Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
航空機用翼前縁
Document Type and Number:
Japanese Patent JP2010510120
Kind Code:
A
Abstract:
An aircraft leading edge, such as, for example, an air intake (22) of a nacelle (14) of a propulsion unit, includes a coating (26) for the acoustic treatment that includes—from the outside to the inside—an acoustically resistive porous layer that has a determined open surface ratio, at least one alveolar structure, and a reflective layer, whereby the coating (26) integrates a frost treatment system, characterized in that a frost treatment system includes at least one vibration emitter (36).

More Like This:
WO/2015/040376ICE ACCRETION PREVENTION
WO/2011/110659DEVICE AND METHOD FOR DETERMINING THE OPERATIONAL STATE OF AN ELECTRO-EXPULSIVE DEICING SYSTEM
Inventors:
Gantier, fabrics
Porte, Align
Application Number:
JP2009536774A
Publication Date:
April 02, 2010
Filing Date:
November 13, 2007
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
AIRBUS FRANCE
International Classes:
B64D15/16; B64D33/02
Domestic Patent References:
JPS57201799A1982-12-10
JPH02122923A1990-05-10
JP2002167290A2002-06-11
JPH04208694A1992-07-30
JP2004034781A2004-02-05
Foreign References:
US2135119A1938-11-01
US4759513A1988-07-26
US20020139900A12002-10-03
Attorney, Agent or Firm:
▲吉▼川 俊雄



 
Previous Patent: JP2010510119

Next Patent: 可動式給仕カート及びこれを組み込んだシステム