|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-009/00 B64C-009/20 B64C-009/32 B64C-009/14|
|미국특허분류(USC)||244/217; 244/215; 244/213; 244/212; 244/214; 244/198; 244/113|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 7|
An aircraft flap system and an associated method are provided to facilitate ground roll breaking without compromising in-flight performance. The aircraft flap system includes a first flap and a panel pivotally attached to the first flap, such as to a rearward portion of the first flap. The aircraft flap system also includes an actuator configured to controllably position the panel in a stowed position and in a deployed position. In the stowed position, the panel serves as a continuation of the first flap, thereby contributing to the lift provided by the ...
1. An aircraft flap system comprising: a first flap;an aft flap positioned rearward of the first flap;a panel pivotally attached to the first flap; andan actuator configured to controllably position the panel in a stowed position in which the panel serves as a continuation of the first flap and in a deployed position in which a forward edge of the panel is raised and an opposed rearward edge of the panel is lowered relative to the first and aft flaps,wherein the aft flap is configured to remain in a fixed position relative to the first flap while the act...