Axel Fink, Donauworth DE
Axel Fink, Donauworth DE
Patent application number | Description | Published |
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20140061366 | COMPOUND HELICOPTER WITH TAIL BOOMS - The present invention is related to a compound helicopter ( | 03-06-2014 |
20140061367 | COMPOUND HELICOPTER - The invention relates to a compound helicopter ( | 03-06-2014 |
20140170372 | GRID TYPE FIBER COMPOSITE STRUCTURE AND METHOD OF MANUFACTURING SUCH GRID TYPE STRUCTURE - The invention is related to a grid type fiber composite structure ( | 06-19-2014 |
20140170373 | GRID TYPE ELEMENT OF OPEN POLYGONAL CELLS - A grid type element ( | 06-19-2014 |
20150030806 | SANDWICH TYPE LOAD BEARING PANEL - A sandwich type load bearing panel ( | 01-29-2015 |
20150118436 | SKIN-STIFFENED COMPOSITE PANEL - A skin-stiffened composite panel ( | 04-30-2015 |
20150136906 | ROTARY WING AIRCRAFT AIRFRAME - A rotary wing aircraft airframe ( | 05-21-2015 |
20150183505 | SUBFLOOR STRUCTURE WITH AN INTEGRAL HULL FOR A ROTARY WING AIRCRAFT - The invention relates to a subfloor structure with an integral hull, for a rotary wing aircraft. The subfloor structure comprises an integral subfloor hull that defines in one piece, upward web portions acting as longerons and a bottom central portion offering both load bearing capabilities and aerodynamical loft features. The subfloor structure is useful for rotary wing aircrafts such as helicopters, and is e.g. made of composite and/or light alloy such as aluminum. | 07-02-2015 |