|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/213 ; 244/216|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 57 인용 특허 : 4|
A flap system for deploying high lift flaps on short takeoff and landing aircraft. The flap system utilizes an activating mechanism 27 that is used to extend a flap 12, a vane 22 and a spoiler 18 for maximum lift. The mechanism 27 utilizes relatively few linkage pieces and attached to the flap at single pivot points 44. The flap is supported by an actuator 46 and flap hinge support bracket 30. Increased mechanism rigidity and single pivot mountings allow use of roller 75 and track 74 guides at flap ends 78, 80 to smoothly guide flap movement and provide ...
A flap system for an aircraft comprising: (a) an aircraft wing having a trailing edge; (b) a flap support fixedly mounted to the trailing edge of said wing; (c) a wing flap having inboard and outboard ends and a fixedly attached flap mounting bracket which is pivotably mounted at a single pivot point to said flap support; (d) a flap linear actuator pivotably attached directly to said flap support and directly attached to said wing flap mounting bracket for adjusting flap position relative to the aircraft wing; (e) a single vane fixedly attached to said w...