|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/172.3; 244/135.R; 244/199.4|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 1|
The present development relates to an improved wing having a tip tank assembly. The tip tank assembly is attached to a distal end of an outer wing section. The tip tank assembly includes a tank, a pair of mounting brackets and a fairing assembly. The fairing assembly includes a nose piece, a central piece, a tail piece, an inner end plate, and an upper close out piece. The inner end plate extends perpendicularly downward from a lower surface of the outer wing section eventually terminating at a bottom portion of the central piece. The inner end plate act...
The invention claimed is: 1. A wing tip tank assembly for installation on a wing portion of an aircraft at a distal end of the wing portion, including: a forward tip portion, an aft tip portion, and a cylindrical portion with the forward tip portion in the general direction of a forward portion of the aircraft and the aft tip portion in the general direction of an aft portion of the aircraft, wherein an upper surface of the wing tip tank assembly is generally level with an upper surface of the wing portion; an end plate fairing disposed along an exterio...