Title:
PROPELLER DRIVING DEVICE FOR AEROPLANE
Document Type and Number:
Japanese Patent JP2004243842
Kind Code:
A
Abstract:
To suppress vibration and noise, stabilize rotational balance of a propeller, improve maneuverability of an aeroplane by suppressing generation of moment of inertia, and make outside dimensions compact, in a propeller driving device for the aeroplane.
In the propeller driving device 10 for the aeroplane interposing a transmission part 15 between an output shaft 12 of an engine 11 and a propeller shaft 14, the transmission part 15 consists of a planetary type friction roller mechanism 20.
Inventors:
HASEGAWA HIROYUKI
YOSHIMOTO SHINYA
YOSHIMOTO SHINYA
Application Number:
JP2003034364A
Publication Date:
September 02, 2004
Filing Date:
February 12, 2003
Export Citation:
Assignee:
HKS CO LTD
International Classes:
B64D35/00; F16H13/08; (IPC1-7): B64D35/00; F16H13/08
Attorney, Agent or Firm:
Shuji Shiokawa