|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 16 인용 특허 : 183|
Link mechanisms for gapped rigid Krueger flaps, and associated methods and systems are disclosed. A system in accordance with one embodiment includes a deployable leading edge assembly that in turn includes a deployable leading edge panel having a generally fixed-shape flow surface, a bullnose coupled to the panel, and a link mechanism coupled to the panel and the bullnose to move the panel between a stowed position and a deployed position. The mechanism can include a first support link, a second support link, and first, second, and third positioning li...
We claim: 1. An aircraft system, comprising: a deployable leading edge assembly that includes: a deployable leading edge panel that forms a gap with an airfoil when in a deployed position, wherein the deployable leading edge panel has a generally fixed-shape flow surface extending from a leading end to the gap when in the deployed position, and has the same generally fixed shape flow surface when in a stowed position; a bullnose pivotably coupled to the leading edge panel; a link mechanism coupled to the leading edge panel and the bullnose at a wing spa...