|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/53B ; 244/219 ; 244/130|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 55 인용 특허 : 5|
An annular nacelle for a turbine engine of an aircraft has a variable contour annular air inlet. The variable contour annular inlet includes annular outer and inner surface-defining radially-spaced structures on the forward portion of the nacelle, an annular member disposed between the annular outer and inner structures and coupled to the annular outer structure for sliding movement along the interiors of the annular outer and inner structures, and a plurality of actuating mechanisms coupled between the nacelle body and the annular member. The actuating ...
In an annular nacelle for a turbine aircraft engine having an annular body with a central axis, a variable contour annular air inlet, comprising: (a) a pair of annular outer and inner surface-defining structures extending axially forwardly from said annular body and being spaced radially from one another with respect to said central axis, said annular outer structure having an annular forward end portion expandable and contractible in diameter; (b) an annular member being disposed between said annular outer and inner structures and coupled to said annula...