Ramesh Rajagopalan

Person

Glastonbury, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Optical detection system for a gas turbine engine combustion assembly
- Patent number 12,331,929
- Issue date Jun 17, 2025
- RTX Corporation
- Orin G. Avidane
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Ground-based aircraft movement
- Patent number 12,258,139
- Issue date Mar 25, 2025
- RTX Corporation
- Stephen A. Witalis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Machine learned aero-thermodynamic engine inlet condition synthesis
- Patent number 12,180,892
- Issue date Dec 31, 2024
- RTX Corporation
- Timothy J. Crowley
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Grant
Gas turbine engine system wear reduction
- Patent number 11,976,589
- Issue date May 7, 2024
- RTX Corporation
- Stephen A. Witalis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Tuning engine parameter estimator using gas path analysis data
- Patent number 11,840,966
- Issue date Dec 12, 2023
- RTX Corporation
- Joshua Adams
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gear and electric amplification of generator motor compressor and t...
- Patent number 11,319,882
- Issue date May 3, 2022
- Raytheon Technologies Corporation
- Daniel Bernard Kupratis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine system wear reduction
- Patent number 11,306,654
- Issue date Apr 19, 2022
- Raytheon Technologies Corporation
- Stephen A. Witalis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine system bowed rotor start mitigation and wear red...
- Patent number 11,199,139
- Issue date Dec 14, 2021
- Raytheon Technologies Corporation
- Ramesh Rajagopalan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Adaptive control for a gas turbine engine
- Patent number 9,342,060
- Issue date May 17, 2016
- United Technologies Corporation
- James W. Fuller
- G05 - CONTROLLING REGULATING
Information Patent Grant
Closed loop propulsion system transient response predictor
- Patent number 8,862,363
- Issue date Oct 14, 2014
- United Technologies Corporation
- Ramesh Rajagopalan
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
OPTICAL DETECTION SYSTEM FOR A GAS TURBINE ENGINE COMBUSTION ASSEMBLY
- Publication number 20240271784
- Publication date Aug 15, 2024
- Orin G. Avidane
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
INTEGRATED THRUST REVERSER AND BRAKE CONTROL FOR AN AIRCRAFT
- Publication number 20240175409
- Publication date May 30, 2024
- Raytheon Technologies Corporation
- David Wasselin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT ENGINE ANOMALY DETECTION BASED ON ODOR, SOUND, AND/OR IMAGE
- Publication number 20240043137
- Publication date Feb 8, 2024
- RTX Corporation
- Stephen A. Witalis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT HYBRID DUPLEX-TRIPLEX CONTROL ARCHITECTURE
- Publication number 20230332547
- Publication date Oct 19, 2023
- Raytheon Technologies Corporation
- Bradley C. Schafer
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GROUND-BASED AIRCRAFT MOVEMENT
- Publication number 20230219693
- Publication date Jul 13, 2023
- Raytheon Technologies Corporation
- Stephen A. Witalis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
FINAL TAKEOFF SPEED DETERMINATION FOR AN AIRCRAFT
- Publication number 20230166857
- Publication date Jun 1, 2023
- Raytheon Technologies Corporation
- David Wasselin
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE SYSTEM WEAR REDUCTION
- Publication number 20220243653
- Publication date Aug 4, 2022
- Raytheon Technologies Corporation
- Stephen A. Witalis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GEAR AND ELECTRIC AMPLIFICATION OF GENERATOR MOTOR COMPRESSOR AND T...
- Publication number 20210071585
- Publication date Mar 11, 2021
- Raytheon Technologies Corporation
- Daniel Bernard Kupratis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
MACHINE LEARNED AERO-THERMODYNAMIC ENGINE INLET CONDITION SYNTHESIS
- Publication number 20200248622
- Publication date Aug 6, 2020
- United Technologies Corporation
- Timothy J. Crowley
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Application
GAS TURBINE ENGINE SYSTEM WEAR REDUCTION
- Publication number 20200200127
- Publication date Jun 25, 2020
- United Technologies Corporation
- Stephen A. Witalis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE SYSTEM BOWED ROTOR START MITIGATION AND WEAR RED...
- Publication number 20200200099
- Publication date Jun 25, 2020
- United Technologies Corporation
- Ramesh Rajagopalan
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
CLOSED LOOP PROPULSION SYSTEM TRANSIENT RESPONSE PREDICTOR
- Publication number 20140081547
- Publication date Mar 20, 2014
- United Technologies Corporation
- Ramesh Rajagopalan
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ADAPTIVE CONTROL FOR A GAS TURBINE ENGINE
- Publication number 20120060505
- Publication date Mar 15, 2012
- United Technologies Corporation
- James W. Fuller
- G05 - CONTROLLING REGULATING

Ramesh Rajagopalan

Person

Patents Grantslast 30 patents

Optical detection system for a gas turbine engine combustion assembly

Ground-based aircraft movement

Machine learned aero-thermodynamic engine inlet condition synthesis

Gas turbine engine system wear reduction

Tuning engine parameter estimator using gas path analysis data

Gear and electric amplification of generator motor compressor and t...

Gas turbine engine system wear reduction

Gas turbine engine system bowed rotor start mitigation and wear red...

Adaptive control for a gas turbine engine

Closed loop propulsion system transient response predictor

Patents Applicationslast 30 patents

OPTICAL DETECTION SYSTEM FOR A GAS TURBINE ENGINE COMBUSTION ASSEMBLY

INTEGRATED THRUST REVERSER AND BRAKE CONTROL FOR AN AIRCRAFT

AIRCRAFT ENGINE ANOMALY DETECTION BASED ON ODOR, SOUND, AND/OR IMAGE

AIRCRAFT HYBRID DUPLEX-TRIPLEX CONTROL ARCHITECTURE

GROUND-BASED AIRCRAFT MOVEMENT

FINAL TAKEOFF SPEED DETERMINATION FOR AN AIRCRAFT

GAS TURBINE ENGINE SYSTEM WEAR REDUCTION

GEAR AND ELECTRIC AMPLIFICATION OF GENERATOR MOTOR COMPRESSOR AND T...

MACHINE LEARNED AERO-THERMODYNAMIC ENGINE INLET CONDITION SYNTHESIS

GAS TURBINE ENGINE SYSTEM WEAR REDUCTION

GAS TURBINE ENGINE SYSTEM BOWED ROTOR START MITIGATION AND WEAR RED...

CLOSED LOOP PROPULSION SYSTEM TRANSIENT RESPONSE PREDICTOR

ADAPTIVE CONTROL FOR A GAS TURBINE ENGINE