Rudolf Maier

Person

Miesbach, DE

People

Patents Grantslast 30 patents

Information Patent Grant
Power generator with an electrical component made from inertial mas...
- Patent number 9,673,375
- Issue date Jun 6, 2017
- Airbus Defence and Space GmbH
- Stefan Storm
- B06 - GENERATING OR TRANSMITTING MECHANICAL VIBRATIONS IN GENERAL
Information Patent Grant
Device for reducing structural vibrations of airfoils
- Patent number 9,327,823
- Issue date May 3, 2016
- Airbus Defence and Space GmbH
- Stefan Storm
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Acoustic absorber for aircraft engines
- Patent number 8,302,733
- Issue date Nov 6, 2012
- Airbus SAS
- Alexander Peiffer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Minimizing dynamic structural loads of an aircraft
- Patent number 8,255,096
- Issue date Aug 28, 2012
- Airbus Operations SAS
- Andreas Wildschek
- G05 - CONTROLLING REGULATING
Information Patent Grant
Device and process for oscillation insulation in a transmission path
- Patent number 8,037,981
- Issue date Oct 18, 2011
- EADS Deutschland GmbH
- Marius Bebesel
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Apparatus for suppressing structure borne noises
- Patent number 6,480,609
- Issue date Nov 12, 2002
- Eurocopter Deutschland GmbH
- Henning Strehlow
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Grant
Apparatus for the active suppression of noise radiated by a surface
- Patent number 6,178,246
- Issue date Jan 23, 2001
- DaimlerChrysler AG
- Marius Bebesel
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Grant
Active acoustic resonator for abating noise
- Patent number 6,151,396
- Issue date Nov 21, 2000
- DaimlerChrysler AG
- Rudolf Maier
- G10 - MUSICAL INSTRUMENTS ACOUSTICS

Patents Applicationslast 30 patents

Information Patent Application
POWER GENERATOR WITH AN ELECTRICAL COMPONENT MADE FROM INERTIAL MAS...
- Publication number 20160035964
- Publication date Feb 4, 2016
- Airbus Defence and Space GmbH
- Stefan Storm
- H01 - BASIC ELECTRIC ELEMENTS
Information Patent Application
NOISE REDUCTION SYSTEM, A METHOD AND A HELICOPTER
- Publication number 20150289056
- Publication date Oct 8, 2015
- Airbus Defence and Space GmbH
- Stefan Storm
- H04 - ELECTRIC COMMUNICATION TECHNIQUE
Information Patent Application
DEVICE FOR REDUCING STRUCTURAL VIBRATIONS OF AIRFOILS
- Publication number 20140341737
- Publication date Nov 20, 2014
- EADS Deutschland GmbH
- Stefan Storm
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
DEVICE AND PROCESS FOR OSCILLATION INSULATION IN A TRANSMISSION PATH
- Publication number 20110266104
- Publication date Nov 3, 2011
- Eurocopter Deutschland GmbH
- Marius Bebesel
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
MINIMIZING DYNAMIC STRUCTURAL LOADS OF AN AIRCRAFT
- Publication number 20090084908
- Publication date Apr 2, 2009
- Airbus France
- Andreas Wildschek
- G05 - CONTROLLING REGULATING
Information Patent Application
Acoustic Absorber for Aircraft Engines
- Publication number 20080223655
- Publication date Sep 18, 2008
- AIRBUS SAS
- Alexander Peiffer
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Rudolf Maier

Person

Patents Grantslast 30 patents

Power generator with an electrical component made from inertial mas...

Device for reducing structural vibrations of airfoils

Acoustic absorber for aircraft engines

Minimizing dynamic structural loads of an aircraft

Device and process for oscillation insulation in a transmission path

Apparatus for suppressing structure borne noises

Apparatus for the active suppression of noise radiated by a surface

Active acoustic resonator for abating noise

Patents Applicationslast 30 patents

POWER GENERATOR WITH AN ELECTRICAL COMPONENT MADE FROM INERTIAL MAS...

NOISE REDUCTION SYSTEM, A METHOD AND A HELICOPTER

DEVICE FOR REDUCING STRUCTURAL VIBRATIONS OF AIRFOILS

DEVICE AND PROCESS FOR OSCILLATION INSULATION IN A TRANSMISSION PATH

MINIMIZING DYNAMIC STRUCTURAL LOADS OF AN AIRCRAFT

Acoustic Absorber for Aircraft Engines