Title:
航空機用流出弁
Document Type and Number:
Japanese Patent JP5368452
Kind Code:
B2
Abstract:
An outflow valve (10) for an aircraft has a frame (12) for arrangement in an opening (14) of an outer shell (16) of the aircraft, a first flap (18) pivotably arranged in the frame (12) for controlling a flow cross-section of at least one first inflow opening (24) and at least one outflow opening (15). To achieve a simplified construction of the ventilation system of the aircraft, the outflow valve (10) has a second inflow opening (26) configured to be closable by means of a drivable adjustable member (28).
Inventors:
Draiskirker, Ralph
Benz, liner
Benz, liner
Application Number:
JP2010526283A
Publication Date:
December 18, 2013
Filing Date:
September 25, 2008
Export Citation:
Assignee:
Nord-Micro Actien Gezel Shaft and Company OH G
International Classes:
B64D13/02; F16K1/22; F16K27/02; F16L55/07
Domestic Patent References:
| JP2001508861A | ||||
| JP11222198A | ||||
| JP7279898A | ||||
| JP2004074888A | ||||
| JP7020471U | ||||
| JP2069056U | ||||
| JP6156050A | ||||
| JP32010162Y1 |
Foreign References:
| US20040217317 | ||||
| WO2005023649A1 | ||||
| EP0298946A2 |
Attorney, Agent or Firm:
Shinki Global IP Patent Corporation