|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-009/34 B64C-009/06 B64C-009/08 B64C-023/06|
|미국특허분류(USC)||244/199.3; 244/099.2; 244/199.4; 244/206|
|우선권정보||DE-10 2008 027 618 (2008-06-10)|
|§371/§102 date||20101209 (20101209)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 8|
A device for the generation of aerodynamic vortices to be arranged on the spanwise side edge of a wing, or a regulating flap adjustably arranged on the latter, which in each case have a chordwise direction and a spanwise direction, wherein the device is formed from one aerofoil component or from a plurality of aerofoil components, wherein the at least one aerofoil component is designed as a part that can be moved relative to the wing or regulating flap in its spanwise direction, wherein the device for vortex generation has an actuation device for the ret...
1. An apparatus, comprising: a regulating flap for a wing of an aircraft having a thickness in a direction of airflow, a spanwise side edge, and a recess in the spanwise side edge;a plurality of aerofoil components adjustably arranged on the spanwise side edge of the regulating flap;an actuation device coupled to the plurality of aerofoil components and operating to: (i) extend and retract the aerofoil components out of and into the recess in a spanwise direction of the regulating flap, (ii) move the plurality of aerofoil components relative to one anoth...