Title:
Fuel Scavenging moisture removal system
Document Type and Number:
Japanese Patent JP6067244
Kind Code:
B2
Abstract:
An aircraft fuel scavenge system incorporates a scavenge pump (30) receiving fuel from a center tank (10) and depositing the fuel in a wing tank (14). A water separator (40) receives fuel through an inlet tube (38) providing a plurality of momentum changes to incoming fuel, the water separator having a fuel outlet (32) connected to the scavenge pump and a water outlet. A water manifold (80) is connected from the water outlet to an input to a fuel supply line to an engine.
More Like This:
| JP2016503150 | Systems and methods for recondensing boil-off gas |
| WO/2015/002716 | ELECTRICALLY HEATED FILTER SCREENS |
| JP6419437 | Aircraft engine pylon and aircraft |
Inventors:
Buchholz, Joseph Em.
Rehi, Matthew Y.
Maue, Paul J.
Ducine, Edward M.
Grote, J. Everett
Nazir, Arshad
Simmons, Michael El.
Weiss, Howard S.
Roden, Peter J.
Longwell, Kevin Kay.
Rehi, Matthew Y.
Maue, Paul J.
Ducine, Edward M.
Grote, J. Everett
Nazir, Arshad
Simmons, Michael El.
Weiss, Howard S.
Roden, Peter J.
Longwell, Kevin Kay.
Application Number:
JP2012114975A
Publication Date:
January 25, 2017
Filing Date:
May 18, 2012
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64D37/32; B64C17/10
Domestic Patent References:
| JP2010509538A |
Foreign References:
| US5143608 | ||||
| WO2010103305A2 |
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori
Kobayashi Yoshinori
Previous Patent: Circular stapling apparatus which has a desorption washer attaching member
Next Patent: DISC BRAKE COVER
Next Patent: DISC BRAKE COVER