Patent ID: 8152447

Claim:
An intermediate casing for an aircraft jet engine, comprising: an outer shell; a front transverse flange; a rear transverse flange arranged parallel to the front transverse flange, the front and rear transverse flanges disposed radially inside with respect to said outer shell; and structural arms which are distributed angularly and extend radially between said front and rear transverse flanges as far as said outer shell, wherein said rear transverse flange includes first receiving means for receiving a first fixing bracket to which a first rod is fixed for absorbing thrust forces of the jet engine, said first receiving means including bosses coming from said rear transverse flange, each boss including at least one through-orifice therethrough, through which a fixing screw of said first fixing bracket passes, and said through-orifices being spaced apart angularly with respect to the structural arms, and wherein at least one of said bosses extends so as to contact one of said structural arms.