Title:
航空機用エンジン装置
Document Type and Number:
Japanese Patent JP6554282
Kind Code:
B2
Abstract:
An aircraft engine apparatus (1) includes: a rotating shaft (6); a fan (10) driven by the rotating shaft; a fan case surrounding the fan from outside in a radial direction of the rotating shaft; a nose cone (13) disposed upstream of the fan; a casing (2) that accommodates at least part of the rotating shaft and supports the fan case; a first motive force transmitter (9) that transmits motive force of the rotating shaft to the fan; and a support member (12) disposed inward of the first motive force transmitter in the radial direction, the support member coupling the nose cone to the casing such that the support member supports the nose cone in a stationary state.
Inventors:
Abe Akira
Tatsuhiko Goi
Masahide
Hidenori Arisawa
Tatsuhiko Goi
Masahide
Hidenori Arisawa
Application Number:
JP2014260650A
Publication Date:
July 31, 2019
Filing Date:
December 24, 2014
Export Citation:
Assignee:
Kawasaki Heavy Industries, Ltd.
International Classes:
F02C7/20; F02C7/00; F02C7/32; F02K3/06
Domestic Patent References:
JP64019124A |
Foreign References:
US20130259638 | ||||
GB2198791A |
Attorney, Agent or Firm:
Patent business corporation Yuko patent office