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Inventor profile of:

Bruno Stefes

City:

Hamburg

Country:

Germany

Published Applications:

13

Last publication date:

2023-09-28

Top Assignees for applications by Bruno Stefes

The entities that hold a legal rights for patent applications filed by inventor Stefes Bruno:

Recent patent applications by Stefes Bruno

Bruno Stefes from Hamburg, DE has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2023-09-28
US20230305035A1
Physics

METHOD AND SYSTEM FOR DETERMINING FLOW PROPERTIES OF A FLUID FLOWING ALONG A SURFACE

 #2 | 2023-02-02
US20230029560A1
Performing operations; transporting

DRAG REDUCTION SYSTEM FOR AN AIRCRAFT

 #3 | 2020-11-26
US20200369380A1
Performing operations; transporting

Method For Active Flow Control, Flow Body, And Aircraft

 #4 | 2020-04-02
US20200102066A1
Performing operations; transporting

Flow guide body for an aircraft

 #5 | 2019-05-23
US20190152587A1
Performing operations; transporting

Vortex generator arrangement and control system for an aircraft

 #6 | 2019-05-23
US20190152586A1
Performing operations; transporting

Vortex generator arrangement for an aircraft

 #7 | 2018-06-07
US20180155013A1
Performing operations; transporting

Aircraft airflow modification device and vortex generator arrangement for an aircraft

 #8 | 2018-05-17
US20180134373A1
Performing operations; transporting

Integral component with an active flow control device

 #9 | 2017-06-01
US20170152025A1
Performing operations; transporting

Vortex generator arrangement for an aircraft

 #10 | 2017-04-06
US20170096214A1
Performing operations; transporting

Vortex generator arrangement, flow control system and method for controlling a flow on a rudder surface

 #11 | 2016-08-11
US20160229526A1
Performing operations; transporting

Vortex generator arrangement

 #12 | 2015-10-08
US20150284099A1
Performing operations; transporting

Varying a cross section of a ram air passage

 #13 | 2014-01-23
US20140023479A1
Mechanical engineering

Aircraft tail region with a cooling system installed in aircraft tail region
InventorID:

621848 ⎘