Andrew Sanderson

Person

Indianapolis, IN, US

People

Patents Grantslast 30 patents

Information Patent Grant
Single movement convergent and convergent-divergent nozzle
- Patent number 11,680,495
- Issue date Jun 20, 2023
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Reconfigurable exhaust nozzle for a gas turbine engine
- Patent number 11,408,368
- Issue date Aug 9, 2022
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Exhaust nozzle having a compliant shell for a gas turbine engine
- Patent number 11,326,551
- Issue date May 10, 2022
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Single movement convergent and convergent-divergent nozzle
- Patent number 11,319,832
- Issue date May 3, 2022
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Exhaust nozzle with centerbody support structure for a gas turbine...
- Patent number 11,313,320
- Issue date Apr 26, 2022
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable area nozzle exhaust system with integrated thrust reverser
- Patent number 11,286,878
- Issue date Mar 29, 2022
- Rolls-Royce North American Technologies Inc.
- Todd S. Taylor
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Methodology for minimizing aerodynamic buzz in an exhaust nozzle
- Patent number 11,274,631
- Issue date Mar 15, 2022
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Exhaust nozzle with vane support structure for a gas turbine engine
- Patent number 11,274,630
- Issue date Mar 15, 2022
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
SINGLE MOVEMENT CONVERGENT AND CONVERGENT-DIVERGENT NOZZLE
- Publication number 20220235668
- Publication date Jul 28, 2022
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
VARIABLE AREA NOZZLE EXHAUST SYSTEM WITH INTEGRATED THRUST REVERSER
- Publication number 20210301761
- Publication date Sep 30, 2021
- Rolls-Royce North American Technologies Inc.
- Todd S. Taylor
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
RECONFIGURABLE EXHAUST NOZZLE FOR A GAS TURBINE ENGINE
- Publication number 20210301760
- Publication date Sep 30, 2021
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SINGLE MOVEMENT CONVERGENT AND CONVERGENT-DIVERGENT NOZZLE
- Publication number 20210270145
- Publication date Sep 2, 2021
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
EXHAUST NOZZLE WITH CENTERBODY SUPPORT STRUCTURE FOR A GAS TURBINE...
- Publication number 20210270208
- Publication date Sep 2, 2021
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
EXHAUST NOZZLE WITH VANE SUPPORT STRUCTURE FOR A GAS TURBINE ENGINE
- Publication number 20210270207
- Publication date Sep 2, 2021
- Rolls-Royce North American Technologies Inc.
- David L. Sutterfield
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHODOLOGY FOR MINIMIZING AERODYNAMIC BUZZ IN AN EXHAUST NOZZLE
- Publication number 20210270206
- Publication date Sep 2, 2021
- Rolls-Royce North American Technologies Inc.
- Andrew Sanderson
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Andrew Sanderson

Person

Patents Grantslast 30 patents

Single movement convergent and convergent-divergent nozzle

Reconfigurable exhaust nozzle for a gas turbine engine

Exhaust nozzle having a compliant shell for a gas turbine engine

Single movement convergent and convergent-divergent nozzle

Exhaust nozzle with centerbody support structure for a gas turbine...

Variable area nozzle exhaust system with integrated thrust reverser

Methodology for minimizing aerodynamic buzz in an exhaust nozzle

Exhaust nozzle with vane support structure for a gas turbine engine

Patents Applicationslast 30 patents

SINGLE MOVEMENT CONVERGENT AND CONVERGENT-DIVERGENT NOZZLE

VARIABLE AREA NOZZLE EXHAUST SYSTEM WITH INTEGRATED THRUST REVERSER

RECONFIGURABLE EXHAUST NOZZLE FOR A GAS TURBINE ENGINE

SINGLE MOVEMENT CONVERGENT AND CONVERGENT-DIVERGENT NOZZLE

EXHAUST NOZZLE WITH CENTERBODY SUPPORT STRUCTURE FOR A GAS TURBINE...

EXHAUST NOZZLE WITH VANE SUPPORT STRUCTURE FOR A GAS TURBINE ENGINE

METHODOLOGY FOR MINIMIZING AERODYNAMIC BUZZ IN AN EXHAUST NOZZLE