|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/087; 244/0992; 244/217|
|우선권정보||DE-2005-0 2005 059370(2005-12-13)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 2|
A rudder of a commercial aircraft is provided that is divided along its longitudinal direction in at least one region and the parts of the rudder can be spread against the air flow surrounding the aircraft by means of an actuator in order to decelerate the aircraft.
What is claimed is: 1. A rudder of a commercial aircraft, comprising:a division along a longitudinal direction of the rudder in at least one region;a plurality of flap parts of the rudder spread against an air flow surrounding the commercial aircraft by means of an actuator for decelerating the commercial aircraft;a joint base that is supported articulatedly on the commercial aircraft and is turnable by means of the actuator for lateral control of the commercial aircraft;a first flap part of the rudder supported in an articulated fashion relative to the ...