

Gas turbine engine having section with thermally isolated area

#65 | 2016-07-21

US20160208713A1

Mechanical engineering

Gas turbine engine with high speed and temperature spool cooling system

#66 | 2016-07-21

US20160208698A1

Mechanical engineering

Gas turbine engine thermal management system

#67 | 2016-07-21

US20160208689A1

Mechanical engineering

Modifying a gas turbine engine to use a high pressure compressor as a low pressure compressor

#68 | 2016-06-30

US20160186571A1

Mechanical engineering

Mixing plenum for spoked rotors

#69 | 2016-05-12

US20160131044A1

Mechanical engineering

Gas turbine engine driving multiple fans

#70 | 2016-04-28

US20160115865A1

Mechanical engineering

GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES

#71 | 2016-04-07

US20160097304A1

Mechanical engineering

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

#72 | 2016-03-24

US20160084090A1

Mechanical engineering

Method and assembly for reducing secondary heat in a gas turbine engine

#73 | 2016-03-17

US20160076381A1

Mechanical engineering

Secondary flowpath system for a gas turbine engine

#74 | 2016-02-25

US20160053688A1

Mechanical engineering

Gas turbine rotors

#75 | 2016-02-18

US20160047306A1

Mechanical engineering

GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES

#76 | 2016-02-18

US20160047268A1

Mechanical engineering

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

#77 | 2016-02-11

US20160040594A1

Mechanical engineering

Counter-rotating low pressure turbine without turbine exhaust case

#78 | 2016-02-04

US20160032828A1

Mechanical engineering

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

#79 | 2016-02-04

US20160032731A1

Mechanical engineering

Thermal barrier coating inside cooling channels

#80 | 2016-01-28

US20160024958A1

Mechanical engineering

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

#81 | 2016-01-28

US20160024957A1

Mechanical engineering

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

#82 | 2016-01-28

US20160023307A1

Performing operations; transporting

Process for manufacturing a gamma titanium aluminide turbine component

#83 | 2016-01-07

US20160003058A1

Mechanical engineering

Rotor and gas turbine engine including same

#84 | 2015-12-31

US20150377142A1

Mechanical engineering

Low spool starter system for gas turbine engine

#85 | 2015-12-31

US20150377073A1

Mechanical engineering

TITANIUM ALUMINIDE TURBINE EXHAUST STRUCTURE

#86 | 2015-12-31

US20150377052A1

Mechanical engineering

Segmented seal for a gas turbine engine

#87 | 2015-12-24

US20150369130A1

Mechanical engineering

Systems and methods for distributing cooling air in gas turbine engines

#88 | 2015-12-17

US20150361890A1

Mechanical engineering

HIGH PRESSURE TURBINE COOLING

#89 | 2015-12-17

US20150361828A1

Mechanical engineering

Engine mounting system

#90 | 2015-12-10

US20150354822A1

Mechanical engineering

Turbine stage cooling

#91 | 2015-12-10

US20150354465A1

Mechanical engineering

TURBINE STAGE COOLING

#92 | 2015-12-10

US20150354456A1

Mechanical engineering

Cooling system for gas turbine engines

#93 | 2015-12-10

US20150354455A1

Mechanical engineering

Thermally isolated turbine section for a gas turbine engine

#94 | 2015-12-10

US20150354389A1

Mechanical engineering

Segmented rim seal spacer for a gas turbine engine

#95 | 2015-12-03

US20150345392A1

Mechanical engineering

Gas turbine engine shaft bearing configuration

#96 | 2015-11-19

US20150330300A1

Mechanical engineering

TWO SPOOL ENGINE CORE WITH A STARTER

#97 | 2015-11-05

US20150315977A1

Mechanical engineering

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

#98 | 2015-11-05

US20150315974A1

Mechanical engineering

TWO SPOOL GAS GENERATOR WITH IMPROVED PRESSURE SPLIT

#99 | 2015-10-22

US20150300250A1

Mechanical engineering

Two spool gas generator to create family of gas turbine engines

#100 | 2015-10-22

US20150300207A1

Mechanical engineering

GAS TURBINE ENGINE WITH LOW STAGE COUNT LOW PRESSURE TURBINE

InventorID:

34620 ⎘