Altmikus
Andree Altmikus, Hohenkirchen-Siegertsbrunn DE
| Patent application number | Description | Published |
|---|---|---|
| 20100181415 | ROTOR BLADE FOR A ROTARY WING AIRCRAFT - The invention relates to a rotor blade ( | 07-22-2010 |
Andree Altmikus, Hoehenkirchen-Siegertsbrunn DE
| Patent application number | Description | Published |
|---|---|---|
| 20090269198 | ROTOR BLADE FOR A ROTARY WING AIRCRAFT - A rotor blade including a rotor blade profile including a profile tip region, a profile trailing edge region including a trailing edge and a profile body having a profile core. A covering skin including an upper skin and a lower skin encase the profile core. A reversibly bendable flexural actuator including a first actuator end disposed at the trailing edge region of the rotor blade profile and a second actuator end projecting past the profile body toward the trailing edge. The second actuator end forms part of the trailing edge region and forms a movable rotor blade flap, the movable rotor blade flap being deformable into an arc-shaped rotor blade flap deflection upon a bending of the flexural actuator. | 10-29-2009 |
| 20120256042 | HELICOPTER WITH CYCLOIDAL ROTOR SYSTEM - The invention is related to a helicopter ( | 10-11-2012 |
Andree Altmikus, Hoehenkrichen-Siegertsbrunn DE
| Patent application number | Description | Published |
|---|---|---|
| 20080226448 | PROFILE DEFORMATION USING THE EXAMPLE OF A ROTOR BLADE - An aerodynamic profile includes a main profile body defining a profile depth direction and being shear-flexible in the profile depth direction, a tension-stiff and compression-stiff upper covering skin, a tension-stiff and compression-stiff lower covering skin, wherein the upper and lower covering skins envelope the main profile body, a bearingless and hingeless rear profile deformation region disposed at a rear edge region, and at least one actuator disposed in the main profile body. The at least one actuator is configured to initiate a flexural motion of the main profile body resulting in a curvature of the upper and lower covering skins and to deform the rear profile deformation region and so as to yield a flap deflection directed opposite to a direction of the flexural motion. | 09-18-2008 |
Andree Altmikus, Aurich DE
| Patent application number | Description | Published |
|---|---|---|
| 20130170985 | ELECTRICAL POWERED TAIL ROTOR OF A HELICOPTER - The invention is related to an electrical powered tail rotor ( | 07-04-2013 |