Title:
流体管システムを有する航空機
Document Type and Number:
Japanese Patent JP4989463
Kind Code:
B2
Abstract:
The aircraft has a fluid duct system (26) for suction of a boundary layer and cleaning of fluid in endangered places of an outer skin of the aircraft. The duct system is connected to a pumping device that is driven, by cabin exhaust air, for production of desired low pressure for suction of the boundary layer though a stop valve (6). The pumping device is a jet pump (3), whose driving jets are generated by the exhaust air.
Inventors:
Meister Jurgen
Application Number:
JP2007512087A
Publication Date:
August 01, 2012
Filing Date:
May 11, 2005
Export Citation:
Assignee:
Airbus Operations GmbH
International Classes:
B64C21/02; B64C21/00; B64D13/00; B64D41/00; B64D47/00; F15D1/12
Domestic Patent References:
| JP4110299A | ||||
| JP2000203495A | ||||
| JP5139385A |
Foreign References:
| US5884873 |
Attorney, Agent or Firm:
Masayuki Masabayashi
Hayashi Ichiyoshi
Hayashi Ichiyoshi