AIRCRAFT ICE PROTECTION SYSTEM AND AIRCRAFT PROVIDED WITH SAME

Title:

AIRCRAFT ICE PROTECTION SYSTEM AND AIRCRAFT PROVIDED WITH SAME

Document Type and Number:

WIPO Patent Application WO/2012/029782

Kind Code:

A1

Abstract:

An aircraft ice protection system (A) for preventing ice from adhering to an aircraft wing (2) and removing ice that has adhered thereto, wherein ice protection is performed by selectively supplying bleed air (S2) from the main engine (3) of the aircraft and outside air (S1') introduced from the air intake (31) provided in the airframe (28) and warmed by the heat of the aircraft airframe to a warm air chamber (32) formed on the inside of the wing (2).

Inventors:

SAITO ISAO (JP)
ISHIGURO TATSUO (JP)
ABE SHIGEKI (JP)
TANAKA HIDEAKI (JP)
TAKASU TOORU (JP)
ATSUMI MOTOHIRO (JP)
NAKANISHI MASAKAZU (JP)
KAMOGARI MINORU (JP)

Application Number:

PCT/JP2011/069609

Publication Date:

March 08, 2012

Filing Date:

August 30, 2011

Export Citation:

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Assignee:

MITSUBISHI HEAVY IND LTD (JP)
SAITO ISAO (JP)
ISHIGURO TATSUO (JP)
ABE SHIGEKI (JP)
TANAKA HIDEAKI (JP)
TAKASU TOORU (JP)
ATSUMI MOTOHIRO (JP)
NAKANISHI MASAKAZU (JP)
KAMOGARI MINORU (JP)

International Classes:

B64D15/04

Domestic Patent References:

WO2009127652A2

2009-10-22

Foreign References:

JP3529911B2	2004-05-24
US6196500B1	2001-03-06
JP2010100285A	2010-05-06
JP2008521693A	2008-06-26
JPH01149894U	1989-10-17
JPH06206593A	1994-07-26
JPH01149894A	1989-06-12
JPH06206593A	1994-07-26

Other References: