|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64D-037/32 B64D-037/00 F16L-027/08 F16L-009/19 F16L-027/12 B64F-005/10|
|우선권정보||FR-14 63146 (2014-12-22)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 8|
In an aircraft duct formed with pipes connected in pairs via connectors in which the pipes are mounted with the possibility of axial displacement, there exists a risk that a pipe of the duct, with a dimension greater that the dimension of the nominal pipe, is mounted instead and in place of the latter. In this case, the wrongly mounted pipe would risk not having sufficient clearance in axial translation. In order to solve this problem, it is disclosed to equip one of the relevant connectors with an obstacle limiting the travel of the nominal pipe and pre...
1. An aircraft portion, comprising: a structure, anda duct configured to circulate a fluid and comprising a plurality of pipes and a plurality of connectors fixed to the structure and connecting the pipes two-by-two,the plurality of pipes includes pipes of different lengths, each pipe having a first end situated on a first side of the duct and a second end, anda first abutment situated on a second side of the duct,each connector including a connector internal passage that fluidically connects two pipe internal passages respectively belonging to the two p...