FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to the turbo jet engines stators designs. Housing structures have surrounding the engine shell comprising plurality of sectors (12A, 12B), plurality of radial supports (14), each of which is mounted between two adjacent shell sectors and comprises base (14A). Shell sectors on the radial supports bases fastening means comprise plurality of plates (20), each of which is flush mounted in grooves (22), which shape corresponds to the shell sectors, and set of captive screws (26A–26D) with head. Screws (26A–26D) are held in the said plate due to the difference in the diameter between their body and their thread. Fastening means comprise fixed to the said bases set of union nuts, each of which, when the captive screw of this head screws set threaded portion is introduced into it, provides fixed connection between the shell sectors and the radial supports.
EFFECT: providing easy access to devices located under the shell and reducing the flow disturbance in the flow path.
8 cl, 3 dwg
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Authors
Dates
2018-08-15—Published
2014-08-25—Filed