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Inventor profile of:

Hermann KLINGELS

City:

Dachau

Country:

Germany

Published Applications:

47

Last publication date:

2026-05-14

Top Assignees for applications by Hermann KLINGELS

The entities that hold a legal rights for patent applications filed by inventor KLINGELS Hermann:

Recent patent applications by KLINGELS Hermann

Hermann KLINGELS from Dachau, DE has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-05-14
US20260132738A1
Mechanical engineering

METHOD FOR OPERATING A COMBUSTION SYSTEM OF A TURBOMACHINE FOR A FLIGHT PROPULSION SYSTEM, AND TURBOMACHINE

 #2 | 2026-01-29
US20260028914A1
Mechanical engineering

TURBINE MODULE FOR A TURBOMACHINE

 #3 | 2025-10-23
US20250327629A1
Mechanical engineering

HEAT EXCHANGER FOR A HIGH INFLOW VELOCITY

 #4 | 2024-06-27
US20240209797A1
Mechanical engineering

METHOD FOR OPERATING A TURBOMACHINE FOR A FLIGHT PROPULSION DRIVE

 #5 | 2024-06-27
US20240209754A1
Mechanical engineering

METHOD FOR OPERATING A FLIGHT-PROPULSION SYSTEM

 #6 | 2023-11-16
US20230366349A1
Mechanical engineering

HEAT ENGINE WITH STEAM SUPPLY DEVICE

 #7 | 2023-10-19
US20230332522A1
Mechanical engineering

Exhaust-gas treatment device for an aircraft engine

 #8 | 2023-09-14
US20230286661A1
Performing operations; transporting

Aircraft

 #9 | 2023-05-18
US20230150678A1
Performing operations; transporting

Aircraft having a heat engine and device for using the exhaust gases from the heat engine

 #10 | 2023-01-26
US20230029124A1
Mechanical engineering

Turbine module for a turbomachine

 #11 | 2022-02-03
US20220032384A1
Performing operations; transporting

METHOD FOR PRODUCING A PLATE OF A TURBOMACHINE

 #12 | 2021-07-08
US20210207500A1
Mechanical engineering

EXHAUST-GAS TREATMENT DEVICE, AIRCRAFT PROPULSION SYSTEM, AND METHOD FOR TREATING AN EXHAUST-GAS STREAM

 #13 | 2021-01-07
US20210001269A1
Performing operations; transporting

Reducing contrails during operation of aircraft

 #14 | 2020-08-27
US20200271002A1
Mechanical engineering

Blade for a high-speed turbine stage having a single sealing element

 #15 | 2020-08-27
US20200270995A1
Mechanical engineering

Shroudless blade for a high-speed turbine stage

 #16 | 2019-10-31
US20190331000A1
Mechanical engineering

Stator vane for a turbine of a turbomachine

 #17 | 2019-10-31
US20190330992A1
Mechanical engineering

Blade or vane, blade or vane segment and assembly for a turbomachine, and turbomachine

 #18 | 2019-07-25
US20190226342A1
Mechanical engineering

Rotor, in particular blisk of a gas turbine, having a broken-up rim and method for producing the same

 #19 | 2018-09-20
US20180266464A1
Mechanical engineering

Oblique flange channel

 #20 | 2018-06-07
US20180156037A1
Mechanical engineering

Turbine blade comprising a cavity with wall surface discontinuities and process for the production thereof

 #21 | 2018-05-24
US20180142567A1
Mechanical engineering

SEALING SYSTEM FOR AN AXIAL TURBOMACHINE AND AXIAL TURBOMACHINE

 #22 | 2018-05-17
US20180135449A1
Mechanical engineering

Seal system for a guide blade system of a gas turbine

 #23 | 2018-04-26
US20180112556A1
Mechanical engineering

Turbine center frame having a connecting element

 #24 | 2017-06-08
US20170159609A1
Mechanical engineering

TURBOFAN AIRCRAFT ENGINE WITH REDUCED NOISE EMISSION

 #25 | 2017-06-08
US20170159573A1
Mechanical engineering

REDUCED NOISE TURBOFAN AIRCRAFT ENGINE

 #26 | 2017-04-20
US20170107843A1
Mechanical engineering

Module for a gas turbine

 #27 | 2016-08-25
US20160245101A1
Mechanical engineering

Locking element and turbomachine

 #28 | 2016-08-18
US20160238028A1
Mechanical engineering

Axially split inner ring for a fluid flow machine, guide vane ring, and aircraft engine

 #29 | 2016-08-18
US20160237855A1
Mechanical engineering

Axially divided inner ring for a turbomachine and guide vane ring

 #30 | 2016-05-26
US20160146041A1
Mechanical engineering

Blade or vane for a turbomachine and axial turbomachine

 #31 | 2016-05-26
US20160146027A1
Mechanical engineering

Guide vane ring and turbomachine

 #32 | 2016-02-04
US20160032826A1
Mechanical engineering

TURBOFAN AIRCRAFT ENGINE

 #33 | 2016-01-21
US20160017797A1
Mechanical engineering

Turbofan aircraft engine

 #34 | 2015-12-17
US20150361893A1
Mechanical engineering

Mid-frame for a gas turbine and gas turbine having such a mid-frame

 #35 | 2015-10-01
US20150275683A1
Mechanical engineering

Guide vane ring, guide vane, inner ring and turbomachine

 #36 | 2015-08-13
US20150226155A1
Mechanical engineering

Thrust deflecting device and aircraft engine

 #37 | 2014-10-09
US20140298772A1
Mechanical engineering

Mixing device and turbofan engine having such mixing device

 #38 | 2013-04-04
US20130084166A1
Mechanical engineering

Segmented component

 #39 | 2012-03-15
US20120063884A1
Mechanical engineering

Clearance control system, turbomachine and method for adjusting a running clearance between a rotor and a casing of a turbomachine

 #40 | 2012-03-08
US20120057958A1
Mechanical engineering

Clearance control system, turbomachine and method for adjusting a running clearance between a rotor and a casing of a turbomachine

 #41 | 2012-02-16
US20120039706A1
Mechanical engineering

COMPRESSOR HAVING A GUIDE VANE ASSEMBLY WITH A RADIALLY VARIABLE OUTFLOW

 #42 | 2010-08-12
US20100202889A1
Performing operations; transporting

METHOD FOR PRODUCING A LIGHTWEIGHT TURBINE BLADE

 #43 | 2009-04-30
US20090111639A1
Mechanical engineering

Planetary gear

 #44 | 2008-05-29
US20080121077A1
Performing operations; transporting

Apparatus and method for rotary machining of rotors

 #45 | 2007-04-26
US20070089420A1
Performing operations; transporting

Gas turbine, in particular aircraft engine and method for generating electrical energy in a gas turbine

 #46 | 2007-03-15
US20070059181A1
Mechanical engineering

Apparatus and method for securing a rotor blade in a rotor of a turbine-type machine

 #47 | 2006-08-24
US20060188376A1
Mechanical engineering

Apparatus and method for securing a rotor blade in a rotor of a turbine-type machine
InventorID:

176087 ⎘