FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to aircraft air jet engine intermediate housing 21. Proposed housing comprises outer case 23 and front and rear flanges 25, 27 mounted radially inside relative to outer case. Housing 21 comprises also structural arms 17 extending radially between said flanges to case 23. Rear flange is furnished with receptacles 34 to receive bracket for locking thrust compensation rod while first receptacles comprises ledges 36 extending from rear flange. Ledges have through holes 38 to receive bracket lock screws. At least, one of said ledges 37 stays in contact with one of aforesaid structural arms 17.
EFFECT: simplified design, smaller weight and sizes.
15 cl, 6 dwg
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