Title:
防氷装置、及び、航空機
Document Type and Number:
Japanese Patent JP6666159
Kind Code:
B2
Abstract:
An anti-icing system according to the present invention includes: a piccolo tube (11) that includes a flow path through which heated gas flows in the longitudinal direction from a rear end to a front end, and a plurality of ejection holes (16) provided along the longitudinal direction to make the flow path communicate with an outside; and an engine serving as a supply source (18) that supplies the heated gas toward the piccolo tube. The piccolo tube is decreased in an area of the flow path in a stepwise manner or in a continuous manner in the longitudinal direction, and has a continuous side surface provided with the ejection holes.
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Inventors:
Masatoshi Morishita
Masanori Tsujida
Satoshi Watanabe
Yoichi Ueto
Kazuhiro Kawai
Toshiyuki Ishida
Gen Ichikawa
Fujita Township
Masanori Tsujida
Satoshi Watanabe
Yoichi Ueto
Kazuhiro Kawai
Toshiyuki Ishida
Gen Ichikawa
Fujita Township
Application Number:
JP2016009788A
Publication Date:
March 13, 2020
Filing Date:
January 21, 2016
Export Citation:
Assignee:
Mitsubishi Aircraft Corporation
International Classes:
B64D15/04
Domestic Patent References:
| JP62157898A | ||||
| JP61160395A |
Foreign References:
| US2556736 | ||||
| US20100017243 | ||||
| US20010023909 | ||||
| WO2014202164A1 | ||||
| DE102010051293A1 | ||||
| GB486549A | ||||
| US5011098 |
Other References:
C.Sreedharan,Q.H.Nagpurwala,S.Subbaramu,”Effect of Hot Air Jets from a Piccolo Tube in Aircraft Wing Anti-Icing Unit”,MSRUAS-SASTech Journal,Faculty of Engineering and technology,M.S.Ramaiah University of Applied Sciences(MSRUAS),2014年 9月,Vol.13,Issue2,1-4,[online],[令和1年10月7日検索],インターネット,URL,http://www.msruas.ac.in/pdf_files/sastechjournals/Sept2014/1_C.Sreedharan,QHN,S.Subbaramu.pdf
Attorney, Agent or Firm:
Mitsuru Oba
Horikawa Miyuki
Yuko Otake
Yamashita Seiko
Horikawa Miyuki
Yuko Otake
Yamashita Seiko