Robert E. Malecki

Person

Storrs, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Gas turbine engine mounted above wing and with camber
- Patent number 11,970,974
- Issue date Apr 30, 2024
- RTX Corporation
- Robert E. Malecki
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Low pressure ratio fan engine having a dimensional relationship bet...
- Patent number 11,781,447
- Issue date Oct 10, 2023
- RTX Corporation
- Wesley K. Lord
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Low pressure ratio fan engine having a dimensional relationship bet...
- Patent number 11,781,505
- Issue date Oct 10, 2023
- RTX Corporation
- Wesley K. Lord
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Elongated geared turbofan with high bypass ratio
- Patent number 11,391,216
- Issue date Jul 19, 2022
- Raytheon Technologies Corporation
- Frederick M. Schwarz
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Low pressure ratio fan engine having a dimensional relationship bet...
- Patent number 11,286,811
- Issue date Mar 29, 2022
- Raytheon Technologies Corporation
- Wesley K. Lord
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Convergent divergent exit nozzle for a gas turbine engine
- Patent number 11,236,701
- Issue date Feb 1, 2022
- Raytheon Technologies Corporation
- Dmitriy B. Sidelkovskiy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Low pressure ratio fan engine having a dimensional relationship bet...
- Patent number 11,015,550
- Issue date May 25, 2021
- Raytheon Technologies Corporation
- Wesley K. Lord
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nacelle short inlet
- Patent number 10,724,541
- Issue date Jul 28, 2020
- United Technologies Corporation
- Yuan J. Qiu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nacelle short inlet for fan blade removal
- Patent number 10,479,519
- Issue date Nov 19, 2019
- United Technologies Corporation
- Yuan J. Qiu
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Track fairing assembly for a turbine engine nacelle
- Patent number 10,450,898
- Issue date Oct 22, 2019
- United Technologies Corporation
- Dmitriy B. Sidelkovskiy
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Exhaust nozzle for an elongated gear turbofan with high bypass ratio
- Patent number 10,436,120
- Issue date Oct 8, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Elongated geared turbofan with high bypass ratio
- Patent number 10,436,121
- Issue date Oct 8, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Convergent divergent exit nozzle for a gas turbine engine
- Patent number 10,371,092
- Issue date Aug 6, 2019
- United Technologies Corporation
- Dmitriy B. Sidelkovskiy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Asymmetric fan nozzle in high-BPR separate-flow nacelle
- Patent number 10,330,047
- Issue date Jun 25, 2019
- United Technologies Corporation
- Wesley K. Lord
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle arrangement for geared turbofan
- Patent number 10,316,757
- Issue date Jun 11, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Low pressure ratio fan engine having a dimensional relationship bet...
- Patent number 10,301,971
- Issue date May 28, 2019
- United Technologies Corporation
- Wesley K. Lord
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle arrangement for geared turbofan
- Patent number 10,294,871
- Issue date May 21, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Nacelle deflection measurement assembly
- Patent number 10,295,420
- Issue date May 21, 2019
- United Technologies Corporation
- Joshua V. Wood
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbomachine thrust reverser
- Patent number 10,145,335
- Issue date Dec 4, 2018
- United Technologies Corporation
- Robert L. Gukeisen
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Nacelle and compressor inlet arrangements
- Patent number 10,054,059
- Issue date Aug 21, 2018
- United Technologies Corporation
- Frederick M. Schwarz
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine engine thrust reverser system
- Patent number 10,006,404
- Issue date Jun 26, 2018
- United Technologies Corporation
- Robert E. Malecki
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Non-circular aft nacelle cowling geometry
- Patent number 9,995,180
- Issue date Jun 12, 2018
- United Technologies Corporation
- Michael J. Murphy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Low pressure ratio fan engine having a dimensional relationship bet...
- Patent number 9,932,933
- Issue date Apr 3, 2018
- United Technologies Corporation
- Wesley K. Lord
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Low pressure ratio fan engine having a dimensional relationship bet...
- Patent number 9,920,653
- Issue date Mar 20, 2018
- United Technologies Corporation
- Wesley K. Lord
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Nacelle bifurcation for gas turbine engine
- Patent number 9,249,731
- Issue date Feb 2, 2016
- United Technologies Corporation
- Dmitriy B. Sidelkovskiy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Non-circular aft nacelle cowling geometry
- Patent number 9,057,286
- Issue date Jun 16, 2015
- United Technologies Corporation
- Michael Joseph Murphy
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER
- Publication number 20220136440
- Publication date May 5, 2022
- RAYTHEON TECHNOLOGIES CORPORATION
- Robert E. Malecki
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER
- Publication number 20220136441
- Publication date May 5, 2022
- Raytheon Technologies Corporation
- Robert E. Malecki
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20220010689
- Publication date Jan 13, 2022
- Raytheon Technologies Corporation
- Wesley K. Lord
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20210285403
- Publication date Sep 16, 2021
- Raytheon Technologies Corporation
- Wesley K. Lord
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20200063603
- Publication date Feb 27, 2020
- United Technologies Corporation
- Wesley K. Lord
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20200025036
- Publication date Jan 23, 2020
- United Technologies Corporation
- Wesley K. Lord
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
ELONGATED GEARED TURBOFAN WITH HIGH BYPASS RATIO
- Publication number 20190271269
- Publication date Sep 5, 2019
- United Technologies Corporation
- Frederick M. Schwarz
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
CONVERGENT DIVERGENT EXIT NOZZLE FOR A GAS TURBINE ENGINE
- Publication number 20190017470
- Publication date Jan 17, 2019
- United Technologies Corporation
- Dmitriy B. Sidelkovskiy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20180209379
- Publication date Jul 26, 2018
- United Technologies Corporation
- Wesley K. Lord
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20180163568
- Publication date Jun 14, 2018
- United Technologies Corporation
- Wesley K. Lord
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE SHORT INLET
- Publication number 20170298954
- Publication date Oct 19, 2017
- United Technologies Corporation
- Yuan J. Qiu
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
NACELLE DEFLECTION MEASUREMENT ASSEMBLY
- Publication number 20170292882
- Publication date Oct 12, 2017
- United Technologies Corporation
- Joshua V. Wood
- G01 - MEASURING TESTING
Information Patent Application
NACELLE SHORT INLET FOR FAN BLADE REMOVAL
- Publication number 20170190438
- Publication date Jul 6, 2017
- United Technologies Corporation
- Yuan J. Qiu
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TRACK FAIRING ASSEMBLY FOR A TURBINE ENGINE NACELLE
- Publication number 20160237856
- Publication date Aug 18, 2016
- United Technologies Corporation
- Dmitriy B. Sidelkovskiy
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
BYPASS DUCT HEAT EXCHANGER PLACEMENT
- Publication number 20160215732
- Publication date Jul 28, 2016
- United Technologies Corporation
- Robert E. Malecki
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST NOZZLE ARRANGEMENT FOR GEARED TURBOFAN
- Publication number 20160201569
- Publication date Jul 14, 2016
- United Technologies Corporation
- Frederick M. Schwarz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST NOZZLE ARRANGEMENT FOR GEARED TURBOFAN
- Publication number 20160201570
- Publication date Jul 14, 2016
- Frederick M. Schwarz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CONVERGENT DIVERGENT EXIT NOZZLE FOR A GAS TURBINE ENGINE
- Publication number 20160195038
- Publication date Jul 7, 2016
- United Technologies Corporation
- Dmitriy B. Sidelkovskiy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20160108854
- Publication date Apr 21, 2016
- Wesley K. Lord
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
NACELLE AND COMPRESSOR INLET ARRANGEMENTS
- Publication number 20160076460
- Publication date Mar 17, 2016
- United Technologies Corporation
- Frederick M. Schwarz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20160061057
- Publication date Mar 3, 2016
- United Technologies Corporation
- Wesley K. LORD
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
NACELLE INTERNAL AND EXTERNAL FLOW CONTROL
- Publication number 20160003091
- Publication date Jan 7, 2016
- United Technologies Corporation
- Robert E. Malecki
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Asymmetric Fan Nozzle in High-BPR Separate-Flow Nacelle
- Publication number 20160003194
- Publication date Jan 7, 2016
- United Technologies Corporation
- Wesley K. Lord
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NON-CIRCULAR AFT NACELLE COWLING GEOMETRY
- Publication number 20150247425
- Publication date Sep 3, 2015
- United Technologies Corporation
- Michael J. Murphy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...
- Publication number 20150044028
- Publication date Feb 12, 2015
- United Technologies Corporation
- Wesley K. LORD
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Elongated Geared Turbofan With High Bypass Ratio
- Publication number 20140286754
- Publication date Sep 25, 2014
- United Technologies Corporation
- Frederick M. Schwarz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ELONGATED GEARED TURBOFAN WITH HIGH BYPASS RATIO
- Publication number 20140283501
- Publication date Sep 25, 2014
- United Technologies Corporation
- Frederick M. Schwarz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOMACHINE THRUST REVERSER
- Publication number 20140246514
- Publication date Sep 4, 2014
- United Technologies Corporation
- Robert L. Gukeisen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Gas Turbine Engine Assembly Including A Thrust Reverser
- Publication number 20140216005
- Publication date Aug 7, 2014
- United Technologies Corporation
- Dmitriy B. Sidelkovskiy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE BIFURCATION FOR GAS TURBINE ENGINE
- Publication number 20130319002
- Publication date Dec 5, 2013
- Dmitriy B. Sidelkovskiy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Robert E. Malecki

Person

Patents Grantslast 30 patents

Gas turbine engine mounted above wing and with camber

Low pressure ratio fan engine having a dimensional relationship bet...

Low pressure ratio fan engine having a dimensional relationship bet...

Elongated geared turbofan with high bypass ratio

Low pressure ratio fan engine having a dimensional relationship bet...

Convergent divergent exit nozzle for a gas turbine engine

Low pressure ratio fan engine having a dimensional relationship bet...

Nacelle short inlet

Nacelle short inlet for fan blade removal

Track fairing assembly for a turbine engine nacelle

Exhaust nozzle for an elongated gear turbofan with high bypass ratio

Elongated geared turbofan with high bypass ratio

Convergent divergent exit nozzle for a gas turbine engine

Asymmetric fan nozzle in high-BPR separate-flow nacelle

Exhaust nozzle arrangement for geared turbofan

Low pressure ratio fan engine having a dimensional relationship bet...

Exhaust nozzle arrangement for geared turbofan

Nacelle deflection measurement assembly

Turbomachine thrust reverser

Nacelle and compressor inlet arrangements

Gas turbine engine thrust reverser system

Non-circular aft nacelle cowling geometry

Low pressure ratio fan engine having a dimensional relationship bet...

Low pressure ratio fan engine having a dimensional relationship bet...

Nacelle bifurcation for gas turbine engine

Non-circular aft nacelle cowling geometry

Patents Applicationslast 30 patents

GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER

GAS TURBINE ENGINE MOUNTED ABOVE WING AND WITH CAMBER

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

ELONGATED GEARED TURBOFAN WITH HIGH BYPASS RATIO

CONVERGENT DIVERGENT EXIT NOZZLE FOR A GAS TURBINE ENGINE

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

NACELLE SHORT INLET

NACELLE DEFLECTION MEASUREMENT ASSEMBLY

NACELLE SHORT INLET FOR FAN BLADE REMOVAL

TRACK FAIRING ASSEMBLY FOR A TURBINE ENGINE NACELLE

BYPASS DUCT HEAT EXCHANGER PLACEMENT

EXHAUST NOZZLE ARRANGEMENT FOR GEARED TURBOFAN

EXHAUST NOZZLE ARRANGEMENT FOR GEARED TURBOFAN

CONVERGENT DIVERGENT EXIT NOZZLE FOR A GAS TURBINE ENGINE

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

NACELLE AND COMPRESSOR INLET ARRANGEMENTS

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

NACELLE INTERNAL AND EXTERNAL FLOW CONTROL

Asymmetric Fan Nozzle in High-BPR Separate-Flow Nacelle

NON-CIRCULAR AFT NACELLE COWLING GEOMETRY

LOW PRESSURE RATIO FAN ENGINE HAVING A DIMENSIONAL RELATIONSHIP BET...

Elongated Geared Turbofan With High Bypass Ratio

ELONGATED GEARED TURBOFAN WITH HIGH BYPASS RATIO

TURBOMACHINE THRUST REVERSER

Gas Turbine Engine Assembly Including A Thrust Reverser

NACELLE BIFURCATION FOR GAS TURBINE ENGINE