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
Shen Yi, Ryu
Cyan, chin-sea
Application Number:
JP2012542013A
Publication Date:
April 18, 2013
Filing Date:
October 21, 2010
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64D41/00; B64D13/00
Domestic Patent References:
| JP2009528207A | 2009-08-06 | |||
| JP2001071999A | 2001-03-21 | |||
| JP2002130860A | 2002-05-09 | |||
| JP2008509049A | 2008-03-27 |
Foreign References:
| US20050173017A1 | 2005-08-11 | |||
| US20090159110A1 | 2009-06-25 |
Attorney, Agent or Firm:
Yoshitaka Sonoda
Kobayashi Yoshinori
Kobayashi Yoshinori