Title:
An ice coating prevention method of a wings structure
Document Type and Number:
Japanese Patent JP6151751
Kind Code:
B2
Abstract:
PROBLEM TO BE SOLVED: To provide a blade structure capable of appropriately preventing icing in an environment exposed to high-speed overcooling water droplets.SOLUTION: On a surface of an aircraft blade, a surface of a blade front edge portion predicted to be collided by high-speed overcooling water droplets at times of take-off and landing is formed as a non-water repellent region having a low surface roughness, and a super-water repellent paint is coated on the other surface regions. The non-water repellent region is heated by an electrothermal heater, whereby ice nuclei generated in the blade front edge portion are molten without being grown to icing, repelled by a water repellent structure of the blade surface subsequent to the blade front edge portion in a blade chord direction, and scattered and eliminated.SELECTED DRAWING: Figure 1
Inventors:
Shigeo Kimura
Tetsuya Kojima
Kei Onoma
Tetsuya Kojima
Kei Onoma
Application Number:
JP2015186978A
Publication Date:
June 21, 2017
Filing Date:
September 24, 2015
Export Citation:
Assignee:
Subaru corporation
International Classes:
B64D15/00; F03D80/00
Domestic Patent References:
JP11181830A | ||||
JP2005177697A | ||||
JP2001259513A | ||||
JP2006514190A | ||||
JP2004017878A | ||||
JP2008137445A | ||||
JP2009298198A |
Foreign References:
WO2008087861A1 | ||||
US20060115362 | ||||
US5921501 |
Other References:
小島徹也 外4名,加熱法による着氷防止策にあたえる表面性状改質の効果,雪氷研究大会講演要旨集,日本,公益社団法人 日本雪氷学会/日本雪工学会,2008年 9月 5日,Vol.2008,P.199
Attorney, Agent or Firm:
Takehiko Yamada
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