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Inventor profile of:

Carsten CLEMEN

City:

Mittenwalde

Country:

Germany

Published Applications:

78

Last publication date:

2026-05-14

Top Assignees for applications by Carsten CLEMEN

The entities that hold a legal rights for patent applications filed by inventor CLEMEN Carsten:

Recent patent applications by CLEMEN Carsten

Carsten CLEMEN from Mittenwalde, DE has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-05-14
US20260132924A1
Mechanical engineering

COMBUSTION CHAMBER FOR A GAS TURBINE, AND ENGINE

 #2 | 2026-05-07
US20260126174A1
Mechanical engineering

NOZZLE FOR FEEDING AIR AND LIQUID FUEL INTO A COMBUSTION CHAMBER, AND ENGINE

 #3 | 2026-04-09
US20260098641A1
Mechanical engineering

PILOT ARRANGEMENT, NOZZLE DEVICE, PRODUCTION METHOD, AND GAS TURBINE ARRANGEMENT

 #4 | 2025-09-25
US20250297739A1
Mechanical engineering

INJECTOR ASSEMBLY FOR A GAS TURBINE AND AIRCRAFT

 #5 | 2025-09-04
US20250276802A1
Performing operations; transporting

METHOD FOR OPERATING AN AIRCRAFT, AND AIRCRAFT

 #6 | 2025-08-14
US20250257693A1
Mechanical engineering

VALVE UNIT FOR CONTROLLING THE FUEL FEED IN A FUEL SUPPLY SYSTEM, IN PARTICULAR OF AN AIRCRAFT

 #7 | 2025-07-24
US20250237381A1
Mechanical engineering

NOZZLE ASSEMBLY FOR A COMBUSTION CHAMBER OF AN ENGINE, AND BURNER SEAL

 #8 | 2025-06-19
US20250198623A1
Mechanical engineering

NOZZLE ASSEMBLY WITH A CENTRAL FUEL PIPE THAT IS SEALED AGAINST AN IN-FLOW OF AIR

 #9 | 2025-06-19
US20250198616A1
Mechanical engineering

NOZZLE ASSEMBLY WITH A CENTRAL FUEL SUPPLY AND AT LEAST ONE AIR CHANNEL

 #10 | 2025-05-08
US20250146666A1
Mechanical engineering

COMBUSTION CHAMBER ASSEMBLY FOR AN ENGINE WITH AT LEAST ONE HEAT EXCHANGER CHANNEL FOR FUEL TO BE INJECTED

 #11 | 2025-02-13
US20250052198A1
Mechanical engineering

Combustion chamber module having an annular combustion chamber

 #12 | 2024-10-17
US20240345605A1
Physics

METHOD FOR PRODUCING A NONLINEAR CYLINDRICAL SPRING AND USE OF SUCH A SPRING

 #13 | 2024-08-15
US20240271786A1
Mechanical engineering

Piloting arrangement, nozzle device, gas turbine arrangement and method

 #14 | 2024-06-20
US20240200521A1
Mechanical engineering

Fuel nozzle having different first and second discharge orifices for providing a hydrogen-air mixture

 #15 | 2024-04-18
US20240125289A1
Mechanical engineering

Drive system for an aircraft, aircraft having a drive system and method for operating an aircraft

 #16 | 2024-02-15
US20240053015A1
Mechanical engineering

COMBUSTION CHAMBER ASSEMBLY FOR OPERATION WITH LIQUID AND/OR GASEOUS FUEL, GAS TURBINE ASSEMBLY AND METHOD

 #17 | 2024-02-15
US20240053014A1
Mechanical engineering

Pilot arrangement, nozzle device, method and gas turbine arrangement

 #18 | 2024-01-25
US20240027070A1
Mechanical engineering

NOZZLE DEVICE FOR FEEDING AT LEAST ONE GASEOUS FUEL AND ONE LIQUID FUEL, SET, SUPPLY LINE SYSTEM, AND GAS TURBINE ASSEMBLY

 #19 | 2024-01-25
US20240027067A1
Mechanical engineering

Nozzle device for feeding fuel into a combustion chamber of a gas turbine assembly, and gas turbine assembly

 #20 | 2024-01-25
US20240026823A1
Mechanical engineering

Connecting apparatus for the flow connection between a fuel feed line system and a nozzle apparatus, nozzle apparatus and gas turbine arrangement

 #21 | 2021-09-16
US20210285640A1
Mechanical engineering

NOZZLE WITH JET GENERATOR CHANNEL FOR FUEL TO BE INJECTED INTO A COMBUSTION CHAMBER OF AN ENGINE

 #22 | 2020-04-02
US20200103113A1
Mechanical engineering

COMBUSTION CHAMBER ASSEMBLY FOR AN ENGINE HAVING HEAT SHIELDS AND/OR BURNER SEALS OF AT LEAST TWO DIFFERENT TYPES

 #23 | 2019-11-28
US20190360895A1
Physics

Measuring device comprising at least one fluid channel for guiding a measurement fluid

 #24 | 2019-05-16
US20190145524A1
Mechanical engineering

Burner seal of a gas turbine and method for manufacturing the same

 #25 | 2019-03-28
US20190093896A1
Mechanical engineering

NOZZLE COMPRISING AXIAL EXTENSION FOR A COMBUSTION CHAMBER OF AN ENGINE

 #26 | 2019-03-28
US20190093893A1
Mechanical engineering

COMBUSTION CHAMBER ASSEMBLY COMPRISING THERMAL SHIELD AND BURNER GASKET AS WELL AS MANUFACTURING METHOD

 #27 | 2019-01-24
US20190024518A1
Mechanical engineering

Nozzle assembly for a combustion chamber of an engine

 #28 | 2019-01-08
US14072498
Mechanical engineering

Combustion chamber tile of a gas turbine and method for its manufacture

 #29 | 2018-09-06
US20180252413A1
Mechanical engineering

Combustion chamber shingle arrangement of a gas turbine

 #30 | 2018-06-07
US20180156459A1
Mechanical engineering

Gas turbine combustion chamber with wall contouring

 #31 | 2018-06-07
US20180156450A1
Mechanical engineering

FUEL NOZZLE OF A GAS TURBINE WITH A SWIRL GENERATOR

 #32 | 2018-04-12
US20180100650A1
Mechanical engineering

Combustion chamber arrangement of a gas turbine and aircraft gas turbine

 #33 | 2017-10-26
US20170307217A1
Mechanical engineering

GAS TURBINE COMBUSTION CHAMBER

 #34 | 2017-06-15
US20170167731A1
Mechanical engineering

Method for mounting a combustion chamber of a gas turbine engine

 #35 | 2017-03-09
US20170067642A1
Mechanical engineering

ASSEMBLY GROUP WITH A COMBUSTION CHAMBER SHINGLE FOR A GAS TURBINE

 #36 | 2017-01-26
US20170023250A1
Mechanical engineering

COWLING PART AND COMBUSTOR ASSEMBLY FOR A GAS TURBINE

 #37 | 2017-01-26
US20170023014A1
Mechanical engineering

Diffuser part for a gas turbine

 #38 | 2017-01-12
US20170009989A1
Mechanical engineering

GAS TURBINE COMBUSTION CHAMBER WITH INTEGRATED TURBINE INLET GUIDE VANE RING AS WELL AS METHOD FOR MANUFACTURING THE SAME

 #39 | 2016-01-14
US20160010869A1
Mechanical engineering

Combustion chamber of a gas turbine with bolted combustion chamber head

 #40 | 2015-09-17
US20150260409A1
Mechanical engineering

Gas turbine combustion chamber and method for manufacturing the same

 #41 | 2015-09-17
US20150260405A1
Mechanical engineering

Combustion chamber of a gas turbine

 #42 | 2015-09-17
US20150260403A1
Mechanical engineering

Combustion chamber of a gas turbine

 #43 | 2015-09-17
US20150260401A1
Mechanical engineering

Combustion chamber of a gas turbine

 #44 | 2015-09-17
US20150260400A1
Mechanical engineering

COMBUSTION CHAMBER SHINGLE OF A GAS TURBINE

 #45 | 2015-05-14
US20150128603A1
Performing operations; transporting

GAS-TURBINE COMBUSTION CHAMBER AND METHOD FOR ITS MANUFACTURE

 #46 | 2015-05-14
US20150128602A1
Mechanical engineering

Heat shield for a gas turbine combustion chamber

 #47 | 2015-01-29
US20150030787A1
Performing operations; transporting

Method for producing a component by direct laser depositioning using first and second lasers operated at different powers

 #48 | 2015-01-29
US20150027127A1
Mechanical engineering

Gas turbine combustion chamber tile having effusion cooling holes including straight and offset sections

 #49 | 2014-10-30
US20140318148A1
Mechanical engineering

Burner seal for gas-turbine combustion chamber head and heat shield

 #50 | 2014-05-15
US20140130501A1
Mechanical engineering

Combustion chamber tile of a gas turbine

 #51 | 2014-03-06
US20140064952A1
Mechanical engineering

Assembly of an axial turbomachine and method for manufacturing an assembly of this type

 #52 | 2013-08-15
US20130205788A1
Mechanical engineering

Gas-turbine premix burner

 #53 | 2013-08-08
US20130199187A1
Mechanical engineering

Gas-turbine combustion chamber having non-symmetrical fuel nozzles

 #54 | 2013-08-01
US20130192232A1
Mechanical engineering

Annular combustion chamber of a gas turbine

 #55 | 2012-10-04
US20120247110A1
Mechanical engineering

Device for mixing fuel and air of a jet engine

 #56 | 2012-09-06
US20120222396A1
Mechanical engineering

Jet engine device with a bypass duct

 #57 | 2012-01-19
US20120014780A1
Mechanical engineering

Fan downstream guide vanes of a turbofan engine

 #58 | 2012-01-19
US20120011827A1
Mechanical engineering

Bleed air outlet in the bypass duct of a turbofan engine

 #59 | 2011-10-20
US20110255964A1
Mechanical engineering

Bypass duct of a turbofan engine

 #60 | 2011-09-15
US20110219782A1
Mechanical engineering

AERODYNAMICALLY SHAPED SUPPORTING AND/OR FAIRING ELEMENT IN THE BYPASS DUCT OF A GAS-TURBINE ENGINE

 #61 | 2011-09-01
US20110211947A1
Mechanical engineering

Bypass duct of a turbofan engine

 #62 | 2011-02-03
US20110027091A1
Mechanical engineering

Axial-flow compressor, more particularly one for an aircraft gas-turbine engine

 #63 | 2011-01-27
US20110016883A1
Mechanical engineering

Cross-sectional profile for the struts or the fairing of struts and service lines of a turbofan engine

 #64 | 2011-01-20
US20110014058A1
Performing operations; transporting

PROPELLER

 #65 | 2011-01-20
US20110014037A1
Mechanical engineering

Axial-flow compressor with a flow pulse generator

 #66 | 2011-01-20
US20110011058A1
Mechanical engineering

TURBOFAN ENGINE

 #67 | 2010-09-16
US20100232954A1
Mechanical engineering

Bypass duct of a turbofan engine

 #68 | 2010-06-10
US20100139278A1
Mechanical engineering

Method and apparatus for the operation of a turboprop aircraft engine provided with pusher propellers

 #69 | 2010-05-06
US20100111702A1
Mechanical engineering

Hub cone for an aircraft engine

 #70 | 2010-04-22
US20100098530A1
Mechanical engineering

COMPRESSOR FOR A GAS TURBINE

 #71 | 2010-01-28
US20100021310A1
Performing operations; transporting

Method for improving the flow conditions on the propeller or fan of an aircraft engine and accordingly designed hub cone

 #72 | 2009-12-10
US20090301102A1
Mechanical engineering

Gas-turbine compressor with bleed-air tapping

 #73 | 2009-09-24
US20090238682A1
Mechanical engineering

Compressor stator with partial shroud

 #74 | 2009-09-24
US20090238677A1
Mechanical engineering

Centrifugal compressor with air extraction and return at the casing

 #75 | 2009-09-10
US20090226322A1
Mechanical engineering

Airfoil design for rotor and stator blades of a turbomachine

 #76 | 2009-08-20
US20090208324A1
Mechanical engineering

Casing structure for stabilizing flow in a fluid-flow machine

 #77 | 2009-02-19
US20090044543A1
Mechanical engineering

Jet engine with compressor air circulation and method for operating the jet engine

 #78 | 2008-11-20
US20080286107A1
Mechanical engineering

Course of leading edges for turbomachine components
InventorID:

359051 ⎘