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Patent Searching and Data


Title:
航空機ブリードシステムの熱電発電機
Document Type and Number:
Japanese Patent JP2013512821
Kind Code:
A
Abstract:
A device for producing electrical power has a thermoelectric device coupled to an aircraft bleed system for generating electrical power using temperature differentials between ram air and bleed air. A system control is coupled to the ram air and the bleed air to control a temperature of the bleed air and to control a temperature gradient of the thermoelectric device.

Inventors:
Gao, Lee Chun
Shen Yi, Ryu
Cyan, chin-sea
Application Number:
JP2012542013A
Publication Date:
April 18, 2013
Filing Date:
October 21, 2010
Export Citation:
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Assignee:
The Boeing Company
International Classes:
B64D41/00; B64D13/00
Domestic Patent References:
JP2009528207A2009-08-06
JP2001071999A2001-03-21
JP2002130860A2002-05-09
JP2008509049A2008-03-27
Foreign References:
US20050173017A12005-08-11
US20090159110A12009-06-25
Attorney, Agent or Firm:
Yoshitaka Sonoda
Kobayashi Yoshinori