Title:
航空機のエンジンマウント、航空機
Document Type and Number:
Japanese Patent JP5642379
Kind Code:
B2
Abstract:
An engine mount of an aircraft and an aircraft are provided, which can reduce a size of an engine mount and can effectively use a space in an engine nacelle even in an engine with a high bypass ratio. An engine core section 20b at a rear of an engine 20 is supported by a rear engine mount 40 comprising an engine side mount member 41 fixed to a side of the engine 20 and a strut side mount member 42 fixed to a side of a pylon strut 11. The rear engine mount 40 is divided into the engine side mount member 41 and the strut side mount member 42, and thereby, even in the engine 20 with a high bypass ratio in which an outside diameter of the fan section 20a and the outside diameter of the engine core section 20b significantly differ, the lengths in the vertical direction of the engine side mount member 41 and the strut side mount member 42 are suppressed.
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Inventors:
竹内 啓
Application Number:
JP2009273593A
Publication Date:
December 17, 2014
Filing Date:
December 01, 2009
Export Citation:
Assignee:
三菱航空機株式会社
International Classes:
B64D27/26; F01D25/28; F02C7/20
Attorney, Agent or Firm:
Mitsuru Oba
beauty -- Yuki Horikawa
beauty -- Yuki Horikawa
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