Title:
エンジン駆動油圧ポンプ
Document Type and Number:
Japanese Patent JP2011511207
Kind Code:
A
Abstract:
Engine-driven hydraulic pump for an aircraft, having a first and a second pump unit which each comprise an adjustable swash plate and a piston assembly coupled with said swash plate and driven by a pump shaft, a control device for adjusting the inclination of the swash plate and a drive shaft via which the hydraulic pump can be driven by an engine of the aircraft while generating hydraulic pressure at an outlet line, characterized in that the pump units are arranged in parallel and have a respective pump shaft, which pump shafts are coupled with the drive shaft by a gear unit.
Inventors:
Vettel, Axel
Muller, Ulrich
Muller, Ulrich
Application Number:
JP2010545439A
Publication Date:
April 07, 2011
Filing Date:
January 29, 2009
Export Citation:
Assignee:
Airbus Opera Zion Gesellschaft Mitt Beschlenktel Haftung
International Classes:
F04B1/22; B64D41/00; F04B1/26; F04B9/00; F04B9/02; F04B17/05; F04B23/06
Attorney, Agent or Firm:
Noboru Fujimoto
Seiichi Yakumaru
Seiichi Yakumaru