Title:
航空機の防除氷システム及びこれを備える航空機
Document Type and Number:
Japanese Patent JP5582927
Kind Code:
B2
Abstract:
An aircraft ice protection system (A) is provided for preventing ice accretion on a wing (2) of an aircraft or removing the accreted ice. Bleed air (S2) extracted from a main engine (3) of the aircraft and air (S1') introduced from an air intake (31) installed on an airframe (28) and heated by a heat source (26) of the airframe of the aircraft are selectively supplied to a hot air chamber (32) formed inside the wing (2), thereby carrying out ice protection.
Inventors:
Isao Saito
Tatsuo Ishiguro
Shigeki Abe
Hideaki Tanaka
Toru Takasu
Motohiro Atsumi
Inside west Masakazu
Minoru Kamogari
Tatsuo Ishiguro
Shigeki Abe
Hideaki Tanaka
Toru Takasu
Motohiro Atsumi
Inside west Masakazu
Minoru Kamogari
Application Number:
JP2010192618A
Publication Date:
September 03, 2014
Filing Date:
August 30, 2010
Export Citation:
Assignee:
Mitsubishi Heavy Industries, Ltd.
International Classes:
B64D15/04
Attorney, Agent or Firm:
Woods Ryuichiro
Masatake Shiga
Norio Takahashi
Tetsuo Yamazaki
Masatake Shiga
Norio Takahashi
Tetsuo Yamazaki