Title:
一体化ドレインマスト構造
Document Type and Number:
Japanese Patent JP6905642
Kind Code:
B2
Abstract:
An integrated drain mast structure for use in draining fluids emanating from aircraft components, such as turbine engines and fuselages, for facilitating the detection of fluids leaking from said components. A self-supporting tube section including a plurality of generally aligned fluid passages each having a peripheral wall, at least a portion of which is common with at least a portion of another aligned adjacent fluid passage is connected to one or more of these aircraft components. An aerodynamic fairing includes a plurality of fairing fluid passages each connected to a respective fluid passage of the tube section and having respective fluid outlets. The tube section and fairing section can comprise a single integral structure.
Inventors:
Hoodie, matthew
Mystery, Scheilesh
Posert, Eric
Mystery, Scheilesh
Posert, Eric
Application Number:
JP2020547050A
Publication Date:
July 21, 2021
Filing Date:
January 09, 2019
Export Citation:
Assignee:
Senior IP GMB
International Classes:
B64D33/00; F01D25/32
Foreign References:
| EP2522574A1 | ||||
| FR2910888A1 | ||||
| US6578361 |
Attorney, Agent or Firm:
Hiroe Associates Patent Office