Assembly for aircraft turbine engine and method for mounting same
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United States of America Patent
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Jan 9, 2018
Grant Date -
Feb 16, 2017
app pub date -
Apr 27, 2015
filing date -
Apr 29, 2014
priority date (Note) -
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Abstract
An assembly for an aircraft turbine engine, including a rolling bearing bracket defining an inner space on either side thereof; a rotary assembly including a first gear; a housing for drawing mechanical power including a second gear mating with the first gear; a shaft for drawing mechanical power, inserted into the housing and rotated by the second gear, the shaft passing through a first opening of the bracket. The assembly includes a mounting device for mounting the housing on the bearing bracket, the mounting device passing through a second opening via the bracket, the mounting device passing through a second opening via the bracket, the second opening being configured so as to allow the housing to be inserted into the space.
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