Title:
推力を反転させる装置を内蔵する航空機ナセル
Document Type and Number:
Japanese Patent JP2010517845
Kind Code:
A
Abstract:
The nacelle has a thrust reversal device comprising a flap (34), and a wall for determining a conduit (16) in which flow passes to deviate. A movable part (30) is interposed between the flow with deviation and the flap in one position, and disengages the flap in another position so as to allow the flap to change the position and to pass from a rest position to an active position. The movable part has a recess (36) placed between the wall corresponding to an outer surface (20) of the nacelle and the wall corresponding to an inner surface (22) of the nacelle.
Inventors:
Burin, Guillaume
Aubert, patrick
Aubert, patrick
Application Number:
JP2009547732A
Publication Date:
May 27, 2010
Filing Date:
January 23, 2008
Export Citation:
Assignee:
AIRBUS FRANCE
International Classes:
B64D29/00; B64D33/00; F02K1/58
Domestic Patent References:
| JPH06193508A | 1994-07-12 |
Foreign References:
| WO1996038661A1 | 1996-12-05 | |||
| GB808608A | 1959-02-04 | |||
| US3598320A | 1971-08-10 |
Attorney, Agent or Firm:
▲吉▼川 俊雄