Title:
Aircraft turbomachinery computer
Document Type and Number:
Japanese Patent JP6329960
Kind Code:
B2
Abstract:
An aircraft turbomachine calculator including a parallelepiped metal casing including an electronic circuit wherein a control channel and a monitoring channel are integrated. The casing includes a first cavity wherein a first electronic board is provided for managing the control channel and a second cavity, independent of the first cavity, wherein a second electronic board is provided for managing the monitoring channel, these electronic boards being provided in two planes oriented with respect to each other at an angle of 90°.
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Inventors:
Pasquier Ludovic
Avre daniel
Joachim Remi
Avre daniel
Joachim Remi
Application Number:
JP2015541221A
Publication Date:
May 23, 2018
Filing Date:
November 12, 2013
Export Citation:
Assignee:
Micro Churvo
International Classes:
F02C7/00; B64D41/00; G06F1/16; H05K7/14
Domestic Patent References:
| JP2004122857A |
Foreign References:
| US5555159 | ||||
| WO2006099627A1 | ||||
| US20030056491 |
Attorney, Agent or Firm:
Shinei Patent Office
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