Syed J. Khalid

Person

Palm Beach Gardens, FL, US

People

Patents Grantslast 30 patents

Information Patent Grant
Gas turbine engine with variable speed turbines
- Patent number 10,378,439
- Issue date Aug 13, 2019
- Rolls-Royce North American Technologies Inc.
- Robert W. Cedoz
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine performance seeking control
- Patent number 9,759,132
- Issue date Sep 12, 2017
- Rolls-Royce Corporation
- Syed Jalaluddin Khalid
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Positionable ejector member for ejector enhanced boundary layer all...
- Patent number 9,630,706
- Issue date Apr 25, 2017
- Rolls-Royce Corporation
- Syed J. Khalid
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Modulated cooling flow scheduling for both SFC improvement and stal...
- Patent number 9,482,236
- Issue date Nov 1, 2016
- Rolls-Royce Corporation
- Syed Jalaluddin Khalid
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method and apparatus for use in control of clearances in a gas turb...
- Patent number 6,272,422
- Issue date Aug 7, 2001
- United Technologies Corporation
- Syed J. Khalid
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Control system for preventing compressor stall
- Patent number 6,231,306
- Issue date May 15, 2001
- United Technologies Corporation
- Syed J. Khalid
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Controlling stall margin in a gas turbine engine during acceleration
- Patent number 6,164,902
- Issue date Dec 26, 2000
- United Technologies Corporation
- Craig W. Irwin
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Method and apparatus for use in control and compensation of clearan...
- Patent number 6,155,038
- Issue date Dec 5, 2000
- United Technologies Corporation
- Craig W. Irwin
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Variable cycle engine with enhanced stability
- Patent number 5,623,823
- Issue date Apr 29, 1997
- United Technologies Corporation
- Steven M. Schirle
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Compressor endwall treatment
- Patent number 5,520,508
- Issue date May 28, 1996
- United Technologies Corporation
- Syed J. Khalid
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Rotating stall recovery
- Patent number 5,375,412
- Issue date Dec 27, 1994
- United Technologies Corporation
- Syed J. Khalid
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Sub-idle stability enhancement and rotating stall recovery
- Patent number 5,269,136
- Issue date Dec 14, 1993
- United Technologies Corporation
- Syed J. Khalid
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Controlling stall margin in a gas turbine engine during acceleration
- Patent number 5,165,845
- Issue date Nov 24, 1992
- United Technologies Corporation
- Syed J. Khalid
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
On-line stall margin adjustment in a gas turbine engine
- Patent number 5,165,844
- Issue date Nov 24, 1992
- United Technologies Corporation
- Syed J. Khalid
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Compressor bleed port
- Patent number 5,059,093
- Issue date Oct 22, 1991
- United Technologies Corporation
- Syed J. Khalid
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Active geometry control system for gas turbine engines
- Patent number 4,947,643
- Issue date Aug 14, 1990
- United Technologies Corporation
- Robert R. Pollak
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
AIRCRAFT BOUNDARY LAYER REMOVAL WITH AUXILLIARY POWER UNIT SUCTION
- Publication number 20170037779
- Publication date Feb 9, 2017
- Rolls-Royce Corporation
- Syed J. Khalid
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
POSITIONABLE EJECTOR MEMBER FOR EJECTOR ENHANCED BOUNDARY LAYER ALL...
- Publication number 20160009377
- Publication date Jan 14, 2016
- Rolls-Royce Corporation
- Syed J. Khalid
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE WITH VARIABLE SPEED TURBINES
- Publication number 20150330301
- Publication date Nov 19, 2015
- Rolls-Royce North American Technologies Inc.
- Robert W. CEDOZ
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE PERFORMANCE SEEKING CONTROL
- Publication number 20150267619
- Publication date Sep 24, 2015
- Rolls-Royce Corporation
- Syed Jalaluddin Khalid
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MODULATED COOLING FLOW SCHEDULING FOR BOTH SFC IMPROVEMENT AND STAL...
- Publication number 20140271113
- Publication date Sep 18, 2014
- Rolls-Royce Corporation
- Syed Jalaluddin Khalid
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
Method and apparatus for use in control of clearances in a gas turb...
- Publication number 20010001845
- Publication date May 24, 2001
- Syed J. Khalid
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Syed J. Khalid

Person

Patents Grantslast 30 patents

Gas turbine engine with variable speed turbines

Gas turbine engine performance seeking control

Positionable ejector member for ejector enhanced boundary layer all...

Modulated cooling flow scheduling for both SFC improvement and stal...

Method and apparatus for use in control of clearances in a gas turb...

Control system for preventing compressor stall

Controlling stall margin in a gas turbine engine during acceleration

Method and apparatus for use in control and compensation of clearan...

Variable cycle engine with enhanced stability

Compressor endwall treatment

Rotating stall recovery

Sub-idle stability enhancement and rotating stall recovery

Controlling stall margin in a gas turbine engine during acceleration

On-line stall margin adjustment in a gas turbine engine

Compressor bleed port

Active geometry control system for gas turbine engines

Patents Applicationslast 30 patents

AIRCRAFT BOUNDARY LAYER REMOVAL WITH AUXILLIARY POWER UNIT SUCTION

POSITIONABLE EJECTOR MEMBER FOR EJECTOR ENHANCED BOUNDARY LAYER ALL...

GAS TURBINE ENGINE WITH VARIABLE SPEED TURBINES

GAS TURBINE ENGINE PERFORMANCE SEEKING CONTROL

MODULATED COOLING FLOW SCHEDULING FOR BOTH SFC IMPROVEMENT AND STAL...

Method and apparatus for use in control of clearances in a gas turb...