Title:
高温空気の機体張り付き対策構造および航空機
Document Type and Number:
Japanese Patent JP6681749
Kind Code:
B2
Abstract:
A structure for anti-adhesion of high-temperature air according to the present invention includes: a high-temperature air duct that is provided in an accessory of an aircraft and allows high-temperature air likely to be higher than a specified temperature to flow through the high-temperature air duct; an exhaust port that discharges a flow of the high-temperature air led through the high-temperature air duct, to an outside of the airframe; and a low-temperature air supplying part that supplies a flow of low-temperature air lower in temperature than the high-temperature air discharged to the outside of the airframe, to an airframe surface. The low-temperature air supplying part is configured to form an air layer made of a flow of low-temperature air between the high-temperature air that is bent toward the airframe surface in flight of the aircraft, and the an airframe surface.
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Inventors:
Nobuhide Hara
Yamada Osamu
Yamada Osamu
Application Number:
JP2016040837A
Publication Date:
April 15, 2020
Filing Date:
March 03, 2016
Export Citation:
Assignee:
Mitsubishi Aircraft Corporation
International Classes:
B64C21/04; F15D1/12
Domestic Patent References:
| JP60216022A | ||||
| JP2009507179A | ||||
| JP2001227302A |
Foreign References:
| US20120126061 | ||||
| WO2009064288A1 | ||||
| US20160288912 |
Attorney, Agent or Firm:
Mitsuru Oba
Horikawa Miyuki
Yuko Otake
Yamashita Seiko
Horikawa Miyuki
Yuko Otake
Yamashita Seiko