Inventor

KLINGELS HERMANN

DE40 patents

⚠️ This page may combine multiple inventors who share the name “KLINGELS HERMANN”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

KLINGELS HERMANN

MTU Aero Engines AG

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

Guide vane ring and turbomachine

Seal system for a guide blade system of a gas turbine

Axially divided inner ring for a turbomachine and guide vane ring

Blade or vane for a turbomachine and axial turbomachine

Turbofan aircraft engine

Reducing contrails during operation of aircraft

Aircraft

Guide vane ring, guide vane, inner ring and turbomachine

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

Module for a gas turbine

Exhaust-gas treatment device for an aircraft engine

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

Shroudless blade for a high-speed turbine stage

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

Oblique flange channel

Stator vane for a turbine of a turbomachine

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

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

Turbine module for a turbomachine

Thrust deflecting device and aircraft engine

Method for producing a plate of a turbomachine

Turbine center frame having a connecting element

Locking element and turbomachine

Mixing device and turbofan engine having such mixing device

MTU AERO ENGINES GMBH

Driving mechanism with counter-rotating rotors

Aircraft engine with separate auxiliary rotor and fan rotor

Segmented component

Rotor of a turbo engine, e.g., a gas turbine rotor

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

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

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

Apparatus and method for rotary machining of rotors

KLINGELS HERMANN

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

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

Planetary gear

DAIMLER CHRYSLER AG

Cooling air system for gas turbine

(unassigned)

Flow machine with rotor and stator

MIU AERO ENGINES GMBH

Rotor for a turbomachine

MTU MUENCHEN GMBH

Gas turbine propulsion unit with a gas generator