Mark Linz

Person

Cincinnati, OH, US

People

Patents Grantslast 30 patents

Information Patent Grant
Compressor bleed for gas turbine engine
- Patent number 12,085,027
- Issue date Sep 10, 2024
- General Electric Company
- John Carl Glessner
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Turbine engine with a cowl door
- Patent number 12,018,575
- Issue date Jun 25, 2024
- General Electric Company
- John Carl Glessner
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Compressor bypass bleed system for a ducted fan engine
- Patent number 11,970,969
- Issue date Apr 30, 2024
- General Electric Company
- Thomas L. Pugh
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Unducted fan turbine engine with a cowl door
- Patent number 11,639,671
- Issue date May 2, 2023
- General Electric Company
- John Carl Glessner
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Method of starting a gas turbine engine including a bowed-rotor coo...
- Patent number 11,268,446
- Issue date Mar 8, 2022
- General Electric Company
- Joseph Daniel Garrett
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Method of starting a gas turbine engine including a cooling phase
- Patent number 10,502,139
- Issue date Dec 10, 2019
- General Electric Company
- Steven Alan Ross
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Monolithic structure for mounting aircraft engine
- Patent number 8,469,309
- Issue date Jun 25, 2013
- General Electric Company
- Alan Roy Stuart
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method and apparatus for mounting and dismounting an aircraft engine
- Patent number 8,262,050
- Issue date Sep 11, 2012
- General Electric Company
- Mark Linz
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
COMPRESSOR BYPASS BLEED SYSTEM FOR A DUCTED FAN ENGINE
- Publication number 20240003292
- Publication date Jan 4, 2024
- GENERAL ELECTRIC COMPANY
- Thomas L. Pugh
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHODS AND APPARATUS FOR MOUNTING A GAS TURBINE ENGINE
- Publication number 20230356853
- Publication date Nov 9, 2023
- GENERAL ELECTRIC COMPANY
- Michael Cline
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
TURBINE ENGINE WITH A COWL DOOR
- Publication number 20230250733
- Publication date Aug 10, 2023
- GENERAL ELECTRIC COMPANY
- John Carl Glessner
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
COMPRESSOR BLEED FOR GAS TURBINE ENGINE
- Publication number 20230073647
- Publication date Mar 9, 2023
- GENERAL ELECTRIC COMPANY
- John Carl Glessner
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
UNDUCTED FAN TURBINE ENGINE WITH A COWL DOOR
- Publication number 20230010841
- Publication date Jan 12, 2023
- GENERAL ELECTRIC COMPANY
- John Carl Glessner
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
METHOD OF STARTING A GAS TURBINE ENGINE
- Publication number 20160348588
- Publication date Dec 1, 2016
- GENERAL ELECTRIC COMPANY
- Steven Alan Ross
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD AND APPARATUS FOR MOUNTING AND DISMOUNTING AN AIRCRAFT ENGINE
- Publication number 20100155566
- Publication date Jun 24, 2010
- Mark Linz
- B66 - HOISTING LIFTING HAULING
Information Patent Application
MONOLITHIC STRUCTURE FOR MOUNTING AIRCRAFT ENGINE
- Publication number 20100155525
- Publication date Jun 24, 2010
- Alan Roy Stuart
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

Person

Patents Grantslast 30 patents

Compressor bleed for gas turbine engine

Turbine engine with a cowl door

Compressor bypass bleed system for a ducted fan engine

Unducted fan turbine engine with a cowl door

Method of starting a gas turbine engine including a bowed-rotor coo...

Method of starting a gas turbine engine including a cooling phase

Monolithic structure for mounting aircraft engine

Method and apparatus for mounting and dismounting an aircraft engine

Patents Applicationslast 30 patents

COMPRESSOR BYPASS BLEED SYSTEM FOR A DUCTED FAN ENGINE

METHODS AND APPARATUS FOR MOUNTING A GAS TURBINE ENGINE

TURBINE ENGINE WITH A COWL DOOR

COMPRESSOR BLEED FOR GAS TURBINE ENGINE

UNDUCTED FAN TURBINE ENGINE WITH A COWL DOOR

METHOD OF STARTING A GAS TURBINE ENGINE

METHOD AND APPARATUS FOR MOUNTING AND DISMOUNTING AN AIRCRAFT ENGINE

MONOLITHIC STRUCTURE FOR MOUNTING AIRCRAFT ENGINE