Ingo Borchers
Inventor
Stats
- 6 US patents issued
- 7 US Applications filed
- most recent filing
This is official USPTO record data
Details
- 6 US Patents Issued
- 7 US Applications Filed
- 114 Total Citation Count
- Feb 23, 2007 Most Recent Filing
- Mar 26, 1998 Earliest Filing
Work History
Patent Owner | Applications Filed | Year |
---|---|---|
AIRBUS OPERATIONS GMBH | 2
2 | 2001
2007 |
DAIMLERCHRYSLER AG | 1
2 | 1999
2002 |
EADS DEUTSCHLAND GMBH | 1
2 | 1998
2004 |
DORNIER GMBH | 1
| 2004
|
Inventor Addresses
Address | Duration |
---|---|
Uhdingen-Muehlhofen, DE | Nov 29, 07 - Nov 29, 07 |
Uhldingen, DE | Jun 12, 01 - Jun 12, 01 |
Uhldingen-Mühlhofen, DE | Jan 17, 12 - Jan 17, 12 |
Uhldingen-Muehlhofen, DE | Sep 19, 00 - Jul 20, 10 |
Uhldingen-Muhlhofen, DE | Nov 21, 02 - Nov 04, 04 |
Uhldingen-muhlhofen, DE | Apr 02, 09 - Apr 02, 09 |
Technology Profile
Technology | Matters | |
---|---|---|
B60J: | WINDOWS, WINDSCREENS, NON-FIXED ROOFS, DOORS, OR SIMILAR DEVICES FOR VEHICLES; REMOVABLE EXTERNAL PROTECTIVE COVERINGS SPECIALLY ADAPTED FOR VEHICLES | 1 |
B64C: | AEROPLANES; HELICOPTERS | 2 |
C08K: | USE OF INORGANIC OR NON-MACROMOLECULAR ORGANIC SUBSTANCES AS COMPOUNDING INGREDIENTS | 1 |
Patents / Publication
Patents / Publication # | Year of Publication / Issued | Title | Citations |
---|---|---|---|
8096513 | 2012 | Aerodynamic flap of an aircraft having a device which influences the flap vortex | 10 |
7758296 | 2010 | Method for reducing the noise of turbo engines | 5 |
2009/0084,905 | 2009 | Aerodynamic Flap Of An Aircraft Having A Device Which Influences The Flap Vortex | 12 |
2007/0274,823 | 2007 | Method For Reducing The Noise Of Turbo Engines | 4 |
2004/0219,351 | 2004 | Component having vibration-damping properties, mixture for manufacturing the component, and method of manufacturing such a component | 1 |
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