Title:
出力分配システム
Document Type and Number:
Japanese Patent JP2012503569
Kind Code:
A
Abstract:
A power distribution system for an aircraft having at least one engine includes at least one torque transmission means that is movably held and is connected to at least one shaft of the engine and extends from the shaft of the engine to an interior region of the aircraft fuselage, and at an end pointing away from the engine has at least one interface for introducing a torque. At the interface of the torque transmission means it is possible both to operate mechanical and to start the engine. Consequently in the aircraft it is possible to essentially do without converting mechanical energy to electrical energy and the subsequent use of electrical energy for generating mechanical power. This is particularly favorable in the case of twin-engine commercial aircraft that are used on short hauls.
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Inventors:
Stolte Ralph-Henning
Application Number:
JP2011528315A
Publication Date:
February 09, 2012
Filing Date:
September 23, 2009
Export Citation:
Assignee:
Airbus Operations GmbH
International Classes:
B64D41/00
Attorney, Agent or Firm:
Masayuki Masabayashi
Hayashi Ichiyoshi
Hayashi Ichiyoshi