|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-003/58 B64C-001/38 F16J-015/00|
|미국특허분류(USC)||244/213 ; 244/130 ; 277/651 ; 277/652 ; 277/644|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 16 인용 특허 : 4|
A blade seal (20) for an aircraft has a mounting structure (22). A composite blade (26) is attached to the mounting structure (22). The composite blade (26) has a plurality of holes (28). An elastomer substance (30) is used to fill the plurality of holes (28).
[ What is claimed is:] [1.] A blade seal for an aircraft comprising:a mounting structure;a composite blade attached to the mounting structure, the composite blade having a plurality of holes; andan elastomer substance filling the plurality of holes.