Heinz Hansen

Person

Weyhe, DE

People

Patents Grantslast 30 patents

Information Patent Grant
Leading edge structure
- Patent number 11,247,766
- Issue date Feb 15, 2022
- Airbus Operations Limited
- Llifon Williams
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aircraft wing with an adaptive shock control bump
- Patent number 10,427,779
- Issue date Oct 1, 2019
- Airbus Defence and Space GmbH
- Heinz Hansen
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
High-lift flap, arrangement of a high-lift flap together with a dev...
- Patent number 10,173,768
- Issue date Jan 8, 2019
- Airbus Operations GmbH
- Burkhard Goelling
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Wing of an aircraft and assembly of a wing comprising a device for...
- Patent number 9,079,657
- Issue date Jul 14, 2015
- Airbus Operations GmbH
- Juergen Frey
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method of controlling an aircraft in flight, especially to reduce w...
- Patent number 8,118,263
- Issue date Feb 21, 2012
- Airbus Operations GmbH
- Florent Laporte
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method of controlling an aircraft in flight, especially to reduce w...
- Patent number 7,874,523
- Issue date Jan 25, 2011
- Airbus Deutschland GmbH
- Florent Laporte
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Aerodynamic profile with an adjustable flap
- Patent number 6,863,245
- Issue date Mar 8, 2005
- EADS Deutschland GmbH
- Andreas Gessler
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
LEADING EDGE STRUCTURE
- Publication number 20190092450
- Publication date Mar 28, 2019
- AIRBUS OPERATIONS LIMITED
- Llifon Williams
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT WING WITH AN ADAPTIVE SHOCK CONTROL BUMP
- Publication number 20170190411
- Publication date Jul 6, 2017
- AIRBUS DEFENCE AND SPACE GMBH
- Heinz Hansen
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
AIRCRAFT WING WITH SPOILER
- Publication number 20170190413
- Publication date Jul 6, 2017
- AIRBUS DEFENCE AND SPACE GMBH
- Heinz Hansen
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
LEADING EDGE STRUCTURE
- Publication number 20150048207
- Publication date Feb 19, 2015
- AIRBUS OPERATIONS LIMITED
- Llifon Williams
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
HIGH-LIFT FLAP, ARRANGEMENT OF A HIGH-LIFT FLAP TOGETHER WITH A DEV...
- Publication number 20120043428
- Publication date Feb 23, 2012
- AIRBUS OPERATIONS GMBH
- Burkhard Goelling
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
WING OF AN AIRCRAFT AND ASSEMBLY OF A WING COMPRISING A DEVICE FOR...
- Publication number 20120001028
- Publication date Jan 5, 2012
- AIRBUS OPERATIONS GMBH
- Juergen Frey
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Method of Controlling an Aircraft in Flight, Especially to Reduce W...
- Publication number 20110101168
- Publication date May 5, 2011
- AIRBUS OPERATIONS GMBH
- Florent LAPORTE
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
Method of controlling an aircraft in flight, especially to reduce w...
- Publication number 20070108350
- Publication date May 17, 2007
- Florent Laporte
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

Heinz Hansen

Person

Patents Grantslast 30 patents

Leading edge structure

Aircraft wing with an adaptive shock control bump

High-lift flap, arrangement of a high-lift flap together with a dev...

Wing of an aircraft and assembly of a wing comprising a device for...

Method of controlling an aircraft in flight, especially to reduce w...

Method of controlling an aircraft in flight, especially to reduce w...

Aerodynamic profile with an adjustable flap

Patents Applicationslast 30 patents

LEADING EDGE STRUCTURE

AIRCRAFT WING WITH AN ADAPTIVE SHOCK CONTROL BUMP

AIRCRAFT WING WITH SPOILER

LEADING EDGE STRUCTURE

HIGH-LIFT FLAP, ARRANGEMENT OF A HIGH-LIFT FLAP TOGETHER WITH A DEV...

WING OF AN AIRCRAFT AND ASSEMBLY OF A WING COMPRISING A DEVICE FOR...

Method of Controlling an Aircraft in Flight, Especially to Reduce W...

Method of controlling an aircraft in flight, especially to reduce w...