Ashok K. Jain

Person

Tempe, AZ, US

People

Patents Grantslast 30 patents

Information Patent Grant
Variable area nozzle assisted gas turbine engine restarting
- Patent number 10,309,315
- Issue date Jun 4, 2019
- United Technologies Corporation
- Ashok K. Jain
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine engine systems involving integrated fluid conduits
- Patent number 9,611,758
- Issue date Apr 4, 2017
- United Technologies Corporation
- Ashok K. Jain
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Variable area nozzle assisted gas turbine engine restarting
- Patent number 9,328,666
- Issue date May 3, 2016
- United Technologies Corporation
- Ashok K. Jain
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Variable contour nacelle assembly for a gas turbine engine
- Patent number 9,228,534
- Issue date Jan 5, 2016
- United Technologies Corporation
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Nacelle flow assembly
- Patent number 9,004,399
- Issue date Apr 14, 2015
- United Technologies Corporation
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Reduced take-off field length using variable nozzle
- Patent number 8,935,073
- Issue date Jan 13, 2015
- United Technologies Corporation
- Wayne Hurwitz
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Variable contraction ratio nacelle assembly for a gas turbine engine
- Patent number 8,727,267
- Issue date May 20, 2014
- United Technologies Corporation
- Ashok K. Jain
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Integrated variable area nozzle and thrust reversing mechanism
- Patent number 8,720,182
- Issue date May 13, 2014
- United Technologies Corporation
- Ashok K. Jain
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Nacelle compartment plenum for bleed air flow delivery system
- Patent number 8,657,567
- Issue date Feb 25, 2014
- United Technologies Corporation
- Thomas G. Cloft
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Bifurcation and aft vent used to vary fan nozzle exit area
- Patent number 8,650,854
- Issue date Feb 18, 2014
- United Technologies Corporation
- Edward F. Migliaro
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Nacelle flow assembly
- Patent number 8,596,573
- Issue date Dec 3, 2013
- United Technologies Corporation
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Nacelle assembly having inlet airfoil for a gas turbine engine
- Patent number 8,408,491
- Issue date Apr 2, 2013
- United Technologies Corporation
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Variable shape inlet section for a nacelle assembly of a gas turbin...
- Patent number 8,402,739
- Issue date Mar 26, 2013
- United Technologies Corporation
- Ashok K. Jain
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Nacelle flow assembly
- Patent number 8,282,037
- Issue date Oct 9, 2012
- United Technologies Corporation
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine systems involving integrated fluid conduits
- Patent number 8,240,979
- Issue date Aug 14, 2012
- United Technologies Corp.
- Ashok K. Jain
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Gas turbine engine system providing simulated boundary layer thickn...
- Patent number 8,209,953
- Issue date Jul 3, 2012
- United Technologies Corporation
- Michael Winter
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Detecting ice buildup on an aircraft engine and actuating the turbo...
- Patent number 8,209,950
- Issue date Jul 3, 2012
- United Technologies Corporation
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Variable geometry nacelle assembly for a gas turbine engine
- Patent number 8,205,430
- Issue date Jun 26, 2012
- United Technologies Corporation
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Actuation of a turbofan engine bifurcation to change an effective n...
- Patent number 8,137,060
- Issue date Mar 20, 2012
- United Technologies Corporation
- Michael Winter
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine providing simulated boundary layer thickness inc...
- Patent number 7,870,721
- Issue date Jan 18, 2011
- United Technologies Corporation
- Michael Winter
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
VARIABLE AREA NOZZLE ASSISTED GAS TURBINE ENGINE RESTARTING
- Publication number 20160290239
- Publication date Oct 6, 2016
- United Technologies Corporation
- Ashok K. Jain
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBIN...
- Publication number 20130170950
- Publication date Jul 4, 2013
- United Technologies Corporation
- Ashok K. Jain
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
NACELLE FLOW ASSEMBLY
- Publication number 20120325978
- Publication date Dec 27, 2012
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE SYSTEMS INVOLVING INTEGRATED FLUID CONDUITS
- Publication number 20120243972
- Publication date Sep 27, 2012
- Ashok K. Jain
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE SYSTEM PROVIDING SIMULATED BOUNDARY LAYER THICKN...
- Publication number 20110072828
- Publication date Mar 31, 2011
- Michael Winter
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
NACELLE FLOW ASSEMBLY
- Publication number 20110020105
- Publication date Jan 27, 2011
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
INTEGRATED VARIABLE AREA NOZZLE AND THRUST REVERSING MECHANISM
- Publication number 20100269485
- Publication date Oct 28, 2010
- Ashok K. Jain
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CONTROLLING ICE BUILDUP ON AIRCRAFT ENGINE AND NACELLE STATIC AND R...
- Publication number 20100043390
- Publication date Feb 25, 2010
- Ashok K. Jain
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
REDUCED TAKE-OFF FIELD LENGTH USING VARIABLE NOZZLE
- Publication number 20090259379
- Publication date Oct 15, 2009
- Wayne Hurwitz
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
ACTUATION OF A TURBOFAN ENGINE BIFURCATION TO CHANGE AN EFFECTIVE N...
- Publication number 20090252600
- Publication date Oct 8, 2009
- UNITED TECHNOLOGES CORPORATION
- Michael Winter
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
VARIABLE AREA NOZZLE ASSISTED GAS TURBINE ENGINE RESTARTING
- Publication number 20090235638
- Publication date Sep 24, 2009
- Ashok K. Jain
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
BIFURCATION AND AFT VENT USED TO VARY FAN NOZZLE EXIT AREA
- Publication number 20090178416
- Publication date Jul 16, 2009
- Edward F. Migliaro
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Nacelle Flow Assembly
- Publication number 20090121083
- Publication date May 14, 2009
- Ashok K. Jain
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Gas Turbine Engine Systems Involving Integrated Fluid Conduits
- Publication number 20090110537
- Publication date Apr 30, 2009
- United Technologies Corp.
- Ashok K. Jain
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
VARIABLE CONTOUR NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE
- Publication number 20090008508
- Publication date Jan 8, 2009
- Ashok K. Jain
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBIN...
- Publication number 20090003997
- Publication date Jan 1, 2009
- Ashok K. Jain
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
VARIABLE GEOMETRY GAS TURBINE ENGINE NACELLE ASSEMBLY WITH NANOELEC...
- Publication number 20080310956
- Publication date Dec 18, 2008
- Ashok K. Jain
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
NACELLE COMPARTMENT PLENUM FOR BLEED AIR FLOW DELIVERY SYSTEM
- Publication number 20080298950
- Publication date Dec 4, 2008
- Thomas G. Cloft
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
VARIABLE CONTRACTION RATIO NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE
- Publication number 20080283676
- Publication date Nov 20, 2008
- Ashok K. Jain
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
VARIABLE GEOMETRY NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE
- Publication number 20080286094
- Publication date Nov 20, 2008
- Ashok K. Jain
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE ASSEMBLY HAVING INLET AIRFOIL FOR A GAS TURBINE ENGINE
- Publication number 20080267762
- Publication date Oct 30, 2008
- Ashok K. Jain
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
Gas turbine engine providing simulated boundary layer thickness inc...
- Publication number 20080112799
- Publication date May 15, 2008
- United Technologies Corporation
- Michael Winter
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...

Ashok K. Jain

Person

Patents Grantslast 30 patents

Variable area nozzle assisted gas turbine engine restarting

Gas turbine engine systems involving integrated fluid conduits

Variable area nozzle assisted gas turbine engine restarting

Variable contour nacelle assembly for a gas turbine engine

Nacelle flow assembly

Reduced take-off field length using variable nozzle

Variable contraction ratio nacelle assembly for a gas turbine engine

Integrated variable area nozzle and thrust reversing mechanism

Nacelle compartment plenum for bleed air flow delivery system

Bifurcation and aft vent used to vary fan nozzle exit area

Nacelle flow assembly

Nacelle assembly having inlet airfoil for a gas turbine engine

Variable shape inlet section for a nacelle assembly of a gas turbin...

Nacelle flow assembly

Gas turbine engine systems involving integrated fluid conduits

Gas turbine engine system providing simulated boundary layer thickn...

Detecting ice buildup on an aircraft engine and actuating the turbo...

Variable geometry nacelle assembly for a gas turbine engine

Actuation of a turbofan engine bifurcation to change an effective n...

Gas turbine engine providing simulated boundary layer thickness inc...

Patents Applicationslast 30 patents

VARIABLE AREA NOZZLE ASSISTED GAS TURBINE ENGINE RESTARTING

VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBIN...

NACELLE FLOW ASSEMBLY

GAS TURBINE ENGINE SYSTEMS INVOLVING INTEGRATED FLUID CONDUITS

GAS TURBINE ENGINE SYSTEM PROVIDING SIMULATED BOUNDARY LAYER THICKN...

NACELLE FLOW ASSEMBLY

INTEGRATED VARIABLE AREA NOZZLE AND THRUST REVERSING MECHANISM

CONTROLLING ICE BUILDUP ON AIRCRAFT ENGINE AND NACELLE STATIC AND R...

REDUCED TAKE-OFF FIELD LENGTH USING VARIABLE NOZZLE

ACTUATION OF A TURBOFAN ENGINE BIFURCATION TO CHANGE AN EFFECTIVE N...

VARIABLE AREA NOZZLE ASSISTED GAS TURBINE ENGINE RESTARTING

BIFURCATION AND AFT VENT USED TO VARY FAN NOZZLE EXIT AREA

Nacelle Flow Assembly

Gas Turbine Engine Systems Involving Integrated Fluid Conduits

VARIABLE CONTOUR NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE

VARIABLE SHAPE INLET SECTION FOR A NACELLE ASSEMBLY OF A GAS TURBIN...

VARIABLE GEOMETRY GAS TURBINE ENGINE NACELLE ASSEMBLY WITH NANOELEC...

NACELLE COMPARTMENT PLENUM FOR BLEED AIR FLOW DELIVERY SYSTEM

VARIABLE CONTRACTION RATIO NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE

VARIABLE GEOMETRY NACELLE ASSEMBLY FOR A GAS TURBINE ENGINE

NACELLE ASSEMBLY HAVING INLET AIRFOIL FOR A GAS TURBINE ENGINE

Gas turbine engine providing simulated boundary layer thickness inc...