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Title:
The thermoelectrical dynamo of an airplane Bleed system
Document Type and Number:
Japanese Patent JP5965320
Kind Code:
B2
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:
August 03, 2016
Filing Date:
October 21, 2010
Export Citation:
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Assignee:
The Boeing Company
International Classes:
B64D41/00; B64D13/00
Domestic Patent References:
JP2009528207A
JP2006518683A
Foreign References:
US20050173017
US20090159110
WO2008030097A1
Attorney, Agent or Firm:
Sonoda/Kobayashi Patent Business Corporation