|국가/구분||United States(US) Patent 등록|
|우선권정보||DE-10 2004 029 194(2004-06-16)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 5 인용 특허 : 7|
A device for damping at least one rigid body mode and/or at least one elastic mode of an aircraft, especially for blast load reduction and increase of stability and comfort, in an airplane having at least one sensor, a regulation unit connected to the sensor, and at least one actuator controlling, guiding and/or regulating surfaces of the aircraft. The controller modifies the rigid body modes and/or the one or more elastic modes of the aircraft. With only one sensor signal of a sensor, which is preferably an acceleration signal, an arbitrary number and ...
What is claimed is: 1. A damping system for damping at least one of at least one rigid body mode of an aircraft and at least one elastic mode of the aircraft for at least one of blast load reduction, increase of stability and increase of comfort in an aircraft, the aircraft having thereon at least one of a controlling surface, a guiding surface and a regulating surface, at least two of the controlling surface, the guiding surface and the regulating surface being formed by at least one of an aileron, a rudder and a spoiler of the aircraft, the damping sy...