Andre HAUSBERG

Person

Kassel, DE

People

Patents Grantslast 30 patents

Information Patent Grant
Electromechanical actuator for setting a collective offset for a he...
- Patent number 11,745,864
- Issue date Sep 5, 2023
- AIRBUS HELICOPTERS TECHNIK GMBH
- Steffen Hahn
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Grant
System for reducing vibrations or stresses in a rotor blade system
- Patent number 11,702,195
- Issue date Jul 18, 2023
- AIRBUS HELICOPTERS TECHNIK GMBH
- Andre Hausberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method for predicting vibrations of an aircraft
- Patent number 11,192,643
- Issue date Dec 7, 2021
- ZF Friedrichshafen AG
- Steffen Hahn
- G01 - MEASURING TESTING
Information Patent Grant
System for reducing vibrations or stresses in a rotor blade system
- Patent number 11,091,253
- Issue date Aug 17, 2021
- ZF Friedrichshafen AG
- Andre Hausberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Control rod for adjusting a rotor blade of a helicopter
- Patent number 10,507,911
- Issue date Dec 17, 2019
- ZF Friedrichshafen AG
- Jürgen Götte
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Rotor head with integrated electronics for a helicopter
- Patent number 10,351,228
- Issue date Jul 16, 2019
- ZF Friedrichshafen AG
- Steffen Hartmann
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotor blade control device
- Patent number 9,555,878
- Issue date Jan 31, 2017
- ZF Friedrichshafen AG
- Uwe Arnold
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Electromechanical linear actuator
- Patent number 8,878,466
- Issue date Nov 4, 2014
- ZF Friedrichshafen AG
- Andre Hausberg
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...

Patents Applicationslast 30 patents

Information Patent Application
SYSTEM FOR REDUCING VIBRATIONS OR STRESSES IN A ROTOR BLADE SYSTEM
- Publication number 20210347471
- Publication date Nov 11, 2021
- ZF Friedrichshafen AG
- Andre Hausberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ELECTROMECHANICAL ACTUATOR FOR SETTING A COLLECTIVE OFFSET FOR A HE...
- Publication number 20210070435
- Publication date Mar 11, 2021
- ZF Friedrichshafen AG
- Steffen HAHN
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHOD FOR PREDICTING VIBRATIONS OF AN AIRCRAFT
- Publication number 20190233093
- Publication date Aug 1, 2019
- ZF Friedrichshafen AG
- Steffen Hahn
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
CONTROL ROD FOR ADJUSTING A ROTOR BLADE OF A HELICOPTER
- Publication number 20180201368
- Publication date Jul 19, 2018
- ZF Friedrichshafen AG
- Jürgen Götte
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Application
ROTOR HEAD WITH INTEGRATED ELECTRONICS FOR A HELICOPTER
- Publication number 20170166303
- Publication date Jun 15, 2017
- ZF Friedrichshafen AG
- Steffen HARTMANN
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
SYSTEM FOR REDUCING VIBRATIONS OR STRESSES IN A ROTOR BLADE SYSTEM
- Publication number 20170158317
- Publication date Jun 8, 2017
- ZF Friedrichshafen AG
- Andre Hausberg
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ROTOR BLADE CONTROL DEVICE
- Publication number 20140377068
- Publication date Dec 25, 2014
- ZF Friedrichshafen AG
- Uwe Arnold
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ELECTROMECHANICAL LINEAR ACTUATOR
- Publication number 20120137799
- Publication date Jun 7, 2012
- ZF Friedrichshafen AG
- Andre Hausberg
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...

Andre HAUSBERG

Person

Patents Grantslast 30 patents

Electromechanical actuator for setting a collective offset for a he...

System for reducing vibrations or stresses in a rotor blade system

Method for predicting vibrations of an aircraft

System for reducing vibrations or stresses in a rotor blade system

Control rod for adjusting a rotor blade of a helicopter

Rotor head with integrated electronics for a helicopter

Rotor blade control device

Electromechanical linear actuator

Patents Applicationslast 30 patents

SYSTEM FOR REDUCING VIBRATIONS OR STRESSES IN A ROTOR BLADE SYSTEM

ELECTROMECHANICAL ACTUATOR FOR SETTING A COLLECTIVE OFFSET FOR A HE...

METHOD FOR PREDICTING VIBRATIONS OF AN AIRCRAFT

CONTROL ROD FOR ADJUSTING A ROTOR BLADE OF A HELICOPTER

ROTOR HEAD WITH INTEGRATED ELECTRONICS FOR A HELICOPTER

SYSTEM FOR REDUCING VIBRATIONS OR STRESSES IN A ROTOR BLADE SYSTEM

ROTOR BLADE CONTROL DEVICE

ELECTROMECHANICAL LINEAR ACTUATOR