Title:
ANTI-ICE DEVICE, WING, AIRCRAFT, AND ANTI-ICE METHOD
Document Type and Number:
WIPO Patent Application WO/2012/098809
Kind Code:
A1
Abstract:
The purpose of the present invention is to provide an anti-ice device, a wing, an aircraft, and an anti-ice method which prevent, with a simple structure, icing on the aircraft which flies in a flying environment under an icing condition. The anti-ice device according to the present invention outputs pressure waves to water drops that float in air in a supercooled state which exists in a traveling direction of the aircraft (10) to change the water drops into ice by the pressure waves. The pressure waves have 0.9 to 3.3 [Pa] on a predetermined position in consideration of attenuation in the case where an acceleration of, for example, 10 G is given to the water drops.
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Inventors:
INOUE, Nobuo (C/O MITSUBISHI HEAVY INDUSTRIES LTD, 16-5, Konan 2-chome, Minato-k, Tokyo 15, 〒1088215, JP)
Application Number:
JP2011/080044
Publication Date:
July 26, 2012
Filing Date:
December 26, 2011
Export Citation:
Assignee:
MITSUBISHI HEAVY INDUSTRIES, LTD. (16-5, Konan 2-chome Minato-k, Tokyo 15, 〒1088215, JP)
三菱重工業株式会社 (〒15 東京都港区港南二丁目１６番５号 Tokyo, 〒1088215, JP)
三菱重工業株式会社 (〒15 東京都港区港南二丁目１６番５号 Tokyo, 〒1088215, JP)
International Classes:
B64D15/00
Attorney, Agent or Firm:
FUJITA, Takaharu et al. (37F The Landmark Tower Yokohama, 2-2-1 Minatomirai, Nishi-ku, Yokohama-sh, Kanagawa 37, 〒2208137, JP)
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Claims: