|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||162/50 ; 106/251 ; 244/129.5 ; 244/130 ; 244/131 ; 277/637 ; 277/652|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 26 인용 특허 : 8|
A hinge (20) an an aircraft (24) has a first plurality of rigid tangs (22) attached to the aircraft (24). A second plurality of rigid tangs (26) are attached to a door (28) and a flexible cover (34) has a cover tang (44). A hinge pin (32) runs inside the first plurality of rigid tangs (22), the second plurality of rigid tangs (26) and the cover tang (44).
[ What is claimed is:] [1.]1. A hinge providing an aerodynamic seal at an external interface of a moving component and a stationary component on an aircraft, comprising:a first plurality of rigid tangs attached to the aircraft;a second plurality of rigid tangs attached to a door;an elastomeric, flexible cover having an aerodynamic shape adapted to be used over external surfaces of said components of said aircraft to provide an aerodynamically efficient transition between said external surfaces, said flexible cover having a cover tang;a hinge pin inside t...