| 摘要 |
PROBLEM TO BE SOLVED: To provide a mounting structure for electronic appliance on jet engine, whereby it is practicable to absorb a thermal expansion, bear a large load at acceleration properly, and reduce vibrational transmission in the axial direction and the gravitational direction. SOLUTION: A mounting structure is to mount a box-shaped electronic appliance 7 on a bypass duct 1a of a jet engine in approx. cylindrical form, wherein in front of the box shape, a first tie-in member 11a is provided having a surface parallel with the box facade and protruding out from the box width, and behind the box shape, a second tie-in member 12a is provided having a surface parallel with the box surface on the bypass duct side and protruding out from the box width, and the bypass duct 1a is equipped with a bracket 13 having a parallel surface with the box facade. The first tie-in member 11a is coupled by bolt in a position ahead of the bracket surface and in such a way as pinching a vibration isolating rubber piece 14, and a pad 17 is provided on the surface confronting the second tie-in member 12a, and the pad 17 and the second member 12a are coupled together by bolt in such a way as pinching vibration isolating rubber.
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