Title:
熱キャパシタを使用した航空機センサへの電力供給
Document Type and Number:
Japanese Patent JP6990017
Kind Code:
B2
Abstract:
An electric power generation system employs a thermoelectric generator placed between an aircraft inner skin and an aircraft outer skin. The thermoelectric generator is configured to utilize a thermal differential between the inner and outer skin to generate an electric current. An electrical interface is provided for access to the electric current generated by said thermoelectric generator.
Inventors:
Hiller, Nathan Dee.
Application Number:
JP2016124217A
Publication Date:
January 12, 2022
Filing Date:
June 23, 2016
Export Citation:
Assignee:
The Boeing Company
International Classes:
H02N11/00; B64D41/00
Domestic Patent References:
| JP2014520499A | ||||
| JP2012129519A | ||||
| JP2006129659A | ||||
| JP2015034601A | ||||
| JP2013045929A |
Foreign References:
| US20130298956 | ||||
| DE102007055090A1 |
Attorney, Agent or Firm:
Sonoda/Kobayashi Patent Business Corporation