Zhijun Zheng

Person

Avon, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Extended orifice plug for a fluid system
- Patent number 11,486,278
- Issue date Nov 1, 2022
- Raytheon Technologies Corporation
- Zhijun Zheng
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Method of regulating air pressure in anti-icing system
- Patent number 11,060,454
- Issue date Jul 13, 2021
- Raytheon Technologies Corporation
- Robert Goodman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Direct-acting valve
- Patent number 10,927,963
- Issue date Feb 23, 2021
- Rohr, Inc.
- Robert Goodman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Nacelle anti ice system
- Patent number 10,450,955
- Issue date Oct 22, 2019
- United Technologies Corporation
- Robert Goodman
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Aircraft anti-icing system
- Patent number 10,421,551
- Issue date Sep 24, 2019
- United Technologies Corporation
- Michael D. Greenberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Thermally biased valve and anti-icing system
- Patent number 10,384,786
- Issue date Aug 20, 2019
- United Technologies Corporation
- Michael D. Greenberg
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Engine mount waiting fail safe lug joint with reduced dynamic ampli...
- Patent number 10,220,950
- Issue date Mar 5, 2019
- United Technologies Corporation
- Zhijun Zheng
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Axial tension system for a gas turbine engine case
- Patent number 10,190,499
- Issue date Jan 29, 2019
- United Technologies Corporation
- Joey Wong
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Nacelle anti-ice system and method with equalized flow
- Patent number 10,054,052
- Issue date Aug 21, 2018
- United Technologies Corporation
- Zhijun Zheng
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Aircraft nacelle anti-ice systems and methods
- Patent number 9,994,327
- Issue date Jun 12, 2018
- United Technologies Corporation
- Zhijun Zheng
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Inline pressure regulating valve assembly with inlet pressure bias
- Patent number 9,849,992
- Issue date Dec 26, 2017
- United Technologies Corporation
- Robert Goodman
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Secondary load path for gas turbine engine
- Patent number 9,227,734
- Issue date Jan 5, 2016
- United Technologies Corporation
- Zhijun Zheng
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Adjustable engine mount
- Patent number 9,217,337
- Issue date Dec 22, 2015
- United Technologies Corporation
- David F Sandy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Assembly for mounting a turbine engine to a pylon
- Patent number 8,985,509
- Issue date Mar 24, 2015
- United Technologies Corporation
- David F. Sandy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine mounting structure with secondary load paths
- Patent number 8,561,942
- Issue date Oct 22, 2013
- United Technologies Corporation
- Zhijun Zheng
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gearbox mount bracket
- Patent number 8,561,501
- Issue date Oct 22, 2013
- United Technologies Corporation
- Chris J. Niggemeier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Three-dimensional vehicle frame
- Patent number 7,862,085
- Issue date Jan 4, 2011
- GM Global Technologies Operations, Inc.
- Weizhang S. Xu
- B62 - LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS

Patents Applicationslast 30 patents

Information Patent Application
EXTENDED ORIFICE PLUG FOR A FLUID SYSTEM
- Publication number 20220178281
- Publication date Jun 9, 2022
- Zhijun Zheng
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
COVER FOR ROTATABLE SHAFT OF GAS TURBINE ENGINE
- Publication number 20200370445
- Publication date Nov 26, 2020
- United Technologies Corporation
- James D. Adams
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD OF REGULATING AIR PRESSURE IN ANTI-ICING SYSTEM
- Publication number 20200003117
- Publication date Jan 2, 2020
- United Technologies Corporation
- Robert Goodman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
NACELLE ANTI-ICING TROUBLESHOOTING FOR A TWO VALVE SYSTEM
- Publication number 20180355797
- Publication date Dec 13, 2018
- United Technologies Corporation
- Mainul M. Islam
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ANTI-ICE CONTROL SYSTEMS AND METHODS
- Publication number 20180170556
- Publication date Jun 21, 2018
- Rohr, Inc.
- ROBERT GOODMAN
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT NACELLE ANTI-ICE SYSTEMS AND METHODS
- Publication number 20180162538
- Publication date Jun 14, 2018
- United Technologies Corporation
- Zhijun Zheng
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
NACELLE ANTI ICE SYSTEM
- Publication number 20180010519
- Publication date Jan 11, 2018
- United Technologies Corporation
- Robert Goodman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INLINE PRESSURE REGULATING VALVE ASSEMBLY WITH INLET PRESSURE BIAS
- Publication number 20170334566
- Publication date Nov 23, 2017
- United Technologies Corporation
- Robert Goodman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THERMALLY BIASED VALVE AND ANTI-ICING SYSTEM
- Publication number 20170225791
- Publication date Aug 10, 2017
- United Technologies Corporation
- Michael D. Greenberg
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE ANTI-ICE SYSTEM AND METHOD WITH EQUALIZED FLOW
- Publication number 20170009653
- Publication date Jan 12, 2017
- United Technologies Corporation
- Zhijun Zheng
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT ANTI-ICING SYSTEM
- Publication number 20160167792
- Publication date Jun 16, 2016
- Michael D. Greenberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Engine Mount Waiting Fail Safe Lug Joint with Reduced Dynamic Ampli...
- Publication number 20150375867
- Publication date Dec 31, 2015
- United Technologies Corporation
- Zhijun Zheng
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AXIAL TENSION SYSTEM FOR A GAS TURBINE ENGINE CASE
- Publication number 20150369131
- Publication date Dec 24, 2015
- United Technologies Corporation
- Joey Wong
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ASSEMBLY FOR MOUNTING A TURBINE ENGINE TO A PYLON
- Publication number 20140061375
- Publication date Mar 6, 2014
- United Technologies Corporation
- David F. Sandy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SECONDARY LOAD PATH FOR GAS TURBINE ENGINE
- Publication number 20140061426
- Publication date Mar 6, 2014
- Zhijun Zheng
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ADJUSTABLE ENGINE MOUNT
- Publication number 20130302157
- Publication date Nov 14, 2013
- David F. Sandy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATHS
- Publication number 20130200211
- Publication date Aug 8, 2013
- Zhijun Zheng
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATH
- Publication number 20130193298
- Publication date Aug 1, 2013
- David F. Sandy
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GEARBOX MOUNT BRACKET
- Publication number 20120304811
- Publication date Dec 6, 2012
- Chris J. Niggemeier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Three-Dimensional Vehicle Frame
- Publication number 20080122213
- Publication date May 29, 2008
- GM Global Technology Operations, Inc.
- Weizhang S. Xu
- B62 - LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS

Zhijun Zheng

Person

Patents Grantslast 30 patents

Extended orifice plug for a fluid system

Method of regulating air pressure in anti-icing system

Direct-acting valve

Nacelle anti ice system

Aircraft anti-icing system

Thermally biased valve and anti-icing system

Engine mount waiting fail safe lug joint with reduced dynamic ampli...

Axial tension system for a gas turbine engine case

Nacelle anti-ice system and method with equalized flow

Aircraft nacelle anti-ice systems and methods

Inline pressure regulating valve assembly with inlet pressure bias

Secondary load path for gas turbine engine

Adjustable engine mount

Assembly for mounting a turbine engine to a pylon

Gas turbine engine mounting structure with secondary load paths

Gearbox mount bracket

Three-dimensional vehicle frame

Patents Applicationslast 30 patents

EXTENDED ORIFICE PLUG FOR A FLUID SYSTEM

COVER FOR ROTATABLE SHAFT OF GAS TURBINE ENGINE

METHOD OF REGULATING AIR PRESSURE IN ANTI-ICING SYSTEM

NACELLE ANTI-ICING TROUBLESHOOTING FOR A TWO VALVE SYSTEM

ANTI-ICE CONTROL SYSTEMS AND METHODS

AIRCRAFT NACELLE ANTI-ICE SYSTEMS AND METHODS

NACELLE ANTI ICE SYSTEM

INLINE PRESSURE REGULATING VALVE ASSEMBLY WITH INLET PRESSURE BIAS

THERMALLY BIASED VALVE AND ANTI-ICING SYSTEM

NACELLE ANTI-ICE SYSTEM AND METHOD WITH EQUALIZED FLOW

AIRCRAFT ANTI-ICING SYSTEM

Engine Mount Waiting Fail Safe Lug Joint with Reduced Dynamic Ampli...

AXIAL TENSION SYSTEM FOR A GAS TURBINE ENGINE CASE

ASSEMBLY FOR MOUNTING A TURBINE ENGINE TO A PYLON

SECONDARY LOAD PATH FOR GAS TURBINE ENGINE

ADJUSTABLE ENGINE MOUNT

GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATHS

GAS TURBINE ENGINE MOUNTING STRUCTURE WITH SECONDARY LOAD PATH

GEARBOX MOUNT BRACKET

Three-Dimensional Vehicle Frame