|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/131 ; 244/123 ; 244/133 ; 244/213 ; 244/219|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 20 인용 특허 : 5|
A hinge line system (52) for an aircraft has a structural block (22) attached to a first edge of a hinge line. The structural block (22) has a flange (28) attached to a first end of an elastic sheet (32). A second structural block (24) is attached to a second edge of the hinge line. The second structural block (24) has a second flange (30) attached to a second end of the elastic sheet (32).
[ What is claimed is:] [1.] A hinge line sock system for an aircraft, comprising:a first stretchable knit fabric;a uniform elastomer skin having a top surface bonded to the stretchable knit fabric;a second stretchable knit fabric bonded to a bottom surface of the elastomer skin;a first rigid structural member attached to a first end of the elastomer skin, the first rigid structural member attached to a control surface of the aircraft and having a shear bonding area; anda second rigid structural member attached to a first end of the elastomer skin, attach...