|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/135B ; 244/135R ; 280/830 ; 280/831|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 12 인용 특허 : 7|
A fuel containment area, and method of forming the same are disclosed herein. A fuel containment area is defined in part by a vehicle interior structure, such as an aircraft wing. Portions of the fuel containment area are provided with elastomeric partial bladders or appliques to bridge sections of the vehicle interior structure, to provide additional container integrity, and/or to segregate fuel from certain areas of the vehicle interior, e.g., about electrical components, mechanical linkages, or high temperature areas. The appliques are sealed to the v...
[ What is claimed is:] [1.] A method of in-situ forming a fluid containment area within an aircraft wing housing, the fluid containment area being defined in part by the internal wing structure, and in part by the elastomeric bladder disposed within the wing structure, the method comprising:a) applying a first sealant layer to the internal surface of the wing structure;b) applying a bladder first side to the first sealant layer;c) applying a flexible joint first portion to the first sealant layer;d) applying a flexible joint second portion to a bladder s...